Document:

Sale Purchase Agreement

 Exhibit 10.4 

 

			
	

	  	

  
 SALE
PURCHASE AGREEMENT 
 BETWEEN 
 CHC Leasing (Ireland) Limited 
 AND 

EUROCOPTER 

FOR THE SUPPLY OF 
 TWENTY (20) FIR 
 M EC 225 HELICOPTERS AND FOUR (4) OPTIONAL
EC225 
 HELICOPTERS 
 WITH RELATED SERVICES 

  

			
	

	  	

  
 SUMMARY

  

					
	 PREAMBLE
	  	 	4	  
	 ARTICLE 1 – SCOPE, OPTIONS AND PRICING OF THE CONTRACT
	  	 	6	  
	 ARTICLE 2 – EXPORT/IMPORT AUTHORIZATION
	  	 	11	  
	 ARTICLE 3 – PAYMENT TERMS
	  	 	12	  
	 ARTICLE 4 – DELIVERY TERMS
	  	 	15	  
	 ARTICLE 5 – SUPPLY MODIFICATIONS
	  	 	17	  
	 ARTICLE 6 – PRODUCT QUALITY AND AIRWORTHINESS DOCUMENTATION
	  	 	19	  
	 ARTICLE 7 – ACCEPTANCE PROCEDURE
	  	 	20	  
	 ARTICLE 8 – WARRANTY
	  	 	22	  
	 ARTICLE 9 – TRAINING
	  	 	25	  
	 ARTICLE 10 – TECHNICAL ASSISTANCE
	  	 	27	  
	 ARTICLE 11 – TECHNICAL DOCUMENTATION
	  	 	28	  
	 ARTICLE 12 – INTELLECTUAL PROPERTY
	  	 	28	  
	 ARTICLE 13 – APPLICABLE LAW AND ARBITRATION
	  	 	30	  
	 ARTICLE 14 – CONTRACTUAL LIABILITY
	  	 	31	  
	 ARTICLE 15 – MISCELLANEOUS
	  	 	32	  
	 ARTICLE 16 – ENTRY INTO FORCE
	  	 	34	  
	 ARTICLE 17 – ***
	  	 	35	  
	 ARTICLE 18 – SPECIAL CONDITIONS
	  	 	36	  
	 ARTICLE 19 – TAX AND duties
	  	 	37	  
	 ARTICLE 20 – REPRESENTATWNS AND WARRANTIWOF THE BUYER
	  	 	38	  
	 ARTICLE 21 – REPRESENTATIONS AND WARRANTIES OF THE SELLER
	  	 	39	  
	 ARTICLE 22 – TERMINATION
	  	 	40	  

  

	
	 ANNEXES
  

	 ANNEX 1 - HELICOPTER CONFIGURATION

	
	 ANNEX 2 - DELIVERIES

	
	 ANNEX 3 - CORRESPONDENCE

	
	 ANNEX 4 - MARKINGS

	
	 ANNEX 5 - CERTIFICATE OF CONFORMITY

  
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	 ANNEX 6 - ***

	
	 ANNEX 7 - ***

	
	 ANNEX 8 - STORAGE CONDITIONS

  
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 PREAMBLE 

THIS AGREEMENT is made on September 13, 2011. BETWEEN: 
  

	(1)	CHC LEASING (IRELAND) LIMITED, a company organized and existing under the laws of Ireland, whose registered office is at Earisfort Court, Earlsfort Terrace,
Dublin 2, Ireland (hereinafter referred to as “the Buyer”) 

  

	(2)	EUROCOPTER, a Société par Actions Simplifiée registered in France, whose Siège Social is at Aéroport International
Marseille-Provence, 13725 Marignane Cedex, France (hereinafter referred to as “the Seller”). 

 Seller and Buyer also
referred to as “Party” or “Parties” 
 RECITALS: 
 Whereas the Parties have already entered into several agreements and a framework agreement amended from time to time, for the sale and purchase of twenty four (24) EC 225 helicopters with given
configuration and a specific set of conditions. 
 Whereas the Parties are willing to enter into a new multiyear contract for the supply of
additional twenty (20) firm Helicopters and several Option Helicopters for delivery from February 2012 through — May 2016 and associated services, under new conditions. 

Whereas the Seller has agreed to procure, manufacture and test the helicopters in Marignane (France) and supply the Services in accordance with the
provisions of this Contract. 
 Whereas the Buyer has agreed to purchase the Helicopters on the term and conditions hereof and has agreed to pay
the Contract Price to the Seller at the times and in the manner provided in this Contract. 
 Whereas each of the Buyer and the Seller has
agreed to carry out and fulfil all of the other obligations imposed on them respectively under this Contract. 
 IT IS AGREED:

 Definitions: In this Contract (including the Recitals, Annexes and any schedules or appendices), unless the context otherwise requires:

 “Acceptance” means: 
  

	 	a.	in respect of any Supplies, the signature of the Acceptance Certificate for that Deliverable by the Buyer; and 

 

	 	b.	in respect of any Services, notice of completion of those Services issued by the Seller, and “Accept” and “Accepted” are to be
construed accordingly; 

  
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“Acceptance Certificate” means, in respect of any Supplies, the certificate signed on behalf of the Buyer acknowledging
that the Deliverable has successfully passed all Acceptance Tests; 
 “Acceptance Test” means the inspection
and/or testing of an EC225 as per Article 7, to ensure that it complies with the Specification of Annex 1; 

“Certificate of Conformance” or “Certificate of Conformity” means the product release documentation that
certifies the item is manufactured in accordance with the original equipment manufacturer’s specification and any other applicable specifications and standards and in the form as set out in Annex 5 to this Contract; Services shall be subject to
Certificate of Completion. 
 “Coface” means Coface, a limited company whose head office is located at 12, Cours
Michelet — La Defense 10 — 92800 Puteaux or any successor or subsidiary therof; 
 “Contract” means
this contract between the Buyer and the Seller and includes all schedules, annexes, appendices and other attachments to this contract; 
 “Contract Effective Date” or “CED” means the date on which all the conditions subsequent referred to in Article 15 have been satisfied; 

“Contract Price” means the aggregate amount payable by the Buyer to the Seller under this Contract for the Deliverables;

 “Deliverables” means the Supplies and the Services; and Deliverable means any one of them; 

“Delivery Date” means the date or dates on which the respective items comprising the Supplies are put at the Buyer’s
disposal subject to the fulfilment of the prerequisites as defined in Article 7.5; 
 “EC 225” or
“Helicopters” means the twenty Eurocopter EC225 helicopters, each in the configuration and according to Technical Specification as described in Annex 1, firmly purchased by the Buyer under this Contract or the Prior Contracts, as
applicable; 
 “Initial Delivery Date” means the date in respect of each Helicopter or Optional Helicopter as
set out in Annex 2, as amended from time to time. 
 “Option Helicopters” means the optional Eurocopter EC225
helicopters each in the configuration and according to Technical Specification as described in Annex 1, that may be purchased by the Buyer under this Contract, in accordance with Article 1.2; 

“Prior Contracts” means the three agreements between Heli-One Canada Inc. and the Seller known as Amendment No HLO 25.00,
Amendment No HLO 26.00 and Amendment No HLO 29.00, each an amendment to the Contract No 45493/2007 signed 

  
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on March 1, 2007 and dated December 22, 2010, December 22, 2010 and June 28, 2011, respectively and having as their subject matter Helicopters described as HLO 25, HLO 26
and HLO 29. 
 “Right of First Refusal Helicopters” or “RFR Helicopters” means the Eurocopter
EC225 helicopters each in the configuration and according to Technical Specification as described in Annex 1, that may be purchased by the Buyer under this Contract, in accordance with Article 1.2 

“Parts” means sub-components to the Helicopter or Option Helicopter 

***; 

“Seller Option Price List” means the Seller’s regular list of prices for optional equipment other than those listed
in Article 1.3.5. 
 “Services” means the Training and the Technical Assistance, to be provided by the Seller to
the Buyer as per Article 9 and 10 of this Contract; 
 “Specification” or “Technical
Specification” means the specifications for the Contract Deliverables as described in Annex 1; 

“Supplies” means the Helicopters, Optional Helicopters, RFR Helicopters and Technical Documentation to be provided by the
Seller to the Buyer as listed in Annex 1 and Article 11 of this Contract 
 “Technical Assistance” means the
technical assistance described in Article 10 to be provided by the Seller to the Buyer; 
 “Technical
Documentation” means the technical documentation described in Article 11 to be provided by the Seller to the Buyer. The set of Services Bulletins excludes the service bulletins made for specific kits, optional equipment, retrofit, equipment
to be fitted on the Helicopter under Buyer’s modifications; 
 “Training” means the training courses
described in Article 9 which are to be provided by the Seller to the Buyer. 
 ARTICLE 1 – SCOPE, OPTIONS AND PRICING OF THE CONTRACT

  

	1.1.	SUPPLIES AND SERVICES 

 The Seller commits to sell and the Buyer commits to buy subject to the provisions of Article 22, the Helicopters, except as specifically agreed upon between the Parties at the time when each Delivery Date
is confirmed pursuant to Article 4.3, and subject to price modification pursuant to Article 1.3.6, together with Technical Documentation (described in Article 11), the Technical Assistance (described in Article 10) and Training (described in Article
9). 

  
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	1.2.	OPTION HELICOPTERS AND RIGHT OF FIRST REFUSAL HELICOPTERS 

 The Seller hereby grants to the Buyer the right to purchase up to four (4) additional EC 225 helicopters each in the configuration and according to Technical Specification as described in Annex 1
(the “Option Helicopters”) under the following conditions: 
 Option exercise: for each one of the Option Helicopters,
the Buyer will confirm its exercise in writing to the Seller at least eighteen (18) months before the proposed delivery date and then, following such notice, this Contract will be amended accordingly. 

 

	 	•	 	 If written notice is not sent within this time the relevant Option will be considered as not exercised and expired, the Buyer losing the benefit of the
deposited funds. For clarity, if notice is provided to the Seller at least eighteen (18) months before the proposed delivery date that the Buyer does not wish to exercise the Option, the deposit funds will be refunded to the Buyer or applied to
a future delivery (to be mutually agreed). 

  

	 	•	 	 Configuration: same as described in Annex 1 except as specifically agreed upon between the Parties at the date of each Option exercise.

  

	 	•	 	 Option cost: the cost of each Option is set at EUR *** 

 

	 	•	 	 Price: unit price of each Option Helicopter will be as indicated in Article 1.3 

 

	 	•	 	 Payment conditions: as per Article 3.2.2 

  

	 	•	 	 Delivery Dates as per Article 4.3 

 And 
 The Seller hereby grants to the Buyer a right of first refusal to purchase
additional EC 225 helicopters (RFR Helicopters) under the following conditions: 
  

	 	•	 	 The Seller, along the duration of this Contract, if production slots become available (i.e. cancelation from another customer) is obligated to request
in writing to the Buyer to exercise a right of first refusal. If the Buyer wants to confirm the Helicopter and its delivery date, the Buyer shall send to the Seller a preliminary written confirmation notice within the following five
(5) business days, and then the Parties shall sign the corresponding Purchase Amendment as soon as practical thereafter. 

  
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	 	•	 	 If preliminary written notice is not sent back by the Buyer within the following five (5) business days , the right of first refusal will be
considered as not exercised and expired, 

  

	 	•	 	 Configuration: same as described in Annex 1 except as specifically agreed upon between the Parties at the date of each RFR exercise.

  

	 	•	 	 Price: unit price of each Helicopter will be as indicated in Article 1.3 

 

	 	•	 	 Payment conditions: as per Article 3.2.2 

 Notwithstanding the above, should The Seller have additional helicopters within the Delivery timeframe of this Contract and should The Buyer have some interest in purchasing such additional Option, the
same conditions will prevail. 
 For each Option Helicopter or RFR Helicopter exercised, the buyer may perform a Firm/Option
Swap. In this event, the buyer may elect to designate one of the remaining firm deliveries as an Option Helicopter. This delivery would from that point on be treated as an Option Helicopter, with all the rights and obligation of an Option, and not
as a Firm Delivery. 
 In the event the firm delivery helicopter being designated as an Option has a deposit balance in excess of
the required Option payment, the excess balance will be transferred to the RFR Helicopter being exercised. 
  

	1.3.	PRICES 

  

	1.3.1.	Prices 

 All prices
in this Contract are: 
  

	 	(i)	in Euro (EUR) currency. 

  

	 	(ii)	discounted prices, meaning they already reflect Buyer’s special conditions application. 

 

	 	(iii)	inclusive of all charges and taxes, including without limitation VAT, attendant to the manufacture of the Supplies. 

 

	 	(iv)	 exclusive of any charges resulting from administrative and legislative regulations in force in the Buyer’s country and of any customs and duty
charges, which are the Buyer’s responsibility. For this, the Buyer will produce reasonable proof promptly after signature that the Supplies are exempted from any taxes, duties, levies or charges of any sort due to Buyer’s country
regulations and grants that should such taxes, duties, levies or charges become due, they will be paid by the Buyer or reimbursed immediately to the Seller. The Seller shall communicate to

  
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the Buyer of any liability for any such charges with sufficient advanced notice to ensure that the Buyer or Seller is able to plan to minimize or avoid such charges, as allowable by law.

 In the event that the Contract does not enter into force as per Article 16 within four (4) weeks of the
Contract signature date, then the prices set out in Article 1 hereto shall be actualized at the prevailing economic conditions, reckoned from the signature date. The delivery times of the products shall be adjusted to the delivery dates the Seller
is then able to offer. 
  

	1.3.2.	Prices Modification 

Prices refer to the Deliverables explicitly mentioned in this Contract. Any configuration changes and/or additional Deliverables to be
provided by the Seller must be previously agreed upon in writing and shall be subject to an amendment to the Contract, setting forth any changes in the price and/or delivery. 
 In case of change to the configuration of a Helicopter, Option Helicopter or RFR Helicopter requested by the Buyer, the Seller agrees that the price for any additional equipment, other than that listed in
Article 1.3.5 of this Contract, added to the Helicopter, Option Helicopter or RFR Helicopter shall be no greater than the Seller’s regular list price for such equipment less a discount of ***% (*** percent). 

 

	1.3.3.	Price escalation 

 For the
purposes of Article 3 (Payment), Article 4.3 (Changes in Delivery Schedule), and for the purpose of budgeting the procurement of the Helicopters, the unit Helicopter prices will be based on a 2012 helicopter delivery reference price of *** Euro.

 For deliveries of Helicopters in 2013 and subsequent years and in the event of confirmation of the Option Helicopters, the
price of such Helicopters would be confirmed by the Seller, ***. 
 For clarity, the Helicopter prices will be: 

Helicopters delivered in year 2012: 
 *** EUR 
 Helicopters delivered in year 2013: 

*** EUR x (lower of 3% and French Euro Zone Consumer Price Index + 1.5%) 

Helicopters delivered in year 2014: 
 2013 delivery price x (lower of 3% and French Euro ZOne Consumer Price Index + 1.5%) 

  
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 Helicopters
delivered in year 2015: 
 2014 delivery price x (lower of 3% and French Euro Zone Consumer Price Index + 1.5%) 

Helicopters delivered in year 2016: 
 2015 delivery price x (lower of 3% and French Euro Zone Consumer Price Index + 1.5%) 
  

	1.3.4.	Contract Price 

  

							
	 	  	QTY	  	TOTAL
PRICE IN
EUR	 
	 EC 225 Firm Equipped Helicopters Ex-works Marignane (France)
	  	20	  	 	***	M€ 
	 As per Technical Configuration in Annex 1
	  		  			
	 EC 225 Option Helicopters
	  	4	  	 	***	M€ 
		  	  
	  	  
	  
	 
	 Training (as per Article 9)
	  		  	 	***	  
	 Technical Assistance (as per Article 10)
	  		  	 	***	  
	 Technical Documentation (as per Article 11)
	  		  	 	***	  
	 Manufacturer Financing support (as per Article 17 and Annex 6)
	  		  	 	***	  
		  		  	  
	  
	 
	 CONTRACT PRICE (assuming 3% escalation applies) ***
	  		  	 	***	M€ 

  

	1.3.5.	Additional Optional Equipment Pricing 

 At the Buyer’s request, the Seller shall install on any Helicopter, Optional Helicopter or RFR Helicopter such additional optional equipment as Seller makes available for such helicopters in the
ordinary course of its business, including without limitation, any or all of the additional optional equipment listed below at the prices set out. Any other additional optional equipment not listed below shall be priced in accordance with the
provisions of Article 1.3.2. 
  

							
	 Reference
	  	 DESIGNATION
	  	Discounted
Unit 
Price
2012	 
	05-42021-00-RP2	  	 Air conditioning system - Removable Parts 2
 (cockpit power unit)
	  	 	***	€ 
	05-50001-00-CI	  	Installation for flight in icing conditions	  	 	***	€ 
	05-81004-00-RP	  	Additional Energy Absorbing pod fuel tanks - Removable parts	  	 	***	€ 
	07-60009-00-RP	  	Luggage compartment in pod – Removable parts	  	 	***	€ 
	06-27013-00-RP	  	Cargo sling with dynamometer 3,8 Tons - Removable parts	  	 	***	€ 

  
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	 Reference
	  	 DESIGNATION
	  	Discounted
Unit 
Price
2012	 
	06-26006-00-RP	  	External mirrors - Removable parts	  	 	***	€ 
	06-21015-00-RP	  	Goodrich 28V electrical hoist (290ft, 6001b) - Removable parts	  	 	***	€ 
	08-44052-01-CI	  	Dual FMS and Dual GPS installation	  	 	***	€ 
	08-10016-00-CI	  	Collins - HF9X00 HF/SSB	  	 	***	€ 

 The Buyer shall notify to the Seller its wish to install any additional optional equipment on a
Helicopter, Option Helicopter or RFR Helicopter no later than eighteen (18) months prior to the Initial Delivery Date for such Helicopter, Option Helicopter or RFR Helicopter as set out in Annex 2. 

Even if the Buyer has selected not to install any additional optional equipment, each Helicopter, Option Helicopter or RFR Helicopter
shall be delivered with all necessary documentation in order to install the following Optional Equipments: Cargo sling, Hoist, Additional Energy Absorbing pod fuel tanks, luggage compartment in pod. 

 

	1.3.6.	Additional Services Pricing 

 At the Buyer’s request, the Seller shall provide additional services associated with the delivery of any Helicopter, Option Helicopter or RFR Helicopter in order to prepare for shipment or ferry the
Helicopter, Option Helicopter or RFR Helicopter to the location specified by the Buyer. 
  

							
	Reference	  	DESIGNATION	  	 Unit Price

2012
	 
	FF	  	 Ferry flight to Stavenger or Aberdeen by Seller’s crew
	  	 	***	€ 
	PACK	  	 Preparation and packaging for air or sea freight
	  	 	***	€ 

 Specific ferry to other destinations or arrangements for transportation can be quoted upon request by the
Buyer. 
 All prices referred in 1.3.5 and 1.3.6 are for deliveries made in 2012. Prices for additional optional equipment or
services in connection with deliveries in subsequent years shall be escalated following the same rules as defined in 1.3.3. 
 ARTICLE 2
– EXPORT/IMPORT AUTHORIZATION 
 All Deliverables may be subject to export laws and regulations including French regulations and foreign
government regulations, and the Parties acknowledge that deviation from such regulations is prohibited. 
 The Seller will perform all necessary
and appropriate procedures for obtaining official licenses (export licenses) for the Supplies. The Buyer agrees to provide any assistance or documentation or certificate requested by the Seller to obtain the necessary licenses or to ensure
compliance with applicable regulations. 

  
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 The Seller shall not be
liable for any damages or losses, whether direct or indirect, incurred by the Buyer if any of such necessary licenses are not granted or are granted with delay or if a license that has been granted is revoked. The Buyer shall have no obligation to
purchase any Helicopter, Option Helicopter or RFR Helicopter for which the necessary licence has not been issued or has been revoked prior to delivery and shall not be liable for any damages or losses, whether direct or indirect, incurred by the
Seller as a result thereof. 
 The Buyer shall obtain in due time any import license required in its country for the Supplies. 

In case governmental regulations do not authorize the Buyer to operate any of the Helicopters or Optional Helicopters in its intended areas, this will
not be considered as default from the Seller and neither will it be a ground for terminating the Contract in part or in whole. 
 ARTICLE 3
– PAYMENT TERMS 
  

	3.1.	GENERAL 

 All
payments to the Seller will be done through bank transfer to the following bank account: 
 BANQUE NATEXIS 

 408 Avenue du Prado 
 13295 - MARSEILLE CEDER 08 
 Account name: *** 

IBAN: *** 

SWIFT code: BANQUE NATIXIS NATXFRPPXXX 
 Notwithstanding the provisions of Article 16, all down-payment and progress payments will not be refundable. 
  

	3.2.	PAYMENTS 

  

	3.2.1.	For the Helicopters: 

 Down payment 
 On the 28th day of September, 2011 the Buyer shall pay
to the Seller as an initial down-payment the sum of EUR *** (being EUR*** per Helicopter less EUR*** per each of the Helicopters that are the subject of the Prior Contracts)), against presentation by the Seller of a Proforma invoice for the
corresponding amounts. 

  
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Progress payments 
 Twenty Four (24) months prior to the Delivery Date of each Helicopter, the Buyer shall pay a progress payment of *** (***%) of the price of each Helicopter as defined in Article 1.3 less
EUR*** per Helicopter against presentation by the Seller of a Proforma invoice for the corresponding amount. 
 Eighteen
(18) months prior to the Delivery Date of each Helicopter, the Buyer shall pay a further progress payment of *** (***%) of the price of each Helicopter as defined in Article 1.3 against presentation by the Seller of a Proforma invoice
for the corresponding amount. 
 Nine (9) months prior to the Delivery Date of each Helicopter, the Buyer shall pay a
further progress payment of *** (***%) based on the price of each Helicopter as defined in Article 1.3 against presentation by the Seller of a Proforma invoice for the corresponding amount. 

Balance payment 
 The Buyer shall pay to the Seller the balance of the Helicopter price, less ***, if any, during the Acceptance phase and prior to the transfer of ownership. Payment shall be executed against presentation
by the Seller of: 
  

	 	•	 	 Commercial invoice for the corresponding amount, and 

  

	 	•	 	 Xerox copy of Certificate of Conformity for the helicopters and optional equipment installed therein. 

 

	3.2.2.	For the Option Helicopters: 

 Option Fee 
 On the 28th day of September, 2011, the Buyer shall pay
to the Seller the sum of EUR *** (being EUR*** per Option Helicopter) as an option fee, against presentation by the Seller of a Proforma invoice for the corresponding amounts. 
 Progress payments 
 Eighteen (18) months prior to the Initial
Delivery Date of each Option Helicopter in respect of which the Buyer has exercised its option, the Buyer shall pay a progress payment of *** percent (***%) of the price of each Option Helicopter as defined in Article 1.3 less the option fee
attributable to such aircraft against presentation by the Seller of a Proforma invoice for the corresponding amounts. 
 Nine
(9) months prior to the Delivery Date of each Option Helicopter, the Buyer shall pay a further progress payment of *** percent (***%) of the price of each Option Helicopter as defined in Article 1.3 against presentation by the Seller of
a Proforma invoice for the corresponding amount. 

  
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 Balance
payment 
 The Buyer shall pay to the Seller the balance of the Option Helicopter price, less ***, if any, during the
Acceptance phase and prior to the transfer of ownership. Payment shall be executed against presentation by the Seller of 
  

	 	•	 	 Commercial invoice for the corresponding amount, and 

  

	 	•	 	 Xerox copy of Certificate of Conformity for the Option Helicopter and optional equipment installed therein. 

 

	3.3.	Reallocation of Payments 

 The Seller agrees to allocate down payments or progress payments to those Helicopters and Option Helicopters as may be requested from time to time by Buyer in connection with Buyer’s financing of
such Helicopters and Option Helicopters, provided that in all cases the aggregate amount of all down payments and progress payments paid by the Buyer shall not be less than the aggregate amount of down payments and progress payments required to be
paid hereunder. 
  

	3.4.	*** 

  
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 ARTICLE 4 – DELIVERY
TERMS 
  

	4.1.	GENERAL 

 The
Seller’s and the Buyer’s respective obligations for delivery of the Supplies and Services shall be according to INCOTERM 2010 (ICC issue N ° 715EF). 
 All Supplies and Services shall be delivered Ex-Works the Seller’s factory in Marignane, France, excluding Training and Technical Assistance, which shall be delivered in accordance with Article 9 and
10. 
 The Supplies will remain insured by the Seller against all risk of damage and fire up to the time of execution and
delivery of the Acceptance Certificate according to Article 7 hereof. 
  

	4.2.	RELAYS 

  

	4.2.1.	Force Majeure 

 The
Seller shall not be held responsible for failure to perform or delay in performing any of the contractual obligations of this Contract if such failure or delay is due to unforeseeable events beyond its reasonable control, including but not limited
to, acts of God, war, insurrection, epidemics, sabotage shortages of labour, other than those resulting from labour disputes, strikes or lock-outs, interruption or delays in transportation, fire, explosion, acts, orders, restrictions or priorities
of any Government agency preventing the Seller to perform its obligations under the Contract (each a “Force Majeure” event). 
 The Seller shall notify the Buyer about the occurrence of any event of Force Majeure within a reasonable time after the commencement thereof, citing this section in said notice. In such a case, the
contractual delivery dates shall be extended by any reasonable period of time required for removing the causes of the delay. 

If due to governmental action the export to the Buyer of the Helicopters or part of the Option Helicopters or substantial part thereof is
not authorized, this situation is recognized expressly by the parties as a case of Force Majeure and the Buyer agrees that it will hold the Seller harmless and will waive any claim for any damage that may result therefrom except for the repayment to
the Buyer of any corresponding portion of the Contract Price. 
  

	4.2.2.	Delays by the Seller 

 If the actual Delivery Date for any Helicopter or Option Helicopter occurs after the date agreed by the Parties and a further grace period of thirty (30) days for reasons other than a Force Majeure
Event or delay caused by the Buyer, the Seller shall pay to the Buyer as liquidated damages the equivalent to the capital cost, charged at a rate of 12% per annum of all sums already paid per delayed Helicopter or Option Helicopter for the time
between the end of the grace period and the actual Delivery Date. 

  
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 Without
prejudice to any other rights of the Buyer under this Contract, the payment of the liquidated damages as stipulated above shall be full and final satisfaction of all claims arising directly or indirectly out of any delays by the Seller. 

Should the Seller fail to have the Helicopter or Option Helicopter available for sale to the Buyer within three (3) months of the
contracted date agreed by all parties, in addition to the liquidated damages above, the Buyer is entitled to cancel the delivery and to receive a refund of all deposit payments made on the aircraft. 

 

	4.3.	CHANGES IN DELIVERY SCHEDULE 

 For the Helicopters: 
 The Buyer shall have the right to postpone the
Delivery Date of any Helicopter to a maximum of twelve (12) months, provided this is confirmed in writing to the Seller at least eighteen (18) months before the Initial Delivery Date. 

In case the Buyer confirms a postponement, the Helicopter price will be revised accordingly, so that price will be that of the year of
actual Delivery, according with Article 1.3.2. 
 If no postponement is requested within the time period above, the Initial
Delivery Date as set forth in Annex 2 and configuration of the Helicopter as per Annex 1 will be considered confirmed, and the corresponding progress payments will be due. 
 For the Option Helicopters: 
 At the time that each of the options is
exercised, notwithstanding the payment of the down payment as per Article 3.2 the Buyer is entitled to postpone by up to three (3) months the Initial Delivery Date of the corresponding Option Helicopter, as set forth in Annex 2. At the
Buyer’s request, the Seller shall endeavour its reasonable effort to advance the delivery date by up to three months. 
 If
the option is exercised and no postponement is requested at this time, the Initial Delivery Date will be considered as the one requested by the Buyer. 

  
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 ARTICLE 5 – SUPPLY
MODIFICATIONS 
  

	5.1.	MODIFICATIONS INCORPORATED PRIOR TO DELIVERY OF THE SUPPLIES 

 The Supplies will be manufactured and produced in accordance with the Seller’s current production configuration for the selected helicopter model. Configuration changes may be made at any time by the
Seller to conform to regulations of the National Civil Aviation Authority (DGAC or EASA wherever applicable). 
 Additionally,
the Seller may carry out modifications to the Supplies pursuant to new manufacturing or engineering requirements without the consent of the Buyer, as long as such modifications (i) do not affect the helicopter performance, contractual price or
delivery time (ii) do not constitute a material change in the configuration of any Supply (including, fit, form, function), and (iii) are specifically described in writing by Seller to Buyer when such change has an impact on the
configuration of the Helicopter, Option Helicopter or RFR Helicopter as soon as possible prior to implementing any such modification. 
  

	5.2.	MODIFICATIONS DECIDED SUBSEOUENT TO DELIVERY OF THE SUPPLIES 

 The Seller will notify the Buyer of any modifications that the competent National Civil Aviation Authority has decided to impose on helicopters of the same type. In the event of such modifications, the
Seller shall make available to the Buyer, within a reasonable time, at the latter’s request and at the latter’s expense, the parts required to incorporate such modifications in the Helicopter or Option Helicopter previously delivered.

  

	5.3.	CONFIGURATION CHANGES 

 The Buyer shall have the right before each Delivery Date to modify the configuration of the Helicopters, Option Helicopters or RFR Helicopters by replacing the existing configuration as indicated in Annex
1 by another one to be agreed between the Parties under the following conditions: 
  

	 	•	 	 for configuration changes communicated in writing to the Seller at least eighteen (18) months before the Delivery Date, the Seller shall make such
changes provided such changes do not have a significant impact on the production cycle of the of the aircraft. The Seller agrees that the Buyer may make changes consisting of adding up to Three (3) items of optional equipment from the list set
out in clause 1.3.5 (excluding the installation for flight in icing conditions) and these will be deemed to be non significant and therefore will not impact the Delivery Date. For other changes, the Buyer acknowledges that the Delivery Date may need
to be adjusted by the parties. 

  
 17 

			
	

	  	

  
  

	 	•	 	 for configuration changes requested less than eighteen (18) months before the Delivery Date, the Seller will employ its reasonable efforts to
accommodate the request. 

  

	 	•	 	 the Helicopter, Option Helicopter or RFR Helicopter price will be modified accordingly as per Article 1.3.3. 

The Buyer and the Seller agree to meet as required to prepare a rolling 24 month forecast for optional equipment listed in 1.3.5.

  
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 ARTICLE 6 – PRODUCT
QUALITY AND AIRWORTHINESS DOCUMENTATION 
 The Deliverables will be manufactured, produced or delivered in accordance with
the quality assurance procedures (the “Quality Assurance Procedures”) of the Seller. 
 Acknowledgment that the
Deliverables have satisfied the Quality Assurance Procedures will be attested by the issuance of the following documents: 
 For
the Helicopter in its standard version and installed optional equipment: 
  

	 	•	 	 a Certificate of Conformity drawn up by the Seller’s Quality Organization to certify compliance with the contractual requirements,

  

	 	•	 	 an Aircraft Statement of Conformity (EASA Form 52) for helicopters sold to customers of EASA member states signed by the Seller’s authorized
certifying staff as per the Seller’s Production Organization Approval. The EASA Form 52 allows the issuance by the National Civil Aviation Authority of the Certificate of Airworthiness for the European countries members of EASA, or

  

	 	•	 	 a Certificate of Airworthiness for Export, for helicopters sold outside the European Union, issued by the National Civil Aviation Authority upon
submission by the Seller to the EASA representative body of the above mentioned original Aircraft Statement of Conformity (EASA Form 52), 

  

	 	•	 	 Upon request by the Buyer, a Certificate of Non-Registration issued by the French Civil Aviation Authority. 

For the optional equipment delivered packed and spare parts: 

 

	 	•	 	 A Certificate of Conformity or other equivalent document issued by the Seller’s authorized certifying staff, for standard components,

  

	 	•	 	 An Authorized Release Certificate (EASA Form 1) issued on behalf of the National Civil Aviation Authority as per the above mentioned Production
Organisation Approval, for other certified components. 

 For miscellaneous parts and tools which are not
subject to installation on the Helicopter (if applicable): 
  

	 	•	 	 A Certificate of Conformity issued by the Seller’s authorized certifying staff. 

  
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 ARTICLE 7 –
ACCEPTANCE PROCEDURE 
  

	7.1.	GENERAL 

 Prior to
Acceptance of each Helicopter or Option Helicopter, the Seller may perform production flight tests and inspection flights on such helicopter that will not exceed fifty (50) hours. Additional hours may be flown in the event that development and
installation of specific equipment is requested by the Buyer. 
 Upon satisfactory completion of Seller’s Quality Assurance
Procedures approved by the French Civil Aviation Authority the Certificate of Conformity will be issued by the Seller’s Quality Department. 
 As from the date of issuance of the Certificate of Conformity, the Helicopter or Option Helicopter shall be deemed ready for Buyer’s inspection and Acceptance. 

Not later than one (1) month prior to the date on which a Helicopter is to be ready for Buyer’s inspection and Acceptance, the
Seller will provide the Buyer with a precise schedule, a delivery program and the process for inspection. 
 Within one
(1) week after receipt of this notice, Buyer will send to the Seller the personal information required from the Buyer’s representatives in order to be admitted to Seller’s premises. The information will include name, date and place of
birth and passport number. 
 The Buyer shall accept the Supplies as being in conformity with the contractual specifications
where the Supplies conform in all material respects to such specifications. The acceptance shall be acknowledged by the Buyer’s signature of the “Acceptance Certificate”. 

The Buyer shall bear its own expenses and cost related to the Acceptance Test, including but not limited to those relating to travel and
accommodation of its representatives during this process. 
  

	7.2.	ACCEPTANCE FLIGHTS BY THE BUYER 

 During the Acceptance Test for each Helicopter or Option Helicopter the Buyer may perform free of charge acceptance flights, the combined time of which shall not exceed five flight hours per Helicopter or
Option Helicopter. 
 Acceptance flights will follow the procedures provided by the Seller and shall be carried out under the
responsibility of a Seller’s pilot acting as pilot in command. 
 Acceptance Test procedures shall be completed within a
target of three (3) days from commencement per Helicopter, Option Helicopter or RFR Helicopter (the “Acceptance Period”). 

  
 20 

			
	

	  	

  
  

	7.3.	TRANSFER OF RISK AND TITLE 

 Upon the signature by the Buyer of the “Certificate of Acceptance”, the Buyer shall provide a copy of a valid insurance policy to the Seller, or reasonable proof of the insurance coverage and
all risks will be transferred simultaneously to the Buyer. 
 Promptly after effective receipt by the Seller of the balance
payment as per Article 3.2, the Seller shall present to Buyer a duly executed Bill of Sale and title shall thereupon transfer to the Buyer. 
  

	7.4.	BUYER’S DELAYS FOR PAYMENT 

 If the Buyer fails to make any progress payment on time as described in 3.2 and following a grace period of 30 days after the due date, the Seller shall grant to the Buyer a further remedy period of
(1) month during which the Buyer shall be liable to pay to the seller liquidated damages, accruing daily, charged at a rate of 12% pa, on the payment due. If the progress payment is still not received at the end of the remedy period, the value
of such progress payment (including the accrued liquidated damages) will be added to the balance price of the next Helicopter to be delivered to the Buyer, and the Seller shall be entitled to withhold delivery of such Helicopter until this overall
sum has been received. 
 If the final payment in respect of a Helicopter, Option Helicopter or RFR Helicopter has not been made
on time pursuant to Article 3.2, the Seller shall grant to the Buyer a remedy period not exceeding three (3) months where the Buyer shall pay to the Seller as liquidated damages the equivalent to the capital cost, charged at a rate of 12% per
annum, of the balance of the price of the relevant Helicopter. Option Helicopter or RFR Helicopter, calculated from the 31st day after the date the payment was first due until such final payment is received in the Seller’s bank account.

