EASA AD No.: 201 4

- 0204

TE. CAP.00110

- 00 4 © European Aviation Safety Agency. All rights reserved. 1 / 3 Proprietary document. Copies are not controlled. Confirm revision status through the EASA

- Internet/Intranet. 

## EASA AIRWORTHINESS DIRECTIVE

AD No

. : 201 4 - 0204 [Correction: 12 September 2014]

Date: 1 1 September 201 4

Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the European Community, its Member States and of the European third countries that participate in the activities of EASA under Article 66 of that Regulation.
This AD is issued in accordance with E U 748/2012 , Part 21

. A.3B. In accordance with EC 2042/2003 Annex I, Part M.A.301, the continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs. Consequently, no person may ope rate an aircraft to which an AD applies, except in accordance with the requirements of that AD , unless otherwise specified by the Agency [EC 2042/2003 Annex I, Part M.A.303] or agreed with the Authority of the State of Registry [EC 216 / 2008 , Article 14 ( 4 ) exemption]. 

### Design Approval Holder’s Name : AIRBUS HELICOPTERS Type/Model designation(s) : AS 332, EC 225, AS 365 and EC 155 helicopters

TCDS Number: EASA .R.002, EASA.R.105
F oreign AD: Not applicable Supersedure: N one



### ATA 11 Placards and Markings

– Inspection / Installation

Manufacturer(s): Airbus Helicopters (formerly Eurocopter, Eurocopter France, Aerospatiale) Applicability: AS 332 C1 , AS 332 L1, AS 332 L2 , EC 225 LP , AS 365 N2 , AS 365 N3 , EC 155 B and EC 155 B1 helicopters , all manufacturer serial numbers , equipped with at least one energy absorbing seat listed in Appendix 1 of this AD , Table 1. Reason: During certification of an energy absorbing seat with a new Part Number, it was observed that the label , which provides information to keep the space under the seat free of any object, was not systematically installed in a helicopter. This condition, if not corrected, may prompt occupants to s tow objects under the seat , thereby reduc ing the efficiency of energy

- absorbing function of the seat , possibly resulting in reduced survivability of occupant(s) in case of accident

. To address this potential unsafe condition, and pending a final solution, Airbus Helicopters issued Alert Service Bulletin (ASB) AS332

- 01.00.85, ASB EC225

- 04A012, ASB AS365

- 01.00.66 and ASB EC155

- 04A013 , to provide ins pection and installation instructions

. For the reasons described above, this AD requires a one - time inspection for the pre sence of warning label(s) and , depending on findings, install ation of label(s) prohibiting stowage of any object under an energy - absorbing seat

. This AD is re

- published to correct the AD number in the header of the document.
Effective Date: 2 5 September 2014EASA AD No.: 201 4

- 0204

TE. CAP.00110

- 00 4 © European Aviation Safety Agency. All rights reserved. 2 / 3 Proprietary document. Copies are not controlled. Confirm revision status through the EASA

- Internet/Intranet. Required Action(s) and Compliance Time(s): Required as indicated, unless accomplished previously: (1) Within 110 flight hours or 30 days, whichever occurs first after the effective date of this AD, inspect the cabin of a helicopter for the presence of a readable label (s) , displayed in a conspicuous place and clearly visible to each occupant , in accordance with the instructions of paragraph 3B of Airbus Helicopters ASB AS332

- 01.00.85, ASB EC225

- 04A012, ASB AS365

- 01.00.66 or ASB EC155

- 04A013 , as applicable to the helicopter model. (2) If, during the inspection as required by paragraph (1) of this AD , a missing or u nreadable label is identified, or a label is not located in a conspicuous place, before next flight, install a locally made label prohibiting stowage of any object under an energy

- absorbing seat in accordance with the instructions of paragraph 3B of Airbus Helicopters ASB AS332

- 01.00.85, ASB EC225

- 04A012, ASB AS365

- 01.00.66 or ASB EC155

- 04A013 , as applicable to the helicopter model.
Ref. Publications: Airbus Helicopters ASB AS332

- 01.00.85 original issue , dated 26 August 2014, Airbus Helicopters ASB EC225

- 04A012 original issue , dated 26 August 2014, Airbus Helicopters ASB AS365

- 01.00.66 original issue , dated 26 August 2014, Airbus Helicopters ASB EC155

- 04A013 original issue , dated 26 August 2014. The use of later approved revisi ons of th e s e document s is acceptable for compliance with the requirements of this AD.
Remarks: 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E

- mail: ADs@easa.europa.eu

. 4. For any question concerning the technical content of the requirements in this AD, please contact: Airbus Helicopters ( EBSESB )

– Aéroport de Marseille Provence 13725 Marignane Cedex, France; Telephone +33 (4) 42 85 97 97; F ax +33 (4) 42 85 99 66; E

- mail: Directive.technical

- support@airbus.com

.EASA AD No.: 201 4

- 0204

TE. CAP.00110

- 00 4 © European Aviation Safety Agency. All rights reserved. 3 / 3 Proprietary document. Copies are not controlled. Confirm revision status through the EASA

- Internet/Intranet. 

### Appendix 1 Table 1 Affected seats
Seat M anufacturer Seat T ype Generic Part Number

Socea Sogerma ST102 2510102

- xx - xx , see Note ST107 2010107

- xx - xx ST120 2520120

- xx
SICMA Aero Seat Zodiac Seats France 192 192xx

- xx - xx
159 1591718

- xx

159110

Fischer + Entwicklungen H110 9606

- ()

- ()

- () , see Note H140 0520

- ()

- ()

- () H160 0718

- ()

- ()

- ()

- () 185

- 410 9507

- ()

- ()

- () 236/406 9608

- ()

- ()

- ()
Note: “ XX ” or “

- ()

- ()

- () ” may represent any alphanumerical value