EASA AD No.: 2014

- 0 001

TE. CAP.0011 0

- 00 3 © Europea n Aviation Safety Agency. All rights reserved

. 1 / 2 Proprietary document. Copies are not controlled. Confirm revision status through the EASA

- Internet/Intranet. 

## EASA AIRWORTHINESS DIRECTIVE

AD No

. : 2014 - 0001

Date : 06 January 2014

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 E uropean 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 Age ncy [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: Costruzioni Aeronautiche TECNAM s

. r

. l

. Type/Model designation(s): P2006T aeroplanes

TCDS Number: EASA A.185

F orei gn AD: N ot applicable
Supersedure: None



### ATA 71 Power Plant
– Engine M ount
– Inspection / R eplacement

Manufacturer : Costruzioni Aeronautiche TECNAM srl ( TECNAM )
Applicability: P2006T aeroplane s, all serial numbers

.
Reason: During a “ 100 hour s” ins pection of a P2006T aeroplane , one engine mount Part Number ( P/N ) 26

- 7

- 1 200

- 000 was found cracked on a node

. This condition, if not detected and corrected, could lead to engine damage, possibly resulting in damage to the aeroplane and injury to the occupan ts

. To address this potential unsafe condition, TECNAM issued Service Bulletin (SB) 138

- CS

- Rev0 , providing inspection instructions

. For the reason s described above, this AD requires a one - time inspection of each engine mount P/N 26

- 7

- 1 200

- 000 and, depe nding on findings, replacement of the engine mount(s)

. This AD is considered an interim action and further AD action may follow.

Effective Date: 20 January 2014EASA AD No.: 2014

- 0 001

TE. CAP.0011 0

- 00 3 © Europea n Aviation Safety Agency. All rights reserved

. 2 / 2 Proprietary document. Copies are not controlled. Confirm revision status through the EASA

- Internet/Intranet. Required A ction ( s ) and Compliance Time (s) : Required as indicated, unless accomplished previou sly: (1) Within the compliance time define d in Table 1 of this AD, as applicable, accomplish a detailed inspection of the left hand and right hand engine mount s P/N 26

- 7

- 1 200

- 000 in accordance with the instructions of T ECNAM SB

- 138

- CS

- Rev0

. Table 1 F light H ours (FH) accumulated on the effective date of the AD Compliance Time

600 FH or more Within 25 FH or 30 days , whichever occurs first after the effective date of this AD Less than 600 FH After accumulating 600 FH but b efore exceeding 625 FH (2) If, duri ng the inspection as required by paragraph (1) of this AD, a crack or any other discrepancy is detected, before next flight , contact Tecnam for approved engine mount replacement instructions and accomplish those instructions accordingly

. Ref. Public ations : Costruzioni Aeronautiche TECNAM srl SB

- 1 3 8

- CS

- Rev 0

. The u se of later approved revisions of th i s document is acceptable for compliance with the requirements of this AD.
Remarks: 1. If requested and appropriately substantiated, EASA can approve Alternative M ethods of Compliance for this AD

. 2. This AD was posted on 12 Dec e m ber 2013 as PAD 13

- 1 83 for consultation until 26 December 2013. No comments were received during the consultation period

. 3. Enquiries regarding this AD should be referred to the Safety Informati on Section, Executive Directorate, EASA. E

- mail: ADs@easa.europa.eu

. 4. For any question concerning the technical conte nt of the requirements in this AD, please contact: Costruzioni Aeronautiche TECNAM Airworthiness Off ice P hone +39 0823 620134 or fax +39 0823 622899 Email: m.oliva@tecnam.com ; airworthiness @tecnam.com

.