 Beyond such remedy period and should the Buyer not have proceeded with the relevant final payment or not have demonstrated its
good faith in structuring the payment with the financial market, the Seller shall market at its sole decision the Helicopter, Option Helicopter or RFR Helicopter and retain the down payment until the Helicopter, Option Helicopter or RFR Helicopter
is either paid by the Buyer or sold to another party. The Seller shall be entitled to terminate the contract for any such Helicopter, Option Helicopter or RFR Helicopter and retain 15% of the price of same to cover financial, reallocation and
reconfiguration costs and shall transfer to other Helicopters, Option Helicopters or RFR Helicopters the balance amount as directed by the Buyer. In the event there are no Helicopters, Option Helicopters or RFR Helicopters remaining to be delivered,
the balance shall be wired forthwith to the bank account designated by the Buyer. 

  
 21 

			
	

	  	

  
  

	7.5.	BUYER’S DELAYS OF ACCEPTANCE 

 Where the Seller complies with its obligation to provide the Supplies according to the requested Specification, should the Buyer fail to present its team without any prior notice to the Buyer or to comply
with the obligations to execute and deliver the Acceptance Certificate, the Seller will promptly notify the Buyer in writing to remedy such failure. All risks related to the Supplies will be deemed to be transferred to the Buyer as of the date of
such notice. 
 After the expiry of fifteen (15) days following receipt by the Buyer of such written notice, if the Buyer
has not remedied the aforementioned default, the Buyer shall pay to the Seller as liquidated damages the equivalent to the capital cost, charged at a rate of 12% per annum, of the balance of the price of the relevant helicopter. If the Buyer fails
to remedy the situation before seventy five (75) days following receipt of such written notice, the Seller may retain 15% of the price of such Helicopter, Option Helicopter or RFR Helicopter and proceed to Termination of the Contract for said
Helicopter, Option Helicopter or RFR Helicopter according to Article 21.2 
  

	7.6.	COLLECTION OF SUPPLIES 

The Buyer shall take delivery of each Helicopter and Option Helicopter within two (2) weeks after the date of transfer of ownership
if they are to be ferry-flown or within one (1) month of the transfer of ownership if they are to be dismantled and conditioned for any form of transportation other than ferry flight. 

Such duration shall be extended by the time required to train the pilots for the Buyer’s helicopters used for this training.

 If the Buyer fails to take delivery within the abovementioned period of time, any expenses incurred by the Seller for
maintenance, storage and insurance shall be paid by the Buyer to the Seller under conditions defined in Annex 8 
 ARTICLE 8 – WARRANTY

  

	8.1.	The Seller warrants that the Supplies manufactured and delivered under this Contract, excluding the materials mentioned in Article 8.1.6, are free from defects
in material and workmanship under normal use and service. 

 The Seller’s obligation under this warranty is
limited to the replacement or repair, at the Seller’s discretion, of allegedly defective Parts, that have been returned to its facility and, at the time of any repair or replacement, have been recognized by the Seller after inspection as
defective. To be eligible under this warranty the alleged failure must have occurred within two thousand (2,000) flying hours or twenty four (24) months after Acceptance of the Helicopter or Option Helicopter and optional equipment,
whichever expires first. 

  
 22 

			
	

	  	

  
  

	8.2.	The warranty period on any repaired or replaced Part shall be the warranty period that was remaining on the defective Part. The Parts removed for which the Seller
supplies a replacement Part shall become the property of the Seller. The parts provided as replacement Parts shall become the property of the Buyer. 

  

	8.3.	As soon as possible but within sixty (60) days of the discovery of any defect, the Buyer shall return the allegedly defective Part or Parts to the Seller.
Prior to or concurrently with shipment of any allegedly defective Part or Parts, the Buyer shall furnish the Seller in writing the full details of its claim and the basis thereof. 

 

	8.4.	Subject to Articles 8.5 and 8.6, the transportation costs outbound, insurance and customs expenses and other charges, as well as the expenses incurred by the Buyer for
the removal, re-installation and adjustment operations with respect to such Parts shall be borne by the Buyer. 

  

	8.5.	For the return of Parts for which the benefit of the warranty has been granted by the Seller, the return transportation costs (cm Tremblay, France) shall be borne by
the Seller and the inbound transportations costs shall be reasonably reimbursed to the Buyer. 

  

	8.6.	The Seller agrees to reimburse the labour cost at *** Euros per labour hour linked with the removal and re-installation and adjustment operations for the Parts
for which the benefit of the warranty has been recognized. The total reimbursement cannot exceed *** Euros (Euros ***) per Helicopter or Option Helicopter during the period of twenty four (24) months. 

 

	8.7.	The Seller’s warranty shall apply only to the extent the Helicopter, Option Helicopter or RFR Helicopter and the Parts installed therein are operated and
maintained in accordance with the instructions contained in the Technical Documentation. 

  

	8.8.	Normal wear and tear of components such as, but not limited to, seals, tires, inner tubes, bulbs, packings and similar consumables Parts, as well as Parts whose
list price is 50.00 Euros or less, are excluded from this warranty. 

  

	8.9.	The turbine engines as well as the radio communication/radio navigation equipment, mission equipment and software incorporated in the Helicopters and Option
Helicopters are covered by the warranty granted by the manufacturers of these items, the benefits of which the Seller hereby assigns to the Buyer to the extent such manufacturer’s warranty exists and is assignable. Any further claims against
the Seller related to these items shall therefore be excluded. In addition, the Seller will have no liability whatsoever for Buyer furnished equipment. 

  

	8.10.	The incorporation by the Buyer in any Helicopter or Option Helicopter of any modification which has not been recommended by or received the prior approval of the
Seller shall cause the warranty to cease in respect of such Helicopter or Option Helicopter. Additionally this warranty shall not apply to any Helicopter, Option Helicopter or Part which, without the prior consent of the Seller, has been repaired or
altered outside the Seller’s factory or approved repair centre. 

  
 23 

			
	

	  	

  
 The warranty
shall cease to apply to any Parts that are put back into service after being removed from a Helicopter or Option Helicopter involved in an accident unless the Buyer can prove that the defect is not the result of the accident. 

 

	8.11.	This warranty is granted to the Buyer personally and shall not be assigned by the Buyer without the Seller’s prior written consent, provided however that the
Seller shall consent to assign this warranty to a financial institution in connection with any novation of rights under this Contract or any sale leaseback of any Helicopter or Option Helicopter to such financial institution.

  

	8.12.	The warranty terms herein defined reflect the conditions valid at the time of the signature of the Agreement. Any improvement in those terms to occur as a
modification of the Seller’s standard warranty terms or as an improvement of the vendors’ warranty conditions to the Seller shall be applicable and or transferable to the Buyer or any person to which Article 8.11 applies.

  
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 ARTICLE 9 – TRAINING

 The Seller shall provide pilot and technician training according to the conditions specified in this Article 9. The
courses are provided free-of-charge in English. 
  

	9.1.	GENERAL 

 The
training shall be completed for the pilots no later than the Delivery Date of the last Helicopter or Option Helicopter and for the technicians no later than six (6) months after the Delivery Date of the last Helicopter or Option Helicopter.

 The following expenses shall be borne by the Buyer for its personnel: 

 

	 	•	 	 Coverage of ground and in-flight risks incurred by its personnel and risks arising from the civil liability of this same personnel,

  

	 	•	 	 Travelling expenses from the Buyer’s country to the place of the training and back, 

Except for cases of negligence of the Seller, the Buyer shall be responsible for loss and damage to the Buyer’s property, at all
times while at the Seller’s facilities. 
 Personal information required from the Buyer’s representatives in order to
be granted access to Seller’s premises shall be forwarded by the Buyer to the Seller at least four (4) weeks prior to their dates of arrival. 
 The schedule, date and place. for the courses will be mutually agreed upon no later than six (6) months prior to the delivery of the Helicopter. If the Buyer fails to send its personnel at the date
agreed upon without informing the Seller within a two (2) month notice, it shall lose the benefit of this training. 
 The
Seller reserves the right to define a set of minimum competency requirements for any pilot to be trained within this Contract and to refuse any pilot not meeting those requirements or to provide additional training and/or professional translation
services, at prevailing rates and dates. 
 In case of training flights conducted by the Seller on the Buyer’s Helicopter at
the Seller’s facility, the risks in flight arising from these instruction flights will be covered by the Seller’s insurance. 
 In case of training flights or on-the-job training conducted by the Seller on the Buyer’s Helicopters at the Buyer’s facility, the Helicopter will be fully insured by Buyer for any loss or
damage. The insurance policy will contain a waiver of subrogation in favour of the Seller and its subcontractor. The Buyer shall produce the insurance certificate including this specific provision before the beginning of training. 

Third party and passenger liability will be fully insured by the Buyer, and the Seller’s instructor will be included as an additional
insured. 

  
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	9.2.	PILOT TRAINING 

 The
Seller will provide ground training and flight conversion training (type rating) according to the program set up by the Seller’s flight training department in France. 
 The conversion training will be given to two (2) trainees per purchased helicopter. 
 Buyer’s trainees will be already proficient multi engine helicopter pilots and fluent in English. This training will be provided for Instrument Flight Rules (IFR) operation when the pilots are
already IFR qualified or for Single Pilot VFR operation when the pilots are not IFR qualified. The Single Pilot VFR type rating with Multi Pilot IFR extension training (TR3) for two (2) pilots is approximately four (4) weeks in duration
including nineteen (19) hours on simulator (test included) and three (3) flight hours. 
 Such practical training will
be conducted by the Seller in Helisim Marignane or in any of its other EASA approved EC225 flight training devices (Aberdeen, UK for the first years of the contract execution). Place of practical training will be communicated by the Seller according
to training means and instructors availability. 
 According to National Civil Aviation Authorities requirements or
simulators’ lack of availability, such training could be performed on the Buyer’s Helicopter. In these cases, flights are always conducted under the responsibility of one of the Seller’s pilots acting as chief pilot. 

During the training conversion, The Seller shall take charge of the 0 level maintenance options on the Helicopter. 

 

	9.3.	TECHNICIAN TRAINING 

 The
Seller will or procure that the engine manufacturer will provide ground training courses for the Buyer’s confirmed technicians at the Seller’s and engine manufacturer’s training departments in France. 

The Seller will provide per delivered Helicopter, Option Helicopter, or RFR Helicopter ground training course for two (2) technicians
for up to four (4) weeks airframe course and one (1) week engine course; and one (1) technician for up to our (4) weeks avionics course. 
  

	9.4.	TRAINING ENTITLEMENT CREDITS 

 The Buyer accepts to entirely forego its rights under the training provisions defined here above within clause 9.1, 9.2 and 9.3. In exchange, upon each Helicopter being paid and delivered, the Seller
shall grant to the Buyer a credit note in the sum of *** Euros (€***). No credit shall be converted into cash. Such credit note shall only be valid for offset against future invoices issued by the Seller for products or services purchased by
the Seller to support its Helicopter (including, but not limited to, training services). 

  
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 ARTICLE 10 –
TECHNICAL ASSISTANCE 
 To complement the training of its specialists and assist the Buyer during the initial operation
period of the Helicopters, the Seller shall detach to the Buyer’s country, at no charge and on a date to be agreed upon, one or more technicians for a cumulated duration, per helicopter purchased of two (2) man months. 

At the Buyer’s election, this detachment shall take place either at the moment of the first basic inspection, or at any time chosen
by the Buyer, but in any case, at the latest fifteen (15) months after the delivery of the last Helicopter in the agreement, failing which the Buyer will lose the benefit of this service. 

The work time of the Seller’s detached personnel shall not exceed forty (40) hours a week. For the detached technicians, only
the following expenses shall be borne by the Buyer: 
  

	 	•	 	 the travelling expenses to the country of the Buyer and back; and, 

 

	 	•	 	 the transport expenses within the Buyer’s country when on duty, including the travel expenses from their place of residence to work and back.

 It is agreed, that the Buyer may use the technical assistance to which it is entitled hereunder on one or
more of the Helicopters, Option Helicopters or RFR Helicopters. In all cases, such planning has to be approved with the Seller Technical Assistance organisation in advance. 
 No technical assistance entitlement hereunder shall be converted into cash, except that after a period of two (2) years from the date of the Helicopter delivery date, where the Buyer has not taken
advantage of this technical assistance service, the Seller shall issue in the Buyer’s favour a credit note for an amount of *** Euros (*** €) for the aforementioned two months. Such credit note will be valid for offset against future
invoices issued by the Seller for products and services purchased by the Buyer or its affiliates from Seller or its affiliates. 

  
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 ARTICLE 11 –
TECHNICAL DOCUMENTATION 
  

	11.1.	The Seller shall provide per delivered Helicopter, Option Helicopter and RFR Helicopter the following technical publications in English:

  

	 	•	 	 one copy of interactive electronic support (DVD ROM) with the documentation necessary for the maintenance of the helicopter and for the identification
of parts for operation and routine servicing, 

  

	 	•	 	 one hard copy of : 

  

	 	•	 	 The Flight Manual (1 copy) 

  

	 	•	 	 A set of Service Bulletins (1 set) 

  

	 	•	 	 The Master Servicing Recommendation Manual (1 copy) 

  

	 	•	 	 access to Technical Information Publication on Internet (T.I.P.I.) for : 

 

	 	•	 	 The Service Bulletins and their subsequent updates; 

  

	 	•	 	 The Master Servicing Manual. 

 The Flight Manual and the Master Servicing Recommendation Manual shall be consistent with the helicopter definition after the completion made by the Buyer as per Annex 1. 

This documentation will be initially provided at the latest available revision level. Customization of the documentation due to new
equipment or installations specific to the Buyer will be provided for maintenance documentation within four (4) months after delivery of the first Helicopter and for identification documents not later than twelve (12) months after same
delivery date. 
 DVD ROM updates of the provided documentation (Flight Manual, the Master Servicing Manual and the Services
Bulletins) will be supplied free of charge by the Supplier as long as the helicopter is in operation. The Master Servicing Manual and the Service Bulletins will be updated on T.I.P.I. on a regular basis. 

The Buyer undertakes to notify the Seller of any change either in the Buyer’s address or in the owner’s name if the helicopter
has been sold in the meantime. 
  

	11.2.	One set of engine documentation on hard copy format per helicopter will be delivered as follows: 

 

	 	•	 	 Engine Maintenance Manual 

  

	 	•	 	 Engine Illustrated spare parts and tools lists 

  

	 	•	 	 Engine Service Bulletins 

ARTICLE 12 – INTELLECTUAL PROPERTY 
 The Seller retains all rights in respect of developments, inventions, production procedures and any intellectual property rights relating to the subject of the Contract. Copying and/or reproducing the
Seller’s Supplies (including software) or publications, either wholly or partially, without the Seller’s express approval is not permitted. 

  
 28 

			
	

	  	

  
 Nothing in
this Contract shall be construed as a legal transfer of any patent, utility or design model, copyright, trademark or other intellectual property right. 
 The Seller will defend the Buyer against any claim that any of the Deliverables sold or otherwise furnished by the Seller to the Buyer under this Contract infringes a patent or copyright in any
jurisdiction where the Seller obtains an export license for such Deliverables. The Seller will pay all costs, damages and legal fees that a court finally awards as a result of such a claim, provided that the Buyer gives the Seller prompt written
notice of the claim, cooperates fully with the Seller in its defence, and gives the Seller sole authority to control the case and any related settlement negotiations. The Seller will not be responsible for any settlement or payment made without its
prior consent. 
 If in the Seller’s opinion any of the Deliverables are likely to become the subject of a claim pursuant to
Article 12.3, the Buyer will permit the Seller, at the Seller’s option and expense, to either secure for the Buyer the right to continue using the Deliverables or replace or modify the Deliverables so that it becomes non-infringing without
materially affecting the performance or specifications of the Deliverables or the Buyer’s ability to use them. If neither of these alternatives is available on terms acceptable to the Seller, then the Buyer will return such Deliverables to the
Seller, at its request, and the Seller will refund the purchase price for such Deliverables to the Buyer. 
 The Seller will not
be obligated to the Buyer under this Article 12 for any claim which is based upon: 
  

	 	(a)	any alteration, modification or repair of the Deliverables made by a person other than the Seller, without the Seller’s prior consent; 

 

	 	(b)	any non-compliance by the Buyer or any other person with the Seller’s Technical Documentation or any other designs, specifications or instruction provided by the
Seller to the Buyer; or 

  

	 	(c)	any use or operation of the Deliverables with other products or equipment not manufactured or supplied by the Seller, unless authorized by the Seller.

  
 29 

			
	

	  	

  
 ARTICLE 13 –
APPLICABLE LAW AND ARBITRATION 
 This Contract shall be governed and interpreted in accordance with French Law. 

The Seller and the Buyer shall take all measures to settle any dispute that may arise out of or in connection with this Contract by way of
negotiation. Either the Buyer or the Seller may request for such negotiation by written notice to the other. 
 In the event the
Buyer and the Seller fail to resolve the dispute, within a period of three (3) months, either of them may refer such dispute to arbitration. Such period shall commence from the date of notification of the dispute, by registered letter with
recorded delivery, addressed by either Party to the other. 
 All unresolved disputes should be finally resolved in accordance
with the arbitration rules of the International Chamber of Commerce by three (3) arbitrators appointed in accordance with the said Rules, unless the Parties agree on the appointment of a sole arbitrator. 

The arbitration shall take place in Paris, France. The language of the arbitration shall be English. Only the English language shall be
used by the Parties to settle any dispute arising here from. Any Party submitting evidence of any kind in another language shall bear the cost of translation or interpretation of such evidence into the English language. 

It is expressly agreed that the arbitration award shall be final and binding upon the Parties. 

The occurrence of any dispute shall not entitle the Parties to suspend performance of the Contract. 

  
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 ARTICLE 14 –
CONTRACTUAL LIABILITY 
 The purchase of the Supplies by the Buyer is performed within the framework of its professional
activities and the Buyer hereby expressly agrees to the limitations of liability as defined in this Contract. 
 Notwithstanding
anything else to the contrary in this Contract or in non-mandatory/dispositive laws, neither the Seller nor the Buyer shall be liable for indirect or consequential damages and/or losses. 

The Parties obligations liabilities, rights and remedies as set forth in this Contract are exclusive and are in replacement of any and all
other remedies under any law or otherwise. 
 The Seller’s liabilities under this Contract for, based on, or by way of any
liquidated damages, damage(s), penalties, compensation(s), retention(s) of payment(s), any interest(s) thereon where applicable, shall in no event exceed in total 50% of the Contract Price. 

The Seller’s product liability shall however be limited to the amounts actually recovered from Seller’s insurance. 

  
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 ARTICLE 15 –
MISCELLANEOUS 
  

	15.1.	ENTIRETY OF THE CONTRACT AND AMENDMENTS 

 These terms and conditions along with the specific conditions explicitly contained and accepted in this Contract including Annexes constitute the entire agreement between the Seller and the Buyer. They
supersede all previous communications or agreements, either oral or written, between the Seller and the Buyer with respect to the object of the Contract. Any amendment of the Contract will only be valid if it is agreed in writing by the Parties.

  

	15.2.	CONFIDENTIALITY 

The Parties shall at all times keep confidential, treat as privileged, and not directly or indirectly make or allow any disclosure of, or
use of, any provision of this Contract or any information relating to any provision or subject matter of this Contract, or any information directly or indirectly obtained from another party under or in connection with this Contract, except to the
extent: 
  

	 	•	 	 required by law or the order of a court of competent jurisdiction, or 

 

	 	•	 	 required by the Buyer to obtain financing of the Supplies, or 

 

	 	•	 	 required for the purpose of conducting the arbitration proceedings hereunder, or 

 

	 	•	 	 it is shared with the Parties’ affiliated companies, or 

 

	 	•	 	 that the Parties otherwise agree in writing. 

  

	15.3.	LANGUAGE 

 This
Contract with its Preamble, Articles and Annexes shall be in English. All correspondence between the Parties shall be in English. 
  

	15.4.	ASSIGNMENT 

Neither Party shall be entitled to directly or indirectly assign, transfer, mortgage, charge, pledge or otherwise dispose of any rights or
interests in, or any of its obligations or liabilities under, or in connection with, or arising out of, this Contract, except with the prior written consent of the other Party, which consent may not be unreasonably withheld. Notwithstanding anything
to the contrary, the Seller and Buyer shall be entitled to directly or indirectly (including due to, or by way of, a change of control) assign, transfer, mortgage, charge, pledge or otherwise dispose of (including by way of sub-contract,
amalgamation or merger) any rights or interests in, or any of its obligations or liabilities under, or in connection with, or arising out of, this Contract, to its parent companies or any of their directly or indirectly controlling, controlled or
participated companies. 

  
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 Further,
Buyer may novate or assign, by way of security or otherwise, all or any part of its rights and obligations hereunder to one or more financial institutions in connection with it’s financing of the Supplies (a “Financier Disposal”).

 Any expenses incurred in relation to a Financier Disposal (including, without limitation, legal expenses for which the Seller
is responsible if any), will be borne by the Buyer. 
 The Buyer agrees to co-operate with the Seller in the event that the
Seller wishes to sell or assign or novate all its rights and obligations under Article 18.1 to any third party (a “Seller Disposal”). 
 Any expenses incurred in relation to a Seller Disposal (including, without limitation, legal expenses for which the Seller is responsible if any), will be borne by the Seller. 

Further if any assignment, transfer, etc. by Seller will have the effect of increasing any cost of Buyer ***, such assignment, transfer,
etc. may only be effected if Seller indemnifies Buyer against such increased costs. 
  

	15.5.	NOTICES AND CORRE$POOKNCE 

 All notices and correspondence between the Parties under this Contract will be provided in accordance with Annex 3. 
  

	15.6.	GRADUATION. MARKINGS, PAIKESCUME 

 Graduation, markings and paint scheme shall be as described in Annex 4 and the detailed Configuration Document in Annex 1. 
  

	15.7.	*** 

  
 33 

			
	

	  	

  
 ARTICLE 16 – ENTRY
INTO FORCE 
 All terms and conditions stipulated herein have been duly noted and approved by both parties. This Contract
shall enter into force upon: 
  

	 	•	 	 signature of the Contract by both Parties, 

  

	 	•	 	 receipt by the Seller of the initial down-payment of EUR*** as per Article 3.2, and 

 

	 	•	 	 approval by the Buyer’s board of directors. 

 In the event that any of the conditions precedent in the immediately preceding paragraph are not fulfilled by September 28th , 2011 this Contract shall not come into force and shall be null and void
and of no effect. 

  
 34 

			
	

	  	

  
 ARTICLE 17 – ***

  
 35 

			
	

	  	

  
 ARTICLE 18 – SPECIAL
CONDITIONS 
  

	18.1.	*** 

  

	18.2.	*** 

  

	18.3.	*** 

  

	18.4.	*** 

  

	18.5.	*** 

  

	18.6.	*** 

  

	18.7.	*** 

  

	18.8.	*** 

  
 36 

			
	

	  	

  
 ARTICLE 19 – TAX AND
DUTIES 
 The Buyer shall be liable for and shall pay all transfer taxes, sales taxes, and all other taxes, duties or other
like charges properly payable in connection with the conveyance and transfer of the Deliverables by the Seller to the Buyer. Therefore, the Buyer shall ensure that the sums received by the Seller for the sale of the Helicopters shall be equal to the
full amounts expressed to be due, without deduction or withholding on account of and free from any and all taxes. If the Seller is compelled by law to make any such deduction or withholding, the Buyer shall pay such additional amounts as may be
necessary in order that the net amount received by the Seller after such deduction or withholding shall equal the amounts which would have been received in the absence of such deduction or withholding. 

Notwithstanding the taxes paid by the Buyer as above mentioned, the Seller shall be liable for and shall pay income, capital gains or
similar taxes in connection with the conveyance and transfer of the Deliverables by the Seller to the Buyer in France. 
 The
Seller will ensure that all reasonable efforts are undertaken to exempt or zero rate for value added tax (or any similar tax, duty or charge) purposes the Deliverables under this contract. 

The Seller shall, acting reasonably, cooperate with the Buyer to mitigate any tax costs payable by the Buyer. 

  
 37 

			
	

	  	

  
 ARTICLE 20 –
REPRESENTATWNS AND WARRANTIWOF THE BUYER 
 The Buyer is a company duly incorporated or continued, organized and validly
existing under the laws of Ireland. 
 The Buyer has all necessary corporate power, authority and capacity to enter into this
Contract and to perform its obligations; the execution and delivery of this Contract and the consummation of the transactions contemplated have been duly authorized by all necessary corporate action on the part of the Buyer. 

This Contract constitutes a valid and binding obligation of the Buyer, enforceable against it in accordance with the terms of this
Contract, subject, however, to limitations with respect to enforcement imposed by law in connection with bankruptcy or similar proceedings and to the extent that equitable remedies such as specific performance and injunction are in the discretion of
the court from which they are sought. 
 The Buyer is not a party to, bound or affected by or subject to any liquidation,
bankruptcy, indenture, mortgage, lease, agreement, instrument, charter or by-law provision, order, judgment or decree which would be violated, contravened or breached by the execution and delivery by it of this Contract or the performance by it of
any of the terms. The Buyer undertakes to inform immediately the Seller of any changes in its situation relating to these aforementioned items. 

  
 38 

			
	

	  	

  
 ARTICLE 21 –
REPRESENTATIONS AND WARRANTIES OF THE SELLER 
 The Seller is an entity duly incorporated or continued, organized and validly
existing under the laws of France. 
 The Seller has all necessary corporate power, authority and capacity to enter into this
Contract and to perform its obligations; the execution and delivery of this Contract and the consummation of the transactions contemplated have been duly authorized by all necessary corporate action on the part of the Seller. 

This Contract constitutes a valid and binding obligation of the Seller, enforceable against it in accordance with the terms of this
Contract, subject, however, to limitations with respect to enforcement imposed by law in connection with bankruptcy or similar proceedings and to the extent that equitable remedies such as specific performance and injunction are in the discretion of
the court from which they are sought. 
 The Seller is not a party to, bound or affected by or subject to any liquidation,
bankruptcy, indenture, mortgage, lease, agreement, instrument, charter or by-law provision, order, judgment or decree which would be violated, contravened or breached by the execution and delivery by it of this Contract or the performance by it of
any of the terms. The Seller undertakes to inform immediately the Buyer of any changes in its situation relating to these aforementioned items. 

  
 39 

			
	

	  	

  
 ARTICLE 22 –
TERMINATION 
  

	22.1.	WALK-AWAY 

Starting from Helicopter n° 11, and to the extent that helicopter prices have not been re-denominated in US Dollars according to
Article 16 above, if the average of the daily fixing EUR/USD exchange rate published by the European Central Bank in the six (6) months preceding the date which is 19 months prior to the Delivery Date of each Helicopter, Option Helicopter or
RFR Helicopter exceeds ***, the Parties agree to meet and further discuss the competitiveness of the EC225 in the new context. In such context if no agreement is met and as a last recourse the Buyer will have the right to terminate any Helicopter,
Option Helicopter or RFR Helicopter in relation to which the aforementioned circumstances apply. 
  

	22.2.	TERMINATION BY DEFAULT OF THE BUYER 

 Should the Buyer fail (i) to pay the final balance due in respect of a Helicopter, Option Helicopter or RFR Helicopter after the remedy period provided in Article 7.4 (ie. 3 months from payment being
due), or (ii) to accept a Helicopter, Option Helicopter or RFR Helicopter after the remedy period provided in Article 7.5 (ie. 75 days from default notice) , the Parties agree that Seller shall be entitled to terminate that part of this
Contract related to the unpaid or unaccepted Helicopter, Option Helicopter or RFR Helicopter. 
 Should any such default occur
more than twice, the Seller may terminate the whole Contract in its sole discretion. In such case, any payments made under the Contract shall be retained by the Seller unless specified differently in the previous articles. • 

This Contract with its Preamble, twenty two (22) Articles and its Annexes 1, 2, 3, 4, 5, 6, and 7 is made in two original copies in
the English language, for each Party to hold one. The English text of this Contract shall be valid and binding upon the Parties hereto. 
 This Contract cancels and supersedes all prior representations, negotiations and commitment whether oral or written, and shall be considered as the entire Contract between the PARTIES with respect to its
scope and there shall be no terms, obligations, covenants, representations, warranties, statement or conditions other than those contained herein 

  
 40 

			
	

	  	

  
 In witness
whereof, the Parties duly authorized have hereunder set their respective hands and seals on the date first before set out herein. 
  

	 	Signed	for and on behalf of the Buyer 

  

	
	  

	William J. Amelio
	CEO CHC Helicopter
	Authorized Signatory

  

	 	Signed	for and on behalf of the Seller 

  

	
	  

	Dr. Lutz Bertling
	CEO Eurocopter
	Authorized Signatory

  
 41 

			
	

	  	

  
 ANNEX 1

 HELICOPTER CONFIGURATION 

 

					
	 	 	Reference	 	Designation
	1.1	 	00-10029-00-CI	 	EC 225 Baseline Aircraft (225 10.100.01 E)
		
	1.2	 	“EC225 Crew Change” package including:
			
		 		 	Space provisions and common basic wirings for the following SAR optional equipments:
		 		 	 •      dual FMS and dual GPS installation with centralized radio management by
FMS

		 		 	 •      hoistman console with joystick (hover trim)

		 		 	 •      second radar altimeter

		 		 	 •      Vertical light for hoisting and sling operation surveillance

			
		 		 	General Items of Equipment
			
		 	05-02012-00-CI	 	Instrument panel and cockpit painted in black
		 	05-03006-00-CI	 	First aid kit - JAR OPS 3 compatible
		 	05-35005-00-CI	 	Crashworthy Floor
		 	05-39026-00-CI	 	Enlarged footstep cabin on both sides
		 	05-39002-00-CI	 	Illuminated Map Holder - JAR OPS 3 compatible
		 	05-50003-00-CI	 	Kit for flight in limited icing conditions
		 	05-51001-00-CI	 	De-iced cockpit center pane with wiper
		 	05-51006-00-CI	 	Goodrich Icing severity indicator (ex-Rosemount)
		 	05-65000-00-CI	 	Hydro electric group
		 	05-81031-00-CI	 	Energy Absorbing central auxiliary fuel tank 318 I (84 US gal)
		 	05-82005-00-CI	 	Pressure refuelling on the ground
			
		 		 	Specific Mission Equipment
			
		 	06-21015-00-CI	 	Goodrich 28V electrical hoist (290ft, 6001b) - Fixed parts
		 	06-26006-00-CI	 	External mirrors (recommended for sling) - Fixed parts
		 	06-27013-00-CI	 	Cargo sling with dynamometer 3,8 Tons - Fixed parts
		 	06-41003-00-CI	 	Hella anticollision strobe light system (instead of standard one)
		 	06-41004-00-CI	 	JPC Anti collision light (belly mounted)
		 	06-42012-00-CI	 	Fixed lights in the sponsons
		 	06-60004-00-CI	 	2 Life rafts - 18 to 27 pax - in the multipurpose sponsons with jettison control in cockpit
		 	06-61011-00-CI	 	Emergency floatation gear with automatic firing
		 	06-65008-00-CI	 	3rd hand held fire extinguisher - JAR OPS 3 compatible
		 	06-65010-00-CI	 	2 Flashlights - JAR OPS 3 compatible
		 	06-66004-00-CI	 	Helicopter Emergency Egress Lighting (HEEL)
		 	06-67023-00-CI	 	HR Smith series 503 ADELT linked to GPS signal

  
 42 

			
	

	  	

  
  

					
		 		 	Interior layout
			
		 	07-10009-00-FP	 	3rd crew man seat - Fixed parts
		 	07-15009-00-CI	 	Pilot and copilot crashworthy seats
		 	07-27002-00-CI	 	19 crashworthy seat installation
		 	07-30007-00-CI	 	Comfort upholstery with improved sound-proofing
		 	07-60016-00-CI	 	Luggage compartment in the intermediate structure
			
		 		 	Avionics
			
		 	08-00016-04-CI	 	Civil Use minimum equipment (IFR dual pilot)
		 	08-12039-00-CI	 	Collins - Praline 21— VHF/AM #1
		 	08-12039-01-CI	 	Collins - Proline 21— VHF/AM #2
		 	08-16023-00-CI	 	NAT DACS IS - Basic set 3 control panels in cockpit
		 	08-22007-00-CI	 	Collins - TDR 94 D-008 (S mode) Transponder
		 	08-25026-00-CI	 	Collins - Proline 21— DME
		 	08-26008-00-CI	 	Collins - Proline 21— VOR/ILS/MKR/ADF #1
		 	08-26008-01-CI	 	Collins - Proline 21 — VOR/ILS/MKR #2
		 	08-12025-00-CI	 	NAT - NPX138 VHF/FM-H
		 	08-16026-00-CI	 	NAT DACS ICS - Complementary set : 4th control panel
		 	08-17049-00-CI	 	NAT - Passenger Address
		 	08-22007-02-CI	 	Collins - TDR94D - 409 instead of Collins - TDR94D — 008
		 	08-27008-00-CI	 	Chelton System 7 - (121,5) VHF/FM Marine dual frequency homer
		 	08-31039-00-CI	 	Telephonics 1600 Weather Radar, displayed on AHCAS
		 	08-35015-00-CI	 	EGPWS - HONEYWELL - MOM integrated to AHCAS
		 	08-35050-00-CI	 	TCAS II - COLLINS - TTR 4000 integrated to AHCAS and coupled to AFCS
		 	08-41016-00-CI	 	Canadian Marconi - CMA5024 - GPS receiver
		 	08-44040-00-CI	 	Canadian Marconi - CMA9000 - Flight Management System
		 	08-83004-01-CI	 	M’ARMS Health & Usage Monitoring System (HUMS) with HOMP & Allied Combi-lite CVFDR
		
	1.3	 	Additional optional equipment
			
		 	05-42021-00-FP	 	Air conditioning system — Fixed Parts (for cockpit and cabin)
		 	05-42021-00-RP1	 	Air conditioning system - Removable Parts 1 (cabin power unit)
		 	05-81004-00-FP	 	Additional Energy Absorbing pod fuel tanks - Fixed parts
		 	05-82005-01-CI	 	Pressure refuelling on the ground (air conditioning compatible)
		 	06-64002-00-CI	 	Sea anchor
		 	06-67026-01-FP	 	Serpe - IESM Kannad 406 AP - Emergency Locator Transmitter connected to GPS instead of Serpe - IESM Kannad 406 AP — ELT
		 	07-60009-00-FP	 	Luggage compartment in pod - Fixed parts
		 	08-15529-00-CI	 	SKYTRACK SATCOM

 The empty weight of each Helicopter or Option Helicopter delivered with the configuration contracted and described above,
will be of a maximum targeted weight of 6660 kg (the “Maximum Targeted Weight”). Modifications to the Helicopters or Option Helicopters in accordance with clauses 5.1 and 5.3 may increase the weight and in the event of any such
modifications the Parties shall agree on the new weight. 

