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Airworthiness Directives; Cessna Aircraft Company Models 208 and 208B Airplanes

airworthiness · Rule · Final rule. · Published 2002-11-12 · Effective 2002-12-31 · 67 FR 68508

Document

Document number
02-28408
Federal Register citation
67 FR 68508
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Cessna
Publication date
2002-11-12
Effective date
2002-12-31
FAA docket
Docket No. 2002-CE-23-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that applies to all Cessna Aircraft Company (Cessna) Models 208 and 208B airplanes. This AD requires you to repetitively inspect the inboard forward flap bellcranks for cracks or replace bellcranks depending on the amount of usage. This AD is the result of Cessna re-evaluating the bellcrank life limit analysis and determining that the original estimate is too high. The actions specified by this AD are intended to detect, correct, and prevent future cracks in the bellcrank, which could result in failure of this part. Such failure could lead to damage to the flap system and surrounding structure and result in reduced or loss of control of the airplane.

Source

Authoritative
Federal Register document
Machine
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