Airworthiness directives › 2014-23-09
AD 2014-23-09 Airworthiness Directives; Fokker Services B.V. Airplanes
Models named: F.28 Mark 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 0100 airplanes; certificated in any category; all serial numbers.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
This paragraph restates the actions required by paragraph (a) of AD 2000-17-03, Amendment 39-11876 (65 FR 52298, August 29, 2000). For airplanes equipped with a Messier-Dowty NLG having part number (P/N) 201071001 or 201071002, on which a main fitting subassembly (MFSA) having P/N 201071200, 201071228, 201071248, or 201071249 is installed: Prior to the accumulation of 7,500 total flight cycles or within 50 flight cycles after October 3, 2000 (the effective date of AD 2000-17-03), whichever occurs later, perform a one-time detailed visual inspection of the NLG main fitting subassembly to detect cracking, in accordance with Part 1 of the Accomplishment Instructions of Fokker Service Bulletin SBF100-32-118, dated October 8, 1999. (1) If no cracking is detected, no further action is required by this paragraph. (2) If any cracking is detected, prior to further flight, accomplish the actions required by paragraph (i) of this AD.
Unsafe condition
This AD was prompted by a report of a nose landing gear (NLG) main fitting failure. We are issuing this AD to prevent cracking of the NLG main fitting, which could lead to collapse of the NLG during takeoff and landing, and possible injury to the flight crew and passengers.
Affected ADs
This AD replaces AD 2000-17-03, Amendment 39-11876 (65 FR 52298, August 29, 2000).
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