  
 43 

			
	

	  	

  
 In the event that the actual
empty weight of a delivered Helicopter or Option Helicopter is above the Maximum Targeted Weight but below 6730kg (i.e., roughly 1% above the Maximum Targeted Weight), the Seller will employ its best efforts to propose a weight reduction solution
(such as but not limited to equipment trade off, pre-wiring or capabilities removal) within 6 months after the delivery to the Buyer. Such weight discrepancy will not constitute a valid ground for refusing to accept a Helicopter or Option
Helicopter. 
 In the event that the actual empty weight of a delivered Helicopter or Option Helicopter is above 6730kg, the Seller will employ
its best efforts to find a solution within 6 months after the initial delivery date. Such weight discrepancy will constitute a valid ground for refusing to accept a Helicopter or Option Helicopter so long as no solution is found by the Seller to
bring the actual empty weight at or below the Maximum Targeted Weight. 
 The above weight guarantee does not apply to RFR helicopters or other
helicopters allocated following a specific request. 
 A detailed specification document will be provided to the buyer 15 months before the
delivery date of each Helicopter, Option Helicopter and RFR Helicopter. This document will contain information such as: pedestal layout, softwares’ version of major systems, interior views and sitting layout, graduation, marking and paint
scheme. 

  
 44 

			
	

	  	

  
 ANNEX 2

 DELIVERIES 
 HELICOPTERS 
 Deliveries are ex-works Marignane, Eurocopter factory. 

 

					
	Rank in this Contract	 	Eurocopter code name	 	Delivery Date
	1st EC225	 	HLO 25	 	End February 2012
	2nd EC225	 	HLO 26	 	End March 2012
	3rd EC225	 	HLO 29	 	End September 2012
	4th EC225	 	HLO 30	 	End December 2012
	5th EC225	 	HLO 31	 	End May 2013
	6th EC225	 	HLO 32	 	End July 2013
	7th EC225	 	HLO 33	 	End October 2013
	8th EC225	 	HLO 34	 	End December 2013
	9th EC225	 	HLO 35	 	End February 2014
	10th EC225	 	HLO 36	 	End April 2014
	11th EC225	 	HLO 37	 	End July 2014
	12th EC225	 	HLO 38	 	End October 2014
	13th EC225	 	HLO 39	 	End December 2014
	14th EC225	 	HLO 40	 	End February 2015
	15th EC225	 	HLO 41	 	End May 2015
	16th EC225	 	HLO 42	 	End July 2015
	17th EC225	 	HLO 43	 	End October 2015
	18th EC225	 	HLO 44	 	End December 2015
	19th EC225	 	HLO 45	 	End February 2016
	20th EC225	 	HLO 46	 	End May 2016

 OPTION HELICOPTERS: 
  

					
	Rank in this Contract	 	Eurocopter code name	 	Delivery Date
		 	HLO Option 1	 	End November 2013
		 	HLO Option 2	 	End December 2013
		 	HLO Option 3	 	End March 2014
		 	HLO Option 4	 	End March 2015

  
 45 

			
	

	  	

  
 ANNEX3

 NOTICES and CORRESPONDENCE 
 Any notice provided for in this Contract to be given by either Party to the other hereunder shall be in writing and shall be delivered by hand, registered mail, return receipt required, or by national
courier service or by facsimile transmission to the following address: 
 The address, facsimile and telephone numbers of the Parties are those
set out below or such other address, facsimile and telephone numbers as may be notified by one party to the other in writing: 
 If to Seller:

 Eurocopter S.A.S. 
 Aeroport
International Marseille-Provence, 
 13725 Marignane Cedex, 
 France, 
 Tel : + 33 442 85 5626 
 Fax : + 33 442 85 8300 
 Attn: Mr.VIGNEAU Alain 

Title: Regional Sales Manager 
 If to Buyer:

 CHC Leasing (Ireland) Limited 
 c/o
Heli-One Canada Inc. 
 4740 Agar Drive, 

Richmond, British Columbia V7B 1A3, 
 Canada

 Tel: + 1 604 276 7500 
 Fax: + 1 604
232 8341 
 Attn: Jeff Scotland 
 Title:
Vice President, Fleet 
 All notices shall be deemed to be delivered: 

 

	a)	if delivered by hand, on the day of delivery; 

  

	b)	if sent by facsimile, on the next business day after the date of sending; or 

 

	c)	if sent by courier or registered mail, upon receipt by the applicable Party. 

  
 46 

			
	

	  	

  
 ANNEX 4

 MARKINGS 
 GRADUATION OF THE INSTRUMENTS, MARKINGS AND EXTERIOR FINISH 
 4.1. Graduation of
Instruments 
 The flight instruments shall be graduated as follows: 

 

	 	•	 	 airspeed indicator : Knots 

  

	 	•	 	 altimeter : Feet 

  

	 	•	 	 rate-of-climb : Feet/mn 

  

	 	•	 	 hydraulic pressure : Bars 

  

	 	•	 	 fuel gauges : Kg 

  

	 	•	 	 fuel tanks capacity : Litres 

  

	 	•	 	 Temperatures : °C 

  

	 	•	 	 Weight and centre of gravity : Kg & m 

 4.1.2 Markings and Exterior Finish and Interior Upholstery 
 Based on a
sample provided timely by the Seller, not later than one (1) month after signature of the Contract, the Buyer shall provide detailed instructions for the external paint scheme, national emblems, identification or registration within two
(2) months after signature of the Contract. 
 The markings shall be in English language. 

  
 47 

			
	

	  	

  
 ANNEX 5

 CERTIFICATE OF CONFORMITY 

 

					
	  
  
 eurocopter
 an EMS Company
 Etablissement de Marignane 13725 Marignane Cedex — France
 Certified under ISO 9001, EN 9100
and AQAP 2110
	  	 Réference du certificat:

Certificate reference number

	
	 Certificat de conformité
 Certificate of conformity

	
	Fourniture : Fourniture Appareil/Aircraft type : N° de serie/serial N° :
	
	 Nous declarons que la fourniture citee est conforme aux exigences du contrat et que, apres verifications et essais, elle
repond en tous points, aux exigences specifiees, aux normes et reglements applicable (navigabilite comprise), sauf exceptions, reserves ou derogations enumerees dans le present certificat de conformite.

 
 We hereby certify that the above mentioned supply complies with the contract
requirements and that after completion of inspections and tests, it fully meets the specifications and applicable standards and regulations (including Airworthiness), except for the deviations, limitations and concessions listed
thereunder.

		
	Marche N° : Contract N°	 	Date du marche : Contract date
	
	Exceptions, reserves ou derogations : Deviations, limitations or concessions

  
 48 

			
	

	  	

  
 ANNEX 6

 *** 

  
 49 

			
	

	  	

  
 ANNEX 7

 *** 

  
 50 

			
	

	  	

  
 ANNEX 8

 STORAGE CONDITIONS 
 The storage fees at Seller’s facilities in Marignane shall be *** Euros (EUR ***) per aircraft and per month and includes: 

 

	 	•	 	 insurance fees 

  

	 	•	 	 line maintenance of the helicopter, including engines 

 

	 	•	 	 storage fees 

  
 51Framework Agreement

 Exhibit 10.5 
 

 
 Framework Agreement 
 between 
 Agusta S.p.A. 

and 

CHC Helicopters International Inc. 

  

					
	CFA October 2007	  	Page 1	  	Contract Number 160507

 This Framework Agreement (hereafter “Agreement”) dated October 2007, by and between 

Agusta S.p.A., an Italian company, with a sole shareholder, having a registered office in Samarate, Cascina Costa (VA), Via Giovanni Agusta n.
520, Italy, stock capital Euro 702.537.000,00 fully paid up, number of registration at the Chamber of Commerce of Varese and Fiscal Code 02512010121, subject to the direction and coordination of Agusta N.V. (hereafter “Agusta”) 

and 
 CHC Helicopters International Inc. -
acting through its division Heli-One - a corporation organized under the laws of Canada, having a registered office at 4740 Agar Dr., Richmond, BC, Canada V7B 1A3 (hereafter “CHC”), 
 together referred to as the ‘Parties” or individually as a “Party”. 

Whereas: 
 Agusta and CHC have entered
into a Purchase Agreement Number 139030901 dated September 24, 2003 and a Contract Framework Agreement Number 139050404 dated April 25, 2005 (as amended, assigned, novated and supplemented from time to time) in respect of the purchase of
AB 139 helicopters (the “Original Purchase Agreement”). 
 Agusta is willing to sell and CHC is willing to purchase thirteen
(13) AW139 medium twin-engine helicopter (hereafter “AW139 helicopters”) and Agusta is willing to grant CHC an option to purchase and additional twenty (20) AW139 helicopters pursuant to the terms and conditions contained herein.

 Now therefore the Parties agree as follows: 
 Part 1: Purchase of Helicopters and Option to Purchase Helicopters 
 Agusta agrees to sell
and CHC agrees to buy against purchase agreements (“PA”) (the precise terms and conditions for each PA will be substantially as set out in the form of the PA attached as in Appendix 7 to this Agreement) thirteen (13) firm AW139
helicopters (the “Finn Helicopters”) and Agusta agrees to grant CHC the option to purchase and CHC agrees to purchase, upon notifying Agusta of its intention to exercise such option, twenty (20) optional AW139 helicopters (the
“Optional Helicopters”), to be delivered in accordance with the following delivery schedule and configurations: 
  

											
	FIRM PURCHASES
	 Calendar
 Year
	  	 Quantity (EMS or

Standard)
	  	 Projected

Delivery Date
	  	 Quantity

(Offshore or

Standard)
	  	 Projected

Delivery Date
	  	 TOTAL

	 2007
	  	1 (one) in EMS Configuration	  	November	  	1 (one) in Offshore Configuration	  	1 (one) in the 4th quarter	  	2

  

					
	CFA October 2007	  	Page 2	  	Contract Number 160507

											
	2008	  	1 (one) in EMS Configuration	  	March	  	2 (two) in Offshore Configuration	  	 1 (one) in the 3rd quarter
 1
(one) in the 4th quarter
	  	3
						
	2009	  	1 (one) in EMS Configuration	  	April	  	1(one) in Offshore Configuration	  	1 (one) in the 1st quarter	  	2
						
	2010	  	-	  	-	  	3 (three) in Offshore Configuration	  	 1 (one) in the 1st quarter
 1
(one) in the 3rd quarter

1 (one) in the
4th quarter
	  	3
						
	2011	  	-	  	-	  	3 (three) in Offshore Configuration	  	 1 (one) in
3rd quarter

1 (one) in the
3rd quarter

1 (one) in the
4th quarter
	  	3
						
		  		  		  		  	TOTAL FIRM PURCHASES	  	13
	
	
	OPTIONAL PURCHASES
	 Calendar
 Year
	  	 Quantity (EMS or

Standard)
	  	 Projected

Delivery Date
	  	 Quantity

(Offshore or

Standard)
	  	 Projected

Delivery Date
	  	 TOTAL

	2009	  	-	  	-	  	1 (one) in Offshore Configuration	  	1 (one) in the 4th quarter	  	1
						
	2010	  	-	  	-	  	2 (two) in Offshore Configuration	  	 1 (one) in the 3rd quarter
 1
(one) in the 4th quarter
	  	2
						
	2011	  	-	  	-	  	3 (three) in Offshore Configuration	  	 1 (one) in the 2nd quarter
 1
(one) in the 3rd quarter

1 (one) in the
4th quarter
	  	3
						
	2012	  	-	  	-	  	4 (four) in Offshore Configuration	  	 1 (one) in the 1st quarter
 1
(one) in the 2nd quarter

1 (one) in the
3rd quarter

1 (one) in the
4th quarter
	  	4

  

					
	CFA October 2007	  	Page 3	  	Contract Number 160507

											
	2013	  	-	  	-	  	5 (five) in Offshore Configuration	  	 1 (one) in the 1st quarter
 2
(two) in the 2nd quarter

1 (one) in the
3rd quarter

1 (one) in the
4th quarter
	  	5
						
	2014	  	-	  	-	  	5 (five) in Offshore Cm-figuration	  	 1 (one) in the 1st quarter
 2
(two) in the 2nd quarter

1 (one) in the
3rd quarter

1 (one) in the
4th quarter
	  	5
						
		  		  		  		  	TOTAL OPTIONAL PURCHASES	  	20

 The configuration of the AW139 helicopters shall be in accordance with Appendix 1 for AW139 standard configuration
(“Standard Configuration”), Appendix 2 for AW139 Offshore configuration (“Offshore Configuration”) and Appendix 3 for AW139 EMS configuration (“EMS Configuration”). Any changes or deviations to such configurations shall
be subject to a price and/or delivery date adjustment. For the purposes of clarification, if CHC performs the completion activities required for Offshore or EMS Configurations CHC shall inform Agusta, at least 12 months prior to the Projected
Delivery Date of its intention then Agusta shall deliver the AW139 helicopter to CHC on the Projected Delivery Date in Standard Configuration or in a partly completed Configuration. 
 In respect of each Firm Helicopter CHC agrees to sign a PA within eighteen (18) months of the Projected Delivery Date and in the case of each Optional Helicopter upon either the date it exercises its
option to purchase an Optional Helicopter or within eighteen (18) months of the Projected Delivery Date, whichever is earlier, in accordance with the terms and conditions shown in Appendix 7 “Purchase Agreement” and reflecting this
Agreement. 
 CHC shall have the option to require Agusta to re-schedule the projected delivery date for AW139 helicopters set forth above
(which for the purpose of this Agreement means the last day of the month or last month of the quarter shown in Part 1 (the “Project Delivery Date”) for up to a maximum of ten (10) AW139 helicopters by a maximum period of one hundred
and fifty (150) calendar days, by providing a written notification to Agusta to be sent no later then eighteen (18) months for EMS Configuration and no later then twelve (12) months for Offshore Configuration prior to the original
contracted Projected Delivery Date. 
 If CHC elects to re-schedule the Projected Delivery Date of an AW 139 helicopter then that AW139
helicopter cannot be re-scheduled again unless agreed to by Agusta. Any re¬scheduling of the Projected Delivery Date shall be subject to a price adjustment and shall be reflected in the applicable PA. 

  

					
	CFA October 2007	  	Page 4	  	Contract Number 160507

 Part 2: Financial Agreements 

 

	a.	AW139 Helicopter Pricing 

 a-1
The price of the thirty three (33) AW139 helicopters shall be in accordance with Agusta’s applicable delivery year price list (excluding applicable discounts as provided for in Part 4), which shall be confirmed in the applicable PA as
follows: 
 Table 1: Offshore pricing — US Dollars 

 

									
	 Delivery year
	  	 Standard

Configuration

(Appendix 1)
	  	 Offshore

Interior,

Provisions &

Installed

Equipment

(Appendix 2)
	  	 Removable

Parts &

Painting
 (Appendix
2)
	  	 Total Offshore

Configuration

(Appendix 2)

	 2007
	  	***	  	***	  	***	  	***
	 2008
	  	***	  	***	  	***	  	***
	 2009
	  	***	  	***	  	***	  	***
	 2010
	  	As per special conditions in Part 4
	 2011
	  
	 2012
	  

 Table 2: EMS pricing — US Dollars 

 

									
	 Delivery year
	  	 Standard

Configuration

(Appendix 1)
	  	 EMS Interior,

Provisions &

Installed

Equipment

(Appendix 3)
	  	 Removable

Parts &

Painting
 (Appendix
3)
	  	 Total EMS

Configuration

(Appendix 3)

	 2007
	  	***	  	***	  	***	  	***
	 2008
	  	***	  	***	  	***	  	***
	 2009
	  	***	  	***	  	***	  	***
	 2010
	  	As per special conditions in Part 4
	 2011
	  
	 2012
	  

 a-2 CHC may at its option, as outlined in Appendix 4 hereof, elect to take delivery of a Standard
Configuration AW139 helicopter and perform the completion activities required for Offshore or EMS Configuration AW139 helicopters purchased under this Agreement or the previous Framework Agreement dated 254 April 2005 , either in whole or in
part, starting from mid 2009, rather than requiring Agusta to do the same. Upon execution of this Agreement, Agusta shall: (i) grant CHC the right to perform the completion activities required for Offshore and/or EMS Configurations; and
(ii) provide to CHC technical assistance and support to perform the completion activities for Offshore and/or EMS Configurations. 

  

					
	CFA October 2007	  	Page 5	  	Contract Number 160507

 a-3 The above prices in respect of the Optional AW139 helicopters are based upon a USD to
EUR exchange rate of USD *** equal to EUR 1.00. At the time of an Optional AW139 helicopter acceptance should the above exchange rate vary by more than *** percent (***%) then the relevant price shall be adjusted accordingly utilizing the exchange
rate published by the European Central Bank two (2) days prior to the acceptance date of the AW139 helicopter. 
  

	b.	AW139 Helicopter Payments 

 b-1
Payment of the AW139 firm helicopter purchases shall be in accordance with the following schedule (to be reflected in each PA): 
  

	 	•	 	 Deposit of a non-refundable US$ *** (*** US Dollars) for each AW139 helicopter, which is the subject of a firm purchase due on the signature of this
Agreement. 

  

	 	•	 	 Intermediate payment of ***% (*** percent) of the price of each AW139 helicopter at twelve (12) months prior to the Projected Delivery Date of
each AW139 helicopter. 

  

	 	•	 	 The remaining Balance payment for each AW139 helicopter shall be paid upon acceptance at Agusta’s facility or such other location as mutually
agreed upon by the parties. 

 b-2 Payment of the AW139 optional helicopter purchases shall be in accordance
with the following schedule (to be reflected in each Purchase Agreement): 
  

	 	•	 	 Deposit of a non-refundable US$ *** (*** US Dollars) for each AW139 Optional helicopter on signature of this Agreement. Such non-refundable deposit can
be transferred to any Firm Helicopter purchase or used as a credit for parts and materials. 

  

	 	•	 	 Intermediate payment of ***% (*** percent) of the price of each AW139 helicopter at twelve (12) months prior to the Projected Delivery Date of
each AW139 helicopter. 

  

	 	•	 	 The remaining Balance payment for each AW139 helicopter shall be paid upon acceptance at Agusta’s facility or such other location as mutually
agreed upon by the parties. 

 b-3 In case the Projected Delivery Date of any AW139 helicopter is less than
twelve (12) months from the signature date of this Agreement then the payment of a non-refundable deposit of US$ *** and ***% (*** percent) of the price of each AW139 helicopter shall be paid by CHC upon signature of this Agreement 

b-4 CHC may at its sole convenience, exercise its option to purchase any one (1) or more the twenty (20), or a part thereof, of the
Optional Helicopters shown in Part 1, by giving written notice to Agnate to be served no later than eighteen (18) months prior to the Projected Delivery Date for the AW139 helicopter concerned 

b-5 Agnate agrees that Deposits, Intermediate payment(s) and Balance payment(s) paid by CHC in respect of (i) Firm and Optional
Helicopters as set out in the Original 

  

					
	CFA October 2007	  	Page 6	  	Contract Number 160507

 
Purchase Agreement; and (ii) Firm and Optional Helicopters as set out in this Part 2b, may be reallocated to other Firm and Optional Helicopter purchases made under the Original Purchase
Agreement and this Framework Agreement, as may be requested from time to time by CHC in connection with CHC’s financing with third party lenders of such helicopters provided that 

1) in all cases the allocations and aggregate amount of all Deposit(s), Intermediate payment(s) and Balance payment(s) paid by CHC and/or
such third party lenders to Agusta at any time shall be not less than the allocation and aggregate amount of Deposit(s), Intermediate payment(s) and Balance payment(s) that would have been assigned and paid if no such reallocation had occurred; and

 2) all payments obligations has been fulfilled in compliance with b1, b2 and b3 above. 

 

	c.	Residual Value Guarantee (“RVG”) 

 Agusta shall provide a RVG 8 years from delivery based upon the principles stated herein, for each of the thirteen (13) firm AW139 helicopter purchases and will provide a RVG upon the principles
stated herein, and on a case-by-case basis for the twenty (20) optional AW139 helicopter purchases when confirmed as firm purchase by CHC Precise terms and conditions for the RVG will be substantially as set out in the form of the RVG attached
as in Appendix 8 to this Agreement (the “RVG Agreement”), subject to negotiations in due course with CRC’s third party lenders and their legal advisers. Agusta shall provide a RVG provided all the following conditions precedent are
complied with: 
  

	 	•	 	 The Maintenance Programme in respect of the AW139 helicopter shall either be the Maintenance Programme contained in Chapter 5 of the Maintenance Manual
or another Maintenance Programme that has been approved by Agusta. Agusta will reasonably consider any requests by CHC for deviations to the Maintenance Programme or another Maintenance Programme subject to the additional approval of the owner or
new owner following a transfer for the purpose of refinancing the helicopter pursuant to Section 1.1 (a) of Schedule III of the applicable RVG Agreement; 

 

	 	•	 	 The RVG shall automatically become invalid for an AW139 helicopter that has been resold to a third party other than a sale pursuant to Section I of the
RVG Agreement or pursuant to Section 1.1 of Schedule III of the RVG Agreement; 

  

	 	•	 	 If CHC elects to perform the completion work of the specific equipment by itself subject to the review and approval of such work by Agusta, the resale
price of the relevant helicopter for the purposes of the RVG and as referred to in Section 2.1 of the RVG Agreement shall, instead of ***% of the Net Purchase Price, be the aggregate of the residual risk for which the Owner takes responsibility
plus an amount, “x”, for which CHC RV Guarantor takes responsibility plus ***% of the Net Purchase Price for which the RV Guarantor and the CHC RV Guarantor take responsibility in the Relevant Proportions; “x” will be an amount
which is greater than ***% of Net Purchase Price but will be a number sufficient to make the aggregate of residual risk taken equal to ***% of Total Cost (defined as the 

  

					
	CFA October 2007	  	Page 7	  	Contract Number 160507

	 	 
aggregate of the Net Purchase Price plus the cost of completion work performed by CHC. It is accepted that the proportion of the cost of the completion work performed by CHC for the purposes of
this calculation will no greater than the cost that would have been incurred if Agusta had performed the work. 

 EXAMPLE: If an AW139 helicopter costs 90 and the completion work performed by CHC is 10 (and this sum is no greater than would have been incurred if the same work had been performed by Agusta) so that the
Total Cost is 100 and the Owner takes a residual risk of ***, the tiering of risk levels would be: Owner ***, CHC RV Guarantor *** and RV Guarantor/CHC RV Guarantor *** (***% of ***) in a ***/*** ratio of ***/***, making a total of ***. 

The intention and effect is that Agusta’s RVG amount would always be a fixed percentage on the price that it receives for the work
that it has done (defined as the Net Purchase Price). 
  

	 	•	 	 With regard to RVG return conditions, CHC may return as a maximum (eight (8) years hence) only the number purchased in any given year eight
(8) years previously, these returns shall not exceed a maximum of two (2) per quarter per year, and may be, at the option of Agusta divided equally throughout the return year. 

 

	 	•	 	 Only in case CHC, within thirty (30) days of execution of this Agreement, confirms all the four (4) of the remaining eight (8) Optional
AW139 helicopters under the Contract Framework Agreement Number 139050404 dated April 25, 2005, then Agusta shall provide a RVG for the three (3) SAR aircrafts (purchased under the Supplemental Agreement No. 11 dated 4 Sept 2007) and
one (1) Optional AW139 Helicopter which terms and conditions will be agreed upon by the Parties. In addition CHC shall provide Agusta within the said thirty (30) days information on the disposition of the remaining four (4) Optional
AW139 Helicopters, and upon exercising the remaining four (4) options, Agusta shall provide a RVG which terms and conditions shall be agreed upon by the Parties. 

 

	 	•	 	 Should CHC not confirm, within thirty (30) days of execution of this Agreement, pertaining to the above four optional AW139 helicopters, then CHC
may elect to purchase the outstanding eight (8) Optional AW139 helicopters under the Contract Framework Agreement Number 139050404 dated April 25, 2005, then Agusta shall provide a RVG which terms and conditions will be agreed upon by the
Parties with the exclusion of the three (3) SAR aircrafts (purchased under the Supplemental Agreement No. 11 dated 4 Sept. 2007). 

 For the purposes of this Part 2, section c., capitalized terms used herein and not defined in this Agreement shall have the same meaning as set forth in the RVG Agreement. 

Part 3: Training 
  

	 	a.	Pilots — AW139 Helicopter IFR Type Rating Training 

  

					
	CFA October 2007	  	Page 8	  	Contract Number 160507

 Visual Flight Rules (“VFR”) / Instrument Flight Rules (“IFR”) type rating training for 5
pilots, per AW139 helicopter purchased by CHC or a third party lender, will be provided by Agusta ***. 
 Pilots must possess a current Pilot
Licence as per JAR-FCL 2 with appropriate ratings or the equivalent licences issued by a military or civil regulatory agency, be instrument-rated on multi-engine/multi-crew turbine helicopters with more than 150 flight hours experience under IFR,
and hold a current flight medical certificate. 
 The objective of the VFR / IFR, Type Rating Training course shall be to train qualified
helicopter pilots to fly the AW139 helicopter under VFR and IFR conditions and to respond safely to emergency situations and malfunctions. 

Further training options, i.e. instructor training and recurrent training for line pilots are also available subject to further discussions. 

The training will be provided in three phases i.e. a ground school phase, a simulator-training phase and a final training phase utilising the AW139
customer helicopter after acceptance commensurate with the delivery of each AW139 helicopter: 
 a. Ground school training of two (2) weeks
duration includes a comprehensive coverage of the systems description and operation, operational characteristics, operating limitations and performance planning. 
 b. Simulator training (14 VFR hours plus 6 IFR hours) includes complete familiarization of the AW139 helicopter, instruction in the turbine engine operation, cockpit procedures, flight instruction in
normal flight manoeuvres and simulated emergency procedures in VFR/IFR conditions. 
 c. Final training (4 VFR hours) will be conducted on the
AW139 helicopter by means of demonstrating specific manoeuvres by the Agusta instructor pilot followed by the student pilot progressively demonstrating the same manoeuvres up to a point acceptable to the instructor pilot. The AW139 helicopter will
be used following its acceptance for flight training and as such CHC will be responsible for the applicable insurance required during the training period. 
  

	 	b.	Engineers — AW139 Helicopter Airframe Maintenance Type Training (Cat. B1.3) 

 Airframe line maintenance training (4 weeks/20 days) for 4 maintenance engineers, per AW139 helicopter purchased by CHC or a third party lender, will be provided by Agusta ***. 

Course Approval: EASA Part-147. The applicants must hold a valid JAR/EASA Category B1.3 Line Maintenance Mechanic (Helicopter Turbine) license or an
equivalent licences issued by a military or civil regulatory agency and have a good knowledge of the English language both written and spoken. Moreover, applicants shall have at least 2.5 years experience in turbine powered helicopter maintenance.
Note: If the applicant is not in possession of the required license, the certificate released at the end of the course will not include any reference to the Agusta MTO and to the approval to Part-147. 

  

					
	CFA October 2007	  	Page 9	  	Contract Number 160507

 The objective of this course shall be to provide the attending technician with a detailed theoretical
understanding of the AW139 helicopter airframe systems, their operations and maintenance, components replacement procedures, use of technical literature and Interactive Electronic Technical Publications (IETP). 

The course will also cover a comprehensive coverage of description, function and maintenance procedures relevant to the AW139 helicopter airframe systems
and provide a description of operation, components location, remove/install of components and troubleshooting procedures described at Maintenance Manual level excluding the power plant. The interface of the engine/airframe systems is addressed by
this course. 
  

	 	c.	Engineers — AW139 Avionic Systems Maintenance Type Training (Cat. B2) 

 Avionic line maintenance training (3 weeks/15 days) for 2 maintenance engineers, per AW139 helicopter purchased by CHC or a third party lender, will be provided by Agusta ***. 

Course Approval: EASA Part-147. The applicants must hold a valid JAR/EASA Category B2 Avionic Line Maintenance (Helicopter Turbine) license or an
equivalent licences issued by a military or civil regulatory agency and have a good knowledge of the English language both written and spoken. Moreover applicants shall have at least 2.5 years experience in turbine powered helicopter maintenance.
Note: If the applicant is not in possession of the required license, the certificate released at the end of the course will not include any reference to the Agusta MTO and to the approval to Part-147. 

The objective of this course is to provide qualified avionic technicians with the knowledge and skill required to troubleshoot, inspect, and perform
maintenance of the AW139 Electrical and Avionic Systems. 
 The course will also cover the description; function and maintenance procedures
relevant to the AW139 helicopter avionic systems and provide a description of operation, components location, remove/install of components and troubleshooting procedures described at Maintenance Manual level excluding the power plant. 

All training will be provided at the Agusta Training Academy at Sesto Calende in Italy (approved FAA Part 142 Training Center). 

Since CHC will train a significant quantity of pilots and maintenance engineers to operate and support the fleet of AW139 helicopters purchased pursuant
to this Agreement, a “Training Needs Analysis” meeting shall be held between CHC and Agusta on or about November 1, 2007, in order to determine the detailed training requirements of CHC and to provide a dedicated training solution
including the quantity and type of courses to be provided, the duration of such courses and the schedule of such courses. 

  

					
	CFA October 2007	  	Page 10	  	Contract Number 160507

 In addition to the pilot and engineer training set out above and to be provided by Agusta ***, Agusta in
conjunction with CHC will assess the following training requirements: 
  

	 	•	 	 Practical Elements training session provisions related to the AW139 Airframe and Avionic Maintenance Courses (2 weeks), using the Helicopter
Maintenance Trainer in Sesto Calende. 

  

	 	•	 	 Pilot Recurrent Training (6 FFS Hours / 1 day class), VFR Refresher Pilot Courses (7 FFS hours / 1 helicopter hour / 2 days class) and IFR Refresher
Pilot Courses (5 FFS) at the prices set out below: 

  

					
	 Price per student Pilot Recurrent Training
	  	€	*	** 
	 Price per student Pilot Refresher VFR Training (With simulator and Customer’s helicopter)
	  	€	*	** 
	 Price per student Pilot Refresher IFR Training (With simulator and Customer’s helicopter)
	  	€	*	** 

 Note: Prices 2007 Economy and will be quoted each year according year applicable pricelist 

 

	 	•	 	 Provision for dry hourly rate (with the Customer FFS Instructor Pilot) for the Full Flight Simulator to be used to train new pilots and to carryout
refresher courses at the prices set out below: 

  

					
	 Price for Simulator Dry Hours
	  	€	*	** 

 Note: Prices 2007 Economy and will be quoted each year according year applicable pricelist 

 

	 	•	 	 Option for Computer Based Training Package (CBT) at the prices set out below: 

 

					
	 AW139 CBT/Multimedia Package
	  	€	*	** 
	 Installation (N°1 Week)
	  	€	*	** 

 Part 4: Special Conditions: 
  

	1.	 Agusta shall limit its yearly increase in price for deliveries of AW139 helicopters in Standard, Offshore and EMS Configurations beyond year 2009 at a
rate of *** percent (***%) per annum for delivery up to 2011 (including 1st quarter 2012) (the “Fixed Price Escalation”). 

 Any
changes or modifications to the specifications of the Standard, Offshore, EMS Configurations set out in Appendices 1, 2 and 3 shall be subject to a price and/or delivery date adjustment. 

 

	2.	The following discounts shall be applied to the AW139 helicopters delivered in Standard, Offshore and EMS Configurations: 

*** 
  

	3.	 Agusta will provide a technical representative to CHC, included in the contract price, for a period of three (3) months for each new delivery to
each new CHC base, from where the AW139 helicopter shall operate. This excludes accommodation, security and personal insurance, which shall be provided by CHC or quoted on a case by case basis by Agusta, based on the local conditions of the country
concerned. On a case-by-case basis Agusta 

  

					
	CFA October 2007	  	Page 11	  	Contract Number 160507

	 	
will, prior to the expiry of the attendance of the technical representative, consider granting an extension of up to three (3) months for the technical representative concerned.

 Agusta shall establish with CHC a provision for additional on-site technical support, against a monthly rate
applicable for each year. This rate shall exclude accommodation, security and personal insurance, which shall be provided by CHC or quoted on a case by case basis by Agusta, based on the local conditions of the country concerned. 

 

	4.	Upon execution of this Agreement (or immediately thereafter), Agusta shall: 

 

	 	•	 	 establish CHC as a certified Agusta AW139 Overhaul Capability Centre and a certified Agusta AW139 Service Centre, as outlined in Appendix 6 hereto;

  

	 	•	 	 establish a dedicated safety stock at certain operational bases, as outlined in Appendix 6 hereto and; 

 

	 	•	 	 assist CHC in providing overhaul capability on the main and tail rotor transmissions of the AW139 helicopters, as outlined in Appendix 6 hereto.

  

	5.	Agusta shall continue with its weight saving campaign so as to quantify and provide certification for an AW139 helicopter weight reduction. Agusta shall regularly keep
CHC updated on the progress in this regard. In parallel Agusta will increase the all-up-maximum gross weight to a threshold of 6,700 kg (threshold), but with the objective of achieving 6,800kg anticipated by June 1, 2009.

  

	6.	The relevant cost for any additional completion activities not listed in the Agreement shall be quoted accordingly to CHC through a separate quotation, if applicable

  

	7.	Agusta and CHC agree to exit from the Aircraft Assurance Plans (“AAPs”) and from the Complete Overhaul and Material Programs (“COMPs”, and together
with the AAPs, the “Programs”) for CHC AW139 Helicopters purchased under this Framework Agreement and the previous Framework Agreement dated 25 April 2005 (the “Helicopters”) in conjunction with the option to select for the
Components Protection Agreement (“CPA”), as ruled under Appendix 5 

 Part 5; Export Licenses: 

 

	1.	The full performance by Agusta under this Agreement and each PA is subject to the receipt of all applicable export licenses and approvals pursuant to all applicable
laws and regulations, including but not limited to the United States Export Administration Regulations and the United States International Traffic in Arms Regulations. Agusta hereby expressly agrees to implement the procedure for any required export
license. The cost for obtaining any license is Agusta’s responsibility. CHC acknowledges and understands that the length of time from application for and receipt of the necessary export licenses is uncertain. Accordingly, Agusta shall apply for
export license in a timely manner to support the delivery of the AW139 helicopters in Standard, Offshore and/or EMS configurations. To the extent an export license is required and Agusta requests CHC’s assistance, CHC hereby agrees to provide
to Agusta with the information and support that it reasonably requests in writing as soon as reasonably practicable for the purposes of obtaining an export license. 

