Airworthiness Directives; Lockheed Model 382 Series Airplanes
airworthiness · Rule · Final rule. · Published 1999-12-03 · Effective 2000-01-07 · 64 FR 67710
Document
Document number
99-31071
Federal Register citation
64 FR 67710
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Lockheed Model 382 Series
Publication date
1999-12-03
Effective date
2000-01-07
FAA docket
Docket No. 98-NM-371-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Lockheed Model 382 series airplanes, that requires a one-time visual inspection of the under floor to ring fittings at fuselage station 817E to verify installation of the correct sized fasteners; and follow-on corrective actions, if necessary. This amendment is prompted by notification from the manufacturer indicating that during production incorrect sized fasteners were installed on the under floor to ring fittings at fuselage station 817E. The actions specified by this AD are intended to prevent fatigue cracking of the fastener holes and adjacent fuselage structure due to installation of the incorrect sized fasteners, which could result in reduced structural integrity of the airplane.