AD 62-01-02

final rule
Data completeness: 70%

LOCKHEED Models 49, 149, 649, 749, and 1049 Series Aircraft

AD Number
62-01-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Lockheed Aircraft Corporation 1049-54 LOCKHEED Models 49, 149, 649, 749, and 1049 Series Aircraft
aircraft Lockheed Aircraft Corporation 1049B-55 (Navy R7V-1) LOCKHEED Models 49, 149, 649, 749, and 1049 Series Aircraft
aircraft Lockheed Aircraft Corporation 1049C-55 LOCKHEED Models 49, 149, 649, 749, and 1049 Series Aircraft
aircraft Lockheed Aircraft Corporation 1049D-55 LOCKHEED Models 49, 149, 649, 749, and 1049 Series Aircraft
aircraft Lockheed Aircraft Corporation 1049E-55 LOCKHEED Models 49, 149, 649, 749, and 1049 Series Aircraft
aircraft Lockheed Aircraft Corporation 1049F-55 (USAF C-121C) LOCKHEED Models 49, 149, 649, 749, and 1049 Series Aircraft
aircraft Lockheed Aircraft Corporation 1049G-82 LOCKHEED Models 49, 149, 649, 749, and 1049 Series Aircraft
aircraft Lockheed Aircraft Corporation 1049H-82 LOCKHEED Models 49, 149, 649, 749, and 1049 Series Aircraft
aircraft Lockheed Aircraft Corporation 149-46 LOCKHEED Models 49, 149, 649, 749, and 1049 Series Aircraft
aircraft Lockheed Aircraft Corporation 49-46 LOCKHEED Models 49, 149, 649, 749, and 1049 Series Aircraft

Unsafe Condition

Failures of the cap weld on main landing gear cylinders which have been returned to service following compliance with AD 59-07-03, as amended.

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

Required Actions

Reinspect or replace landing gear cylinders with cap welds using techniques in Lockheed Field Service Letter No. FS/254049L or FAA-approved equivalent. Replace cracked cylinders before further flight. Periodic reinspections every 5,000 hours' time in service.

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

Compliance Time

Within the next 400 or 1,200 hours' time in service after the effective date (January 9, 1962), depending on prior inspection method. Periodic reinspections must be done within 5,000 hours' time in service following the previous inspection.

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

Affected Aircraft

Lockheed Models 49, 149, 649, 749, and 1049 Series Aircraft with Cleveland Pneumatic Tool Company Main Landing Gear Cylinders, P/N's 9040-2, 9040A-2, 9106-2, 9291-2, 9291B-2, 9291B-2B, or 9291D-2.

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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