  

					
	CFA October 2007	  	Page 12	  	Contract Number 160507

 Part 6: Taxes: 
 Agusta will ensure that all reasonable assistance is provided to CHC for the purposes of Italian VAT tax legislation. For US deliveries transfer of title for each AW139 will take place in Wilmington,
Delaware. 
 Local taxes custom duties or other fiscal charges, due in Italy or the U.S., depending on the Agusta’s
Production facilities, related to the performance of this Agreement and each PA, shall be borne by Agusta. 
 Part 7: Patent Infringement

  

	1.	Agusta shall conduct, at its own expense, the entire defense of any claim, suit or action alleging that, without further combination, the use or resale by CHC or any
subsequent purchaser or user of any AW139 helicopter or part delivered hereunder directly infringes any world-wide patent, but only on the conditions that (A) Agusta receives prompt written notice of such claim, suit, or action and full
opportunity and authority to assume the sole defense thereof, including settlement and appeals, and all information available to CHC and defendant for such defense; (B) said AW139 helicopter or part is made according to a specification or
design furnished by Agusta or, if a process patent is involved, the process performed by the AW139 helicopter is recommended in writing by Agusta; and (C) the claim, suit, or action is brought against CHC or one expressly indemnified by CHC.
Provided all of the foregoing conditions have been met, Agusta shall, at its own expense, either settle said claim, suit, or action or shall pay all damages awarded by the court therein, and, if the use or resale of such AW139 helicopter or part is
finally enjoined, Agusta shall, at Agusta’s option: (i) procure for defendant the right to use or resell the AW139 helicopter or part, (ii) replace them with an equivalent no infringing AW 139 helicopter or part, (iii) modify
them so they become non-infringing but equivalent, or (iv) remove them and refund the purchase price (less a reasonable allowance for use, damage, and obsolescence). 

 Part 8: General Conditions: 
  

	1.	Agusta shall bear any and all risk of loss, damage, theft or destruction, partial or complete, of an AW139 helicopter until such time as the AW139 helicopter has been
accepted and a Certificate of Acceptance has been executed. by CHC or by one of its third party lenders. 

  

	2.	This Agreement shall become effective from the date of its signature and the receipt by Agusta of the refundable deposits pursuant to Part 2 Article b-1 and shall
continue in force and until each of the AW139 helicopters have been ordered pursuant to PAs and the obligations related to each AW139 helicopters have been fulfilled, unless terminated earlier in accordance with a provision of this Agreement.

  

					
	CFA October 2007	  	Page 13	  	Contract Number 160507

 The Appendices form part of this Agreement. If and to the extent that there is any conflict
between the Articles of this Agreement and the Appendices of this Agreement, the Articles of this Agreement shall prevail. If and to the extent that there is any conflict between Appendix 1 and the other Appendices, Appendix 1 shall prevail

 If and to the extent that there is any conflict between a provision of this Agreement and a provision of a PA the provision in
this Agreement shall prevail. 
  

	3.	In case CHC shall be in breach of any of its obligations under this Agreement and such breach has not been cured within thirty (30) days of Agusta providing
written notice to CHC of such breach, Agusta shall have the right to terminate this Agreement at any time prior to its natural expiry. 

  

	4.	Any Amendment required to this Agreement shall be effective when agreed in writing between the Parties. 

 

	5.	The failure of either Party at any time to require performance of the other Party for any provision of this Agreement shall not affect in any way the full right to
require such performance at any time thereafter, nor shall the waiver by either Party of a breach of the same or any other such provisions, constitute a waiver of the provision itself. 

 

	6.	This Agreement is construed and governed according to Italian law. 

  

	7.	Any dispute concerning the validity, interpretation, performance or breach of this Agreement which the Parties can not amicably compose shall be finally settled under
the Rules of Arbitration of the International Chamber of Commerce by three arbitrators appointed one by the CHC, one by Agusta and the third one by the first two arbitrators, or, failing to reach an agreement, by the International Chamber of
Commerce, as provided by said Rules. 

 The arbitration shall be held in Milan. 

 

	8.	Any notice given hereunder shall be in writing by facsimile or through registered mail. 

The following address shall be used for AGUSTA 
 AGUSTA Spa 
 Via G. Agusta, 520 

21017 CASCINA COSTA DI SAMARATE 
 Varese – Italy 
 Attention: Contracts Management 

Facsimile: +39 0331 229930 
 The following address shall be used for CHC. 
 CHC HELICOPTERS INTERNATIONAL INC.

 4740 AGAR DRIVE 

  

					
	CFA October 2007	  	Page 14	  	Contract Number 160507

 
RICHMOND, BRITISH COLUMBIA 
 CANADA, V7B 1A3 

Attention: Director (Contracts) 
 Facsimile: +1 604 232 8359 
  

	9.	CHC shall not assign the benefits and obligations of this Agreement without the written consent of Agusta. CHC shall have the right to novate or assign any PA by way of
security or otherwise, to one or more third party lenders or any affiliates or subsidiaries of CHC only in connection with the financing of an AW139 helicopter. 

 

	10.	All communications between the Parties in relation to this Agreement shall be in the English language. 

[The remainder of this page is left intentionally blank.] 

 

	11.	With exception for the existence of this Agreement, the parties hereby agree that neither party shall disclose to any third party the contents of this Agreement without
the prior written approval of the other party unless required by applicable laws and regulations; provided that, each party may make such disclosures on a confidential basis to its financial and legal advisors as may be required in the performance
of this Agreement. 

  

					
	CFA October 2007	  	Page 15	  	Contract Number 160507

 IN WITNESS WHEREOF, the Parties agree to this Agreement as of the date first set forth above. 

 

			
	Agusta S.p.A.	  	CHC Helicopters International Inc.
		
	By:	  	By:
		
	Title:	  	Title:
		
	Date:	  	Date:
		
	Witness	  	Witness:

  

					
	CFA October 2007	  	Page 16	  	Contract Number 160507

 APPENDIX 1 
 AW139 Standard configuration 

  

					
	CFA October 2007	  	Page 17	  	Contract Number 160507

 STANDARD CONFIGURATION (EASA / ENAC / FAA IFR CONFIGURATION) 

THF139-0607-1 
  

	a)	AIRFRAME: 

  

	 	•	 	 Aluminum alloy fuselage 

  

	 	•	 	 Polycarbonate Windshields 

  

	 	•	 	 Overhead cockpit windows 

  

	 	•	 	 Lower cockpit windows 

  

	 	•	 	 Cockpit ram air adjustable outlets 

  

	 	•	 	 Forced fan ventilation 

  

	 	•	 	 Bleed air heater and defroster with air noise suppressions 

 

	 	•	 	 Heated Pitot tubes (2) with Pilot heat failure warning (2) 

 

	 	•	 	 Heated static intakes (2) 

  

	 	•	 	 One cockpit and one pilot cabin fire extinguisher 

  

	 	•	 	 Pilot doors (2) with push-out emergency exit window (with “storm window” on pilot side) 

 

	 	•	 	 Plug in sliding doors (2) for passengers cabin access with four locking latches 

 

	 	•	 	 Six cabin push-out emergency exit windows (two on each passenger cabin door) 

 

	 	•	 	 Baggage compartment with 2 lockable baggage compartment doors, LH & RH side. 

 

	 	•	 	 Baggage compartment cargo tie-down fittings 

  

	 	•	 	 Wheeled retractable tricycle landing gear (two wheels on nose gear and brakes on main landing gear) 

 

	 	•	 	 Structural provisions for nose landing gear doors 

  

	 	•	 	 Landing gear mooring 

  

	 	•	 	 Upper deck mooring provisions 

  

	 	•	 	 Hoisting and jacking fittings 

  

	 	•	 	 Tail boom and vertical fin 

  

	 	•	 	 Stabilizers with composite “winglets” 

  

	 	•	 	 Pilot and copilot windshield wipers 

  

	 	•	 	 Maintenance steps for access to upper deck on both sides 

 

	 	•	 	 Upper deck cowlings (one front forward sliding, two side opening for engine access) 

 

	 	•	 	 Steps for cockpit access 

  

	 	•	 	 Anti-vibration masses (2) under cabin floor 

  

	b)	ROTORS AND CONTROLS: 

  

	 	•	 	 Fully articulated Main Rotor (M/R) with five composite blades, five elastomeric bearings and five hydraulic dampers 

 

	 	•	 	 Rotating M/R flight controls Main rotor hub beanie 

  

	 	•	 	 Three main dual servo actuators 

  

	 	•	 	 Fully articulated Tail Rotor (T/R) with four composite blades, four elastomeric bearings and four elastomeric dampers 

 

	 	•	 	 Rotating T/R flight controls One T/R dual servo actuator Force trim system 

 

	 	•	 	 Pilot fixed flight controls (cyclic, collective, anti-torque pedals) 

 

	 	•	 	 Copilot fixed flight controls (cyclic, collective, anti-torque pedals) 

 

	 	•	 	 Dual digital 3-axis linear actuators Rotor brake 

  

	 	•	 	 Provision for main rotor tracking (magnetic pick-up) 

  

					
	CFA October 2007	  	Page 18	  	Contract Number 160507

	c)	ELECTRICAL SYSTEMS: 

  

	 	•	 	 DC primary power generation: 28 V DC regulated voltage provided by two independent 300 A starter generators 

 

	 	•	 	 DC External Power Receptacle 

  

	 	•	 	 Two Nickel-Cadmium Batteries: one 40 Ah main battery plus one 13 Ah auxiliary battery 

 

	 	•	 	 DC Starter Generator Control Units (2) 

  

	 	•	 	 Navigation lights (3) 

  

	 	•	 	 Anticollision light 

  

	 	•	 	 External emergency landing lights on the sponsons (2) Fixed landing/taxi lights on the sponsons (2) 

 

	 	•	 	 Rotating/ retracting landing light 

  

	 	•	 	 Baggage compartment lighting (3) and smoke sensor 

 

	d)	TRANSMISSION DRIVE SYSTEM AND HYDRAULIC SYSTEM: 

  

	 	•	 	 Main transmission with two direct drive engine inputs 

 

	 	•	 	 Three main transmission chip detectors/debris collectors with burning capability - Two freewheel units 

 

	 	•	 	 Four strut rods for upper deck attachment and one anti—torque plate Intermediate gearbox with sight gauge and magnetic drain plug/chip detector
Tail gearbox with sight gage and magnetic drain plug/chip detector 

  

	 	•	 	 Dual independent, redundant hydraulic systems 

  

	 	•	 	 Two hydraulic Power Control Modules (PCMs) 

  

	 	•	 	 Three main transmission driven hydraulic mechanical pumps for controls, landing gear and wheel 

 

	 	•	 	 brake actuation 

  

	 	•	 	 One electrical pump for control checks on ground (engines off) Air conditioning compressor quill 

 

	e)	POWER PLANT & FUEL SYSTEM: 

  

	 	•	 	 Two Pratt & Whitney Canada PT6C-67C engines 

  

	 	•	 	 Two independent FADEC systems (one on each engine) with autostart and engine control functions for normal, emergency and training operations Two
magnetic chip detectors 

  

	 	•	 	 Two integrated and independent engine oil coolers Separate firewall protection for each engine 

 

	 	•	 	 Fire detection system 

  

	 	•	 	 Fire extinguisher system (2 bottles) 

  

	 	•	 	 Engine exhausts and ejectors 

  

	 	•	 	 Two independent crashworthy fuel cells 

  

	 	•	 	 Two supply pumps on engines 

  

	 	•	 	 Two booster pumps submerged in fuel tanks 

  

	 	•	 	 Two fuel filter assemblies 

  

	 	•	 	 Two engine back—up controls, mechanical and electrical Two manual engine start and ignition systems 

  

					
	CFA October 2007	  	Page 19	  	Contract Number 160507

	f)	STANDARD AVIONICS PACKAGE: 

  

	 	•	 	 1st PFD (Pilot Primary Flight Display 8” x 10” color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data

  

	 	•	 	 2nd PFD (Copilot Primary Flight Display 8” x 10” color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data

  

	 	•	 	 1st MFD (Pilot Multifuncion Display 8” x 10” color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data

  

	 	•	 	 2nd MFD (Copilot Multifunction Display 8” x 10” color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data

  

	 	•	 	 One Electronic Standby Instrument System (ESLS) (attitude, aitspeed, altitude, vertical speed, compass, and ILS data) 

 

	 	•	 	 Two Attitude and Heading Reference Systems (AHRSs) 

  

	 	•	 	 Two Air Data Modules (ADMs) 

  

	 	•	 	 Two flux valves 

  

	 	•	 	 Two Display Controllers (DCs) 

  

	 	•	 	 Two Cursor Control Devices (CCDs) 

  

	 	•	 	 One Reversion Control Panel (RCP) 

  

	 	•	 	 One Display Dimming Control Panel (DCP) 

  

	 	•	 	 One Stability Augmentation System (SAS) control panel 

 

	 	•	 	 Two Remote Instrument Controllers (RICs) 

  

	 	•	 	 Two Modular Avionic Units (MAUs) incorporating the following major subsystems and/or functions: 

 

	 	•	 	 Vehicle Monitoring System — VMS (dual) 

  

	 	•	 	 Monitor Warning System — MWS (dual) 

  

	 	•	 	 Aural Warning Generator — AWG (single) 

  

	 	•	 	 Central Maintenance Computer — CMC (single) 

  

	 	•	 	 3—Axis Digital Automatic Flight Control System— DAFCS (dual) with autotrim function 

 

	 	•	 	 Provision for CVR/FDR data interface (single) 

  

	 	•	 	 Flight Director System (dual) 

  

	 	•	 	 Pilot and copilot microphone and headset 

  

	 	•	 	 Pilot and Copilot interphone control (cyclic grip and floor switches) 

 

	 	•	 	 La Modular Radio Cabinet (MRC) with the following modules: 

 

	 	•	 	 One VHF Comm. 

  

	 	•	 	 One VOR/LOC/GS/MB 

  

	 	•	 	 Right Modular Radio Cabinet (MRC) with the following modules: 

 

	 	•	 	 One VHF Comm. 

  

	 	•	 	 One Mode—S diversity transponder 

  

	 	•	 	 One VOR/LOC/GS/MB 

  

	 	•	 	 One ADF 

  

	 	•	 	 One DME 

  

	•	 	 Two pedestal mounted MCDUs (Multi Control Function Display Units) 

 

	•	 	 1st Radar Altimeter (RT — 300) 

  

					
	CFA October 2007	  	Page 20	  	Contract Number 160507

	 	•	 	 2nd Radar Altimeter System (RT — 300) 

  

	 	•	 	 Emergency Locator Transmitter (ELT — 121.5/243/406 MHz) 

 

	 	•	 	 One Flight Guidance Controller 

  

	 	•	 	 Honeywell GPS module with Flight Plan Management System (FPMS) 

 

	 	•	 	 Pilot and copilot digital audio panels with remote ICS audio port for ground operation Pilot clock (digital) 

 

	 	•	 	 Copilot clock (digital) 

  

	 	•	 	 One magnetic compass 

  

	 	•	 	 One Outside Air Temperature indicator 

  

	 	•	 	 Two Master Warning Lights (MWLs) 

  

	 	•	 	 Two Master Caution Lights (MCLs) 

  

	 	•	 	 Engine 1 Fire Light 

  

	 	•	 	 Engine 2 Fire Light 

  

	 	•	 	 Baggage compartment smoke detector light 

  

	 	•	 	 Dual electrical power connection for CVR/FDR (FAA requirement compliant) 

 

	 	•	 	 Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon (ULB) 

 

	g)	INTERIOR TRIM: 

  

	 	•	 	 Cabin, cockpit and baggage compartment utility finishing interior Pilot/ Copilot crashworthy seats (with inertial reels and safety belts) Cockpit
dome/storm light 

  

	 	•	 	 Cockpit utility lights (2) 

  

	 	•	 	 28V DC cockpit/cabin power outlet 

  

	 	•	 	 Cockpit panel sun-glare shields 

  

	 	•	 	 Overhead cockpit windows sun shades 

  

	 	•	 	 Floor provisions for 15-seat configuration 

  

	 	•	 	 Fluorescent lighted emergency exit signs 

  

	h)	EXTERIOR PAINTING: 

  

	 	•	 	 Two color polyurethane painting in accordance with Agusta standard painting scheme 

Miscellaneous 
  

	 	•	 	 Covers and flags: engine exhaust pipes (2), engine air inlets (2) and Pitot tubes (2), battery connector warning flag (I)

  

	 	•	 	 Manuals: aircraft log, engines operations, flight and maintenance and overhaul, illustrated parts catalogue 

 

	 	•	 	 Tie down—assemblies for main rotor blades (5) 

  

	 	•	 	 Tail rotor blades flapping block (I) 

  

	 	•	 	 Main rotor blade sock pole (1) 

  

	 	•	 	 Main landing gear wheel chocks (2) 

  

	 	•	 	 Main rotor balance and tracking chart, tail rotor balance chart 

 

	 	•	 	 Nose landing gear center pin (1) and landing gear handle locking pin (1) 

 

	 	•	 	 Jacking dome assy (1) 

  

	 	•	 	 Tow bar (1) 

  

	 	•	 	 Loose equipment bag (1) 

  

					
	CFA October 2007	  	Page 21	  	Contract Number 160507

 APPENDIX 2 
 AW139 Offshore completion 

  

					
	CFA October 2007	  	Page 22	  	Contract Number 160507

 STANDARD CONFIGURATION (EASA / ENAC / FAA IFR CONFIGURATION) 

THF139-0607-1 
  

	a)	AIRFRAME: 

  

	 	•	 	 Aluminum alloy fuselage 

  

	 	•	 	 Polycarbonate Windshields 

  

	 	•	 	 Overhead cockpit windows 

  

	 	•	 	 Lower cockpit windows 

  

	 	•	 	 Cockpit ram air adjustable outlets 

  

	 	•	 	 Forced fan ventilation 

  

	 	•	 	 Bleed air beater and defroster with air noise suppressions Heated Pitot tubes (2) with Pilot heat failure warning (2) Heated static intakes
(2) 

  

	 	•	 	 One cockpit and one pilot cabin fire extinguisher 

  

	 	•	 	 Pilot doors (2) with push-out emergency exit window (with “storm window” on pilot side) 

 

	 	•	 	 Plug in sliding doors (2) for passengers cabin access with four locking latches 

 

	 	•	 	 Six cabin push-out emergency exit windows (two on each passenger cabin door) 

 

	 	•	 	 Baggage compartment with 2 lockable baggage compartment doors, LH & RH side. 

 

	 	•	 	 Baggage compartment cargo tie-down fittings 

  

	 	•	 	 Wheeled retractable tricycle landing gear (two wheels on nose gear and brakes on main landing gear) 

 

	 	•	 	 Structural provisions for nose landing gear doors Landing gear mooring 

 

	 	•	 	 Upper deck mooring provisions 

  

	 	•	 	 Hoisting and jacking fittings 

  

	 	•	 	 Tail boom and vertical fin 

  

	 	•	 	 Stabilizers with composite “winglets” 

  

	 	•	 	 Pilot and copilot windshield wipers 

  

	 	•	 	 Maintenance steps for access to upper deck on both sides 

 

	 	•	 	 Upper deck cowlings (one front forward sliding, two side opening for engine access) 

 

	 	•	 	 Steps for cockpit access 

  

	 	•	 	 Anti-vibration masses (2) under cabin floor 

  

	b)	ROTORS AND CONTROLS: 

  

	 	•	 	 Fully articulated Main Rotor (M/R) with five composite blades, five elastomeric bearings and five hydraulic dampers 

 

	 	•	 	 Rotating M/R flight controls - Main rotor hub beanie 

  

	 	•	 	 Three main dual servo actuators 

  

	 	•	 	 Fully articulated Tail Rotor (T/R) with four composite blades, four elastomeric bearings and four elastomeric dampers 

 

	 	•	 	 Rotating T/R flight controls - One T/R dual servo actuator Force trim system 

 

	 	•	 	 Pilot fixed flight controls (cyclic, collective, anti-torque pedals) 

 

	 	•	 	 Copilot fixed flight controls (cyclic, collective, anti-torque pedals) 

 

	 	•	 	 Dual digital 3-axis linear actuators - Rotor brake 

  

	 	•	 	 Provision for main rotor tracking (magnetic pick-up) 

 

	c)	ELECTRICAL SYSTEMS: 

  

	 	•	 	 ­ DC primary power generation: 28 V DC regulated voltage provided by two independent 300 A starter generators 

  

					
	CFA October 2007	  	Page 23	  	Contract Number 160507

	 	•	 	 DC External Power Receptacle 

  

	 	•	 	 Two Nickel-Cadmium Batteries: one 40 Alt main battery plus one 13 Ah auxiliary battery 

 

	 	•	 	 DC Starter Generator Control Units (2) 

  

	 	•	 	 Navigation lights (3) 

  

	 	•	 	 Anticollision light 

  

	 	•	 	 External emergency landing lights on the sponsons (2) Fixed landing/taxi lights on the sponsons (2) 

 

	 	•	 	 Rotating/ retracting landing light 

  

	 	•	 	 Baggage compartment lighting (3) and smoke sensor 

 

	d)	TRANSMISSION / DRIVE SYSTEM AND HYDRAULIC SYSTEM: 

  

	 	•	 	 Main transmission with two direct drive engine inputs 

 

	 	•	 	 Three main transmission chip detectors/debris collectors with burning capability - Two freewheel units 

 

	 	•	 	 Four strut rods for upper deck attachment and one anti—torque plate Intermediate gearbox with sight gauge and magnetic drain plug/chip detector
Tail gearbox with sight gage and magnetic drain plug/chip detector 

  

	 	•	 	 Dual independent, redundant hydraulic systems 

  

	 	•	 	 Two hydraulic Power Control Modules (PCMs) 

  

	 	•	 	 Three main transmission driven hydraulic mechanical pumps for controls, landing gear and wheel 

 

	 	•	 	 brake actuation 

  

	 	•	 	 One electrical pump for control checks on ground (engines off) Air conditioning compressor quill 

 

	e)	POWER PLANT & FUEL SYSTEM: 

  

	 	•	 	 Two Pratt & Whitney Canada PT6C-67C engines 

  

	 	•	 	 Two independent FADEC systems (one on each engine) with autostart and engine control 

 

	 	•	 	 functions for normal, emergency and training operations Two magnetic chip detectors 

 

	 	•	 	 Two integrated and independent engine oil coolers Separate firewall protection for each engine 

 

	 	•	 	 Fire detection system 

  

	 	•	 	 Fire extinguisher system (2 bottles) 

  

	 	•	 	 Engine exhausts and ejectors 

  

	 	•	 	 Two independent crashworthy fuel cells 

  

	 	•	 	 Two supply pumps on engines 

  

	 	•	 	 Two booster pumps submerged in fuel tanks 

  

	 	•	 	 Two fuel filter assemblies 

  

	 	•	 	 Two engine back—up controls, mechanical and electrical 

 

	 	•	 	 Two manual engine start and ignition systems 

  

	f)	STANDARD AVIONICS PACKAGE: 

  

	 	•	 	 1st PFD (Pilot Primary Flight Display 8” x 10” color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data

  

					
	CFA October 2007	  	Page 24	  	Contract Number 160507

	 	•	 	 2nd PFD (Copilot Primary Flight Display 8” x 10” color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data

  

	 	•	 	 1st MFD (Pilot Multifunction Display 8” x 10” color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data

  

	 	•	 	 2nd MFD (Copilot Multifunction Display 8” x 10” color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data

  

	 	•	 	 One Electronic Standby Instruments System (ESIS) (attitude, airspeed, altitude, vertical speed, compass, and ILS data) 

 

	 	•	 	 Two Attitude and Heading Reference Systems (Mins) 

  

	 	•	 	 Two Air Data Modules (ADMs) 

  

	 	•	 	 Two flux valves 

  

	 	•	 	 Two Display Controllers (DCs) 

  

	 	•	 	 Two Cursor Control Devices (CCDs) 

  

	 	•	 	 One Reversion Control Panel (RCP) 

  

	 	•	 	 One Display Dimming Control Panel (DCP) 

  

	 	•	 	 One Stability Augmentation System (SAS) control panel 

 

	 	•	 	 Two Remote Instrument Controllers (RICs) 

  

	 	•	 	 Two Modular Avionic Units (MAUs) incorporating the following major subsystems and/or functions: 

 

	 	•	 	 Vehicle Monitoring System — VMS (dual) 

  

	 	•	 	 Monitor Warning System — MWS (dual) 

  

	 	•	 	 Aural Warning Generator — AWG (single) 

  

	 	•	 	 Central Maintenance Computer — CMC (single) 

  

	 	•	 	 3—Axis Digital Automatic Flight Control System — DAFCS (dual) with autotrim function 

 

	 	•	 	 Provision for CVR/FDR data interface (single) 

  

	 	•	 	 Flight Director System (dual) 

  

	 	•	 	 Pilot and copilot microphone and headset 

  

	 	•	 	 Pilot and Copilot interphone control (cyclic grip and floor switches) 

 

	 	•	 	 Left Modular Radio Cabinet (MRC) with the following modules: 

 

	 	•	 	 One VHF Comm_ 

  

	 	•	 	 One VOR/LOCJGS/MB 

  

	 	•	 	 Right Modular Radio Cabinet (MRC) with the following modules: 

 

	 	•	 	 One VHF Comm. 

  

	 	•	 	 One Mode—S diversity transponder 

  

	 	•	 	 One VOR/LOC/GS/M13 

  

	 	•	 	 One ADF 

  

	 	•	 	 One DME 

  

	 	•	 	 Two pedestal mounted MCDUs (Multi Control Function Display Units) 

 

	 	•	 	 1st Radar Altimeter (RT — 300) 

  

	 	•	 	 2nd Radar Altimeter System (RT — 300) 

  

	 	•	 	 Emergency Locator Transmitter (ELT — 121.5/243/406 MHz) 

 

	 	•	 	 One Flight Guidance Controller 

  

					
	CFA October 2007	  	Page 25	  	Contract Number 160507

	 	•	 	 Honeywell GPS module with Flight Plan Management System (FPMS) 

 

	 	•	 	 Pilot and copilot digital audio panels with remote ICS audio port for ground operation Pilot clock (digital) 

 

	 	•	 	 Copilot clock (digital) 

  

	 	•	 	 One magnetic compass 

  

	 	•	 	 One Outside Air Temperature indicator 

  

	 	•	 	 Two Master Warning Lights (41WLs) 

  

	 	•	 	 Two Master Caution Lights (MCLs) 

  

	 	•	 	 Engine I Fire Light 

  

	 	•	 	 Engine 2 Fire Light 

  

	 	•	 	 Baggage compartment smoke detector light 

  

	 	•	 	 Dual electrical power connection for CVR/FDR (FAA requirement compliant) 

 

	 	•	 	 Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon (ULT)) 

 

	g)	INTERIOR TRIM: 

  

	 	•	 	 Cabin, cockpit and baggage compartment utility finishing interior Pilot/ Copilot crashworthy seats (with inertial reels and safety belts) Cockpit
dome/storm light 

  

	 	•	 	 Cockpit utility lights (2) 

  

	 	•	 	 28V DC cockpit/cabin power outlet 

  

	 	•	 	 Cockpit panel sun-glare shields 

  

	 	•	 	 Overhead cockpit windows sun shades 

  

	 	•	 	 Floor provisions for 15-seat configuration 

  

	 	•	 	 Fluorescent lighted emergency exit signs 

  

	h)	MISCELLANEOUS 

  

	 	•	 	 Covers and flags: engine exhaust pipes (2), engine air inlets (2) and Pitot tubes (2), battery connector warning flag (I)

  

	 	•	 	 Manuals: aircraft log, engines operations, flight and maintenance and overhaul, illustrated parts catalogue 

 

	 	•	 	 Tie down—assemblies for main rotor blades (5) 

  

	 	•	 	 Tail rotor blades flapping block (1) 

  

	 	•	 	 Main rotor blade sock pole (1) 

  

	 	•	 	 Main landing gear wheel chocks (2) 

  

	 	•	 	 Main rotor balance and tracking chart, tail rotor balance chart 

 

	 	•	 	 Nose landing gear center pin (1) and landing gear handle locking pin (1) 

 

	 	•	 	 Jacking dome assy (1) 

  

	 	•	 	 Tow bar (1) 

  

	 	•	 	 Loose equipment bag (1) 

  

	i)	OFFSHORE INTERIOR TRIM 

  

	 	•	 	 12 Padded Crashworthy Pax Seats 

  

	j)	AGUSTA INSTALLED PROVISIONS: 

  

	 	•	 	 4-Axis autopilot 

  

	 	•	 	 TCAS I 

  

					
	CFA October 2007	  	Page 26	  	Contract Number 160507

	 	•	 	 VHF/FM Tactical radio NAT NPX 138 

  

	 	•	 	 Weather/Search Radar Honeywell Primus 660 

  

	 	•	 	 Auxiliary Fuel Tanks 

  

	 	•	 	 Cargo hook 

  

	 	•	 	 Emergency Floats 

  

	 	•	 	 Rescue Hoist Breeze 

  

	 	•	 	 EGPWS 

  

	 	•	 	 Pax door stop in full open position 

  

	k)	EQUIPMENT INSTALLED BY AGUSTA 

  

	 	•	 	 Locked Sliding Windows on pilot/copilot side 

  

					
	CFA October 2007	  	Page 27	  	Contract Number 160507

 MISSION EQUIPMENT INSTALLED 

 

	a)	CUSTOMER REQUIRED CONFIGURATION EQUIPMENT INSTALLED BY AGUSTA OR CHC 

 

	 	•	 	 ADELT (Automatic Deployable ELT w/ Nay interface w/ GPS) Additional strobe light on the sponsons 

 

	 	•	 	 Additional under fuselage anti-collision strobe light 

 

	 	•	 	 HEELS 

  

	 	•	 	 HUMS 

  

	 	•	 	 TCAS 1 (removable parts) 

  

	 	•	 	 VHF/FM Tactical radio NAT NPR 138 (removable parts) + TH250 Weather/Search Radar Honeywell Primus 660 (removable part) Approach Plates Chart Holders
Lighted for both pilot/copilot Auxiliary Fuel Tanks 132 USGaI (removable parts) 

  

	 	•	 	 Emergency Floats (removable parts) 

  

	 	•	 	 Life Rafts (2) up to 17 passengers each 

  

	 	•	 	 Baggage Load increase to 300 Kg 

  

	 	•	 	 EGPWS (removable part) 

  

	 	•	 	 HOMP 

  

	 	•	 	 Separate 4 Points Seat Belts 

  

	 	•	 	 Main Battery M3 44 A/h 

  

	 	•	 	 Steel Ejector Ducts 

  

	b)	PAINTING 

  

	 	•	 	 Customized painting scheme 

  

					
	CFA October 2007	  	Page 28	  	Contract Number 160507

 

 
 Table 1: Prices for Customer required Configuration Equipment (removable) installed by Agusta or CHC 

 

																	
	 Y/N*
	  	 DESCRIPTION
	  	Q/TY	  	PRICES
2007	 	  	PRICES
2008	 	  	PRICES
2009	 
		  	Additional Equipment	  		  	 	USD	  	  	 	USD	  	  	 	USD	  
		  	Customized external Paint Scheme	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	ADELT (Automatic Deployable ELT w/Nav interface w/GPS	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	Additional strobe light on the sponsors	  	SET	  	 	***	  	  	 	***	  	  	 	***	  
		  	Additional under fuselage anticollision strobe light	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	BGPWS (removable part)	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	HOMP	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	HEELS (Helicopter Emergency Exit Lighting System)	  	SET	  	 	***	  	  	 	***	  	  	 	***	  
		  	HUMS (Health & Usage Monitoring System)	  	SET	  	 	***	  	  	 	***	  	  	 	***	  
		  	TCAS I Bendix King (KTA-970 model)	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	VHF/FM Tactical radio NAT NFX 138 + TH250 control panel	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	Weather Radar Honeywell Primus 550	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	4 Points Seat Belts	  	2	  	 	***	  	  	 	***	  	  	 	***	  
		  	44AH Battery installation (in lieu of 40 AH)	  	SET	  	 	***	  	  	 	***	  	  	 	***	  
		  	Steel Exhaust Ducts	  	2	  	 	***	  	  	 	***	  	  	 	***	  
		  	Approach Plates Chart Holders Lighted for both pilot/copilot	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	Auxiliary Fuel Tanks 132 USGal	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	Emergency Floats (removable parts)	  	SET	  	 	***	  	  	 	***	  	  	 	***	  
		  	Life Rafts (2) up to 17 passenger each	  	2	  	 	***	  	  	 	***	  	  	 	***	  
		  	Baggage load capacity increase to 300 Kg.	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	TOTAL ADDITIONAL EQUIPMENT	  	USD	  	 	***	  	  	 	***	  	  	 	***	  

  

	*	Yes/No: Upon CHC selection Agusta to install or CHC to complete by itself 

  

					
	CFA October 2007	  	Page 29	  	Contract Number 160507

 APPENDIX 3 
 AW139 EMS completion 

  

					
	CFA October 2007	  	Page 30	  	Contract Number 160507

 STANDARD CONFIGURATION (EASA / ENAC / FAA IFR CONFIGURATION) 

THF139-0607-1 
  

	a)	AIRFRAME: 

  

	 	•	 	 Aluminum alloy fuselage 

  

	 	•	 	 Polycarbonate Windshields 

  

	 	•	 	 Overhead cockpit windows 

  

	 	•	 	 Lower cockpit windows 

  

	 	•	 	 Cockpit ram air adjustable outlets 

  

	 	•	 	 Forced fan ventilation 

  

	 	•	 	 Bleed air heater and defroster with air noise suppressions 

 

	 	•	 	 Heated Pitot tubes (2) with Pitot heat failure warning (2) 

 

	 	•	 	 Heated static intakes (2) 

  

	 	•	 	 One cockpit and one pilot cabin fire extinguisher 

  

	 	•	 	 Pilot doors (2) with push-out emergency exit window (with “storm window” on pilot side) 

 

	 	•	 	 Plug in sliding doors (2) for passengers cabin access with four locking latches 

 

	 	•	 	 Six cabin push-out emergency exit windows (two on each passenger cabin door) 

 

	 	•	 	 Baggage compartment with 2 lockable baggage compartment doors, LH & RH side. 

