AD 60-04-04

final rule
Data completeness: 60%

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

AD Number
60-04-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Lockheed Aircraft Corporation 149-46 LOCKHEED Models 049, 149, 649, and 749 Series Aircraft
aircraft Lockheed Aircraft Corporation 49-46 LOCKHEED Models 049, 149, 649, and 749 Series Aircraft
aircraft Lockheed Aircraft Corporation 649-79 LOCKHEED Models 049, 149, 649, and 749 Series Aircraft
aircraft Lockheed Aircraft Corporation 649A-79 LOCKHEED Models 049, 149, 649, and 749 Series Aircraft
aircraft Lockheed Aircraft Corporation 749-79 LOCKHEED Models 049, 149, 649, and 749 Series Aircraft
aircraft Lockheed Aircraft Corporation 749A-79 LOCKHEED Models 049, 149, 649, and 749 Series Aircraft

Unsafe Condition

Fatigue failures in the main landing gear outer cylinder at the 0.125-inch radius of the shoulder where the drag strut-side brace collar retaining nut bears.

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

Required Actions

Inspect for cracks using ultrasonic shear wave, magnetic particle, or radiographic methods. Rework the cylinder area by cleaning, polishing, and shotpeening. Replace cracked cylinders before further flight. Reinspect every 1,000 hours until rework is done, then reinspect every 9,000 hours post-rework.

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

Compliance Time

Within 400 hours' time in service for initial inspection. Rework must be done within 3,000 or 4,000 hours' time in service depending on inspection method. Reinspections required every 1,000 hours until rework, then every 9,000 hours post-rework.

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

Affected Aircraft

Lockheed Models 049, 149, 649, and 749 Series Aircraft with Cleveland Pneumatic Model 8298 Series Main Landing Gear Struts and removable side brace attachment collar.

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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