Airworthiness Directives; Lockheed Model L-1011-385 Series Airplanes
airworthiness · Rule · Final rule. · Published 1999-03-26 · Effective 1999-04-30 · 64 FR 14580
Document
Document number
99-7116
Federal Register citation
64 FR 14580
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Lockheed Model L-1011-385 Series
Publication date
1999-03-26
Effective date
1999-04-30
FAA docket
Docket No. 96-NM-256-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to all Lockheed Model L-1011-385 series airplanes, that requires repetitive external visual inspections and internal borescope inspections to detect discrepancies of the elevator assembly; and either repair or repair/modification of certain identified discrepancies. This amendment is prompted by a report of fretting at the diagonal truss to web joint of the elevator and cracking in the cap fillet radius adjacent to the joint, apparently due to loose fasteners as a result of local vibration. The actions specified by this AD are intended to detect and correct such fretting and cracking, which could result in reduced structural integrity of the elevator and consequent flutter instability if coupled with other structural failures.