# ASB No. AS365-11.00.02

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### Civil version: N3



# ALERT SERVICE BULLETIN

SUBJECT : PLACARDS AND MARKINGS

Basic and optional marking change

Corresponds to MODs 0711B67 and 0711B68



### Revision No. Date of issue

Revision 0 2011

- 10

- 26

Revision 1 2015

- 01

- 26

Revision 2 2015

- 0 4

- 23



### Summary:

The purpose of this ALERT SERVICE BULLETIN is to provide detailed information on the different locations of the cabin internal evacuation markings.



### Reason for last revision:

The purpose of Revision 2 of this ALERT SERVICE BULLETIN is to add details in order to facilitate the positioning of the evacuation label on the front passenger door, and to provide general information for the local production of an additional label, if necessary, in another language as required by the customer, which will be placed near the English label.



### Compliance:

Airbus Helicopters renders compliance with this ALERT SERVICE BULLETIN mandatory. For the attention of

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### 1. PLANNING INFORMATION

CAUTION

THIS ALERT SERVICE BULLETIN WAS DRAWN

UP BASED ON THE ORIGINAL HELICOPTER CONFIGURATION (AS DEFINED IN INDIVIDUAL INSPECTION RECORD (RIC)).

IT TAKES INTO ACCOUNT ALL AIRBUS

HELICOPTERS-APPROVED CONFIGURATION
CHANGES MADE AFTER DELIVERY, PROVIDED

THAT AIRBUS HELICOPTERS WAS ADVISED

THEREOF. IT DEVOLVES ON THE OPERATOR TO

CHECK THE COMPATIBILITY OF ANY

MODIFICATIONS WITH THE CURRENT AIRCRAFT

CONFIGURATION. IN CASE OF
INCOMPATIBILITY, IT DEVOLVES ON THE

OPERATOR TO DESIGN THE NECESSARY

ADAPTATIONS AND HAVE THEM APPROVED BY

THE AIR TRANSPORT AUTHORITIES IN THE
CONCERNED COUNTRY, AND TO ENSURE

AIRWORTHINESS FOLLOW-UP THEREOF.

1.A. EFFECTIVITY

1.A.1. Helicopters/Installed equipment

- For helicopters with external life rafts: Helicopters pre-MOD 0711B67 (Changes in emergency flotation gear and external life raft markings) and 0711B68 (Changes in cabin door and front and rear passenger door markings).

- For all helicopters: Helicopters pre-MOD 0711B68 (Changes in cabin door and front and rear passenger door markings).

Helicopters on which revisions 0 and 1 of this ALERT SERVICE BULLETIN have been complied with are not concerned by this revision 2, unless the local airworthiness authorities require the production of a label translated into a language required by this authority.



### NOTE

Refer to the aircraft individual inspection Log Book (RIC AMS) and the aircraft log book to identify the actual

modification status of the aircraft.

Helicopters with overhead life raft optional equipment are not concerned by MOD 0711B67.

1.A.2. Non-installed equipment

Not applicable.

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### 1. B. ASSOCIATED REQUIREMENTS

CAUTION

BEFORE ANY WORK, CHECK WHETHER YOUR FLIGHT MANUAL (PMV) AS APPROVED BY THE COMPETENT AUTHORITIES WAS UPDATED (SEE PARAGRAPH 3.D.).

1.C. PURPOSE

The purpose of this ALERT SERVICE BULLETIN is to provide detailed information on the different locations of the cabin internal evacuation markings.

Deviations in the locations of the cabin internal evacuation markings as well as missing markings have been noted at delivery of new helicopters. This Revision of the ALERT SERVICE BULLETIN enables such

differences and absences to be corrected.

The purpose of Revision 1 of this ALERT SERVICE BULLETIN was to render the embodiment of MODs 0711B67 and 0711B68 mandatory.

The purpose of Revision 2 of this ALERT SERVICE BULLETIN is to add details in order to facilitate the positioning of the evacuation label on the front passenger door, and to provide general information for the local production of an additional label, if necessary, in another language as required by the customer, which will be placed near the English label.

The revision 2 does not affect compliance with revisions 0 and 1 of this ALERT SERVICE BULLETIN.



### 1.D. DESCRIPTION

- For all helicopters, this ALERT SERVICE BULLETIN consists in replacing or installing the pilot door, copilot door and front and rear passenger door evacuation labels (MOD 0711B68).

- For helicopters with sliding rear doors and external life raft optional equipment, this ALERT SERVICE BULLETIN consists in removing the evacuation label from the sliding doors and replacing it with a new label on the LH and RH sides of the 9° frame (MOD 0711B67).



### 1.E. COMPLIANCE

1.E.1. Compliance at the works

Not applicable.

1.E.2. Compliance in service

The works must be performed on helicopter by the Operator.