 

	 	•	 	 Baggage compartment cargo tie-down fittings 

  

	 	•	 	 Wheeled retractable tricycle landing gear (two wheels on nose gear and brakes on main landing gear) 

 

	 	•	 	 Structural provisions for nose landing gear doors 

  

	 	•	 	 Landing gear mooring 

  

	 	•	 	 Upper deck mooring provisions Hoisting and jacking fittings 

 

	 	•	 	 Tail boom and vertical fin 

  

	 	•	 	 Stabilizers with composite “winglets” 

  

	 	•	 	 Pilot and copilot windshield wipers 

  

	 	•	 	 Maintenance steps for access to upper deck on both sides 

 

	 	•	 	 Upper deck cowlings (one front forward sliding, two side opening for engine access) 

 

	 	•	 	 Steps for cockpit access 

  

	 	•	 	 Anti-vibration masses (2) under cabin floor 

  

	b)	ROTORS AND CONTROLS: 

  

	 	•	 	 Fully articulated Main Rotor (M/R) with five composite blades, five elastomeric bearings and five hydraulic dampers 

 

	 	•	 	 Rotating M/R flight controls - Main rotor hub beanie 

  

	 	•	 	 Three main dual servo actuators 

  

	 	•	 	 Fully articulated Tail Rotor (T/R) with four composite blades, four elastomeric bearings and four elastomeric dampers 

 

	 	•	 	 Rotating T/R flight controls 

  

	 	•	 	 One T/R dual servo actuator - Force trim system 

  

	 	•	 	 Pilot fixed flight controls (cyclic, collective, anti-torque pedals) 

 

	 	•	 	 Copilot fixed flight controls (cyclic, collective, anti-torque pedals) 

 

	 	•	 	 Dual digital 3-axis linear actuators - Rotor brake 

  

	 	•	 	 Provision for main rotor tracking (magnetic pick-up) 

  

					
	CFA October 2007	  	Page 31	  	Contract Number 160507

	c)	ELECTRICAL SYSTEMS: 

  

	 	•	 	 DC primary power generation: 28 V DC regulated voltage provided by two independent 300 A starter generators 

 

	 	•	 	 DC External Power- Receptacle 

  

	 	•	 	 Two Nickel-Cadmium Batteries: one 40 Ali main battery plus one 13 Ah auxiliary battery 

 

	 	•	 	 DC Starter Generator Control Units (2) 

  

	 	•	 	 Navigation lights (3) 

  

	 	•	 	 Anticollision light 

  

	 	•	 	 External emergency landing lights on the sponsons (2) Fixed landing/taxi lights on the sponsons (2) 

 

	 	•	 	 Rotating/ retracting landing light 

  

	 	•	 	 Baggage compartment lighting (3) and smoke sensor 

 

	d)	TRANSMISSION / DRIVE SYSTEM AND HYDRAULIC SYSTEM: 

  

	 	•	 	 Main transmission with two direct drive engine inputs 

 

	 	•	 	 Three main transmission chip detectors/debris collectors with burning capability 

 

	 	•	 	 Two freewheel units 

  

	 	•	 	 Four strut rods for upper deck attachment and one anti-torque plate 

 

	 	•	 	 Intermediate gearbox with sight gauge and magnetic drain plug/chip detector 

 

	 	•	 	 Tail gearbox with sight gage and magnetic drain plug/chip detector 

 

	 	•	 	 Dual independent, redundant hydraulic systems Two hydraulic Power Control Modules (PCMs) 

 

	 	•	 	 Three main transmission driven hydraulic mechanical pumps for controls, landing gear and wheel brake actuation 

 

	 	•	 	 One electrical pump for control checks on ground (engines off) 

 

	 	•	 	 Air conditioning compressor quill 

  

	e)	POWER PLANT & FUEL SYSTEM: 

  

	 	•	 	 Two Pratt & Whitney Canada PT6C-67C engines 

  

	 	•	 	 Two independent FADEC systems (one on each engine) with autostart and engine control functions for normal, emergency and training operations

  

	 	•	 	 Two magnetic chip detectors 

  

	 	•	 	 Two integrated and independent engine oil coolers Separate firewall protection for each engine 

 

	 	•	 	 Fire detection system 

  

	 	•	 	 Fire extinguisher system (2 bottles) 

  

	 	•	 	 Engine exhausts and ejectors 

  

	 	•	 	 Two independent crashworthy fuel cells 

  

	 	•	 	 Two supply pumps on engines 

  

	 	•	 	 Two booster pumps submerged in fuel tanks 

  

	 	•	 	 Two fuel filter assemblies 

  

	 	•	 	 Two engine back—up controls, mechanical and electrical Two manual engine start and ignition systems 

  

					
	CFA October 2007	  	Page 32	  	Contact Number 160507

	f)	STANDARD AVIONICS PACKAGE: 

  

	 	•	 	 1st PFD (Pilot Primary Flight Display 8” x 10” color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data

  

	 	•	 	 2nd PFD (Copilot Primary Flight Display 8” x 10” color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visuali7•tion of flight and navigation data

  

	 	•	 	 1st MFD (Pilot Multifunction Display 8” x 10” color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data

  

	 	•	 	 2nd MFD (Copilot Multifunction Display 8” x 10” color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data

  

	 	•	 	 One Electronic Standby Instrument System (ESIS) (attitude, airspeed, altitude, vertical speed, compass, and IIS data) 

 

	 	•	 	 Two Attitude and Heading Reference Systems (AIIRSs) 

  

	 	•	 	 Two Air Data Modules (ADMs) 

  

	 	•	 	 Two flux valves 

  

	 	•	 	 Two Display Controllers (DCs) 

  

	 	•	 	 Two Cursor Control Devices (CCDs) 

  

	 	•	 	 One Reversion Control Panel (RCP) 

  

	 	•	 	 One Display Dimming Control Panel (DCP) 

  

	 	•	 	 One Stability Augmentation System (SAS) control panel 

 

	 	•	 	 Two Remote Instrument Controllers (RICs) 

  

	 	•	 	 Two Modular Avionic Units (MAUs) incorporating the following major subsystems and/or functions: 

 

	 	•	 	 Vehicle Monitoring System — VMS (dual) 

  

	 	•	 	 Monitor Warning System — MWS (dual) 

  

	 	•	 	 Aural Warning Generator — AWG (single) 

  

	 	•	 	 Central Maintenance Computer — CMC (single) 

  

	 	•	 	 3—Axis Digital Automatic Flight Control System — DAFCS (dual) with autotrim function 

 

	 	•	 	 Provision for CVR/FDR data interface (single) 

  

	 	•	 	 Flight Director System (dual) 

  

	 	•	 	 Pilot and copilot microphone and headset 

  

	 	•	 	 Pilot and Copilot interphone control (cyclic grip and floor switches) 

 

	 	•	 	 Left Modular Radio Cabinet (MRC) with the following modules: 

 

	 	•	 	 One VHF Comm. 

  

	 	•	 	 One VOR/1.0C/GS/MB 

  

	 	•	 	 Right Modular Radio Cabinet (MRC) with the following modules: 

 

	 	•	 	 One VHF Comm. 

  

	 	•	 	 One Mode—S diversity transponder 

  

	 	•	 	 One VOR/LOC/GS/MB 

  

	 	•	 	 One ADF 

  

	 	•	 	 One DME 

  

	 	•	 	 Two pedestal mounted MCDUs (Multi Control Function Display Units) 

  

					
	CFA October 2007	  	Page 33	  	Contract Number 160507

	 	•	 	 1st Radar Altimeter (RT — 300) 

  

	 	•	 	 2nd Radar Altimeter System (RT — 300) 

  

	 	•	 	 Emergency Locator Transmitter (ELT — 121.5/243/406 MHz) 

 

	 	•	 	 One Flight Guidance Controller 

  

	 	•	 	 Honeywell GPS module with Flight Plan Management System (FPMS) 

 

	 	•	 	 Pilot and copilot digital audio panels with remote ICS audio port for ground operation Pilot clock (digital) 

 

	 	•	 	 Copilot clock (digital) 

  

	 	•	 	 One magnetic compass 

  

	 	•	 	 One Outside Air Temperature indicator 

  

	 	•	 	 Two Master Warning Lights (MWLs) 

  

	 	•	 	 Two Master Cluttion Lights (MCLs) 

  

	 	•	 	 Engine I Fire Light 

  

	 	•	 	 Engine 2 Fire Light 

  

	 	•	 	 Baggage compartment smoke detector light 

  

	 	•	 	 Dual electrical power connection for CVR/FDR (FAA requirement compliant) 

 

	 	•	 	 Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator Beacon (ULB) 

 

	g)	INTERIOR TRIM: 

  

	 	•	 	 Cabin, cockpit and baggage compartment utility finishing interior Pilot/ Copilot crashworthy seats (with inertial reels and safety belts) Cockpit
dome/storm light 

  

	 	•	 	 Cockpit utility lights (2) 

  

	 	•	 	 28V DC cockpit/cabin power outlet 

  

	 	•	 	 Cockpit panel sun-glare shields 

  

	 	•	 	 Overhead cockpit windows sun shades 

  

	 	•	 	 Floor provisions for 15-seat configuration 

  

	 	•	 	 Fluorescent lighted emergency exit signs 

  

	h)	MISCELLANEOUS 

  

	 	•	 	 Covers and flags: engine exhaust pipes (2), engine air inlets (2) and Pitot tubes (2), battery connector warning flag (1)

  

	 	•	 	 Manuals: aircraft log, engines operations, flight and maintenance and overhaul, illustrated parts catalogue 

 

	 	•	 	 Tie down-assemblies for main rotor blades (5) 

  

	 	•	 	 Tail rotor blades flapping block (1) 

  

	 	•	 	 Main rotor blade sock pole (1) 

  

	 	•	 	 Main landing gear wheel chocks (2) 

  

	 	•	 	 Main rotor balance and tracking chart, tail rotor balance chart 

 

	 	•	 	 Nose landing gear center pin (1) and landing gear handle locking pin (1) 

 

	 	•	 	 Jacking dome assy (1) 

  

	 	•	 	 Tow bar (1) 

  

	 	•	 	 Loose equipment bag (1) 

  

	i)	EMS INTERIOR TRIM 

  

	 	•	 	 Cabin basic EMS settlement 

  

					
	CFA October 2007	  	Page 34	  	Contract Number 160507

	 	•	 	 Standard ceiling EMS unit with cabin lights 

  

	 	•	 	 Heavy duty EMS floor (longitudinal) - without drainage holes 

 

	 	•	 	 EMS electrical system 

  

	 	•	 	 Floor and ceiling attachment points 

  

	 	•	 	 Equipment rails in ceiling unit 

  

	 	•	 	 Oxygen distribution System (piping flash with liner) 

  

	 	•	 	 IV Hooks (part of ceiling unit) 

  

	 	•	 	 ICS iaw with Australian solution 

  

	 	•	 	 Shelf in Auxiliary Fuel Tank Area (Australian solution) - without inverter 

 

	 	•	 	 Auxiliary Role battery 

  

	 	•	 	 One high (1) density padded crashworthy utility passenger seats (with inertia reels and safety belts) aft facing 

 

	 	•	 	 Three (3) medical seats swiveling and tracking (LH/RH) 

 

	 	•	 	 Baggage retaining net (qt. 2) 

  

	j)	PROVISIONS INSTALLED BY AGUSTA: 

  

	 	•	 	 Night sun search light SX-16 

  

	 	•	 	 Auxiliary fuel tank 

  

	 	•	 	 Search /weather radar primus 701 

  

	 	•	 	 EOPWS Mark XXII 

  

	 	•	 	 Rescue hoist - Breeze 

  

	 	•	 	 Radio Wulfsberg Flexcom II - v/uhf am/fin Multiband - Cockpit/Cabin Separation Curtain 

 

	 	•	 	 Moving Map EuroNav IV 

  

	 	•	 	 Emergency Floats 

  

	 	•	 	 Fastroping - External (on right side) 

  

	 	•	 	 TCAS 1 

  

	k)	EQUIPMENT INSTALLED BY AGUSTA 

  

	 	•	 	 NVG Compatibility (Cockpit) 

  

	 	•	 	 Locked Sliding Windows on pilot/copilot side 

  

					
	CFA October 2007	  	Page 35	  	Contract Number 160507

 MISSION EQUIPMENT INSTALLED 

 

	a)	CUSTOMER REQUIRED CONFIGURATION EQUIPMENT INSTALLED BY AGUSTA OR CHC 

 

	 	•	 	 Wire strike protection system 

  

	 	•	 	 Windshield washing system 

  

	 	•	 	 Night sun search light SX-16 (installation) 

  

	 	•	 	 Night sun search light SX-16 1R filter 

  

	 	•	 	 Auxiliary fuel tank (installation) 

  

	 	•	 	 Pilot/copilot alternative adjustable seats 

  

	 	•	 	 Rappelling kit (including tie-down fitting on FRAME STA3900 / STA5700) 

 

	 	•	 	 High visibility main rotor blades 

  

	 	•	 	 Search/weather radar primus 701 (installation) 

  

	 	•	 	 Emergency flotation system (installation) with hardcovers 

 

	 	•	 	 Rescue hoist —Breeze (installation) 

  

	 	•	 	 TCAS I 

  

	 	•	 	 Direction finder Chehon DF 935-2 SATCOM SkyConnect 

  

	 	•	 	 Radio Wulfsberg Flexcom II - v/uhf am/fm Multiband (installation) 

 

	 	•	 	 Approach Plates Chart Holders Lighted for both pilot/copilot 

 

	 	•	 	 2nd Transponder Mode S 

  

	 	•	 	 Baggage compartment Load increase from 200 kg to 300 kg 

 

	 	•	 	 Lockable Fuel Cap (in lieu of standard) 

  

	 	•	 	 Pedestal Extension (intermediate) 

  

	 	•	 	 Moving Map EuroNav IV (removables) - 5th Display 

  

	 	•	 	 DMU (Data Management Unit 

  

	 	•	 	 44 ah Battery Installation (in lieu of 40 ah) 

  

	 	•	 	 27ah Battery Installation (in lieu of 13 ah) - Surrounding Passenger Lights (LH/RH) 

 

	 	•	 	 Strobe Lights on Sponsons 

  

	 	•	 	 Glass Windshield (in lieu of standard) - 2nd GPS 

  

	 	•	 	 Steel Ejector Duets 

  

	 	•	 	 EGPWS Mark XXII 

  

	b)	PAINTING 

  

	 	•	 	 Customized painting scheme 

  

					
	CFA October 2007	  	Page 36	  	Contract Number 160507

 Table 1: Prices for Customer required Configuration Equipment (removables) installed by Agusta or CHC

  

																	
	 Y/N*
	  	 DESCRIPTION
	  	QTY	  	PRICES
2007	 	  	PRICES
2008	 	  	PRICES
2009	 
		  	 Additional Equipment
	  		  	 	USD	  	  	 	USD	  	  	 	USD	  
		  	 Wire Strike Protection
	  	1 SET	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Windshield Washing System
	  	1 SET	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Pilot/Copilot adjustable seats (delta price)
	  	2	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Rappelling system (LH/RH), including tie-down fitting on Frame STA3900 I sta5700
	  		  	 	***	  	  	 	***	  	  	 	***	  
		  	 High visibility main rotor blades
	  	5	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Customized external Paint Scheme
	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Weather/Search Radar Honeywell Primus 701
	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Emergency Floats removable parts (with Kevlar covers)
	  	1 SET	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Rescue Hoist Breeze 600 lbs removable parts
	  	1 SET	  	 	***	  	  	 	***	  	  	 	***	  
		  	 TCAS I Bendix King (KTA-970 model)
	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Direction Finder Chelton 935-2
	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Iridium SATCOM SkyConnect
	  	SET	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Approach Plates Chart Holders Lighted for both pilot/copilot
	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	 2nd Transponder XS-856A Honeywell, including 2 Antennas - Dome & Margolin
	  		  	 	***	  	  	 	***	  	  	 	***	  
		  	 Baggage reinforced (to 300 kg)
	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Lockable fuel Cap (in lieu of std Fuel Cap)
	  	11	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Pedestal extension Equipment
	  		  	 	***	  	  	 	***	  	  	 	***	  
		  	 Moving Map EURONAV TV - Euroavionics with std aeronautical charts
	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	 5th Display standalone in cockpit
	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	 DMU (Data Management Unit) Honeywell
	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	 44AH Battery installation (in lieu of 40 AH)
	  	SET	  	 	***	  	  	 	***	  	  	 	***	  
		  	 27AH Battery installation (in lieu of 13 AH)
	  	SET	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Extimal Surrounding Passenger Lights (LH/RH)
	  	SET	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Auxiliary Fuel Tanks 132 USGaI
	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Additional strobe light on the sponsons
	  	SET	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Glass windshield (in lieu of std)
	  		  	 	***	  	  	 	***	  	  	 	***	  
		  	 Steel Exhaust Ducts
	  		  	 	***	  	  	 	***	  	  	 	***	  
		  	 2nd GPS CMC-3024 (CMC Electronics / Marconi)
	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Night sun search light SX-16 Spectrolab removable parts
	  	1 SET	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Night sun search light SX-16 IR filter
	  	SET	  	 	***	  	  	 	***	  	  	 	***	  
		  	 Flexcomm II multiband radio V/UHF RT5000
	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	 EGPWS
	  	1	  	 	***	  	  	 	***	  	  	 	***	  
		  	 TOTAL ADDITIONAL EQUIPMENT
	  	USD	  	 	***	  	  	 	***	  	  	 	***	  

  

	*	Yes / No: Upon CHC selection Agusta to install or CHC to complete by itself 

  

					
	CFA October 2007	  	Page 37	  	Contract Number 160507

 APPENDIX 4 
 CHC completions 
 CHC may at its option elect to take delivery of a Standard Configuration
helicopter and perform the Completion Activities (as listed and defined under Table 1 of Appendix 2: AW139 Offshore Completion and Table 1 of Appendix 3: AW139 EMS Completion) required for Offshore or EMS Configuration AW139 helicopter itself either
complete or partly complete starting from June 1, 2009. 
 In case CHC elects to install Agusta Technical Bulletins, then this activity is
dependent on the availability of such Technical Bulletin, which are published on the Agusta website. Technical Bulletins shall be managed between Agusta and CHC under a separate contract, allowing CHC to introduce the completion of the relevant
configurations. The separate contract will cover policy guidelines to be able to exchange specific engineering interface data and the necessary technical coordination assistance, if so agreed and deemed required by the Parties, to allow CHC in
performing the completion activities. 
 Agusta shall ensure that all the required Technical Bulletins, in Appendix 2 and Appendix 3, shall be
made available, by 1’ quarter 2009, to CHC prior the completion work being commenced by CHC. The Technical Bulletins will be updated and amended as required per Agusta standard practice. 
 If CHC introduces any modification to the completions, these modifications shall not interface nor affect the Honeywell Primus Epic System and will not use any Agusta parts nor Agusta part numbers (i.e..
for STC, Engineering Orders or other recognized EASA/FAA document for installation on the AW139 helicopter). 
 Agusta accepts no liability in
relation to the work performed by CHC under this Agreement. CHC hereby indemnifies Agusta against any and all claims from any party in relation to such work. Agusta grants no warranty in relation to the work performed by CHC, as well as any impact
thereto to the unmodified part of the helicopter. 
 Any Intellectual Property (“IP”) required to perform the Offshore and EMS
completions will be made available by Agusta to CHC. Such IF shall remain the property of Agusta and shall be used by CHC only for the purposes of CHC performing the completions of the AW 139 helicopter for Offshore or EMS purchased under this
Framework Agreement and the previous Framework Agreement dated 25 April 2005, provided such aircraft are not sold to any third party other than for the purposes of refinancing. 
 Intellectual Property (“IP”) shall mean any and all information and technical data, whether transmitted or disclosed in oral, written, printed, or electronic format, including, but not limited
to: product drawings, technical reports and specifications, software, patent submissions, patents, inventions, training materials, techniques, and procedures owned by Agusta, whether or not subject to copyright, patent or other legal protection.

 The [P shall be provided free of charge by Agusta, safe CHC shall pay Agusta reasonable cost related to copying charges and the like related
to such IP. CHC shall ensure that CHC shall not 

  

					
	CFA October 2007	  	Page 38	  	Contract Number 160507

 
disclose the IP to any third party without Agusta’s prior written approval. Should Agusta provide its approval of disclosure, CHC shall ensure that any such disclosure is undertaken under a
suitable non-disclosure agreement to be approved by Agusta. 
 Agusta warrants that the provisions for Completions shall have no further cost to
CHC associated therewith. 

  

					
	CFA October 2007	  	Page 39	  	Contract Number 160507

 APPENDIX 5 
 Exit from the Aircraft Assurance Plans (“AAPs”) and from the Complete Overhaul and Material Programs (“COMPs”, and together with the AAPs, the “Programs”) for CHC AW139
Helicopters purchased under this Framework Agreement and the previous Framework Agreement dated 25 April 2005 (the “Helicopters”) in conjunction with the option to select for the Components Protection Agreement (“CPA”).

  

	1.	Termination of the Programs and Future Support 

 Agusta and CHC hereby agree that effective as from the signature date of this Framework Agreement (the “Termination Date”), CHC may exit from the Programs for all Helicopters and from each
agreement for the Programs (the “Support Agreements”), upon providing thirty (30) days prior written notice to Agusta at any time after execution of this Agreement. 

CHC will have the option to enroll the Helicopters under the Agusta CPA at an EC2007 hourly rate of *** USD/FH applicable to the Agusta
standard CPA contractual terms and conditions and coverage, for a period of three (3) years from execution of this Agreement. 
 Should CHC elect to exercise the option of exiting the current Agusta AAP and COMP and entering concurrently the Agusta CPA, then Agusta will evaluate the AAP and COMP buy-out figure to the credit of CHC
in accordance with the relevant contractual clauses and will determine the complete buy-in figure for the CPA to the debt of CHC. If after the above computation, no residual balance is due by Agusta to CHC, then the helicopter is transferred from
AAP or COMP into the CPA agreement. If after the above computation, a residual balance is due by Agusta to CHC, then the helicopter is transferred from AAP or COMP into the CPA agreement and the balance is credited on CHC CPA account. 

CHC will also have the option to have the Helicopters not covered under any Agusta Service Plan. 

 

	2.	Exchange Prices and Major Spares Prices 

 For the Helicopters’ major components, the exchange price and the exchange applicable terms and conditions, and the spares price, will be incorporated in Appendix 9, as agreed by the Parties, to this
Agreement within 10 days after signing the Agreement, and are valid until June 1, 2009, to include discount structures agreed in this Agreement 
  

	3.	Delivery Service Level Agreements 

AOG — Delivered DDP (INCOTERMS 2000) twenty-four (24) hours from receipt of the order by Agusta to Heli-One facility Amsterdam

 Consigned Inventory — to be replenished upon use by Heli-One within seven (7) days delivered DDP (INCOTERMS 2000) upon receipt of
the order by Agusta to Hell-One facility Amsterdam. 

  

					
	CFA October 2007	  	Page 40	  	Contract Number 160507

 APPENDIX 6 
 Certified Agusta Overhaul Capability Centre, Certified Agusta Service 
 Centre and
Materials Support 
 A. CERTIFIED OVERHAUL CAPABILITY CENTRE 
 Agusta shall provide a training analysis by March 31, 2008 for on-the-job training at Augusta’s facility for qualified personnel from the applicable maintenance unit of CHC in order to provide
them the knowledge and skill level to overhaul the main and tail rotor transmission for the AW 139 helicopters. 
 The Parties will agree, based
on the training analysis, further progressive steps to implement an overhaul capability starting by June 1, 2009, It is understood by the Parties that such a date can be achieved provided that CHC performs all the activities and meets the
requirements necessary to be certified as an Agusta Overhaul Capability Centre by the end of 2008. CHC will be responsible for the incidental costs incurred of personnel being trained, for such items as travel, lodgings, rental car, etc. 

Certification of CHC as an Agusta Overhaul Capability Centre is subject to the terms and conditions that will be specified in the Agusta Overhaul
Capability Centre Agreement to be executed by the Parties. Such an Agreement shall reflect the terms and conditions set herein, and may contain necessary further additional provisions. Agusta and CHC hereby agree to establish the Overhaul Capability
Center in Norway or Canada. 
 In order to assess the suitability of CRC’s personnel for such on-the-job-training, CHC’s personnel
will be required to pass an entrance qualification test and undergo evaluation by Agusta. 
 For the purposes of clarification, Agusta will
provide CHC the following ***: 
  

	 	•	 	 twelve (12) weeks of on-the-job training for qualified personnel from the applicable maintenance unit of CHC taking into consideration the
specificities of the D level maintenance of the mechanical assemblies of the AW139 helicopter. This training will concluded with a final exam for CHC) and the qualified personnel in order for CHC to be certified as a Augusta Overhaul Capability
Centre; 

  

	 	•	 	 the relevant drawings of the specific D level tooling of the AW139 mechanical assemblies, when applicable; 

 

	 	•	 	 the Overhaul Technical Manual; and 

  

	 	•	 	 the 1st audit of the AW139 maintenance capabilities as a certified Agusta Overhaul Capability Centre of CHC at no extra cost.

 Upon becoming a Certified Agusta Overhaul Capability Centre, CHC will qualify for the following AW139 discounts:

  

	
	Discount on parts to perform the Overhaul in-house
	***%

  

					
	CFA October 2007	  	Page 41	  	Contract Number 160507

 Upon CHC becoming a Certified Agusta Overhaul Capability Centre, Agusta shall provide the foregoing discount
on parts required to overhaul AW139 helicopters owned and/or operated by CHC. Third party overhauls shall require Agusta prior written authorization. 
 After CHC is certified as an Agusta Overhaul Capability Center , CHC shall provide a price list to Agusta, and Agusta may evaluate this offer with regard to use CHC as an Agusta overflow Overhaul
Capability Centre. 
 Agusta will use its best endeavours to support CHC if applicable, in negotiations with Pratt & Whitney relating
to spare part discounts and licenses required for D-level overhaul capability for the PT6C-67C product. 
 B. CERTIFIED AGUSTA SERVICE CENTRE

 Since CHC will be operating an extensive AW139 helicopter fleet on a worldwide basis, Agusta is prepared to establish CHC as certified
Agusta AW139 service centre, not only providing maintenance services in-house, but also to third parties in conjunction with the execution of this Agreement. In addition (as per table below), as an Agusta Service Centre, CHC will also qualify for a
***% discount on spare parts with an Agusta part number and a ***% discount on avionic spare parts. Special to type tools with an Agusta part number will also be available at a ***% discount to CHC. Certification of CHC as a Service Centre is
subject to the terms and conditions as specified in the Agusta Service Centre agreement to be executed by the Parties. 
 CHC is required to be,
and remain, FAA and/or EASA and/or Transport Canada certified for both operations and maintenance as applicable, in order to qualify for the above mentioned service plans and to become an Agusta Service Center. As a Certified Agusta Service Center,
CHC will qualify therefore for the following AW139 discounts: 
  

									
	 New Parts &
 Tools Routine
	  	New Parts &
AOG	  	Used Parts &
Routine	  	New Parts
Avionics	  	Overhauled Parts
	*** %	  	***%	  	***%	  	***%	  	***%

 CHC and Agusta will agree after signing the Agusta Service Centre Agreement which country or region will be selected to
establish the Service Center. 
 C. MATERIAL SUPPORT 
 Since CRC has demanding operational requirements, Agusta is prepared to implement a dedicated CHC maintenance stock at certain operational locations where the AW139 helicopters will be operated.

  

	 	•	 	 Low Value Items 

 CHC will buy low value items (less than 15.000 USD item unit price) to establish first level maintenance stocks at each operative location. Agusta will support CHC in preparing an adequate spare parts
modelling analysis, based on the requirements and inputs provided by CHC, taking into consideration mission availability requirements of contracts with CHC end-customers. 

  

					
	CFA October 2007	  	Page 42	  	Contract Number 160507

	 	•	 	 High-Value Items 

 For certain high-value items (more than 15.000 USD item unit price), Agusta will establish a stock at appropriate locations agreed with CHC (e.g. Heli-One Global Distribution Center in Hoofddorp,
Netherlands). 
 Agusta will provide for these high-value items an agreed stock of AW139 parts of at least US$ *** in value, from
which CHC will purchase ***% of the value, established at the nominal price list to which a special discount of ***% will be applicable (the “CHC AW139 Stock”). CHC will pay for ***% of the “CHC AW139 Stock” value (US$ *** in
value taking into account the special discount of ***%) each year, and after five (5) years all material will become the property of CHC. 
 The other part of the stock (the “Agusta Consignment AW139 Stock for CHC” — ***% of the total value) will be provided *** to CHC by Agusta at the appropriate agreed location. CHC will pay
Agusta at the time of the usage of these parts, to which a special discount of ***% will be applicable. 
 The “Agusta
Consignment AW139 Stock for CHC” will include D-level parts, with applicable discount of *** (***%), and consumables used in connection with the overhaul/repair of the components of the main and tail rotor transmission for the AW139.

  

					
	CFA October 2007	  	Page 43	  	Contract Number 160507

 APPENDIX 7 
 Purchase Agreement 

  

					
	CFA October 2007	  	Page 44	  	Contract Number 160507

 CONTRACT 
 BETWEEN 
 CHC HELICOPTERS INTERNATIONAL INC. 

AND 

AGUSTA S.p.A. 
 Number XXX 
 (— Offshore or EMS —) 

 

			
	CFA October 2007	  	Contract Number 160507

 INDEX 

 

							
	 	 	 	  	Page	 
			
	 1.
	 	SUPPLIES	  	 	2	  
			
	 2.
	 	PRICE	  	 	2	  
			
	 3.
	 	PAYMENT	  	 	3	  
			
	 4.
	 	DELIVERY	  	 	3	  
			
	 5.
	 	COUNTRY OF DESTINATION	  	 	3	  
			
	 6.
	 	NOTICES	  	 	3	  
			
	 7.
	 	SIGNATURE	  	 	4	  
			
		 	GENERAL TERMS	  			
			
	 1.
	 	TAXES	  	 	5	  
			
	 2.
	 	INSPECTION. ACCEPTANCE AND TITLE	  	 	5	  
			
	 3.
	 	CERTIFICATION	  	 	6	  
			
	 4.
	 	PAINTING SCHEME	  	 	6	  
			
	 5.
	 	CHANGES	  	 	6	  
			
	 6.
	 	LIABILITY	  	 	7	  
			
	 7.
	 	WARRANTY	  	 	7	  
			
	 8.
	 	EXCUSABLE DELAYS	  	 	7	  
			
	 9.
	 	LIQUIDATED DAMAGES	  	 	8	  
			
	 10.
	 	TERMINATION	  	 	8	  
			
	 11.
	 	WAIVER	  	 	9	  
			
	 12.
	 	APPLICABLE LAW AND DISPUTES	  	 	9	  
			
	 13.
	 	EFFECTIVE DATE	  	 	9	  
			
	 14.
	 	ASSIGNMENT	  	 	9	  
			
	 15.
	 	ENTIRE UNDERSTANDING	  	 	9	  

 LIST OF ENCLOSURES 

 

			
	ENCLOSURE 1:	  	HELICOPTER CONFIGURATION
	ENCLOSURE 2:	  	TRAINING
	ENCLOSURE 3:	  	TECHNICAL PUBLICATIONS
	ENCLOSURE 4:	  	SERVICES
	ENCLOSURE 5:	  	WARRANTY POLICY OPTIONS

  

			
	CFA October 2007	  	Contract Number 160507

 CONTRACT 
 By and between: 
 AGUSTA S.p.A., an Italian company, with a sole shareholder,
having a registered office in Samarate, Cascina Costa (VA), Via Giovanni Agusta n. 520, Italy, stock capital Euro 702.537.000,00 fully paid up, number of registration at the Chamber of Commerce of Varese and Fiscal Code 02512010121, subject to the
direction and coordination of Agusta Westland N.V. (herein referred to as “SELLER”)and 
 CHC Helicopters International
Inc. a corporation organized under the laws of Canada, having a registered office at 4740 Agar Dr., Richmond, BC, Canada V7B 1A3 (hereafter ‘CHC”), (hereinafter referred to as “BUYER”), 

collectively referred to as “Parties”, 
 Whereas the BUYER wishes to purchase and the SELLER is willing to sell the under listed products and services at the terms and conditions set out in this CONTRACT and in the Framework Agreement
[                    date & number to be inserted
                    ] to be agreed by and between SELLER and CHC Helicopters International Inc. (hereinafter referred to as ‘Framework
Agreement”). 
 This CONTRACT consists of the Contract terms, the General terms, Enclosure 1, Enclosure 2, Enclosure 3,
Enclosure 4 and Enclosure 5. In case of any conflict, the following order of precedence shall apply in descending order: the Contract terms, the General terms, Enclosure 1, Enclosure 2, Enclosure 3, Enclosure 4 and Enclosure 5. 

Now therefore the Parties agree as follows: 
  

	1.	SUPPLIES 

 BUYER
agrees to buy and SELLER agrees to sell the following products and services (hereinafter referred to as ‘SUPPLIES”): 
  

	 	•	 	 Quantity     helicopter(s) model AW139 in the configuration as specified in 

 

	 	•	 	 Enclosure 1 - Helicopter Configuration (hereinafter referred to as the “HELICOPTER(S)”). 

 

	 	•	 	 TRAINING as per Enclosure 2 and In accordance with the Framework Agreement. 

 

	 	•	 	 TECHNICAL PUBLICATIONS as per Enclosure 3. 

  

	 	•	 	 SERVICES as per Enclosure 4. 

  

			
	CFA October 2007	  	Contract Number 160507

	2.	PRICE 

 The total
CONTRACT value corresponding to the price of the SUPPLIES as per Article 1 is
US$        (                    ) - – Including     % discount as agreed under the
Framework Agreement - as follows: 
  

			
	 •     HELICOPTER
	    	     (    ) AW139 helicopter as detailed in Enclosure 1
		
	 •     TRAINING
	    	No additional charge
		
	 •     TECHNICAL PUBLICATIONS
	    	No additional charge
		
	 •     SERVICES
	    	No additional charge

  

	3.	PAYMENT 

 3.1 Payment of the total
CONTRACT value shall be made through direct bank transfer to the Bank designated by SELLER, against SELLER’s commercial invoices as follows: 
  

	 	(a)	Intermediate payment of
$        (                    USD) shall be made within 10 days from the date of signature of this CONTRACT.

  

	 	(b)	Balance payment of
$        (                    USD), shall be made upon acceptance of the HELICOPTER in accordance with
Article 2 of the General terms hereto. 

 Payments for any additional training and other benefits shall be made in
accordance with the Framework Agreement. All banking costs and expenses shall be at BUYER’s charge. 
  

	4.	DELIVERY 

 4.1 HELICOPTER(S).
equipped as provided in Enclosure 1- Helicopter Configuration, shall be scheduled for acceptance and delivery ex SELLER’s factory in
                    , within (        -
(                    ) months from the CONTRACT Effective Date as defined at Article 13 of the General terms hereto. 

 

	4.2	TRAINING shall be provided as per Enclosure 2- TRAINING and in accordance with the Framework Agreement. 

 

	4.3	TECHNICAL PUBLICATIONS shall be delivered together with the HEUCOPTER, as per Enclosure 3- TECHNICAL PUBLICATIONS. 

 

	4.4	SERVICES shall be provided as per Enclosure 4- SERVICES. 

  

	5.	COUNTRY OF DESTINATION 

 BUYER declares and SELLER acknowledges that the HELICOPTER(S) shall be exported to and registered in as its country of destination. 

 

	6.	NOTICES 

 All
notices under this CONTRACT shall be in writing and either delivered by hand or sent by facsimile (to be confirmed by registered mail), or by registered mail or by courier to the following addresses 

 

			
	CFA October 2007	  	Contract Number 160507

			
	For the SELLER:	  	 AGUSTA S.p.A. — Via G. Agusta 520
 21017 Cascina Costa di Samarate (Varese) —ITALY
 Attn: Contracts Management

Fax +39 0331 229 930

		
	For the BUYER:	  	 CHC HEUCOPTERS INTERNATIONAL INC.
 4740 AGAR DRIVE
 RICHMOND, BRITISH COLUMBIA
 CANADA, V7B 1A3
 Attention: Director (Contracts)

Facsimile: +1 604 232 8359

  

	7.	SIGNATURE 

 This
CONTRACT is signed in two originals by the Parties, each one retaining an original thereof. 
  

			
	For BUYER	  	For SELLER
		
	name	  	name R. Lunardi
		
	title	  	title : VP Commercial Business Unit
		
	signature                            
                         	  	Signature
                                         
       
		
	date	  	date

 In accordance with the Italian law (art. 1341 and art. 1342 of the Italian Civil Code) BUYER specifically
accepts with his signature here below Articles of the General terms : 2 – INSPECTION, ACCEPTANCE AND TITLE; 5 – CHANGES; 6 –LIABILITY ; 7– WARRANTY (including Enclosure 5); 8 – EXCUSABLE DELAYS; 9 – LIQUIDATED
DAMAGES;10 – TERMINATION; 12 – APPLICABLE LAW AND DISPUTES; and 14 –ASSIGNMENT, of this CONTRACT 
  

			
	For BUYER	  	
		
	Signature                            
                     	  	Date

  

			
	CFA October 2007	  	Contract Number 160507

 GENERAL TERMS 

 

	1.	TAXES 

 Local taxes,
custom duties, levies or other fiscal charges, due In SELLER’, country related to the performance of this CONTRACT, shall be borne by SELLER. 
 Local taxes, custom duties, levies or other fiscal charges, due outside of the SELLER’S country for the performance of this CONTRACT, shall be borne by BUYER. 

