Airworthiness directives › 2016-25-04
AD 2016-25-04 Airworthiness Directives; Fokker Services B.V. Airplanes
Models named: F28 Mark 0070, 0100. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to all Fokker Services B.V. Model F28 Mark 0070 and 0100 airplanes, certificated in any category.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
Within 12 months after the effective date of this AD: Do a detailed inspection for cracking of the trailing edge rib at wing station 8700, in accordance with the Accomplishment Instructions of Fokker Service Bulletin SBF100-57-048, dated October 27, 2014. If any crack is found, before further flight, repair using a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the European Aviation Safety Agency (EASA); or Fokker Services B.V.'s EASA Design Organization Approval (DOA).
Unsafe condition
This AD was prompted by report of cracking in the secondary structure of the wing at station 8700. We are issuing this AD to detect and correct cracking that could lead to failure of the affected rib and consequent reduced control of the airplane.
Affected ADs
None.
Read the original on the Federal Register →
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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