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Airworthiness Directives; Fokker Model F.28 Mark 0070 and Mark 0100 Airplanes

airworthiness · Rule · Final rule. · Published 2008-09-29 · Effective 2008-11-03 · 73 FR 56452

Document

Document number
E8-22210
Federal Register citation
73 FR 56452
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Fokker Model F.28 Mark 0070 and Mark 0100
Publication date
2008-09-29
Effective date
2008-11-03
FAA docket
Docket No. FAA-2008-0675

Abstract

The FAA is superseding an existing airworthiness directive (AD), which applies to certain Fokker Model F.28 Mark 0070 and 0100 airplanes. That AD currently requires a one-time inspection of the main landing gear (MLG) main fitting for cracks, and repair if necessary. The existing AD also currently requires installing a placard and revising the airplane flight manual to include procedures to prohibit the application of brakes during backward movement of the airplane. This new AD requires repetitive eddy current inspections of the MLG main fitting and rework before further flight as applicable. This AD results from reports that a final solution eliminating the cause of the crack initiation mechanism is not yet available and that repetitive inspections are necessary. We are issuing this AD to detect and correct cracks in the MLG main fitting, which could result in reduced structural integrity of the MLG main fitting.

Source

Authoritative
Federal Register document
Machine
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