EASA AD No.: 2013-0093

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EASA AIRWORTHINESS DIRECTIVE

AD No.: 2013-0093

[Correction: 17 April 2013]

Date: 15 April 2013

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 EU 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 operate 

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:

EUROCOPTER

Type/Model designation(s):

EC 120 B and EC 130 B4 Helicopters

TCDS Number: DGAC France No.189 and EASA.R.008

Foreign AD: Not applicable

Supersedure: None

ATA 52 Doors – Sliding Door Star Support – Modification

Manufacturer(s): Eurocopter (formerly Eurocopter-France)

Applicability: EC 120 B helicopters, all Serial Numbers (S/N) below 1368, equipped with 

sliding door P/N C526A2370101, and

EC 130 B4 helicopters, all S/N, equipped with sliding door P/N 

C526S1101051, 

except those helicopters that have incorporated Eurocopter modification 

(MOD) 07 3796 (reinforcement of the sliding door star support attachment) in 

production, or have incorporated Eurocopter MOD 07 2921 (industrialized 

sliding door) in production.

Reason: A case has been reported where, after landing, the passengers of an 

Eurocopter helicopter could not open the sliding door from inside. The 

passengers had to leave the helicopter through the pilot door.

The investigation revealed a sliding door star axle support failure.

This condition, if not corrected, could delay the evacuation from the helicopter

in case of emergency, possibly resulting in injury to the occupants.

For the reason described above, this AD requires modification of the sliding 

door star support.

This AD was republished to correct one typo in the header and another one in 

Ref. publication.

Effective Date: 29 April 2013
EASA AD No.: 2013-0093

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Required Action(s) 

and Compliance

Time(s):

Required as indicated, unless accomplished previously:

(1) Within 165 flight hours or 24 months, whichever occurs first after the

effective date of this AD, modify the sliding door star support attachment

in accordance with the instructions of § 3 of Eurocopter Alert Service 

Bulletin (ASB) EC120 No 52A014 Revision 1, or ASB EC130 No 52A009 

Revision 1, depending on the helicopter type.

(2) Accomplishment of Eurocopter SB EC120 No 52A014 original issue or 

SB EC130 No 52A009 original issue before the effective date of this AD is 

acceptable to comply with the requirements of paragraph (1) of this AD.

(3) From the effective date of this AD, do not install any sliding door P/N 

C526A2370101 on an EC 120 helicopter, or a sliding door P/N 

C526S1101051 on an EC 130 B4 helicopter, unless in compliance with 

the requirements of this AD. 

Ref. Publications: Eurocopter ASB EC120 No 52A014 original issue dated 16 January 2004, or 

Revision 1 dated 25 January 2013;

Eurocopter ASB EC130 No 52A009 original issue dated 30 March 2010, or 

Revision 1 dated 25 January 2013;

The use of later approved revisions of these documents 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. This AD was posted on 21 February 2013 as PAD 13-037 for consultation 

until 21 March 2013. No comments were received during the consultation 

period.

3. Enquiries regarding this AD should be referred to the Safety Information 

Section, Executive Directorate, EASA. E-mail: ADs@easa.europa.eu.

4. For any question concerning the technical content of the requirements in 

this AD, please contact:

EUROCOPTER (STDI) – Aéroport de Marseille Provence, 13725 

Marignane Cedex, France; telephone +33 (4) 12 85 97 97; facsimile +33 

(4) 85 99 66; E-mail: Directive.technical-support@eurocopter.com.