Value added tax, wherever due, shall be borne by BUYER. 
  

	2.	INSPECTION. ACCEPTANCE AND TITLE 

  

	2.1.	SELLER shell give BUYER 15 (fifteen) days written notice of the date on which the HELICOPTER shat be scheduled to be ready for Inspection, acceptance and delivery.

 BUYER shall start the acceptance process at the SELLER’s designated factory within the aforementioned 15
(fifteen) day period, arranging at its own expense and risk, for Its authorised and qualified representative, to perform the inspection and acceptance of the HELICOPTER(S). 
 Upon successful completion of the Inspection, BUYER or its representative shall sign an acceptance certificate prepared by the SELLER in respect of the HELICOPTER, confirming that It is in accordance with
the CONTRACT, and accepted by BUYER and is ready for delivery. 
  

	2.2.	Should BUYER fail to attend the Inspection within the 15 (fifteen) day period referred to In Article 2.1 of the General terms, the HELICOPTER(S) shall be deemed as
accepted by BUYER based on the SELLER’s Inspection and the certificate of conformity Issued by SELLER’S Quality Control Service shall replace In full the acceptance certificate. 

 

	2.3.	Upon acceptance, In accordance with this Article 2 of the General tams and provided that the obligations for payment in accordance with Article 3 of the Contract terms
have been fulfilled by BUYER, tide to the HELICOPTER(S) and other SUPPLIES delivered hereunder shall be transferred to and vest In BUYER free and clear of any encumbrances, liens, privileges, claims and rights of others. 

BUYER shall bear, from the time of acceptance, all risks, costs and expenses relating to the HELICOPTER(S) and other SUPPLIES delivered,
such as but not limited to storage charges, loss or damage, transportation, Insurance, maintenance. 
  

	2.4.	Should BUYER reject the HELICOPTER(S) on Inspection end test due to demonstrated discrepancies which cannot be corrected during the acceptance process, then the SELLER
shall take the necessary corrective action and shall notify to the BUYER. In the shortest possible time, a new date on which the HELICOPTER(S) shall be ready for acceptance. The Buyer shall not be entitled to reject the HELICOPTER purely on account
of minor 

  

			
	CFA October 2007	  	Contract Number 160507

 
deficiencies and In the event of there being any such minor deficiencies the extent of these and remedial action for their removal by the SELLER shall be jointly agreed between the BUYER and the
SELLER during the inspection and acceptance process. 
  

	2.5.	BUYER agrees to keep Indemnified the SELLER against all costs, expenses, claims and liabilities whatsoever arising out of the BUYER and/or its representative’s
participation in the acceptance of the HELICOPTER and against all liability whatsoever for their death or injury or the loss of or damage to their belongings, except where the seine resulted directly from the fault of the SELLER

  

	3.	CERTIFICATION 

 The
HELICOPTER(S) shAll be delivered with an Airworthiness Certificate for Export (Certificato di Aeronevigabilité per l’Esportazione) to the country of destination released by either European Aviation Safety Agency (EASA), Federal Aviation
Authority (FAA), as the case may be. 
 In the event that the HELICOPTER type is not certificated In the country of destination
SELLER shall make available the technical documentation as reasonably required by the local aviation authority and will support the BUYER to this effect. 
  

	4.	PAINTING SCHEME 

  

	4.1.	As soon as possible after the CONTRACT Effective Date, BUYER shall confirm to SELLER In writing the final choice of the painting scheme and interior finishing details
for the HELICOPTER, in accordance with Enclosure 1- HELICOPTER Configuration 

  

	4.2.	In case the BUYER falls to provide confirmation of the painting scheme and details by the tater of: either (I) the 156 day after the signature date of this
CONTRACT, or (II) the 1806 day before the scheduled delivery data for the HELICOPTER, then the SELLER shall have the right to proceed without delay In the preparation of the HELICOPTER and to deliver it to the BUYER In pre-finishing condition, i.e.:

  

	 	a)	airframe painted with primer only; 

  

	 	b)	cabin liners trimmed but unfinished and not installed: and 

  

	 	c)	seats adjusted and trimmed but uncovered. 

 No compensation whatsoever shag be due from the SELLER to the BUYER In such a case on account of the un-finished HELICOPTER condition. 

 

	5.	CHANGES 

  

	

	5.1.	Engineering changes and improvements, which result In modifications, changes or replacements In the SUPPLIES, but do not affect price, schedule, Installation or
Interchangeability of major assemblies thereof, may be made at any time at SELLER’S option. 

  

			
	CFA October 2007	  	Contract Number 160507

	5.2.	SELLER shall, without BUYER’, consent, incorporate in any of the SUPPLIES any change, which in SELLER’s judgment is as a result of a compulsory modification
required by the EASA, and must necessarily be carded out for reasons of flight safety. 

  

	5.3.	SELLER may propose to BUYER modifications which SELLER deems desirable and which may cause changes to the price and/or to the scheduled acceptance and delivery date.
When proposing such modification to BUYER, SELLER that Indicate the resulting change in price and/or scheduled acceptance and delivery date. Should BUYER accept the proposed modification, BUYER shall give written confirmation to SELLER within 15
(fifteen) days from the date of SEU.ER’s notice. If no reply Is received by SELLER within the said period, the proposed modification shell be considered as unaccepted by BUYER. 

 

	6.	LIABILITY 

 Except in case
of SELLER’s fraud or gross negligence, SELLER shell not be liable for and BUYER hereby assumes liability for any and at losses, damages or complaints of whatsoever nature, as regards both personal injury and property, arising out of or In any
way connected with handling, possession, operation or use of the HELICOPTER(S) and relevant parts after acceptance thereof in accordance with Article 2 of the General terms. 
 BUYER hereby agrees to release SELLER from and fully Indemnify SELLER In respect of any proceedings, actions, claims and suits, which may be instituted by any third party against SELLER in respect to the
foregoing. 
  

	7.	WARRANTY 

 The warranty
provisions granted by the SELLER under Enclosure 5- Warranty, are accepted by the BUYER In place of any other warranty, express or implied, including but not limited to any warranty of merchantability and fitness for purpose. 

Upon acceptance of the HELICOPTER, BUYER shall provide by notice its selection of the warranty option from those provided for in Enclosure
5 - Warranty Policy Options. 
  

	8.	EXCUSABLE DELAYS 

  

	8.1.	The scheduled acceptance and delivery date provided at Article 4 of the Contract terms represents the best estimate and is based on: (1) timely receipt by SELLER
of all Information necessary to permit SELLER to proceed with work without delay and without Interruption, (2) BUYER’s mince with the payment terms. 

 

	8.2.	Whilst SELLER shall exercise Its reasonable effort to achieve the scheduled acceptance and delivery date, SELLER shall not be liable or responsible for delays or
non-compliance resulting from any event beyond the reasonable control of SELLER, Including, but not limited to compliance with any applicable regulation of civil or military authority, technical changes due to flight safety reasons, acts of any
Government or on behalf of them, war declared or undeclared, insurrection, riot or other acts of civil disobedience, embargo or trade restriction, delays or shortages In transportation, fuel, 

 

			
	CFA October 2007	  	Contract Number 160507

	 	
vendors’ and/or subcontractors’ delays, strikes, lockouts, slowdowns, labour disputes, Ike, accident, explosion, epidemic, unusually severe weather, flood, earthquake, delay to
certification, failure in performance of a subcontractor or other acts of God. 

 SELLER shall give written notice
to BUYER of the events causing the excusable delay. Any such event shall extend the delivery data to the extent of the delay so Incurred. 
  

	8.3.	In the event of an excusable delay exceeding 180 days, either Party may cancel the undelivered portion of this CONTRACT, by giving the other Party written notice and
the sole liability of SELLER shell be for the return of any payment received on such undelivered portions. No Interest shall be paid by SELLER to BUYER on such amounts. 

 

	8.4.	Delays deriving from changes as per Article 5.2 of the General terms shall be considered “excusable” and ruled by the provisions of this Article 8. In such
circumstances, Article 8.3 of General terms shall not be applicable. 

  

	8.5.	Any delay in payments will entitle SELLER to postpone the delivery data as a consequence of such delay, without prejudice to SELLER’s rights under Article 9.2 of
General terms hereinafter. 

  

	9.	LIQUIDATED DAMAGES 

  

	9.1.	In case of a delay to the scheduled acceptance and delivery data due to SELLER; failure, and where such delay shall exceed 90 (ninety) working days beyond the scheduled
acceptance and delivery date for the HELICOPTER concerned, BUYER shall have the right to claim , as liquidated damages as Is sole remedy, an amount of 0.15% (zero point fifteen percent) of the price of each delayed HELICOPTER for each complete week
following the said 90 (ninety) working day period for a maximum period of 20 (twenty) weeks. 

  

	9.2.	For any case under this CONTRACT, Including the case of delivery delays, the maximum applicable amount for all damages duo from SELLER shall not exceed 3% (three
percent) of the total CONTRACT value together with the return to BUYER of any Down Payment received by SELLER, on the undelivered portion of the CONTRACT. Such amount shall be BUYER’s sole remedy under this Contrast In lieu of any other rights
and will fully Indemnify BUYER for any damages suffered. 

  

	10.	TERMINATION 

  

	10.1.	In case of SELLER’s failure, for any cause other than that caused by an event described In Article 8 of the General terms, to deliver SUPPLIES in accordance with
this CONTRACT and where the failure has remained unresolved at the date of reaching the maximum amount of liquidated damages, as provided for under Article 9 of General terms, BUYER may terminate this CONTRACT by giving written notification to
SELLER of the termination, such notice shall be effective from the 18th day of its receipt by SELLER. In such event the sole liability of SELLER, In addition to the return to BUYER of any down payment resolved by SELLER, on the undelivered portion
of the CONTRACT, shall be for the payment of the liquidated damages In accordance with Article 9 of General terms, for the amount corresponding to the undelivered SUPPLIES. 

  

			
	CFA October 2007	  	Contract Number 160507

	10,2.	In case of BUYER’s failure to ‘amply with any payment terms, where such payment remains unpaid beyond 45 (forty five) days from Its due data, SELLER shall
have the right to terminate this CONTRACT by giving written notice to BUYER of the termination; such termination shall be effective from the 18th day of its receipt by BUYER. In such event all payments previously made by BUYER shall be retained by
SELLER as liquidated damages, without prejudice to SELLER’s right to recover further damages SELLER may have suffered. 

  

	11.	WAIVER 

 Any failure of
either Party to exercise any right, power, or remedy hereunder shall not act as a waiver thereof, nor shell any single or partial exercise thereof preclude any further exercise of any such right, power or remedy. 

 

	12.	APPLICABLE LAW AND DISPUTES 

 The construction, interpretation, validity and performance of this CONTRACT shall be governed by the laws of the Republic of Italy. 
 The Court (Tribunale) of Busto Arsizio (Italy) shall have exclusive jurisdiction. 
  

	13.	EFFECTIVE DATE 

 This
CONTRACT shall be valid from the date of signature by both Parties and shall become effective (“CONTRACT Effective Date’) on the date that the Down Payment to be made by BUYER pursuant to Article 3.1.a. of the Contract terms has been
received by the SELLER. 
 Notwithstanding the provisions of Article 10.2, In the event the Down Payment has not been received by
the SELLER within 15 days from its due date, the SELLER shall be entitled to declare this Contract null and void with Immediate effect by giving written notice to the BUYER. 

 

	14.	ASSIGNMENT 

 This CONTRACT
or Its benefits and obligations shall not be assignable or transferable by BUYER without the SELLER’. written consent (which may be withheld in the SELLER’s absolute discretion). SFI I FR has the right to assign or transfer this CONTRACT
or Its rights and obligations to Its controlling, controlled or participated companies. 
  

	15.	ENTIRE UNDERSTANDING 

  

	15.1.	This CONTRACT inclusive of its Enclosures constitutes the entire understanding between the Parties In respect of the subject hereof and supersedes all prior
representations, arrangements, undertakings or agreements, whether written or oral, between the Parties. 

  

			
	CFA October 2007	  	Contract Number 160507

	15.2.	Any amendment to this CONTRACT shall be valid only when made in writing and signed by the Parties. 

 

			
	CFA October 2007	  	Contract Number 160507

 ENCLOSURE 1 
 HELICOPTER CONFIGURATION 
  

			
	CFA October 2007	  	Contract Number 160507

	1.	  AW1 39 STANDARD CONFIGURATION AND OPTIONAL EQUIPMENT LIST  

 

	1.1.	  STANDARD CONFIGURATION (EASA / ENAC / FAA IFR CONFIGURATION) 

 

	1.1.1.	 Basic Configuration 

  

	 	a)	AIRFRAME: 

  

	 	•	 	 Aluminum alloy fuselage 

  

	 	•	 	 Polycarbonate Windshields 

  

	 	•	 	 Overhead cockpit windows 

  

	 	•	 	 Lower cockpit windows 

  

	 	•	 	 Cockpit ram air adjustable outlets 

  

	 	•	 	 Forced fan ventilation 

  

	 	•	 	 Bleed air heater and defroster with air noise suppressions 

 

	 	•	 	 Heated Pitot tubes (2) with Pilot heat failure warning (2) 

 

	 	•	 	 Heated static intakes (2) 

  

	 	•	 	 One cockpit and one pilot cabin fire extinguisher 

  

	 	•	 	 Pilot doors (2) with push—out emergency exit window (with “storm window° on pilot side) 

 

	 	•	 	 Plug in sliding doors (2) for passengers cabin access with four locking latches Six cabin push—out emergency exit windows (two on each
passenger cabin door) 

  

	 	•	 	 Baggage compartment with 2 lockable baggage compartment doors, LH & RH side. 

 

	 	•	 	 Baggage compartment cargo tie—down fittings 

  

	 	•	 	 Wheeled retractable tricycle landing gear (two wheels on nose gear and brakes on main landing gear) 

 

	 	•	 	 Structural provisions for nose landing gear doors 

  

	 	•	 	 Landing gear mooring 

  

	 	•	 	 Upper deck mooring provisions 

  

	 	•	 	 Hoisting and Jacking fittings 

  

	 	•	 	 Tail boom and vertical fin 

  

	 	•	 	 Stabilizers with composite ‘winglete 

  

	 	•	 	 Pilot and copilot windshield wipers 

  

	 	•	 	 Maintenance steps for access to upper deck on both sides 

 

	 	•	 	 Upper deck cowlings (one front forward sliding, two side opening for engine access) Steps for cockpit access 

 

	 	•	 	 Anti-vibration masses (2) under cabin floor 

  

	 	b)	ROTORS AND CONTROLS: 

  

	 	•	 	 Fully articulated Main Rotor (WR) with five composite blades, five elastomeric bearings and five hydraulic dampers 

 

	 	•	 	 Rotating WR flight controls 

  

	 	•	 	 Main rotor hub beanie 

  

	 	•	 	 Three main dual servo actuators 

  

			
	CFA October 2007	  	Contract Number 160507

	 	•	 	 Fully articulated Tail Rotor (T/R) with four composite blades, four elastomeric bearings and four elastomeric dampers 

 

	 	•	 	 Rotating T/R flight controls 

  

	 	•	 	 One T/R dual servo actuator 

  

	 	•	 	 Force trim system 

  

	 	•	 	 Pilot fixed flight controls (cyclic, collective, anti-torque pedals) 

 

	 	•	 	 Copilot fixed flight controls (cyclic, collective, anti-torque pedals) 

 

	 	•	 	 Dual digital 3-axis linear actuators 

  

	 	•	 	 Rotor brake 

  

	 	•	 	 Provision for main rotor tracking (magnetic pick-up) 

 

	 	c)	ELECTRICAL SYSTEMS: 

  

	 	•	 	 DC primary power generation: 28 V DC regulated independent 300 A starter generators 

 

	 	•	 	 DC External Power Receptacle 

  

	 	•	 	 Two Nickel-Cadmium Batteries: one 40 Ah main auxiliary battery 

 

	 	•	 	 DC Starter Generator Control Units (2) 

  

	 	•	 	 Navigation lights (3) 

  

	 	•	 	 Anticollislon light 

  

	 	•	 	 External emergency landing lights on the sponsons (2) 

 

	 	•	 	 Fixed landing/taxi lights on the sponsons (2) 

  

	 	•	 	 Rotating/ retracting landing light 

  

	 	•	 	 Baggage compartment lighting (3) and smoke sensor voltage provided by two battery plus one 13 Ah 

 

	 	d)	TRANSMISSION / DRIVE SYSTEM AND HYDRAULIC SYSTEM: 

  

	 	•	 	 Main transmission with two direct drive engine inputs 

 

	 	•	 	 Three main transmission chip detectors/debris collectors with burning capability - Two freewheel units 

 

	 	•	 	 Four strut rods for upper deck attachment and one anti-torque plate Intermediate gearbox with sight gauge and magnetic drain plug/chip detector Tail
gearbox with sight gage and magnetic drain plug/chip detector 

  

	 	•	 	 Dual independent, redundant hydraulic systems 

  

	 	•	 	 Two hydraulic Power Control Modules (PCMs) 

  

	 	•	 	 Three main transmission driven hydraulic mechanical pumps for controls, landing gear and wheel brake actuation 

 

	 	•	 	 One electrical pump for control checks on ground (engines off) 

 

	 	•	 	 Air conditioning compressor quill 

  

	 	e)	POWER PLANT & FUEL SYSTEM: 

  

	 	•	 	 Two Pratt & Whitney Canada PT6C-67C engines 

  

	 	•	 	 Two independent FADEC systems (one on each engine) with autostart and engine control functions for normal, emergency and training operations

  

	 	•	 	 Two magnetic chip detectors 

  

			
	CFA October 2007	  	Contract Number 160507

	 	•	 	 Two integrated and independent engine oil coolers 

  

	 	•	 	 Separate firewall protection for each engine 

  

	 	•	 	 Fire detection system 

  

	 	•	 	 Fire extinguisher system (2 bottles) 

  

	 	•	 	 Engine exhausts and ejectors 

  

	 	•	 	 Two independent crashworthy fuel cells 

  

	 	•	 	 Two supply pumps on engines 

  

	 	•	 	 Two booster pumps submerged in fuel tanks 

  

	 	•	 	 Two fuel fitter assemblies 

  

	 	•	 	 Two engine back—up controls, mechanical and electrical 

 

	 	•	 	 Two manual engine start and ignition systems 

  

	 	f)	STANDARD AVIONICS PACKAGE: 

  

	 	•	 	 1st PFD (Pilot Primary Flight Display 8’ x 10’ color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data

  

	 	•	 	 2nd PFD (Copilot Primary Flight Display 8” x 10” color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data

  

	 	•	 	 1st FD (Pilot Multifunction Display 8” x 10” color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data

  

	 	•	 	 2nd MFD (Copilot Multifunction Display 8” x 10’ color Active Matrix Liquid Crystal Display) as part of Honeywell Primus Epic System for visualization of flight and navigation data

  

	 	•	 	 One Electronic Standby Instrument System (ESIS) (attitude, airspeed, attitude, vertical speed, compass, and ILS data) 

 

	 	•	 	 Two Attitude and Heading Reference Systems (AHRSs) 

  

	 	•	 	 Two Air Data Modules (ADMs) 

  

	 	•	 	 Two flux valves 

  

	 	•	 	 Two Display Controllers (DCs) 

  

	 	•	 	 Two Cursor Control Devices (CCDs) 

  

	 	•	 	 One Reversion Control Panel (RCP) 

  

	 	•	 	 One Display Dimming Control Panel (DCP) 

  

	 	•	 	 One Stability Augmentation System (SAS) control panel 

 

	 	•	 	 Two Remote instrument Controllers (RICs) 

  

	 	•	 	 Two Modular Avionic Units (MAUs) incorporating the following major subsystems and/or functions: 

 

	 	•	 	 Vehicle Monitoring System — VMS (dual) 

  

	 	•	 	 Monitor Warning System — MWS (dual) 

  

	 	•	 	 Aural Warning Generator — AWG (single) 

  

	 	•	 	 Central Maintenance Computer — CMC (single) 

  

	 	•	 	 3—Axis Digital Automatic Flight Control System — DAFCS (dual) with autotrim function 

 

	 	•	 	 Provision for CVR/FDR data interface (single) 

 

			
	CFA October 2007	  	Contract Number 160507

	 	•	 	 Flight Director System (dual) 

  

	 	f)	STANDARD AVIONICS PACKAGE: 

  

	 	•	 	 Pilot and copilot microphone and headset 

  

	 	•	 	 Pilot and Copilot interphone control (cyclic grip and floor switches) 

 

	 	•	 	 Left Modular Radio Cabinet (MRC) with the following modules: 

 

	 	•	 	 One VHF Comm. 

  

	 	•	 	 One VOR/LOC/GS/MB 

  

	 	•	 	 Right Modular Radio Cabinet (MRC) with the following modules: 

 

	 	•	 	 One VHF Comm. 

  

	 	•	 	 One Mode—S diversity transponder 

  

	 	•	 	 One VOR/LOC/GS/MB 

  

	 	•	 	 One ADF 

  

	 	•	 	 One DME 

  

	 	•	 	 Two pedestal mounted MCDUs (Multi Control Function Display Units) 

 

	 	•	 	 1st Radar Altimeter (RT — 300) 

  

	 	•	 	 2nd Radar Altimeter System (RT — 300) 

  

	 	•	 	 Emergency Locator Transmitter (ELT — 121.5/243/406 MHz) 

 

	 	•	 	 One Flight Guidance Controller 

  

	 	•	 	 Honeywell G PS module with Flight Plan Management System (FPMS) 

 

	 	•	 	 Pilot and copilot digital audio panels with remote ICS audio port for ground operation 

 

	 	•	 	 Pilot clock (digital) 

  

	 	•	 	 Copilot clock (digital) 

  

	 	•	 	 One magnetic compass 

  

	 	•	 	 One Outside Air Temperature Indicator Two Master Warning Lights (MWLs) Two Master Caution Ughts (MCLs) 

 

	 	•	 	 Engine 1 Are Light 

  

	 	•	 	 Engine 2 Fire Light 

  

	 	•	 	 Baggage compartment smoke detector light 

  

	 	•	 	 Dual electrical power connection for CVR/FDR (FAA requirement compliant) 

 

	 	•	 	 Cockpit Voice Recorder & Flight Data Recorder (CVR/FDR) with Underwater Locator 

 

	 	•	 	 Beacon (ULB) 

  

	 	g)	INTERIOR TRIM: 

  

	 	•	 	 Cabin, cockpit and baggage compartment utility finishing interior 

 

	 	•	 	 Pilot/ Copilot crashworthy seats (with inertial reels and safety belts) 

 

	 	•	 	 Cockpit dome/storm light 

  

	 	•	 	 Cockpit utility lights (2) 

  

	 	•	 	 28V DC cockpit/cabin power outlet 

  

			
	CFA October 2007	  	Contract Number 160507

	 	•	 	 Cockpit panel sun-glare shields 

  

	 	•	 	 Overhead cockpit windows sun shades 

  

	 	•	 	 Floor provisions for 15-seat configuration 

  

	 	•	 	 Fluorescent lighted emergency exit signs 

  

	 	h)	EXTERIOR PAINTING: 

  

	 	•	 	 Two color polyurethane painting in accordance with SELLER’s standard painting scheme 

 

	1.1.2	Miscellaneous 

  

	 	•	 	 Covers and flags: engine exhaust pipes (2), engine air Inlets (2) and Pitot tubes (2), battery connector warning flag (1)

  

	 	•	 	 Manuals: aircraft log, engines operations, flight and maintenance and overhaul, illustrated parts catalogue 

 

	 	•	 	 Tie down—assemblies for main rotor blades (5) 

  

	 	•	 	 Tail rotor blades flapping block (1) 

  

	 	•	 	 Main rotor blade sock pole (1) 

  

	 	•	 	 Main landing gear wheel chocks (2) 

  

	 	•	 	 Main rotor balance and tracking chart, tail rotor balance chart 

 

	 	•	 	 Nose landing gear center pin (1) and landing gear handle locking pin (1) Jacking dome assy (1) 

 

	 	•	 	 Tow bar (1) 

  

	 	•	 	 Loose equipment bag (1) 

  

	1.2.	ADDITIONAL EQUIPMENT LIST 

  

	
	 INTERIOR COMPLETION

	  
	  
	 EQUIPMENT

	
	
	

  

			
	CFA October 2007	  	Contract Number 160507

 ENCLOSURE 2 
 TRAINING 
  

			
	CFA October 2007	  	Contract Number 160507

 STANDARD TRAINING 

Training will be conducted either at SFI I PR’S facility in Italy or in USA. 

 

	1.	INTRODUCTION 

SELLER is a Type Rating Training Organisation and a Maintenance Training Organization certified by the competent Aviation Authority as
applicable In Italy or USA. 
 The training program developed has been designed to provide the aircrew and the technical
personnel with the knowledge and skills that are required to safely operate and maintain the AW139 HELICOPTER In accordance with the applicable manuals. 
 The training program will be harmonized with the delivery of the HELICOPTER so that training delivered at the appropriate time might ensure the most updated skill. 

 

	2.	STUDENT CERTIFICATION 

 At the end of each course the instructor(s) will conduct academic and practical examinations In accordance with the course programs. The Training School will release to the students a Certificate and a
Log of the activities performed. It will be the BUYER responsibility to qualify the students as per the applicable rules in BUYERS country. 
  

	3.	TRAINING PROGRAM 

Syllabus and detailed contents of the training courses shall be as applicable at the time of their performance in accordance with the
applicable JAR/FAR directives. 
  

	3.1.	PILOT TRAINING 

 Pilot
Training consists of Ground training and Right training. Ground training will include traditional classroom instruction while Flight training will consist of briefing/debriefings, Instructor demonstrations as necessary and student practice of flying
skills and procedures. 
 At the Italian Training facilities, Flight training activity will be conducted both simulator and the
helicopter. 
 SELLER shall provide the following pilot training: 

3.1.1. AW139 TYPE RATING GROUND SCHOOL 
 - Number of students:            2 
 3.1.2. AW139 VFR TYPE RATING FLYING TRAINING 
 - Number of
students:            2 
  

			
	CFA October 2007	  	Contract Number 160507

	3.2.	TECHNICIAN TRAINING 

Maintenance courses cover the HELICOPTER and/or system maintenance procedure as described in the related maintenance manuals. 

 

	3.2.1.	 AW139 AIRFRAME TYPE TRAINIG COURSE  

 - Number of students:             2 
 GENERAL CONDITIONS RULING TRAINING AT THE TRAINING SCHOOL 
  

	a)	The courses shall be conducted at Aguita Westland facilities. 

  

	b)	Pilots shall possess a current Helicopter Pilot Licence issued by a civil or military Aviation Authority, be instrument rated, qualified multi-crew, mufti-engine, and
hold a current flying medical category. 

  

	c)	Technicians shall possess a current Aircraft Maintenance Licence Issued by a civil or military regulatory agency, and shall have at least a 2.5-year experience in
turbine powered helicopter maintenance. 

  

	d)	Pilot flying training will require the use of the BUYER’s HELICOPTER, which wit need to be made available for this purpose, after acceptance and delivery within
the Contract. Daily Inspections and normal servicing of HEUCOPTER during flying training conducted at SELLER facilities will be performed free of charge. BUYER’s HELICOPTER, systems, special tools and GSE, will be utilized, if necessary, for
maintenance training. 

  

	e)	Course Planning. Courses shall be planned with the SELLER Training School Manager at least two months before the course starling date. 

 

	f)	Course Group Leader. BUYER will appoint one group-leader for each course, who will be responsible for the students and for all communications with the SELLER School
staff. To this extent SR IFFrs liability Is limited to the accomplishment of the instruction required. 

  

	g)	Board, lodging and local transportation. All students’ expenses for travel. transportation to school location, boarding and lodging, insurance coverage and medical
assistance will be borne by the Buyer. 

  

	h)	Language. The courses and the classroom texts are In English. Therefore students shall have a good command of the English language, both written and spoken. If
translation is required, the BUYER will supply a translator for each course. In such case, the course duration has to be reconsidered. 

  

			
	CFA October 2007	  	Contract Number 160507

	i)	Helicopter Insurance during the training. Buyer at its sole expenses shall procure and maintain in full force for the entire duration of the trebling activities a
policies of insurance as below: 

  

	 	•	 	 HEUCOPTER Liability (Including Trainees and other Passenger Liability and Public Liability) in respect of the BUYER-owned HEUCOPTER on board of which
the training is carried out in the minimum amounts USD 20.000.000 or equivalent in other currencies any one occurrence/ HELICOPTER. 

  

	 	•	 	 The BUYER shall cause SELLER Its officers, directors, employees, agents, the pilot and SELLER’s training services suppliers to be named as
Additional Insureds In the policy. 

  

	 	•	 	 HELICOPTER Hull All Risks (ground and in flight) including War risks in respect of the BUYER-owned HELICOPTER on board of which the training is carried
out Limit: The BUYER-owned HELICOPTER value. 

 The BUYER shall furthermore cause the Insurers of the policies
to waive their rights of subrogation against SELLER, Its officers, directors, employees, agents, the pilot and SELLER’s training services suppliers. 
 An insurance certificate evidencing compliance with the present clause shall be submitted to SELLER at least 7 (seven) days before to start the training activity. 

BUYER will also undertake to relieve SELLER, its officers, directors, employees, agents, the pilot and SELLER’s training services
suppliers from any damage or claims that may arise from the activity connected with training, including any accident to the HELICOPTER body and/or to a third party. 

 

			
	CFA October 2007	  	Contract Number 160507

 ENCLOSURE 3 
 TECHNICAL PUBLICATIONS 
  

			
	CFA October 2007	  	Contract Number 160507

 TECHNICAL PUBLICATIONS 

One set of the following technical publications, in English language, will be supplied by the SELLER to the BUYER, together with the HELICOPTER :

 AIRFRAME 
  

	•	 	 HELICOPTER IETP (Interactive Electronic Technical Publication) In CD-ROM 

 

	•	 	 HELICOPTER RFM (Rotorcraft Flight Manual) In paper format 

 ENGINES 
  

	•	 	 PT6C-67C IETM Pratt & Whitney Canada In CD-ROM 

 VENDOR ITEMS 
 A standard list of Vendor Items technical publications selected by the
SELLER will be supplied to the BUYER in PDF format through AW139 CMP (Component Maintenance Publications) CD-ROM. 

TECHNICAL PUBLICATIONS UPDATING 
 Updating of one set of the Airframe technical publications shall be provided free of charge by the SELLER to the BUYER, for a minimum of 5 years from the HELICOPTER delivery. 

Updating of the technical publications for the Engines shall be provided to the BUYER by the relevant manufacturer in accordance with their policy.

 Updating of the technical publications for the Vendor items shall be provided to the BUYER by the relevant manufacturers in accordance with
their policy. 
  

			
	CFA October 2007	  	Contract Number 160507

 ENCLOSURE 4 
 SERVICES 
  

			
	CFA October 2007	  	Contract Number 160507

 SERVICES 

(As per Framework Agreement) 
  

			
	CFA October 2007	  	Contract Number 160507

 ENCLOSURE 4 
 SERVICES 
  

			
	CFA October 2007	  	Contract Number 160507

 ENCLOSURE 5 
 WARRANTY POLICY OPTIONS 
  

			
	CFA October 2007	  	Contract Number 160507

 WARRANTY 

New HELICOPTER Commercial Aircraft 
 Three Years / 2,000 Hours Non-Prorated 
 WARRANTY AND REMEDY: SELLER warrants each new
commercial HEUCOPTER aircraft to be free from defect in material or workmanship under normal use and service. SELLER’s sole obligation under this warranty is limited to the replacement or repair of parts which are determined to SELLER’S
reasonable satisfaction to have been defective within 2,000 flight hours of operation or three (3) years after delivery, whichever occurs first and reimbursement of reasonable freight charges. During the first 300 flight hours of use SELLER
will reimburse the BUYER for labor charges associated with warranty related issues, but not thereafter. Spare parts installed as warranty replacement on aircraft which are covered by this New HELICOPTER Commercial Aircraft Warranty, will be
warranted for the balance of the original ship warranty. Defective parts must be reported in writing to the SELLER’S Warranty Administration within 90 days of being found defective. Warranty adjustment is contingent upon the BUYER complying
with SELLER’s Warranty Administration disposition instructions for defective parts. Failure to comply with all of the terms of this paragraph may, at SELLER’s sole option, void this warranty. 

THIS WARRANTY IS GIVEN AND ACCEPTED IN PLACE OF (I) ALL OTHER WARRANTIES OR CONDITIONS, EXPRESS OR IMPLIED, INCLUDING BUT NOT LIMITED TO THE IMPUED
WARRANTIES OR CONDITIONS OF MERCHANTABIUTY AND FITNESS FOR A PARTICULAR PURPOSE AND (ii) ANY OBLIGATION, UABILITY, RIGHT, CLAIM OR REMEDY IN CONTRACT OR IN TORT (DELICT), INCLUDING PRODUCT UABIUTIES BASED UPON STRICT UABIUTY, NEGLIGENCE, OR
IMPLIED WARRANTY IN LAW AND BUYER HEREBY WAIVES SUCH RIGHTS AND CLAIMS. 
 This warranty is the only warranty made by SELLER. The BUYER’S
sole remedy for a breach of this warranty or any defect in a part is the repair or replacement of aircraft parts and reimbursement of reasonable freight charges as provided herein. SELLER excludes liability, whether as a result of a breach of
contract or warranty, negligence or strict product liability, for incidental or consequential damages, including, but not limited to, damage to the aircraft or other property, costs and expenses resulting from required changes or modifications to
aircraft components and assemblies, changes in retirement lives and overhaul periods, local customs fees and taxes, and costs or expenses for commercial losses or lost profits due to loss of use or grounding of aircraft or otherwise. 

SELLER makes no warranty and disclaims all liability in contract or in tort (delict), including, without limitation, negligence and strict tort
(delictual) liability with respect to work performed by third parties at BUYER’s request and with respect to engines, engine accessories, batteries, radios, avionics, and BUYER-furnished equipment, or equipment manufactured by others and
installed at BUYER’s request. For each of the aforementioned items, in particular for equipment from Honeywell International Incorporated, Aerospace Electronic Systems and Pratt and Whitney Canada Corp., the warranty for which is provided for
in this Enclosure 5, SELLER assigns to BUYER the original manufacturer’s warranty and agrees to administer on BUYER’s behalf each manufacturer’s warranty to the extent such manufacturers warranty exists and is assignable. 

 

			
	CFA October 2007	  	Contract Number 160507

 This warranty shall not apply to any aircraft or part thereof which has been repaired or altered outside
SELLER’s factory in any way so as, in SELLER’s sole Judgment, to affect its stability, safety or reliability, or which has been subject to misuse, negligence or accident. Repairs and alterations which use or incorporate parts and
components other than SELLER genuine parts, or parts approved by SELLER for direct acquisition from sources other than SELLER itself are not warranted by SELLER, and this warranty shall be void to the extent that such repairs and alterations, in
SELLER’s sole Judgment, affect the stability, safety or reliability of the aircraft or any part thereof, or damage SELLER genuine part or SELLER-approved parts. No person, corporation or organization, including SELLER Service Facilities, is
authorized by SELLER to assume for it any other liability in connection with the sale of its aircraft and parts, nor to make any warranties beyond the foregoing warranty nor to change any of the terms hereof. No statement, whether written or oral,
made by any person, corporation or organization including SELLER Service Facilities may be taken as a warranty nor will it bind SELLER. 
  

