AD 71-02-03

final rule
Data completeness: 70%

Airworthiness Directives; GENERAL DYNAMICS Model 340, 440 and C-131E Airplanes

AD Number
71-02-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Kelowna Flightcraft R & D Ltd. 340 Airworthiness Directives; GENERAL DYNAMICS Model 340, 440 and C-131E Airplanes
aircraft Kelowna Flightcraft R & D Ltd. 440 Airworthiness Directives; GENERAL DYNAMICS Model 340, 440 and C-131E Airplanes
aircraft Kelowna Flightcraft R & D Ltd. Military C-131E Airworthiness Directives; GENERAL DYNAMICS Model 340, 440 and C-131E Airplanes

Unsafe Condition

Failures of the left and right main landing gears due to cracks in the main landing gear cylinders (P/N 528002 or P/N 528402) and their fulcrum arms.

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

Required Actions

Inspect the outer surface of main landing gear cylinders (P/N 528002 or P/N 528402) and fulcrum arms for cracks using magnetic particle, dye penetrant, or approved methods. If cracks are found, rework cylinders per approved method or replace with inspected/crack-free cylinders. For reworked cylinders, record rework details, limit use to aircraft below 55,000 lbs take-off weight, and reinspect every 1,000 hours time in service. If no cracks and less than 14,000 hours time in service, reinspect before 15,000 hours. If over 14,000 hours, reinspect every 1,000 hours.

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

Compliance Time

within the next 50 hours time in service after the effective date of this AD unless already accomplished within the last 200 hours time in service

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

Affected Aircraft

GENERAL DYNAMICS Model 340, 440, and C-131E airplanes, including those converted to turbopropeller power under STC SA4-1100 (Model 580)

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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