AD 47-49-07

final rule
Data completeness: 60%

LOCKHEED Model 49

AD Number
47-49-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Lockheed Aircraft Corporation 49-46 LOCKHEED Model 49

Unsafe Condition

The NAS 58A65 bolt used to connect the two halves of each MLG upper drag link assembly may fail due to insufficient strength.

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

Required Actions

Replace the NAS 58A65 bolt with a 5/8-inch diameter high strength bolt (LAC P/N 297902) and reduce MLG shock strut inflation pressures to achieve a static extension of 2 inches at maximum landing weight.

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

Compliance Time

prior to February 1, 1948

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

Affected Aircraft

Lockheed Aircraft Corporation Model 49 serials up to and including 2088, unless equipped with MLG Drag Strut Dampers.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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