AD 2008-14-10

final rule
Data completeness: 70%

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

AD Number
2008-14-10
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2008-0740
FR Citation
73 FR 38311

Applicability

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

Unsafe Condition

Failure of upper engine mount bolts, specifically part number NAS 636 with 'AFC' or 'A' stamped on the bolt head, which could result in reduced structural capability of an engine mount and possible separation of a strut and engine from the airplane during flight.

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

Required Actions

Inspect the visible surface head of each upper engine mount bolt to determine if part number NAS 636 is stamped across the top and if the manufacturer's code 'AFC' or 'A' is stamped across the bottom. Replace any discrepant upper engine mount bolt with a new one, P/N NAS 636, having a manufacturer's code other than 'AFC' or 'A', before further flight.

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

Compliance Time

Within 10 days after the effective date of the AD, with replacement actions completed before further flight.

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

Affected Aircraft

All Lockheed Model 382, 382B, 382E, 382F, 382G, and 382J 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 4, 2026

Rights: U.S. Government Public Domain

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