			
	CFA October 2007	  	Contract Number 160507

 WARRANTY. 

New HELICOPTER Commercial Aircraft 
 Three Years / 3,000 Hours Prorated 
 WARRANTY AND REMEDY: SELLER warrants each new
HELICOPTER commercial aircraft to be free from defect in material or workmanship under normal use and service. SELLER’S sole obligation under this warranty is limited to replacement or repair of parts which are determined to SELLER’S
reasonable satisfaction to have been defective within 3,000 flight hours of operation or three (3) years after delivery, whichever occurs first and reimbursement of reasonable freight charges. During the first 300 flight hours of use SELLER
will reimburse the BUYER for labor charges associated with warranty related issues, but not thereafter. After 300 flight hours of use, there will be a prorated charge to the BUYER for replacement parts (prorating the hours of total use against the
then applicable part life or 3,000 flight hours, whichever is the lesser). Spare parts installed as warranty replacement on aircraft which are covered by this New HELICOPTER/AB139 Commercial Aircraft Warranty will be warranted for the balance of the
original ship warranty or for the Commercial Spare Parts Warranty, whichever is the greater. Defective parts shall be reported in writing to SELLER’S Warranty Administration within 90 days of being found defective. Warranty adjustment is
contingent upon the BUYER complying with SELLER’s Warranty Administration disposition instructions for defective parts. Failure to comply with all of the terms of this paragraph may, at SELLER’S sole option, void this warranty. 

THIS WARRANTY IS GIVEN AND ACCEPTED IN PLACE OF (i) ALL OTHER WARRANTIES OR CONDITIONS, EXPRESS OR IMPLIED, INCLUDING BUT NOT
LIMITED TO THE IMPLIED WARRANTIES OR CONDITIONS OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE AND (i1) ANY OBLIGATION, LIABILITY, RIGHT, CLAIM OR REMEDY IN CONTRACT OR IN TORT (DEUCT), INCLUDING PRODUCT UABIUTIES BASED UPON STRICT
LIABILITY, NEGLIGENCE, OR IMPLIED WARRANTY IN LAW AND BUYER HEREBY WAIVES SUCH RIGHTS AND CLAIMS. 
 For each of the aforementioned items, in
particular for equipment from Honeywell International Incorporated, Aerospace Electronic Systems and Pratt and Whitney Canada Corp. the warranty for which is provided for in this Enclosure 5, SELLER assigns to BUYER the original manufacturer’s
warranty and agrees to administer on BUYER’S behalf each manufacturer’s warranty to the extent such manufacturers warranty exists and is assignable. 
 This warranty shall not apply to any aircraft or part thereof which has been repaired or altered outside SELLER’s factory in any way so as, in SELLER’s sole judgment, to affect its stability,
safety or reliability, or which has been subject to misuse, negligence or accident. Repairs and alterations which use or incorporate parts and components other than genuine SELLER parts or parts approved by SELLER for direct acquisition from sources
other than SELLER itself are not warranted by SELLER, and this warranty shall be void to the extent that such repairs and alterations, in SELLER’s sole judgment, affect the stability, safety or reliability of the aircraft or any part thereof,
or damage genuine SELLER or SELLER-approved parts. No person, corporation or organization, including SELLER Service Facilities, is authorized by SELLER to 
  

			
	CFA October 2007	  	Contract Number 160507

 
assume for it any other liability in connection with the sale of its aircraft and parts, nor to make any warranties beyond the foregoing warranty nor to change any of the terms hereof. No
statement, whether written or oral, made by any person, corporation or organization including SELLER Service Facilities may be taken as a warranty nor will it bind SELLER. 

 

			
	CFA October 2007	  	Contract Number 160507

 WARRANTY 

Commercial Spare Parts 
 One Year / 1,000 Hours Prorated 
 WARRANTY AND REMEDY: SELLER warrants each new commercial
aircraft part, or commercial aircraft part reconditioned by SELLER, to be free from defect in material or workmanship under normal use and service. SELLER’s sole obligation under this warranty is limited to replacement or repair of parts which
are determined to SELLER’s reasonable satisfaction to have been defective within 1,000 flight hours of operation or one (1) year after installation, whichever occurs first and reimbursement of reasonable freight charges. After 200 flight
hours of use, there will be a prorated charge to the BUYER for replacement parts (prorating the hours of total use against the then applicable part life or 2,000 flight hours, whichever is the lesser). Defective parts shall be reported in writing to
SEI I FR’s Warranty Administration within 90 days of being found defective. Warranty adjustment is contingent upon the BUYER complying with SELLER’s Warranty Administration disposition instructions for defective parts. Failure to comply
with all of the terms of this paragraph may, at SELLER’S sole option, void this warranty. 
 THIS WARRANTY IS GIVEN AND ACCEPTED IN PLACE
OF (I) ALL OTHER WARRANTIES OR CONDITIONS, EXPRESS OR IMPLIED, INCLUDING BUT NOT LIMITED TO THE IMPLIED WARRANTIES OR CONDITIONS OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE AND (ii) ANY OBLIGATION, LIABILITY, RIGHT, CLAIM OR
REMEDY IN CONTRACT OR IN TORT (DELICT), INCLUDING PRODUCT LIABILITIES BASED UPON STRICT LIABILITY, NEGLIGENCE, OR IMPLIED WARRANTY IN LAW AND BUYER HEREBY WAIVES SUCH RIGHTS AND CLAIMS. 
 This warranty is the only warranty made by SELLER. The BUYER’s sole remedy for a breach of this warranty or any defect in a part is the repair or replacement of aircraft parts and reimbursement of
reasonable freight charges as provided herein. SELLER excludes liability, whether as a result of a breach of contract or warranty, negligence or strict product liability, for incidental or consequential damages, including, but not limited to, damage
to the aircraft or other property, costs and expenses resulting from required changes or modifications to aircraft components and assemblies, changes in retirement lives and overhaul periods, local customs fees and taxes, and costs or expenses for
commercial losses or lost profits due to loss of use or grounding of aircraft or otherwise. 
 SELLER makes no warranty and disclaims all
liability in contract or in tort (delict), including, without limitation, negligence and strict tort (delictual) liability with respect to work performed by third parties at BUYER’s request and with respect to engines, engine accessories,
batteries, radios, and avionics. For each of the aforementioned items, SELLER assigns to BUYER the original manufacturer’s warranty and agrees to administer on BUYER’s behalf each manufacturer’s warranty to the extent such
manufacturer’s warranty exists and is assignable. 
 This warranty shall not apply to any aircraft part which has been repaired or altered
outside SELLER’s factory in any way so as, in SELLER’s sole judgment, to affect its stability, safety or 
  

			
	CFA October 2007	  	Contract Number 160507

 
reliability, or which has been subject to misuse, negligence or accident. Repairs and alterations which use or incorporate parts and components other than genuine SELLER parts or parts approved
by SELLER for direct acquisition from sources other than SR I FR Itself are not warranted by SELLER, and this warranty shall be void to the extent that such repairs and alterations, in SELLER’s sole Judgment, affect the stability, safety or
reliability of the aircraft or any part thereof, or damage genuine SELLER or SELLER-approved parts. No person, corporation or organization, including SELLER Service Facilities, is authorized by SELLER to assume for it any other liability in
connection with the sale of its aircraft and parts, nor to make any warranties beyond the foregoing warranty nor to change any of the terms hereof. No statement, whether written or oral, made by any person, corporation or organization including
SELLER Service Facilities may be taken as a warranty nor will it bind SELLER. 
  

			
	CFA October 2007	  	Contract Number 160507

 Honevwell International Incorporated, Aerospace Electronic Systems 

Warranty Terms: 
 HONEYWELL warrants that
at time of delivery to BUYER, its PRODUCTS will comply with applicable HONEYWELL drawings and specifications as agreed in writing, and will be free from defects in workmanship and material. These warranties shall run to CUSTOMER, its successors and
assigns. This warranty shall be valid for thirty-six (36) months after delivery of HELICOPTER to BUYER. 
 BUYER shall notify HONEYWELL or
a HONEYWELL authorized dealer or service facility in writing of a NONCONFORMANCE within the warranty period and return the PRODUCT to HONEYWELL within sixty (60) calendar days after such discovery. HONEYWELL’S obligation and BUYER’s
remedy under this warranty is limited to either repair or replacement, at HONEYWELL’S option, of any PRODUCT NONCONFORMANCE. All PRODUCTS repaired or replaced hereunder shall be warranted only for the un- expired portion of the original
warranty period. HONEYWELL will pay reasonable allowances for PRODUCT removal and re¬installation in the HELICOPTER, and reasonable costs incurred for troubleshooting HONEYWELL’S avionics system to identify the faulty PRODUCT, providing
such work is accomplished by a HONEYWELL authorized dealer or service facility. Such payment shall be in accordance with removal and reinstallation policies established between HONEYWELL and its authorized service facility/dealer network, and cost
reasonableness shall be determined solely by HONEYWELL. HONEYWELL will not reimburse costs related to removal and/or reinstallation problems. 

HONEYWELL agrees to assume round-trip FREIGHT charged by the HONEYWELL directed carrier to transport the NONCONFORMING PRODUCT to the repair facility
designated by HONEYWELL in an amount not to exceed normal surface shipping charges. HONEYWELL shall not pay for any taxes, tariffs, duties, freight forwarding charges, broker fees, special handling and/or expediting charges. The CUSTOMER shall bear
the risk of loss until delivery of the potentially faulty PRODUCT to HONEYWELL, at which time the risk of loss transfers to HONEYWELL. Risk of loss for tested, repaired or replaced PRODUCTS shall transfer from HONEYWELL to CUSTOMER upon delivery to
the carrier. 
 If PRODUCTS sent to HONEYWELL under warranty are diagnosed as No Fault Found, then the CUSTOMER shall refund FREIGHT costs and
removal and reinstallation charges, and pay a test fee to HONEYWELL, if HONEYWELL submits such an invoice to CUSTOMER. 
 HONEYWELL shall not be
liable for warranty if the PRODUCT has been exposed or subjected to any of the following: 
  

	1.	Fair wear and tear. 

  

	2.	Failure to use, store, maintain, install or operate the PRODUCT in accordance with sound aviation practice, including any reasonable instruction supplied to SELLER.

  

			
	CFA October 2007	  	Contract Number 160507

	3.	Any alteration, not authorized by HONEYWELL, which has impaired the safety of operation or efficiency of the PRODUCT. 

 

	4.	Operated or used in a manner not envisaged in the PRODUCT specification. 

  

	5.	Any PRODUCT on or from which HONEYWELL’S trademark or serial number has been intentionally altered, removed, or obliterated. 

 

	6.	Any PRODUCT repaired at a facility not authorized by HONEYWELL. 

  

	7.	Any accident, contamination, foreign object damage, abuse, neglect or negligence to PRODUCT after delivery to CUSTOMER. 

THIS WARRANTY IS EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES, WHETHER WRITTEN OR ORAL, EXPRESS, IMPLIED OR STATUTORY, INCLUDING, BUT NOT LIMITED TO,
ANY IMPLIED WARRANTIES OF MERCHANTABILITY, FITNESS FOR PARTICULAR PURPOSE, OR NON-INFRINGEMENT, ALL OF WHICH ARE HEREBY EXPRESSLY DISCLAIMED. NO EXTENSION OR EXPANSION OF THIS WARRANTY SHALL BINDING UPON SELLER UNLESS SET FORTH IN WRITING AND SIGNED
BY SELLER’S AUTHORIZED REPRESENTATIVE. 
 IN NO EVENT SHALL SELLER BE LIABLE FOR SPECIAL INDIRECT, INCIDENTAL OR CONSEQUENTIAL DAMAGES
UNDER THIS WARRANTY EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGES INCLUDING, WITHOUT LIMITATION, INTERRUPTION OF BUSINESS, LOSS OF PROFITS, OR LOSS OF USE THE EXCLUSION OF INCIDENTAL AND CONSEQUENTIAL DAMAGES AS SET FORTH IN THIS WARRANTY SHALL
BE DEEMED INDEPENDENT OF, AND SHALL SURVIVE, ANY FAILURE OF THE ESSENTIAL PURPOSE OF ANY LIMITED REMEDY UNDER THE TERMS OF THIS WARRANTY. 

Points of Contact: 
 HONEYWELL may be
contacted twenty-four hours a day, 7 days a week, every day of the year at the following phone numbers: 
  

	 	•	 	 SPEX/AOG Toll Free: (800) 872-7739 

  

	 	•	 	 SPEX/AOG Direct Dial (Phoenix, Arizona, USA): (602) 436-5977 

 

	 	•	 	 Orders Email: crc-ces-omg@honeywell.com 

  

	 	•	 	 Orders Fax (602) 822-7272 or (877) 484-2980 

 

	 	•	 	 General Orders (parts, spares, pubs) Toll Free: (877) 484-2979 

 

	 	•	 	 General Orders Direct Dial (Phoenix, Arizona, USA) (parts, spares, pubs): (602) 436-0272 

 

	 	•	 	 Technical Assistance Toll Free: (877) 436-2005 

  

	 	•	 	 Technical Assistance Direct Dial (Phoenix, Arizona, USA): (602) 436-2005 

 

	 	•	 	 Technical E-Mail: crc-ces-tag@honeywell.com 

  

	 	•	 	 Technical Fax: (602) 822-8005 or (877) 484-2981 

 

			
	CFA October 2007	  	Contract Number 160507

 The following information will be required by HONEYWELL in order to process a warranty claim: 

 

	 	•	 	 HELICOPTER Type 

  

	 	•	 	 HELICOPTER Model Number 

  

	 	•	 	 HELICOPTER Tail Number 

  

	 	•	 	 HELICOPTER Serial Number 

  

	 	•	 	 Part Number of faulty PRODUCT 

  

	 	•	 	 Serial Number of faulty PRODUCT 

  

	 	•	 	 Squawk 

 If there are any
differences between the information in this booklet and the warranty as set forth in the Vendor’s warranty document, the terms and conditions of the Vendor’s document will prevail. 

Pratt & Whitney Canada Corp. 
 PT6C-67 Series Turboshaft Engines operated in civilian or utility helicopters 
  

			
	CFA October 2007	  	Contract Number 160507

 WARRANTY FOR NEW ENGINES 

This Warranty for New Engines is applicable to PT6C-67 series turboshaft engines operated in civilian or utility helicopters, and is for the benefit of
the owners of such engines and their authorized operators. This Warranty is transferable to subsequent owners with written notification to P&WC. 
 Basic Coverage Period 
 The Engine is covered for 2500 engine operating hours or 5 years
from the date of delivery of the Engine to the original operator, whichever occurs first. The terms and conditions applicable to this Warranty shall take effect immediately upon delivery of the Engine to the original operator, either installed on
the aircraft or delivered as a spare. 
 Coverage 
 P&WC warrants that, at the time of delivery to the original operator, the Engine will be free from defects(1) In material and/or manufacturing workmanship and will conform to the applicable P&WC
specification. 
 P&WC will, at its option, repair or replace any Engine parts found to be defective (as defined above), including resultant
damage to the Engine, during the Basic Coverage Period. Replacement parts may be new parts or serviceable parts. 
 When P&WC supplies a
replacement part, or issues credit towards the acquisition of a new part, the removed part becomes the property of P&WC. 
 P&WC will
pay reasonable removal and reinstallation labour for your Engine, and reasonable transportation charges (excluding insurance, duties, brokerage fees, and taxes) to and from the facility designated by P&WC Warranty Administration, during the
Basic Coverage Period. 
  

	(1)	A defect means the breakage or failure of a part which is determined to P&WC’s satisfaction to be due to a defect in material and/or manufacturing workmanship.
Such event will be considered by P&WC to be ‘engine chargeable”, subject to the Warranty and Service Policies. Removal of a part from service because of hourly, cyclic or other limitations on its continued use will not, in the absence
of breakage or failure verifiable by non-destructive inspection, constitute a defect. 

  

	(2)	A part will be considered new if and only if it is accompanied by either the P&WC Manufacturers Release Certificate or Canadian Department of Transport Certificate
of Airworthiness (as applicable), or P&WC’s Suppliers Release Certificate for that specific part and has not been subjected to running time (e.g. a part which has been subjected to engine test time and which must be subsequently
re-inspected and tagged as serviceable will not be considered as new). 

  

			
	CFA October 2007	  	Contract Number 160507

 EXTENDED ENGINE SERVICE POLICY 

In addition to the Warranty for New Engines, P&WC also offers the following Extended Engine Service Policy (“EESP”), which is applicable
after the expiration of the Warranty for New Engines. 
 The EESP shall assist in case of extensive damage to the engine resulting from an
engine chargeable event and where P&WC Warranty Administration determines, at its discretion, that a premature overhaul is required. In such an event, P&WC will, at its discretion, either limit the cost of the overhaul to be performed at a
facility designated by P&WC Warranty administration pursuant to the Limited Cost Overhaul (“LCO”) mechanism described below, or exchange the Engine with a like-value engine upon satisfactory
                     of clear title. 
 This
LCO is calculated based on engine operating hours and cycles since new or last overhaul, the Engine’s age environmental, operational and maintenance conditions. The rates for calculating the LCO are communicated to you through the publication
of a P&WC Service Information Letter (“SIL”). 
 In the event that P&WC elects to exchange your and offers a like-value
engine, the engine exchange                      will be limited to the LCO Maximum Event Cost (that would normally have been payable had there been
no exchange), calculated in accordance with the above referenced SIL. In the event a like-value engine is not available and an alternate engine is offered for exchange, the engine exchange charge will be the Maximum Event Cost plus or minus the
value difference when compared with your Engine, based on Time Since New or Time Since Overhaul, and Low Cycle                      (“LCF”)
parts. 
 The usage cost of LCF parts, optional Services Bulletins, missing parts, repairs required due to factors beyond P&WC;s control,
exchange premiums, transportation, insurance, duties, brokerage fees, and taxes are not covered and are chargeable to you. 
 P&WC reserves
the right to cancel or change the EESP at any time. Shop visits required as a result of an event which occur prior to such change shall not be affected. 
 COMMERCIAL SUPPORT PROGRAMS 
 P&WC may also provide commercial assistance for certain
Airworthiness Directives (ADs) or product improvements through Commercial Support Programs. These programs will be published through Commercial Support Program Notifications (CSPNs) where a credit allowance is offered. 

COVERAGE 
 Costs of normal scheduled maintenance
services: 
  

	 	•	 	 routine line maintenance and adjustment costs; 

  

	 	•	 	 Hot Section Inspection (HSI) and refurbishment costs; 

 

	 	•	 	 engine overhaul or major refurbishment costs; 

 

			
	CFA October 2007	  	Contract Number 160507

	 	•	 	 any other costs related to engine maintenance not specifically covered under this Warranty for New Engines and Extended Engine Service Policy.

 Normal deterioration: 
 any normal wear and tear and deterioration (note: a worn part capable of continued operation which, because it has been accessed, must be restored using repair schemes fully described in the applicable
P&WC Engine Overhaul and Maintenance Manuals, is considered normal). 
 Unsupported parts: 

P&WC reserves the right to exclude Warranty coverage (I) for the following parts, as applicable, and (ii) to the extent that subsequent
repairs or damages are directly attributable to the use of parts which: 
  

	 	•	 	 are not originally supplied by P&WC or its authorized distributors and accompanied by the P&WC Manufacturer’s Release Certificate or
Canadian Department of Transport Certificate of Airworthiness, as applicable; or 

  

	 	•	 	 are not identified in the applicable P&WC Illustrated Parts Catalogue (1PC) and accompanied by the Supplier’s Release Certificate; or

  

	 	•	 	 are not repaired in accordance with P&WC approved repair processes; or are not traceable, e.g. insufficient supporting documentation.

  

	 	•	 	 P&WC excludes Warranty coverage for parts that have been involved in an accident and where subject parts’ or Engine’s failure is
attributable to that part. 

 Factors beyond P&WC’s control: 

 

	 	•	 	 improper storage, usage, maintenance or operation of an Engine, part or accessory (e.g. non- compliance with the applicable P&WC Engine Maintenance
and Overhaul Manuals, P&WC Service Bulletins, Aircraft Flight Manuals, and airworthiness regulations. Any work performed on Engines without due cause such as pre-purchase Inspections, or scheduled maintenance performed at other than P&WC
recommended intervals, will be considered improper maintenance for the purposes of this Warranty for New Engines and Extended Engine Service Policy.); 

  

	 	•	 	 accidents including collisions, rotor strikes, fire, flood, lightning strike, theft, explosion, riot, war, rebellion, seizure or any other belligerent
acts; 

  

	 	•	 	 foreign object damage (F013), erosion, corrosion, sulphidation or any other damage due to the operating environment; 

 

	 	•	 	 alteration to, modification of, or tampering with any Engine, part or accessory after delivery by P&WC, other than strictly in accordance with the
applicable P&WC manuals and this Warranty for New Engines and Extended Engine Service Policy 

  

	 	•	 	 use of stolen or Unsupported Parts, or use of a part or Engine from which P&WC’s name, part number, identification mark or serial number has
been removed or defaced; 

  

	 	•	 	 workmanship performed by a facility other than P&WC’s own manufacturing facilities; 

 

			
	CFA October 2007	  	Contract Number 160507

	 	•	 	 Engines operated by a military, pare-military or government service unless it is determined, at the sole discretion of P&WC, that the Engine has
not been used on operations or flight missions which compromise Engine or parts life or reliability when compared to typical civilian or utility operations; 

 

	 	•	 	 repair or overhaul of a defective part or Engine at a facility other than a facility designated by P&WC Warranty Administration;

  

	 	•	 	 unused cycles (stub life) of an LCF part removed at the operator’s request prior to reaching the service limit; 

 

	 	•	 	 insurance, duties, brokerage fees, and taxes; 

  

	 	•	 	 any other factor beyond P&WC’s control which is not specifically listed herein. 

BUYER RESPONSIBILITIES 
 Maintenance

 BUYER shall be responsible for operating and maintaining the Engine in accordance with P&WC’s written instructions including,
without limitation, the applicable P&WC Engine Maintenance and Overhaul Manuals, P&WC Service Bulletins and your Aircraft Flight Manual. References to “repairs*, ‘replacements” and “overhauls” in this Warranty for
New Engines and Extended Engine Service Policy shall have the meanings contained in the applicable P&WC Engine Maintenance and Overhaul Manuals. 
 Maintenance records 
 BUYER shall be responsible for keeping adequate records of Engine
operation and maintenance. This information is required to substantiate that the Engine has been operated and maintained within the recommended parameters. Upon request, P&WC is entitled to have access to your records. 

For warranty service 
 BUYER shall notify
P&WC of any warrantable defect within thirty (30) days of discovery. 
 P&WC may refuse any warranty claim received more than one
hundred and eighty (180) days after the discovery of any Engine or Engine part defect 
 Warranty claims, which may Include the return of
defective parts, shall be made through the P&WC source of supply (identified In the applicable P&WC IPC), or the P&WC-designated facility or distributor which will furnish or has furnished the replacement parts. 

For any warranty work (including, without limitation, disassembly), BUYER shall send Engine to a facility designated by P&WC Warranty Administration,
in accordance with P&WC’s written instructions. Any work performed at a facility other than a facility designated by P&WC Warranty Administration, without prior written authorization from P&WC Warranty Administration, will be at
your own expense. 
  

			
	CFA October 2007	  	Contract Number 160507

 LIMITATION OF P&WC’S LIABILITY 

THIS IS THE ONLY WARRANTY APPLICABLE TO PT6C-87 SERIES TURBOSHAFT ENGINES OPERATED IN CIVILIAN OR UTILITY HEUCOPTERS AND IS GIVEN AND ACCEPTED IN PLACE
OF ALL OTHER EXPRESS, IMPLIED OR STATUTORY TERMS, REPRESENTATIONS, WARRANTIES OR CONDITIONS, IN CONTRACT OR IN TORT, INCLUDING WITHOUT LIMITATION, ANY WARRANTY OR CONDITION OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE AND ALL SUCH OTHER
TERMS. REPRESENTATIONS. WARRANTIES OR CONDITIONS ARE HEREBY EXPRESSLY DISCLAIMED. THE ONLY REMEDY FOR BREACH OF THIS WARRANTY IS AS SET OUT HEREIN. FOR GREATER CERTAINTY IN NO EVENT SHALL P&WC BE RESPONSIBLE FOR ANY SPECIAL, INCIDENTAL OR
CONSEQUENTIAL DAMAGES ARISING OUT OF OR IN CONNECTION WITH EITHER A BREACH OF THIS WARRANTY OR ANY TORTIOUS OR NEGLIGENT ACT OR OMISSION BY P&WC. SPECIAL INCIDENTAL OR CONSEQUENTIAL DAMAGES INCLUDE, WITHOUT LIMITATION, ECONOMIC LOSS, LOSS OR
DAMAGE TO ANY PROPERTY OR PERSON OR ANY OTHER EXEMPLARY, PUNITIVE OR SIMILAR DAMAGES, AS WELL AS EXPENSES INCURRED EXTERNAL TO THE ENGINE AS A RESULT OF AN ENGINE OR PART DEFECT. NO VARIATION OR EXTENSION OF THIS WARRANTY OR REMEDIES SHALL BE
BINDING UNLESS IN WRITING AND SIGNED BY A DULY AUTHORIZED REPRESENTATIVE OF P&WC. 
 YOUR ACCEPTANCE OF THIS WARRANTY FOR NEW ENGINES AND
EXTENDED ENGINE SERVICE POLICY, OR THE MAKING OF ANY CLAIM OR RECEIPT OF ANY BENEFIT HEREUNDER, CONSTITUTES YOUR ACCEPTANCE OF ALL THE FOREGOING TERMS, CONDITIONS AND UMITAT1ONS. 
 THIS WARRANTY IS GOVERNED BY THE LAWS OF THE PROVINCE OF ONTARIO, CANADA. 
 If you have any
questions or require assistance regarding this Warranty, please call or write to: 
 Manager, Warranty Administration (01 RD4) Pratt &
Whitney Canada Corp. 
 1000 Marie-Victorin Longueuil, Quebec Canada J4G 1A1 
 Telephone: 1 450 647-2816 
 Fax: 1 450 647-2831 or 7282 

E-mail: warranty@ pwc.ca 
 or contact P&WC
Customer Help Desk 
 U.S.A. & Canada: 1 800 268-8000 
 International: 1 450 647-8000, or 
 IAC + 8000-268-8000 (where facilities exist) 

Website: www.pwc.ca 
  

			
	CFA October 2007	  	Contract Number 160507

 If there are any differences between the information in this booklet and the warranty as set forth in the
Vendor’s warranty document, the terms and conditions of the Vendor’s document will prevail. 
  

			
	CFA October 2007	  	Contract Number 160507

 APPENDIX 8 
 RVG Agreement 

  

					
	CFA October 2007	  		  	Contract Number 160507

 TBD MSN TBD 
 Messrs. 
 AGUSTA S.p.A. 
 Cascina Costa di Samarate (VA), Italy; and 
 CHC HELICOPTERS INTERNATIONAL INC. 

4740 Agar Drive 
 Richmond 

British Columbia 
 V7B 1A3 

Canada 

—, this     Day of         , 2007

 Residual Value Guarantee Agreement 
 Dear Sirs, 
 Further to our previous understandings, you will hereinafter find the terms of the
Residual Value Guarantee Agreement (the “Agreement”) set forth below: 
 RECITALS 

 

	A.	CHC Helicopters International Inc. and Agusta S.p.A. have entered into a Framework Agreement on August —, 2007 (the
“Framework Agreement”) providing for the sale to CHC of thirteen (13) AgustaWestland AW139 helicopters with an option for twenty (20) additional AgustaWestland AW139 helicopters, as more fully described in the Framework
Agreement. The purchase of each such helicopters is subject to the execution of separate purchase agreement. 

  

	B.	CHC Helicopters International Inc. and Agusta S.p.A. have entered into a Purchase Agreement dated —, — for the purchase and sale of an one (1) AgustaWestland AW139 helicopter with Manufacturer’s Serial Number TBD (the “Aircraft”). [NM: Consider deleting this clause if the
Novation Agreement will serve as the Purchase Agreement] 

  

	C.	CHC Helicopters International Inc., Agusta S.p.A. and — (the “Owner”) have entered into a Novation Agreement
dated —, — whereby the Owner will buy the Aircraft from Agusta S.p.A. in place of CHC Helicopters International Inc. 

 

	D.	 The Owner and — (the “Lessee”) have entered into a Lease Contract comprising
(a) the terms and conditions of a — dated —, — entered into between the Owner and —. (“—”) and (b) a — Lease Schedule entered into between the Owner and the CHC Helicopters
International Inc. (“the Lease Schedule”) [NTD: Confirm whether a Lease Schedule has been entered into.] (together with the — “the Lease Contract”) whereby
the Owner 

  

					
	CFA October 2007	  		  	Contract Number 160507

	 	
has agreed to lease to the Lessee and the Lessee has agreed to take on lease from the Owner the Aircraft for a Lease period expiring on —, —. A copy of the — (minus schedules) is attached as Schedule IV hereto. 

 

	E.	It is a condition precedent to the obligation of the Owner to purchase the Aircraft from Agusta S.p.A. and/or CHC Helicopters International Inc. and of the Owner to
lease the Aircraft to the Lessee that Agusta S.p.A. (the “RV Guarantor”) and CHC Helicopters International Inc. (as the “CHC RV Guarantor”) shall have executed and delivered this Agreement with respect to the
expected value of the Aircraft and not as a financial guarantee of the Lessee obligations under the Lease Contract or any other document associated with this transaction. 

 NOW, THEREFORE, in consideration of the premises and other good and valuable consideration, the receipt and sufficiency of which are hereby acknowledged, the Parties hereto hereby agree as follows:

 SECTION I - REMARKETING OF THE AIRCRAFT 

 

	1.1	RV Guarantor Obligations 

 All the
RV Guarantor’s obligations under this Agreement are subject to the condition that the Lease Contract shall expire on —, —. For the avoidance of
doubt, the RV Guarantor shall have no obligations under this Agreement in the event that the Aircraft is sold by the Owner prior to such date save only where such sale takes place in association with an assignment made pursuant to Schedule 3 hereof.

  

	1.2	Remarketing Obligation 

  

	(a)	The Owner must provide notification to the RV Guarantor and the CHC RV Guarantor at least eleven (11) months in advance of the Expiry Date indicating whether the
Lessee intends to return the Aircraft to the Owner on the Expiry Date. 

  

	(b)	If the Owner so notifies the RV Guarantor and the CHC RV Guarantor, then the RV Guarantor and the CHC RV Guarantor shall actively market the Aircraft during the
Remarketing Period. Such Parties agree to co-ordinate all remarketing activities and to co-operate with each other to ensure a co-ordinated marketing effort. Each of the RV Guarantor and the CHC 1W Guarantor will use reasonable endeavours to
re-market the Aircraft on the best terms obtainable in the circumstances and will for such purpose nominate an officer of the relevant company no later than 9 months before the Expiry Date to act as its nominated co-ordinator and mutually agree
satisfactory terms and conditions applicable to any proposed sale on the basis set out in Section 1.7 below. 

  

	(c)	For the avoidance of doubt it is hereby declared that nothing in this Agreement appoints or should be construed as appointing the RV Guarantor or the CHC RV Guarantor
as the agent of the Owner for the purpose of concluding any sale of the Aircraft, or otherwise, and neither of them shall have any right or ability to bind the Owner in respect of any such sale or at all. 

  

					
	CFA October 2007	  		  	Contract Number 160507

	1.3	Return Conditions 

The Return Conditions are set out in Schedule I. The return location shall be that specified by the Owner in the Lease Contract.

  

	1.4	Access and Inspections 

  

	(a)	The Owner shall provide in the Lease Contract that the Lessee shall provide upon reasonable notice access to the Aircraft and its Aircraft Documents to the RV Guarantor
and the CHC RV Guarantor and their respective representatives (including any sales agent) to arrange for prospective purchasers to inspect that Aircraft and the Aircraft Documents. 

 

	(b)	Unless otherwise agreed, the RV Guarantor and the CHC RV Guarantor must give the Owner not less than 10 Banking Days’ prior notice of a proposed inspection. The
Owner must give the person authorised to inspect reasonable assistance, including obtaining any necessary consents. 

  

	1.5	Resale Offers 

  

	(a)	The Owner shall immediately present to the RV Guarantor and the CHC RV Guarantor, any Offer received during the Remarketing Period for the Aircraft. The RV Guarantor
and the CHC RV Guarantor will consider all Offers received promptly. The RV Guarantor will not discriminate in remarketing the Aircraft and undertakes to remarket the Aircraft on an equal basis with all other AB or AW139 aircraft in the same
configuration and in the equivalent condition then being remarketed by it. 

  

	(b)	Subject to the terms of this Agreement, for any Offer received during the Remarketing Period in respect of which the date for the execution of the sale contract of the
Aircraft pursuant to such Offer is within the expiry of the Remarketing Period: 

  

	 	(i)	the Parties shall accept any such Offer at or above 75% of the Net Purchase Price; 

 

	 	(ii)	the Owner shall accept any such Offer below 75% and at or above 53% of the Net Purchase Price, provided that the RV Guarantor and the CHC RV Guarantor agree that such
Offer shall be accepted; and 

  

	 	(iii)	the Owner shall accept any other such Offer, subject to unanimous agreement of the Parties. 

In the case of Clauses (i) and (ii) above, it is agreed that if, in the reasonable judgement of the Owner, the prospective
purchaser is not creditworthy or is otherwise considered unlikely to complete the purchase in accordance with the agreed terms, the RV Guarantor and the CHC RV Guarantor will not cease to remarket the Aircraft and will use all reasonable efforts to
seek alternative Offers until the sale to the prospective purchaser is concluded. 

  

					
	CFA October 2007	  		  	Contract Number 160507

	(c)	If any Offer is accepted pursuant to the foregoing provisions then the sale shall be completed on the Expiry Date or as soon as possible thereafter as the Parties may
agree. 

  

	1.6	Right of First Refusal 

 RV
Guarantor and the CHC RV Guarantor shall have the right (the “Purchase Right”) to purchase or otherwise acquire the Aircraft on the same terms and conditions as contained in any Offer made during the Remarketing Period which the
Owner has decided to and is authorized to accept pursuant to Section 1.5 (b). The Purchase Right shall be exercisable in writing and only within ten (10) Business Days of the Owner notifying the RV Guarantor and the CHC RV Guarantor of
such an Offer. As between the RV Guarantor and the CHC RV Guarantor, the RV Guarantor shall have the right of first refusal to exercise the Purchase Right under this Section 1.6. 

 

	1.7	Sale of the Aircraft 

 Any sale of
the Aircraft pursuant to an Offer shall comply with each of the conditions set forth below unless the Parties shall have agreed to waive such condition: 
  

	(i)	the sale price shall be payable to the Owner in full in cash in United States Dollars on completion of the sale. 

