Airworthiness Directives; Lockheed Model 382, 382B, 382E, 382F, and 382G Series Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 2009-05-20 · Effective 2009-06-04 · 74 FR 23614
Document
Document number
E9-11590
Federal Register citation
74 FR 23614
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2009-05-20
Effective date
2009-06-04
FAA docket
Docket No. FAA-2009-0462
Abstract
We are adopting a new airworthiness directive (AD) for all Lockheed Model 382, 382B, 382E, 382F, and 382G series airplanes. This AD requires an inspection to identify discrepant barrel nuts in the upper wing joint, engine truss, and rear beam pylon support; and replacement of any discrepant barrel nut with a new barrel nut, if necessary. This AD results from a report of severe cracking of multiple barrel nuts in the wing station (WS) 220 upper wing joint found during scheduled maintenance. We are issuing this AD to prevent cracking of the barrel nuts in the upper wing joint, engine truss, and rear beam pylon support, which could result in reduced structural integrity of the affected part and consequent detachment of the wing or engine from the airplane.