AD 61-24-04

final rule
Data completeness: 70%

LOCKHEED Models 049, 149, 649, 749, and 1049 Series Aircraft

AD Number
61-24-04
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 049, 149, 649, 749, and 1049 Series Aircraft
aircraft Lockheed Aircraft Corporation 1049B-55 (Navy R7V-1) LOCKHEED Models 049, 149, 649, 749, and 1049 Series Aircraft
aircraft Lockheed Aircraft Corporation 1049C-55 LOCKHEED Models 049, 149, 649, 749, and 1049 Series Aircraft
aircraft Lockheed Aircraft Corporation 1049D-55 LOCKHEED Models 049, 149, 649, 749, and 1049 Series Aircraft
aircraft Lockheed Aircraft Corporation 1049E-55 LOCKHEED Models 049, 149, 649, 749, and 1049 Series Aircraft
aircraft Lockheed Aircraft Corporation 1049F-55 (USAF C-121C) LOCKHEED Models 049, 149, 649, 749, and 1049 Series Aircraft
aircraft Lockheed Aircraft Corporation 1049G-82 LOCKHEED Models 049, 149, 649, 749, and 1049 Series Aircraft
aircraft Lockheed Aircraft Corporation 1049H-82 LOCKHEED Models 049, 149, 649, 749, and 1049 Series Aircraft
aircraft Lockheed Aircraft Corporation 149-46 LOCKHEED Models 049, 149, 649, 749, and 1049 Series Aircraft
aircraft Lockheed Aircraft Corporation 49-46 LOCKHEED Models 049, 149, 649, 749, and 1049 Series Aircraft

Unsafe Condition

Cracking in the horizontal stabilizer rear spar-to-fuselage attachment due to fatigue.

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

Required Actions

Inspect the rear spar web (P/N 271488-4) for cracks in the 0.38 inch radius adjacent to the stabilizer-to-fuselage fitting on both sides. Repair cracks prior to further flight per Lockheed Service Letter FS/250615 or FAA-approved equivalent. Discontinue inspections after implementing the specified repair or reinforcement.

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

Compliance Time

Within 400 hours' time in service after effective date (December 14, 1961), unless already accomplished within the last 4,300 hours' time in service and at intervals of 4,700 hours' time in service.

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

Affected Aircraft

Lockheed Models 049, 149, 649, 749, and 1049 Series Aircraft with 25,000 or more hours' time in service.

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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