AD 2009-11-03

final rule
Data completeness: 70%

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

AD Number
2009-11-03
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2009-0462
FR Citation
74 FR 23614

Applicability

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

Unsafe Condition

Severe cracking of multiple barrel nuts in the wing station (WS) 220 upper wing joint, which could result in reduced structural integrity and detachment of the wing or engine from the airplane.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect the upper wing joint, engine truss, and rear beam pylon support for discrepant barrel nuts. Replace any discrepant barrel nut with a new barrel nut, if necessary.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 30 days after the effective date of this AD.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

All Lockheed Model 382, 382B, 382E, 382F, and 382G series airplanes, certificated in any category.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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