E ASA AD No .: 20 1 5

- 002 7

TE. CAP.0011 0

- 00 4 © European 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

. : 20 1 5

- 002 7

Date: 20 February 2015

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 EU 1321/2014 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 [ EU 1321/2014 Annex I, Part M.A.303] or agreed with the Authority of the State of Registry [EC 216/2008, Article 14(4) exemptio n]

.


### Design Approval Holder’s Name:

FOKKER SERVICES B.V

. Type/Model designation(s):

F2 8 aeroplanes

TCDS Number: EASA.A.03 7

F oreign AD: Not applicable

Supersedure: None



### ATA 05 Time Limits / Maintenance Checks

– ALS Part 1

– Certification Maintenance Requirements

– Implementation

Manufacturer(s): Fokker Aircraft B.V.

Applicability: F28 Mark 0070 and Mark 0100 aeroplanes, all serial numbers

.

Reason: Fokker Services published issue 1 1 of Engineering R eport SE

- 473 , containing Certification Maintenance Requirements (CMRs) . Th is report is P art 1 of the Airworthiness Limitations Section (ALS Part 1 ) of the Instructions for Continued Airworthiness, referred to in Section 06, Appendix 1, of the Fokker 70/10 0 Maintenan ce Review Board (MRB) document. The complete ALS currently consists of:

Part 1

- R eport SE

- 473 (CMRs), Part 2

- R eport SE

- 623

, Airworthiness Limitation Items (ALIs) and Safe Life Items (SLIs) , and Part 3

- R eport SE

- 672

, Fuel ALIs and Critical Design Configuration Control Limitations (CDCCLs)

. The instructions contained in those reports have been identified as mandatory actions f or continued airworthiness. For the reasons described above, this AD requires implementation of the maintenance actions as specified in ALS Part 1 of the Instructions for Continued Airworthiness, Fokker Services Engineering R eport SE

- 473 at issue 11

.

Effective Date: 0 6 March 2015E ASA AD No .: 20 1 5

- 002 7

TE. CAP.0011 0

- 00 4 © European 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 previously: (1) From the effective date of this AD, accomplish all applicable maintenance tasks described in, and w ithin the thresholds and intervals as specified in

, Fokker Services Engineering Report SE

- 473 at issue 1 1

, hereafter referred to as ‘ALS Part 1 ’

. (2) I f, during accomplishment of any task as required by paragraph (1) of this AD,

a n y discrepancies (as defined in ALS Part 1 ) are found, within the applicable compliance time specified in ALS Part 1

, accomplish the applicable maintenance procedures for corrective actions in accordance with the approved maintenance documentation. If no com pliance time is identified in ALS Part 1 , accomplish the applicable corrective actions before next flight. If a detected discrepancy is not identified in ALS Part 1 , before next flight, contact Fokker Services for approved instructions and accomplish those instructions accordingly. (3) Within 12 months after the effective date of this AD, revise the approved aircraft maintenance programme (AMP), on the basis of which the operator or the owner ensures the continuing airworthiness of each operated aeroplane, by incorporating the tasks and associated thresholds and intervals described in ALS Part 1 , as applicable to the aeroplane configuration

. (4) For an AMP that, on the effective date of this AD, is already updated to incorporate the maintenance tasks as specified in Fokker Services Engineering R eport SE

- 473 at issue 1 0 , the new and /or more restrictive tasks, as defined in ALS Part 1 , must be incor porated into the AMP to comply with paragraph (3) of this AD

. (5) Compliance with the requirements of paragraph (3) constitutes compliance with the requirements of paragraphs (1) and (2) of this AD. After revising the AMP, as required by paragraph (3) or ( 4) of this AD, as applicable, it is not necessary that accomplishment of individual tasks is recorded for demonstration of AD compliance on a continued basis

. Note: For affected Fokker F2 8 Mark 0 07 0 and Mark 0 1 0 0 aeroplanes registered in Europe, complying with the approved AMP as specified in paragraph (3) of this AD is required by Commission Regulation ( E U ) No 1321/201 4 , Part M.A.301, paragraph 3. (6) Compliance with the requirements of paragraph (3) also constitutes compliance with the requirements of EASA AD 2014

- 0224

, when related to tasks described in Fokker Services Engineering Report SE

- 473 at issue 10

.

Ref. Publications: Fokker 70/100 Instructions for Continued Airworthiness, ALS Part 1, Fokker Services Engineering Report SE

- 473 issue 1 1

, release date 19 January 2015

. The use of later approved revisions of th i s report 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. Th is AD was posted on 20 January 201 5 as PAD 1 5

- 00 2 for consultation until 17 February 2015 . No comments were received during the consultation peri o d

. 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 conte nt of the requirements in this AD, please contact: Fokker Services B.V., Technical Services Dept., P.O. Box 1357, 2130 E L, Hoofddorp, The Netherland s; T elephone +31

- 88

- 6280

- 350; Fax +31

- 88

- 6280

- 111; E

- mail: technicalservices@fokker.com

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

.