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Airworthiness Directives; Boeing Model 727, 727C, 727-100, 727-100C, 727-200, and 727-200F Series Airplanes

airworthiness · Rule · Final rule. · Published 2005-07-11 · Effective 2005-08-15 · 70 FR 39647

Document

Document number
05-13434
Federal Register citation
70 FR 39647
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2005-07-11
Effective date
2005-08-15
FAA docket
Docket No. FAA-2004-19679

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 727, 727C, 727-100, 727-100C, 727-200, and 727- 200F series airplanes. This AD requires repetitive inspections of the carriage attach fittings on the foreflaps of each wing for cracking and other discrepancies, and corrective actions if necessary. For certain airplanes, this AD also concurrently requires various other actions related to the subject area. This AD also provides for an optional terminating action for the repetitive inspection requirements and for an optional replacement that defers the repetitive inspections. This AD is prompted by reports of damaged or failed outboard foreflaps with a cracked or failed carriage attach fitting of the foreflap sequencing carriage. We are issuing this AD to detect and correct fatigue cracking of the attach fittings of the foreflap carriage of the wings, which could result in partial or complete loss of the foreflap and consequent loss of controllability of the airplane.

Source

Authoritative
Federal Register document
Machine
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