Helicopters/Installed equipment:

Comply with paragraph 3.B. of this ALERT SERVICE BULLETIN within 3 months from receipt of this ALERT SERVICE BULLETIN, Revision1, issued on January 26, 2015.

# ASB No. AS365-11.00.02

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The works must be performed on non-installed equipment by Operator.

Before installation on helicopter, modify stock as per paragraph 3.B.6. of this ALERT SERVICE BULLETIN.



### 1.F. APPROVAL

Approval of modifications

The information or instructions relate to Modification 0711B67 which was approved on November 02, 2010 by EASA for civil version helicopters subject to an Airworthiness Certificate.

The information or instructions relate to Modification 0711B68 which was approved on November 02, 2010 by EASA for civil version helicopters subject to an Airworthiness Certificate.

Approval of this document:

The technical information contained in this Service Bulletin No. 11.00.02 Revision 0 was approved on May 30, 2011 under the EASA Design Organization Approval No. 21J.056 for civil version helicopters subject to an Airworthiness Certificate.

The technical information contained in this ALERT SERVICE BULLETIN No. 11.00.02 Revision 1 was approved on January 22, 2015 under the authority of EASA Design Organization Approval No. 21J.056 for civil version helicopters subject to an Airworthiness Certificate.

The technical information contained in this ALERT SERVICE BULLETIN No. 11.00.02 Revision 2 was approved on April 22, 2015 under the authority of EASA Design Organization Approval No. 21J.056 for civil version helicopters subject to an Airworthiness Certificate.



### 1.G. MANPOWER

For compliance with this ALERT SERVICE BULLETIN, Airbus Helicopters recommends the following personnel qualifications: 1 Airframe Technician.

Time for the operations is indicated for reference, for a standard configuration. Time for the operations: 4 hours approximately.

Helicopter grounding time: 1 half-day.



### 1.H. WEIGHT AND BALANCE

Not applicable.



### 1.I. EFFECT ON ELECTRICAL LOADS

Not applicable.

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### 1.J. SOFTWARE MODIFICATION EMBODIMENT RECORD

Not applicable.



### 1.K. REFERENCES

The following documents are necessary for compliance with this ALERT SERVICE BULLETIN.

MTC: 20.06.01.101: Bonding with adhesives - General rules for bonding with adhesives, MTC: 20.07.02.201: Helicopter parked in a repair shop, MTC: 20.07.03.408: Technical instructions - General principles applicable for visual cleanliness and

appearance checks on an aircraft after an inspection or a repair,

PMV: Section 2.7: NR14 of 10- 22, PMV: Supplement 12: NR3 of 10- 22, PMV: Supplement 14: NR6 of 10- 22.



### 1.L. DOCUMENTS AFFECTED

The modifications will be integrated in the new aircraft documents.

Publications for retrofitted aircraft will not be updated. The updated IPC must be ordered by Customer.

The modifications will be integrated by Airbus Helicopters in the following document:

- PMV.



### 1.M. INTERCHANGEABILITY OR MIXABILITY OF PARTS

Interchangeability:

Labels pre- and post-MOD are not interchangeable.

Mixability:

Mixability of labels pre- and post-MOD is prohibited.

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### 2. MATERIAL INFORMATION

2.A. MATERIAL: PRICE - AVAILABILITY - PROCUREMENT

For any information concerning cost of modification kits and components or for assistance, contact the Airbus Helicopters Network Sales and Customer Relations Department.

Delivery deadlines will be indicated by Sales and Customer Relations Department on the Operator's request.

Order the required quantity from the Airbus Helicopters Network Customer Support Sales Department.

Airbus Helicopters Etablissement de Marignane

Direction Ventes et Relations Client

13725 MARIGNANE CEDEX

FRANCE

Configuration Material P/N Qty

For helicopters with cabin sliding rear passenger

doors. 365A08

- 4481

- 0071 1

For helicopters with cabin rear passenger swing

doors. 365A08

- 4481

- 00 71

365A00

- 0602

- 77

365A00

- 0602

- 76 1

1

1
For helicopters with external life rafts 365A00

- 0631

- 64 2



### NOTE

On the purchase order, please specify the mode of transport, the destination and the serial numbers of the

aircraft to be modified.



### 2.B. INFORMATION CONCERNING INDUSTRIAL SUPPORT

Not applicable.



