# ASB No. EC155-04A013

Revision 0 2014-08-26 Page 1/7

This document is available on the internet: www.airbushelicopters.com/techpub 

### Civil version(s): B, B1



# ALERT SERVICE BULLETIN

SUBJECT: LIMITATIONS - Energy-absorbing seats

Label "Do not stow anything under the seat"

ATA: 25



### Revision No. Date of issue

Revision 0 2014-08-26



### Summary:

Compliance with this ALERT SERVICE BULLETIN consists in affixing a label which indicates that nothing must be

stowed under the energy -absorbing seats.



### Compliance:

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

# ASB No. EC155-04A013

Revision 0 2014-08-26 Page 2/7

This document is available on the internet: www.airbushelicopters.com/techpub 

### 1. PLANNING INFORMATION

1.A. EFFECTIVITY

1.A.1. Helicopters/installed equipment

Helicopters equipped with at least one of the seats listed in paragraph 1.A.2.

1.A.2. Non-installed equipment

Pilot, copilot and/or passenger seats listed in the t able below and not equipped with the label given in the

Appendix.



### 1.B. ASSOCIATED REQUIREMENTS

Not applicable.



### 1.C. REASON

During certification of an energy-abs orbing seat with a new Part Num ber, it was observed that the label

which indicates that the space under the seats must remain free was not systematically installed.

Objects stowed under this type of seat may reduce t he efficiency of its energy-absorbing function and thus

jeopardize the occupant's surviv al in the event of a crash.

Consequently, and pending a definitive solution, Airbus Heli copters makes it mandatory to affix a label which

indicates that nothing must be stowed under the energy-absorbing seats. Equipment manufacturer Seat type Generic Part Number

(MP/N)

Sicma Aero Seat

Zodiac Seats France Sicma 159 1591718-xx

159110

Socea

Sogerma ST102 2510102-xx-xx

F+E

(Fischer + Entwicklungen) 185-410 9507-()-()-()

F+E

(Fischer + Entwicklungen) 236/406 9608-()-()-()

F+E

(Fischer + Entwicklungen) H110 9606-()-()-()

F+E

(Fischer + Entwicklungen) H140 0520-()-()-()

# ASB No. EC155-04A013

Revision 0 2014-08-26 Page 3/7

This document is available on the internet: www.airbushelicopters.com/techpub 

### 1.D. DESCRIPTION

Compliance with this ALERT SERVICE BULLETIN consists in:

- preparing one or several (locally made) label(s) wh ich indicate(s) that nothi ng must be stowed under the

energy-absorbing seats,

- affixing this (these) label(s) so that it is (they are) visible to the occupants of these seats.



### 1.E. COMPLIANCE

1.E.1. Compliance at the works

Not applicable.

1.E.2. Compliance in service

Helicopters/installed equipment:

Comply with paragraph 3. within 110 flying hours, wi thout exceeding 1 month following receipt of Revision 0

of this ALERT SERVICE BULLETIN issued on t he date indicated at the bottom of the page.

Non-installed equipment:

When installing a seat, comply with paragraph 3.



### 1.F. APPROVAL

Approval of modifications:

Not applicable.

Approval of this document:

The technical information contained in this AL ERT SERVICE BULLETIN Revision 0 was approved

on August 26, 2014 under t he authority of EASA Design Organization Approval No. 21J.056 for helicopters

of civil versions subject to an Airworthiness Certificate.



### 1.G. MANPOWER

For compliance with this ALERT SERVICE BULLETIN, Airbus Helicopters recommends the following

personnel qualifications:

Qualification: 1 Technician.

The time for the operations is given for information purposes, for a standard configuration.

Time for the operations: approximately 15 minutes.

# ASB No. EC155-04A013

Revision 0 2014-08-26 Page 4/7

This document is available on the internet: www.airbushelicopters.com/techpub 

### 1.H. WEIGHT AND BALANCE

Not applicable.



### 1.I. EFFECT ON ELECTRICAL LOADS

Not applicable.



### 1.J. SOFTWARE MODIFICATION EMBODIMENT RECORD

Not applicable.



### 1.K. REFERENCES

Not applicable.



### 1.L. DOCUMENTS AFFECTED

Not applicable.



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

Not applicable.

# ASB No. EC155-04A013

Revision 0 2014-08-26 Page 5/7

This document is available on the internet: www.airbushelicopters.com/techpub 

### 2. MATERIAL INFORMATION

2.A. MATERIAL: PRICE - AVAILABILITY - PROCUREMENT

Not applicable.



### 2.B. INFORMATION CONCERNING INDUSTRIAL SUPPORT

Not applicable.



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

Not applicable.



### 2.D. MATERIAL TO BE RETURNED

Not applicable.

# ASB No. EC155-04A013

Revision 0 2014-08-26 Page 6/7

This document is available on the internet: www.airbushelicopters.com/techpub 

### 3. ACCOMPLISHMENT INSTRUCTIONS

3.A. GENERAL

Not applicable.



### 3.B. OPERATIONAL PROCEDURE

For each seat listed in paragraph 1.A.:

- Prepare a label in accordance with the Appendix.

- Affix the label to one of the seat legs so that it is visible and legible.



### 3.C. IDENTIFICATION

Identification of this document:

Record compliance with this document, with the revision number, in the helicopter documents.



### 3.D. OPERATING AND MAINTENANCE INSTRUCTIONS

Not applicable.

# ASB No. EC155-04A013

Revision 0 2014-08-26 Page 7/7

This document is available on the internet: www.airbushelicopters.com/techpub 

# DO NOT STOW ANYTHING

UNDER THE SEAT

DO NOT STOW ANYTHING

UNDER THE SEAT 4. APPENDIX

- Label marking characteristics:

. text to be marked: " DO NOT STOW ANYTHING UNDER THE SEAT ",

. black text on white background or white text on black background,

. font size: between 6mm and 10mm,

. the marking must not be easily erasable,

. the text is given in English but can be tran slated into another language, according to the local

regulations in force.

- The label must not be easily damaged.

- Examples of labels: