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 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 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 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]. 

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 Requirements – 

Implementation 

Manufacturer(s): Fokker Aircraft B.V. 

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

Reason: Fokker Services have published issue 8 of report SE-623 dated 17 March 2011, 

which is part of the Airworthiness Limitations Section 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 consists of: 

- Certification Maintenance Requirements (CMRs) – report SE-473, issue 8, 

- Airworthiness Limitation Items (ALIs) and Safe Life Items (SLIs) – report SE623, issue 8, 

- Fuel ALIs and Critical Design Configuration Control Limitations (CDCCLs) – 

report SE-672, issue 2. 

The instructions contained in those reports have been identified as mandatory 

actions for continued airworthiness. 

For the reasons described above, this AD retains the requirements of EASA AD 

2011-0046, which is superseded, and requires the implementation of the 

inspections and limitations as specified in the Airworthiness Limitation Section of 

the Instructions for Continued Airworthiness, referred 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 2011 
EASA AD No: 2011-0157 

EASA Form 110 Page 2/2 

Required Action(s) 

and Compliance 

Time(s): 

Required as indicated, unless accomplished previously. 

(1) Accomplish the tasks described in Fokker Services 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 indicated 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 maintenance programme 

and standard practices on the basis of which the operator 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 maintenance programme 

described in paragraph (2.1) of this AD. 

Ref. Publications: Fokker 70/100 Airworthiness Limitation 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 reports 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 14 July 2011 as PAD 11-067 for consultation until 

11 August 2011. 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: 

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.