### 2.C. MATERIAL REQUIRED FOR EACH HELICOPTER/COMPONENT

Kits or components to be ordered for one helicopter or one assembly:

Cabin internal evacuation marking retrofit labels for helicopters with rear passenger swing doors (MOD 0711B68)

Key Word Qty New P/N Item Former P/N Instruction

Label (LH door jettison) 1 365A00

- 0602

- 77 5 Label ( R H door jettison) 1 365A00

- 0602

- 76 6

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Key Word Qty New P/N Item Former P/N Instruc tion

Basic label kit 365A08

- 4481

- 0071

Label (LH door jettison ) 1 365A00

- 0600

- 75 1 Label ( R H door jettison) 1 365A00

- 0600

- 74 2 Label (LH door jettison ) 1 365A00

- 0601

- 77 3 Label ( R H door jettison) 1 365A00

- 0601

- 76 4 Label (LH door opening) 1 365A00

- 0632

- 75 8 Label (RH door opening) 1 365A00

- 0632

- 74 9 Label (1, LH door ) 1 365A00

- 0600

- 77 10 Label (1

, RH door) 1 365A00

- 0600

- 76 11 Label (2, LH door ) 1 365A00

- 0600

- 79 12 Label (2

, RH door) 1 365A00

- 0600

- 78 13

Label (3, LH door ) 1 365A00

- 0600

- 81 14 Label (3

, RH door) 1 365A00

- 0600

- 80 15 Label (4, LH door ) 1 365A00

- 0600

- 83 16 Label (4

, RH door) 1 365A00

- 0600

- 82 17

Cabin internal evacuation marking retrofit labels for helicopters with external life raft opt ional equipment (MOD 0711B68)

Key Word Qty New P/N Item Former P/N Instruction

Label (sliding door) 2 365A00

- 0631

- 64 7

Products to be ordered separately:

The products can be ordered separately, from the INTERTURBINE AVIATION LOGISTICS compan y:

Website: http://www.interturbine.com
Telephone: +49.41.91.809.300

AOG: +49.41.91.809.444.



### 2.D. MATERIAL TO BE RETURNED

Not applicable.

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### 3. ACCOMPLISHMENT INSTRUCTIONS

3.A. GENERAL

- Comply with general rules for bonding with adhesive as per Work Card 20.06.01.101 (MTC). - Comply with safety instructions for helicopters parked in a repair shop as per Work Card 20.07.02.201 (MTC).



### 3.B. OPERATIONAL PROCEDURE

Only LH side procedure is described. Proceed on RH side following same procedure for labels (2), (4), (6), (7), (9), (11), (13), (15) and (17).

3.B.1. Preliminary steps

- Park aircraft in hangar.

- Install suitable access means.

3.B.2. Procedure

As per Figures 1 and 3 (pre-MOD)

- Remove and disca rd : . label (a) from copilot door (Figure 1, Detail A), . label (b) from front passenger door (Figure 1, Detail B), . rear passenger swing door: label (c) (Figure 1, Detail C), . sliding rear door: - label (e) (Figure 3, Detail A), - label (f), if external life raft optional equipment is installed (Figure 3, Detail B).

- Clean work zones.

As per Figures 2, 4, 5 and 6 (post-MOD) - Install LH label (1) on copilot door between 2 bolts (d) (Figures 2 and 5, Details A and B). - Install LH label (3) on front passenger door as per dimension (Figures 2 and 5, Details E and F). - Install LH label (10) on inside of canopy post as per dimensions (Figure 6, Detail A). - Install LH labels (12), (14) and (16) on inside of copilot door as per dimensions (Figure 6, Details B and C). - According to configuration, install: . rear passenger swing door: LH label (5) on door as per dimensions (Figure 2, Details C and D), . sliding rear door: - LH label (8) on door as per dimensions (Figure 5, Details C and D), - label (7) on rear face of 9° frame upholstery, as per dimensions, if optional external life raft equipment is installed (Figure 4, Detail B).

If required, it is possible to produce a label in compliance with the local operational rules and the

recommended characteristics belo w for the text of the label (3): - label dimensions: according to the need and in relation to the character size, - label background color : matt white,

- character color : matt vivid red orange,

- character size : clearly visible.

3.B.3. Tests

Not applicable.

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- Clean and recondition work zones as per Work Card 20.07.03.408 (MTC).

- Remove access means. - Set helicopter into flight condition.

3.B.6. Operational procedure on non-installed equipment

Retrofit stocks of pilot and copilot doors, front and rear cabin swing doors and sliding doors as per Paragraph 3.B.2.



### 3.C. IDENTIFICATION

Identification of this document:

Record full compliance with this ALERT SERVICE BULLETIN No. 11.00.02 Revision 2 in the aircraft

documents.

Identification of modifications on the documentation:

- For all helicopters

Record embodiment of Modification 0711B68 in the aircraft documents.

- Helicopters with external life rafts

Record embodiment of Modifications 0711B67 and 0711B68 in the aircraft documents.



### 3.D. OPERATING AND MAINTENANCE INSTRUCTIONS

Operating instructions:

Refer to Flight Manual (PMV):
- Section 2.7 Normal Revision 14 of 10-22 or further, - Supplement 12 Normal Revision 3 of 10-22 or further for helicopters with sliding doors, - Supplement 14 Normal Revision 6 of 10-22 or further for helicopters with emergency flotation gear and external life raft optional equipment (if installed).

# ASB No. AS365-11.00.02

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