 

	(ii)	the sale shall be on the basis of a willing seller and a willing buyer; 

  

	(iii)	on the date of disposition, the Aircraft shall (a) be free and clear of all Owner’s Encumbrances and (b) be free of all encumbrances created by the
Lessee; 

  

	(iv)	the Aircraft shall be sold “as is, where is”; and 

  

	(v)	the Owner shall warrant that on the completion date specified for the sale there shall be vested in the Owner such title to the Aircraft and the Aircraft Documents and
other technical records as was transferred by the Assignee to the Owner pursuant to the Sale Agreement. 

SECTION II - RESIDUAL VALUE GUARANTEE (RVG) 
  

	2.1	The agreement between the Parties concerning the RVG is as follows: 

  

	 	•	 	 all RVG guarantee amounts are based upon a resale price equal to 75% of the Net Purchase Price; 

 

	 	•	 	 the Owner’s responsibility is the first 53% of the Net Purchase Price; 

 

	 	•	 	 the next 3% (i.e 54-56% inclusive) is CHC RV Guarantor’s responsibility; 

 

	 	•	 	 any remaining amount from 57% up to the above-mentioned amount of 75% is to be paid by the RV Guarantor and the CHC RV Guarantor in the Relevant
Proportions. 

  

					
	CFA October 2007	  		  	Contract Number 160507

 In the event of any conflict between the principles set out in this Clause 2.1 and the
remainder of this Clause, the provisions of Clauses 2.2 to 2.5 (inclusive) shall prevail 
  

	2.2	At the date of completion of the sale: 

  

	 	(a)	If the gross sale proceeds of the Aircraft (“Sale Proceeds”) exceed an amount equal to 75% of the Net Purchase Price, then no amount shall be paid
hereunder. 

 The following is an explanatory example of the principle contained in such sub clause (a):

 Sale Proceeds above or equal 75% of Net Purchase Price: 

no amount due 
  

	 	(b)	If the Sale Proceeds are less than 75% of the Net Purchase Price but equal to or greater than an amount equal to 56% of the Net Purchase Price, then the CHC RV
Guarantor and the RV Guarantor will each pay to the Owner its Relevant Proportion of an amount (the “deficiency”) equal to the difference between the Sale Proceeds and an amount equal to 75 % of the Net Purchase Price (such
deficiency subject to a maximum of 19% of the Net Purchase Price). 

 The following is an explanatory example of
the principle contained in such sub clause (b): 
 Sale Proceeds 64% of Net Purchase Price: 

 

					
	75% - 64%	  	=	  	11.0% payable:
			
	RV GUARANTOR	  	pays	  	7.7% (70% of 11%)
			
	CHC RV GUARANTOR	  	pays	  	3.3% (30% of 11%)
			
	Total paid	  		  	11.0%

  

	 	(c)	If Sale Proceeds are less than 56% of the Net Purchase Price then: 

  

	 	(i)	the CHC RV Guarantor and the RV Guarantor will each pay to the Owner its Relevant Proportion of an amount equal to 19% of the Net Purchase Price; and

  

	 	(ii)	the CRC RV Guarantor shall pay to the Owner an amount equal to the difference between the Sale Proceeds and an amount equal to 53% of the Net Purchase Price (such
deficiency subject to a maximum of 3% of the Net Purchase Price); 

  

	 	(iii)	The following is an explanatory example of the principle contained in such sub clause (c): 

  

					
	CFA October 2007	  		  	Contract Number 160507

 Sale Proceeds 54% of Net Purchase Price: 

The first 19% is paid as follows: 
  

					
	RV GUARANTOR	  	pays	  	13.3%(70% of 19%)
			
	CHC RV GUARANTOR	  	pays	  	5.7% (30% of 19%)
			
	The next 2% is paid by the CHC RV Guarantor	  		  	
			
	Total paid	  	21.0%	  	

  

	 	(d)	Any amount payable under this Section 2 shall be payable on the date of completion of such sale. 

 

	 	(e)	If the Aircraft has not been sold by the end of the Remarketing Period, then on that date: 

 

	 	(i)	the CHC RV Guarantor shall pay to the Owner an amount equal to 3% of the Net Purchase Price; and 

 

	 	(ii)	the CHC RV Guarantor and the RV Guarantor will each pay to the Owner its Relevant Proportion of an amount equal to 19% of the Net Purchase Price.

  

	 	(f)	The payment obligations of the RV Guarantor and the CHC RV Guarantor under this Section 2 are several and neither the RV Guarantor nor the CRC RV Guarantor shall
have any liability to the other or to the Owner for the payment obligations of the other. 

  

	2.3	Conditions to Payment of the Guarantee Amount 

 The obligations of each of the RV Guarantor and the CHC RV Guarantor to make any payment under this Section 2 above are in all respects subject to satisfaction of each of the following conditions
precedent 
  

	(a)	No event shall have occurred which constitutes, or, with the passage of time would constitute, a Total Loss of the Aircraft. 

 

	(b)	There shall be no governmental restriction (including export control, currency exchange restriction or other law, regulation, ruling, order or official directive) or
any change in the administration, application or interpretation thereof binding upon the RV Guarantor, the CHC RV Guarantor or the Owner, the effect of which is to prohibit or make illegal the ability of the RV Guarantor and / or the CHC RV
Guarantor to make a payment contemplated in this Agreement 

  

	(c)	The Aircraft Return Conditions shall have been met or the amount of the Compliance Cost, if any, shall have been determined. 

  

					
	CFA October 2007	  		  	Contract Number 160507

 If Section 2.3 (b) applies, then the RV Guarantor and the CHC RV Guarantor (as appropriate) shall
notify the Owner in writing of such governmental restriction and the RV Guarantor and/or the CHC RV Guarantor (as appropriate) and the Owner shall negotiate in good faith for an alternative structure to the transaction which does not violate such or
any other governmental restriction. 
  

	2.4	Aircraft Return Conditions 

  

	(a)	At any time requested within the last two months prior to the Expiry Date, the Owner shall procure that the Lessee shall make the Aircraft available for inspection by
the RV Guarantor or its representative and the CHC RV Guarantor or its representative. In the event that following such an inspection there is any material adverse change in the condition of the Aircraft or any change which would materially affect
the anticipated results of any of the calculations made under the Return Conditions as specified in Schedule I hereto after the date of any such inspection, the Owner shall notify, or procure that both the RV Guarantor and the CHC RV Guarantor are
notified, of such event and each of such parties shall have the opportunity to carry out a further inspection in order to re-verify compliance with such Return Conditions calculations prior to the Expiry Date. 

 

	(b)	If on the foregoing inspection the Aircraft does not meet the Aircraft Return Conditions set forth in Schedule I, the RV Guarantor shall prepare an estimate of the cost
(the “Compliance Cost”) to place the Aircraft in a condition that meets the Aircraft Return Conditions. In the event the Parties are unable to agree on the Compliance Cost (i) the RV Guarantor, the CHC RV Guarantor and the Owner shall
together appoint an internationally recognized independent helicopter engineer (an “Engineer”) (the identity of whom they all agree) who shall determine the Compliance Cost, which determination shall be binding on the Parties hereto and,
if they can not so agree (ii) each of the RV Guarantor, the CHC RV Guarantor and the Owner shall each select an Engineer, who shall together select a fourth Engineer, who shall determine the Compliance Cost, which determination shall be binding
on the Parties hereto. The fees and expenses of the Engineer or, as the case may be, the fourth Engineer, shall be paid by the RV Guarantor, the CHC RV Guarantor and the Owner, each of whom shall pay 1/3 of such fees and costs, except that each
Party shall pay all of the fees and costs of the Engineer selected by it as described in Section (ii) above. Any amount payable by the RV Guarantor and the CHC RV Guarantor under Section 2.1 and 2.2 above shall be reduced pro rats by the
amount of the Compliance Cost, if any.xxx 

  

	2.5	Withholding Taxes 

The RV Guarantor shall be entitled to make a deduction or withholding on account of or comprising taxes required by applicable law for any
sum which may be payable by it hereunder, and the RV Guarantor will not be obliged to gross-up the amount of such payment or otherwise indemnify the Owner or the Lessee against the consequence of such deduction or withholding. The RV Guarantor
shall, in consultation with the Lessor, take all reasonable steps to mitigate any circumstances which arise and which would result in any deduction or withholding referred to in this Section 2.5. 

  

					
	CFA October 2007	  		  	Contract Number 160507

 SECTION III - TERMINATION 

 

	3.1	Termination on Total Loss 

 The
obligations of the RV Guarantor and CHC RV Guarantor hereunder shall cease upon the occurrence of a Total Loss of the Aircraft. 
  

	3.2	Material Breach 

 Upon the
occurrence of a Material Breach and the delivery by the RV Guarantor of a written notice of breach to the Owner, the Owner shall have 30 days within which to remedy, or procure that the Lessee remedies, the Material Breach. “Material
Breach” for the purposes of this Clause 3.2 shall mean: 
  

	 	(a)	failure by the Owner to maintain or procure that the Lessee maintains the Aircraft for the entire duration of the Lease Contract in accordance with the Maintenance
Programme or other program approved by the RV Guarantor;. 

 or 

 

	 	(b)	a material breach by the Lessee (or any relevant sub-lessee) of the Operations and Maintenance undertakings contained in Clause 20 of the Lease (including, without
limitation, a failure by the Owner to procure that the Lessee (i) complies with the Approved Maintenance Programme (as defined in the Lease Contract) and (ii) operates the Aircraft within the limits of the Rotorcraft flight programme
applicable to the Aircraft). 

  

	3.3	In the event that the Material Breach consists of a failure by the Owner to procure the maintenance of the Aircraft in accordance with Clause 3.7 below, which remains
unremedied after a period of 30 days from notice to the Owner, the RV Guarantor shall have the right to terminate this Agreement. The RV Guarantor agrees that in the event of a breach of Section 3.7, its sole remedy will be to terminate this
Agreement and that it will not have any recourse to the Owner for the consequences of any such breach. 

  

	3.4	In the event that the Material Breach consists of a failure by the Owner to procure the maintenance or operation of the Aircraft in accordance with Section 3.2
(b) above, which remains unremedied after a period of 30 days from notice to the Lessor, the RV Guarantor shall determine whether, in its reasonable opinion, the breach in question materially affects the value of the Aircraft. In the event that
the RV Guarantor so determines that the market value of the Aircraft has been diminished, it shall promptly notify the Owner of the amount of such diminution (“the Reduction Amount”) and the Net Purchase Price used for the purpose
of calculating any amount due under Clause 2 above shall be reduced by the Reduction Amount 

  

	3.5	The Owner shall notify the 1W Guarantor and the CHC RV Guarantor promptly upon becoming aware of any breach as described in Section 3.2 (a) and (b) above
or Section 3.7 below. The RV Guarantor will similarly advise the Owner as soon as it becomes aware of any breach as described in either Section 3.2 (a) or (b) above. 

  

					
	CFA October 2007	  		  	Contract Number 160507

	3.6	At all times (i) the Owner shall perform all of its obligations hereunder, and (ii) the Owner shall not amend the Lease Contract, in respect of the use,
ownership, storage, maintenance or utility of the Aircraft without the prior written consent of the RV Guarantor (such consent not to be withheld unless the RV Guarantor reasonably determines that such change adversely affects the value of the
Aircraft or its rights and obligations hereunder). 

  

	3.7	Maintenance 

 The
maintenance programme in respect of the Aircraft shall either be the Maintenance Programme contained in Chapter 5 of the Maintenance Manual or another maintenance programme that has been approved by the RV Guarantor. The RV Guarantor will reasonably
consider any requests by CHC for deviations to the Maintenance Programme or another maintenance programme subject to the additional approval of the Owner or new owner following a Transfer for the purpose of refinancing the Aircraft pursuant to
section 1.1 (a) of Schedule III. 
 In addition: 

 

	 	•	 	 Over and above the Maintenance Programme referred to above, the Owner shall ensure that the Lessee’s personnel carrying out maintenance on the
Aircraft hold valid and appropriate licences and endorsements (FAA or EASA) are fully qualified in their respective capacities and experienced in current practise. 

 

	 	•	 	 The Owner shall ensure that all maintenance undertaken on the Aircraft, will only be executed in, and by, approved EASA part 145 maintenance
organizations or FAA part 145 approved maintenance organisations. 

  

	 	•	 	 All maintenance shall be executed in accordance with the relevant AW139 publications set valid at the time, and as updated from time to time, including
as mandatory, any corrosion inspections and applied remedies as specified in these manuals. 

  

	 	•	 	 The Owner will ensure that the Lessee will only use spare parts and tools as provided by the Aircraft manufacturer or as provided by approved service
stations or approved vendors. 

  

	 	•	 	 Any repair scheme required for maintenance that is not defined in the AW139 publication set, shall be provided to the Aircraft manufacturer for
approval before implementation, unless such repair scheme is a modification and is approved under EASA, in which event no such approval from the Aircraft manufacturer shall be required. 

 

	 	•	 	 The Aircraft logbooks and historical component log cards shall reflect the latest and updated (as on the date of return of the Aircraft) status and
utilization information of the Aircraft configuration, per Aircraft and per component serial number. 

  

					
	CFA October 2007	  		  	Contract Number 160507

 SECTION IV - MISCELLANEOUS 

 

	4.1	Amendments, Etc. 

 No amendment or
waiver of any provision of this Agreement, nor consent to any departure therefrom by either party to this Agreement, shall in any event be effective unless the same Anil be in writing and signed by the RV Guarantor and each of the other Parties
hereto, and then such waiver or consent shall be effective only in the specific instance and for the specific purpose for which given. 
  

	4.2	Notices, Etc. 

 Any notice to be
given under this Agreement shall be sufficient if sent by certified mail, commercial courier, or facsimile to the intended recipient at the address as shown below, or such other address as shall have been provided by notice by either party to the
other party 
  

			
	To the RV Guarantor at	  	AGUSTA S.p.A.
		  	Via G. Agusta, 520
		  	21017 Cascina Costa, Samarate (VA)
		  	ITALY
		
		  	Attn. Contract Administration Dept.
		  	Fax no. 0039 0331 229930
		  	Phone no. 0039 0331 940235
		
	To the CHC RV Guarantor at	  	CHC Helicopters International Inc.
		  	4740 Agar Drive
		  	Richmond B.C.
		  	Canada
		  	V7B 1A3
		
		  	Attn. Blake Fizzard
		  	Fax no. +1 (604) 232 8359
		
	To the Owner at	  	—
		  	—
		  	—
		  	—
		  	—
		  	Attention: —
		  	Fax Number +353 1448 3390—

  

  

					
	CFA October 2007	  		  	Contract Number 160507

			
	with a copy to:	  	—
		  	—
		  	—
		  	—
		  	—
		  	Attention: —

  

	4.3	Severability  

 To the fullest
extent permitted by applicable law, any provision of this Agreement that is prohibited or unenforceable in any jurisdiction shall, as to such jurisdiction, be ineffective to the extent of such prohibition or =enforceability without invalidating the
remaining provisions hereof, and any such prohibition or =enforceability in any jurisdiction shall not invalidate or render unenforceable such provision in any other jurisdiction. 

 

	4.4	No Waivers 

 No failure on the part
of a Party to exercise, no delay in exercising, and no course of dealing with respect to, any right or remedy hereunder will operate as a waiver thereof, nor will any single or partial exercise of any right or remedy hereunder preclude any other
further exercise of any other right or remedy. The remedies provided hereunder are cumulative, and not exclusive of remedies at law or equity. 
  

	4.5	Headings, Etc. 

 Article, section
and paragraph headings in this Agreement are included herein for convenience and reference only and shall not modify, define, expand or limit any of the terms or provisions of this Agreement. 

 

	4.6	Confidentiality 

 Each of the
Parties acknowledges that the existence of, and the terms and conditions of, this Agreement and the commercial and financial arrangements evidenced by this Agreement are considered by the Parties to be confidential information. Each Party shall
maintain such information in confidence and shall not, without the prior written consent of the other Parties, disclose such information to any person, except (a) as necessary to such Party’s legal advisors or accountants or (b) as
may be required by any applicable law or regulation. 
  

	4.7	Execution in Counterparts 

 This
Agreement may be executed in any number of counterparts and by the Parties in separate counterparts, each of which when so executed shall be deemed to be an original and all of which taken together shall constitute one and the same Agreement.

  

					
	CFA October 2007	  		  	Contract Number 160507

	4.8	Assignment 

 Subject to Schedule
Ill, this Agreement is not assignable by the Parties except that: 
  

	 	(i)	the CHC RV Guarantor may assign its rights and obligations hereunder to another subsidiary of CHC Helicopter Corporation of equal or better financial standing than the
CHC RV Guarantor, subject to the RV Guarantor’s and the Owner’s prior written consent, not to be unreasonably withheld and provided such assignment has no material adverse effect on the Owner or the RV Guarantor, and

  

	 	(ii)	the RV Guarantor may assign its rights or delegate its duties hereunder without the consent of the Owner or the CHC RV Guarantor to an affiliate / parent company of the
RV Guarantor provided that (a) such affiliate is wholly owned by directly or indirectly by Finmeccanica S.p.A. and of equal or better financial standing than RV Guarantor, (b) any associated costs and expenses of the Owner and the CHC RV
Guarantor are paid by RV Guarantor, (c) there is no decrease in rights or increase in obligations of the Owner or CHC RV Guarantor as a result of such assignment or delegation, (d) such affiliate / parent company provides to the Owner a
residual value guarantee in substantially the form hereof and (e) the Owner has satisfactorily completed all applicable “know your client” checks in relation to the proposed affiliate or parent company (but only if a “know your
client” check has not already been completed in respect of such affiliate or parent company by the Owner) in accordance with standard internal procedures and provided that such checks are started promptly after a request for a transfer is
given. The RV Guarantor will use all reasonable efforts to assist the Owner in obtaining all the documents required by the Owner to complete its “know your client” checks. 

 

	4.9	Governing Law 

 This Agreement
shall in all respects be governed by, and construed in accordance with, the laws of England without reference to principles of conflicts of law. 
  

	4.10	Arbitration 

 Any dispute arising
out of this Agreement that the Parties are unable to amicably resolve within 45 days, shall be finally settled under the Rules of Conciliation and Arbitration of the International Chamber of Commerce (ICC) by three arbitrators appointed in
accordance with such Rules; the award rendered by the arbitrators shall be final and binding. 
 The arbitration shall be held in England in the
English language. 

  

					
	CFA October 2007	  		  	Contract Number 160507

 SCHEDULE I 
 RETURN CONDITIONS 
  

	1.	Aircraft - 

  

	 	a.	The Aircraft shall have installed all Engines and Parts as is normally installed in such Aircraft, and shall be in a utility condition suitable for operation, all
installed systems to be fully operational. 

  

	 	b.	The Aircraft shall comply with the specification, as modified by the incorporation of all service bulletins as required by the terms of the Lease Contract up to the
date of redelivery and as modified. 

  

	 	c.	All outstanding airworthiness directives, structural inspection requirements and mandatory orders, directives and instructions affecting such model of Aircraft issued
by the manufacturer of the Aircraft, the manufacturer of the Engines and the manufacturer of any main component, or by the Aviation Authority shall have been accomplished (such accomplishment to be on a terminating action basis where it is customary
for the Lessee or other operators of like aircraft to take terminating action) and all maintenance discrepancies cleared from the logbook. If the Lessee has obtained a waiver or deviation from the Aviation Authority from having to comply with any
such mandatory orders, directives or instructions, the Lessee shall, irrespective of such waiver or deviation, comply with all such mandatory orders, directives and instructions covered by such waiver or deviation prior to the return of the Aircraft
to the Owner. 

  

	 	d.	The Aircraft shall be in airworthy condition with a fresh annual inspection, specifically correcting any structural deficiencies. Paint and interior shall be in above
average condition. 

  

	2.	Components 

 All components
shall: 
  

	 	a)	be mid-time on average on a weighted average cost basis (labour and parts). 

 

	 	Such	weighted average cost shall be based upon the specific component’s then-year published price. 

 

	 	b)	be in compliance with all mandatory manufacturer’s and regulatory directives. 

 

	 	c)	the average time remaining on components that are time limited will on, a weighted average cost basis, be 50%; 

and all “On condition” and “Condition Monitored” components shall be serviceable and shall meet the requirements of
the applicable maintenance manual. 

  

					
	CFA October 2007	  		  	Contract Number 160507

 For the avoidance of doubt, it is agreed that to the extent that the same is within the
power and control of the RV Guarantor, nothing contained in any power by the hour agreements or in the Maintenance Programme referred to in Section 3.2 (a) shall affect the obligation contained in the foregoing sub-clauses 2 (a),
(b) and (c) to return the Aircraft in average half life condition. 
  

	3.	Engines – 

 The Lessee will
insure that any discrepancies which may be discovered during the inspections provided in this Schedule 1 from guidelines set out by the engine manufacturer are corrected in accordance with the engine manufacturer’s maintenance manual covering
Pratt & Whitney PT6C-67C engines. 
  

	4.	Fuselage, windows, and doors – 

  

	 	a.	The Fuselage shall be free of major dents and abrasions, and loose, pulled or missing rivets, and minor or significant corrosion. External repairs should have been
carried out only if approved by the Manufacturer or in accordance with Manufacturer documentation. 

  

	 	b.	Windows shall be free of delamination, blemishes and grazing and shall be properly sealed. 

 

	 	c.	Doors shall be free moving, correctly rigged and be fitted with serviceable seals. 

 

	5.	Rotors, cowlings and fairings - 

  

	 	a.	All blade leading edges shall be free from damage which would effect the performance and airworthiness of the aircraft or be outside the airframe manufacturer’s
acceptable tolerances. 

  

	 	b.	All unpainted cowlings and fairings shall be polished to industry standards. 

 

	6.	Interior - 

  

	 	a.	Ceilings, side walls and bulk head panels shall be clean and free of cracks and stains. 

 

	 	b.	All carpets and seat covers shall be in good condition, clean and free of stains, rips and tears and shall meet Aviation Authority fire resistance regulations.

  

	 	c.	All seats, including the 4-point harness restraint systems, shall be free of rips and tears and shall be serviceable, in good condition and meet Aviation Authority fire
resistance regulations. 

  

	 	d.	All required signs and decals shall be clean, legible and in English. 

  

					
	CFA October 2007	  		  	Contract Number 160507

	 	e.	All emergency equipment having a calendar life shall have minimum of one year or 100% of its total approved life, whichever is less, remaining.

  

	7.	Cockpit - 

  

	 	a.	All required decals shall be clean, secure, legible and in English. 

  

	 	b.	All control and instruments panels shall be free of stains and cracks, shall be clean, secure and repainted as necessary and any illegible placards replaced.

  

	 	c.	Floor coverings shall be clean and effectively sealed. 

  

	 	d.	Seat covers shall be in good condition, clean and shall conform to Aviation Authority fire resistance regulations. 

 

	 	e.	Seats, including seat belts, shall be fully serviceable and shall be repainted as necessary. 

 

	8.	Cargo Compartments - All panels shall be in good condition without cracks or brakes. 

 

	9.	Wheel Wells - 

  

	 	a.	Wheel wells shall be clean, free of leaks, repaired as necessary and shall have no exposed metal surfaces which are unprotected from corrosion.

  

	 	b.	All required decals shall be clean, secure and legible. 

  

	10.	Corrosion - 

  

	 	a.	On redelivery the entire Aircraft shall be substantially free from corrosion by reference to inspection by the RV Guarantor, such inspection to be in accordance with
generally accepted industry practices. 

  

	 	b.	Fuel tanks shall be substantially free from contamination by reference to manufacturer’s tolerance levels and airworthiness requirements. 

 

	11.	Test Flight/Ground Run - 

  

	 	a.	If required by the RV Guarantor, the aircraft shall prior to redelivery be test flown by the Lessee using appropriate qualified flight test personnel, for not greater
than two hours, for the purpose of demonstration to the RV Guarantor the satisfactory operation of the aircraft and its equipment and systems. During such test flight command, care, custody and control of the aircraft shall remain at all time with
the Lessee. Two of the RV Guarantor’s representatives may participate in such flight as observers. 

  

	 	b.	All systems must be shown to be in good working order within the tolerances specified in the appropriate maintenance manuals. 

  

					
	CFA October 2007	  		  	Contract Number 160507

	 	c.	The Engines must meet all tolerances specified in the appropriate manual for a ground run. 

 

	 	d.	The Aircraft must be free of fuel, hydraulic, pneumatic, water or waste systems leaks and this is to be demonstrated by topping off the tanks and reservoirs and
executing a functioning check on all systems. 

  

	12.	Documents - 

 All historical
aircraft records and a full and completely amended set of technical publications relation to the aircraft shall be redelivered in the English language with the aircraft 
 Any reference in this Schedule 1 to a manual or program shall refer to that manual, or as, the case may be, program as may be amended, updated or replaced from time to time in accordance with the
manufacturer’s requirements or recommendations. 

  

					
	CFA October 2007	  		  	 Contract Number 160507

 SCHEDULE II 
 DEFINITIONS 
 In this Agreement (unless the context otherwise requires) the following words
and expressions are defined as follows: 
 “Aircraft” means the AW139 helicopter with
— registration mark — and manufacturer’s serial number covering the complete configuration as defined in the including the engines and all
accessories installed, additional equipment and loose equipment provided installed. 
 “Aircraft Documents” means whether in
paper, photographic, digital, electronic or other medium all records, logs, manuals, technical data and other materials and documents (whether kept or to be kept in compliance with any regulation of the Aviation Authority or otherwise) relating to
the Aircraft or any part thereof; 
 “Aircraft Return Conditions” means the requirements relating to the condition of the
Aircraft set out in Schedule I; 
 “Aviation Authority” shall have the meaning given to such expression in the Lease Contract;
“Banking Day” “shall have the meaning given to such expression in the Lease Contract “Compliance Cost” means the Compliance Cost as determined in clause 2.4; 
 “Encumbrance” means a mortgage, charge, pledge, lien, assignment by way of security, retention of title provision, trust or flawed asset arrangement (for the purpose of, or which has the
effect of, granting security) or other security interest securing any obligation of any person or any other agreement or arrangement in any jurisdiction having a similar effect; 
 “Expiry Date” means ——, —;

 “Lessee” means • together with its successors and assigns; 
 “Maintenance Programme” means the Approved Maintenance Programme as defined in the Lease Contract; 
 “Net Purchase Price” means U.S. $—.00 (US Dollars —); 

“Offer” means a bona fide written offer from a willing and able purchaser to purchase the Aircraft. 

“Owner’s Encumbrances” means any Encumbrance created by any act or default of the Owner other than any such Encumbrance which is
permitted by, or created pursuant to, the terms of the Lease Contract 
 “Parent” means CHC Helicopter Corporation. 

“Parties” means the RV Guarantor, the CHC RV Guarantor and the Owner; 

  

					
	CFA October 2007	  		  	Contract Number 160507

 “Relevant Proportions” means, in respect of the RV Guarantor, 70%, and, in respect of the
CHC RV Guarantor, 30%; 
 “Remarketing Period” means the period beginning 9 months prior to the Expiry Date and ending on the
Expiry Date; 
 “Total Loss” shall have the meaning given to such expression in the Lease Contract. 

  

					
	CFA October 2007	  		  	Contract Number 160507

 SCHEDULE III 

 

	1.1	Assignment and dealings by the Owner 

 The Owner may: 
  

	 	(a)	transfer (including by way of security) any of its rights and obligations in respect of the Lease Contract, the Aircraft and this Agreement ( a “Transfer”) to
another person reasonably acceptable to the RV Guarantor and the CHC RV Guarantor provided that 

  

	 	(i)	the Transfer is effected for the purpose of refinancing the Aircraft; 

  

	 	(ii)	the Original Lease Contract either: 

  

	 	(a)	following such Transfer is in full force and effect on terms which impose conditions which are equal to or better than those contained in the Original Lease Contract in
respect of ownership, use, storage, maintenance and utility of the Aircraft; or 

  

	 	(b)	is replaced by another lease facility or lease agreement (“New Lease Contract”) with the Original on terms which impose conditions which are equal to
or better than those contained in the Original Lease Contract in respect of the ownership, use, storage, maintenance or utility of the Aircraft 

  

	 	(iii)	the RV Guarantor and CHC RV Guarantor are paid all costs and expenses incurred by them in connection with the Transfer; and 

 

	 	(iv)	the value and marketability of the Aircraft would not be prejudiced as a result of such Transfer; or 

 

	 	(b)	make a Transfer to any affiliate of the Owner or to the Parent or any affiliate of the Parent reasonably acceptable to the RV Guarantor. 

 

	1.2	Replacement Lease Agreement 

 The Owner shall not enter into any lease agreement of the Aircraft other than: 
  

	 	(a)	the Original Lease Contract; or 

  

	 	(b)	a New Lease Contract; or 

  

	 	(c)	a lease agreement entered into in circumstances where: 

  

	 	(i)	the Owner has terminated the Lease Contract before the Expiry Date; 

  

	 	(ii)	before the Expiry Date the Owner has regained possession of the Aircraft and has re-leased it to another lessee reasonably acceptable to the RV Guarantor on terms set
out above which comply with those applicable to a New Lease Contract; and 

  

					
	CFA October 2007	  		  	Contract Number 160507

	 	(iii)	the value and marketability of the Aircraft shall not be prejudiced as a result of such lease agreement. 

For the avoidance of doubt, the Owner is not required to enter into any hire agreement of the Aircraft provided that the Owner stores and
maintains the Aircraft and the value and marketability of the Aircraft shall not be prejudiced as a result 
  

	1.3	Definition 

 In this
Schedule: 
 “Original Lessee” means • ( as Lessee). 

“Original Lease Contract” means the lease agreement so, • between the Owner and the Original Lessee in respect of
the Aircraft 

  

					
	CFA October 2007	  		  	Contract Number 160507

 SCHEDULE IV 
 COPY OF THE MASTER LEASE AGREEMENT 
 (EXCLUDING SCHEDULES) 

(INTENTIONALLY DELETED) 

  

					
	CFA October 2007	  		  	Contract Number 160507

 If you agree with the foregoing, please rewrite this Agreement on your letter head and resend it to us duly
signed and initialled on each page (including the Schedules) for acceptance. 
  

			
	Best Regards,
		
	By:	 	  

	Title:	 	

  

					
	CFA October 2007	  		  	Contract Number 160507

 APPENDIX 9 
 Helicopters’ major components exchange price & exchange applicable 

terms and conditions 

  

					
	CFA October 2007	  		  	Contract Number 160507

 

 
  

									
	 To:
  

HELI-ONE (NORWAY) AS
 P.O. BOX 535
 N-4055 STAVACKER,

LUFTEVAN, NORWAY
	 	 OPPERTA PARTI ROCAMBO
 SPARE PARTS OFFER
  

PRESENT OFFER IS BEING PROVIDED
 AS PER YOUR
REQUEST
  
 AW139 MAIN COMPONENTS

 
 DATED:
                                   24/09/2007

 
 OFFER VALIDITY:
                   30 DAYS
	  	 Offer
  

07/0001914
  

Customer Code
  

250643
	    	 Date
  

24/09/2007
  

Currency
  
 USD

  

																			
	 ITEM
	  	 REQUESTED

SUPPLY PIN
	  	 CHANGE CODE
	 	 U.M.
	 	QUANTITY	  	UNIT
PRICE	 	  	TOTAL	 	 	DAYS
	0001 / 001	  	30412000234	  	 GEARBOX ASSY Main
	 	N	 	1.00	  	 	***	  	  	 	***	  	 	128
	0001 / 002	  	306120A00134	  	 GEARBOX ASSY Main
	 	N	 	1.00	  	 	***	  	  	 	***	  	 	140
	0001 / 003	  	306320A00114	  	 GEARBOX ASSY Main
	 	N	 	1.00	  	 	***	  	  	 	***	  	 	650
	0002 / 001	  	DT052A00241	  	 GEARBOX ASSY, TAIL ROTOR
	 	N	 	1.00	  	 	***	  	  	 	***	  	 	300
	0002 / 002	  	3T6521A00243	  	 GEARBOX ASSY, TAIL ROTOR
	 	N	 	1.00	  	 	***	  	  	 	***	  	 	360
	0003 / 001	  	3T4521A0Q149	  	 GEARBOX ASSY, INTERMEDIATE
	 	N	 	1.00	  	 	***	  	  	 	***	  	 	120
	0003 / 002	  	DT6321A0Q149	  	 GEARBOX ASSY, INTERMEDIATE
	 	N	 	1.00	  	 	***	  	  	 	***	  	 	360
	0004 / 001	  	304410A00231	  	 TAIL ROTOR BLADE ASSY
	 	N	 	2.00	  	 	***	  	  	 	***	  	 	100
	0005 / 001	  	3G5218A00111	  	 MAIN ROTOR BLADE ASSY
	 	N	 	2.00	  	 	***	  	  	 	***	  	 	100
	0006 / 001	  	3G4730V08731	  	 TAIL ROTOR ACTUATOR II
	 	N	 	1.00	  	 	***	  	  	 	***	  	 	100
	0007 / 001	  	30473#V00531	  	 MAIN ROTOR ACTUATOR II
	 	N	 	1.00	  	 	***	  	  	 	***	  	 	120
	0007 / 002	  	3Q6730V00531	  	 MAIN ROTOR ACTUATOR II
	 	N	 	3.00	  	 	***	  	  	 	***	  	 	360
	0008 / 001	  	3Q0210V08133	  	 LEFT MAIN LANDING GEAR ASSY
	 	N	 	3.00	  	 	***	  	  	 	***	  	 	140
	0009 / 001	  	3Q1220V30133	  	 NOSE LANDING GEAR ASSY
	 	N	 	1.00	  	 	***	  	  	 	***	  	 	250
	0010 / 001	  	10321V30333	  	 RIGHT MAIN LANDING GEAR ASSY
	 	N	 	1.00	  	 	***	  	  	 	***	  	 	190
	0011 / 001	  	1152546-2	  	 DC GENERATOR
	 	N	 	2.00	  	 	***	  	  	 	***	  	 	180

 

 
  

											
	 To:
  

HELI-ONE (NORWAY) AS
 P.O. BOX 535
 N-4055 STAVACKER,

LUFTEVAN, NORWAY
	  		 	 OPPERTA PARTI ROCAMBO
 SPARE PARTS OFFER
  

PRESENT OFFER IS BEING PROVIDED
 AS PER YOUR
REQUEST
  
 AW139 MAIN COMPONENTS

 
 DATED:
                                   24/09/2007

 
 OFFER VALIDITY:
                   30 DAYS
	  	 Offer
  

07/0001914
  

Customer Code
  

250643
	    	 Date
  

24/09/2007
  

Currency
  
 USD

  

																			
	 ITEM
	  	 REQUESTED
SUPPLY PIN
	  	 CHANGE CODE
	 	U.M.	 	QUANTITY	  	UNIT
PRICE	 	  	TOTAL	 	  	DAYS
								
	0011 / 001	  	1152546-2	  	DC GENERATOR	 	N	 	5.00	  	 	***	  	  	 	***	  	  	340
						
	Payment Terms	  	AGAINST DOCUMENTS	 	TOTAL:	 		  	 	USD	  	  	 	***
							
		  		  		 	GRAND TOTAL:	 		  	 	USD	  	  	 	***
	DELIVERY TERMS ARE SUBJECT TO PRIOR SALE	 		 		  				  				  	

  

					
	CFA October 2007	  		  	Contract Number 160507

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