EASA AD No: 2011-0157

EASA Form 110 Page 1/2 

## EASA AIRWORTHINESS DIRECTIVE

AD No.: 2011-0157

Date: 25 August 2011

Note: This Airworthiness Directive (AD) is issued b y EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the European Communit y, its Member States and of the European third countries that participate in the ac tivities of EASA under Article 66 of that Regulation.
This AD is issued in accordance with EC 1702/2003, Part 21A.3B. In accordance with EC 2042/2003 Annex I, Part M.A.301, the continuing airworthiness of an aircraft shall be en sured by accomplishing any applicable ADs. Conseque ntly, no person may operate an aircraft to which an AD applies, except in accordan ce with the requirements of that AD unless otherwis e 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, A rticle 14(4) exemption]. 

### Type Approval Holder’s Name :
Fokker Services B.V. Type/Model designation(s) : F28 Mark 0070 and Mark 0100 Aeroplanes

TCDS Number: EASA.A.037

Foreign AD: Not applicable

Supersedure: This AD supersedes EASA AD 2011-0046 dated 21 March 2011.



### ATA 05 Time Limits / Maintenance Checks – Maintenance Requ irements –

Implementation

Manufacturer(s): Fokker Aircraft B.V.

Applicability: F28 Mark 0070 and Mark 0100 aeroplan es, all serial numbers

Reason: Fokker Services have published issue 8 of r eport SE-623 dated 17 March 2011, which is part of the Airworthiness Limitations Sect ion of the Instructions for Continued Airworthiness, referred to in Section 06, Appendix 1, of the Fokker 70/100 Maintenance Review Board (MRB) document. The complete Airworthiness Limitations Section currently consist s of: - Certification Maintenance Requirements (CMRs) – r eport SE-473, issue 8, - Airworthiness Limitation Items (ALIs) and Safe Li fe Items (SLIs) – report SE623, issue 8, - Fuel ALIs and Critical Design Configuration Contr ol Limitations (CDCCLs) – report SE-672, issue 2. The instructions contained in those reports have be en identified as mandatory actions for continued airworthiness. For the reasons described above, this AD retains th e requirements of EASA AD 2011-0046, which is superseded, and requires the im plementation of the inspections and limitations as specified in the Air worthiness Limitation Section of the Instructions for Continued Airworthiness, refer red to in Section 06, Appendix 1 of the Fokker 70/100 MRB document, reports SE-473 , SE-623 and SE-672 at the above-mentioned issues.

Effective Date: 08 September 2011EASA AD No: 2011-0157

EASA Form 110 Page 2/2 Required Action(s) and Compliance Time(s): Required as indicated, unless accomplished previous ly. (1) Accomplish the tasks described in Fokker Servic es reports SE-473 issue 8 (CMRs), SE-623 issue 8 (ALIs and SLIs) and SE-672, issue 2 (Fuel ALIs and CDCCLs), within the thresholds and intervals in dicated in those reports. (2) Compliance with the requirements of paragraph ( 1) of this AD can be demonstrated by: (2.1) Revising as follows the approved aircraft mai ntenance programme and standard practices on the basis of which the op erator or the owner ensures the continuing airworthiness of each operated aeroplane: Incorporate the limitations, tasks and associated thresholds and intervals described in reports SE-473 (issue 8), SE -623 (issue 8) and SE-672 (issue 2),
and (2.2) Complying with the approved aircraft maintena nce programme described in paragraph (2.1) of this AD.

Ref. Publications: Fokker 70/100 Airworthiness Limi tation Section of the Instructions for Continued Airworthiness: report SE-473, issue 8 dated 01 September 2009, report SE-623, issue 8 dated 17 March 2011, and report SE-672, issue 2 dated 01 December 2006. The use of later approved revisions of these report s is acceptable for compliance with the requirements of this AD.

Remarks : 1. If requested and appropriately substantiated, EA SA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 14 July 2011 as PAD 11-067 for consultation until 11 August 2011. No comments were received during th e consultation period. 3. Enquiries regarding this AD should be referred t o the Safety Information Section, Executive Directorate, EASA; E-mail ADs@easa.europa.eu

. 4. For any question concerning the technical conten t of the requirements in this AD, please contact: Fokker Services B.V., Technical Services Dept., P.O . Box 231, 2150 AE Nieuw-Vennep, The Netherlands; telephone +31 (0)252-627-350; facsimile +31 (0)252- 627-211; e-mail: technicalservices@fokker.com

. The referenced publication can be downloaded from www.myfokkerfleet.com

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