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Airworthiness directives › 2016-11-22

AD 2016-11-22 Airworthiness Directives; Fokker Services B.V. Airplanes

2016-07-12
2016-06-07
39-18549
FAA-2016-0464
Airframe
—

Models named: F.28 Mark 0070, 0100. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Fokker Services B.V. Model F.28 Mark 0070 and 0100 airplanes, certificated in any category, all serial numbers.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

(1) Within 12 months after the effective date of this AD, revise the maintenance or inspection program, as applicable, to incorporate the certification maintenance requirements (CMR) specified in “Fokker 70/100 Certification Maintenance Requirements,” of Fokker Services B.V. Engineering Report, Airworthiness Limitations Section (ALS), SE-473, Issue 11, released January 19, 2015. (2) Do the applicable initial CMR inspection at the time specified in paragraph (g)(2)(i) or (g)(2)(ii) of this AD, as applicable, as specified in “Fokker 70/100 Certification Maintenance Requirements,” of Fokker Services B.V. Engineering Report, ALS, SE-473, Issue 11, released January 19, 2015. If any discrepancy is found during any inspection, repair using a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the European Aviation Safety Agency; or Fokker B.V. Service's EASA Design Organization Approval (DOA). Repair any discrepancy before further flight. (i) For CMR inspection 783100-CM-01: Within 1 year or 3,000 flight hours after the effective date of this AD, whichever occurs first, but not later than 12,000 flight hours after accomplishing Maintenance Review Board (MRB) Task 783100-00-04. (ii) For CMR inspection 783500-CM-01: Within 1 year or 3,000 flight hours after the effective date of this AD, whichever occurs first, but not later than 10,000 flight hours after accomplishing MRB Task 783100-01-01.

Unsafe condition

This AD was prompted by the need for more restrictive airworthiness limitations. We are issuing this AD to reduce the potential for significant failure conditions and consequent loss of controllability of the airplane.

Affected ADs

None.

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1