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 2015-04-23

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
 ASB No. AS365-11.00.02

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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. 
 ASB No. AS365-11.00.02

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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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Non-installed equipment: 

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. 
 ASB No. AS365-11.00.02

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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.

365A08-4481-0071

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 (RH door jettison) 1 365A00-0602-76 6
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Marking retrofit label kit 

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

Basic label kit 365A08-4481-0071

Label (LH door jettison) 1 365A00-0600-75 1

Label (RH door jettison) 1 365A00-0600-74 2

Label (LH door jettison) 1 365A00-0601-77 3

Label (RH 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 optional 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 company:

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 discard: 

. 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 below 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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3.B.4. Final steps 

- 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). 
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Figure 1 - pre-MOD with rear passenger swing doors 
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Figure 2 - post-MOD with rear passenger swing doors 
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Figure 3 - pre-MOD with rear passenger sliding doors 
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Figure 4 - post-MOD with rear passenger sliding doors 
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Figure 5 - post-MOD with rear passenger sliding doors 
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Figure 6 - post-MOD pilot and copilot doors