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Airworthiness Directives; Boeing Model 747-200C and 747-200F Series Airplanes

airworthiness · Rule · Final rule. · Published 2005-05-23 · Effective 2005-06-27 · 70 FR 29442

Document

Document number
05-9981
Federal Register citation
70 FR 29442
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Boeing Model 747-200C and 747-200F Series
Publication date
2005-05-23
Effective date
2005-06-27
FAA docket
Docket No. FAA-2005-20024

Abstract

The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 747-200C and 747-200F series airplanes. This AD requires repetitive inspections for cracking of the left and right C-3 frame upper closure fittings of the nose cargo door, and corrective actions if necessary. This AD also provides an optional modification that, if done, terminates inspections in certain areas. This AD is prompted by reports indicating that fatigue cracking was found in the inboard flange above the flight deck floor on the C-3 frame upper closure fittings of the nose cargo door. We are issuing this AD to detect and correct cracking of the C-3 frame upper closure fittings, which could extend and result in rapid depressurization of the airplane.

Source

Authoritative
Federal Register document
Machine
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