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AD FAA-2009-0462

Airworthiness Directives; Lockheed Model 382, 382B, 382E, 382F, and 382G Series Airplanes

Summary

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.

Directive Details

AD Number

FAA-2009-0462

Document Number

E9-11590

Type

Rule

Publication Date

May 20, 2009

Effective Date

June 4, 2009

Affected Manufacturer

Lockheed Model 382, 382B, 382E, 382F, and 382G Series

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2009-0462

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Lockheed Model 382, 382B, 382E, 382F, and 382G Series →

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AD FAA-2009-0462 — Airworthiness Directives; Lockheed Model 382, 382B, 382E, 382F, and 382G Series Airplanes