AD 87-17-10

final rule
Data completeness: 70%

Airworthiness Directives; GENERAL DYNAMICS (Convair) Models 340, 440, and C-131 (Military) Series Airplanes

AD Number
87-17-10
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 (Convair) Models 340, 440, and C-131 (Military) Series Airplanes
aircraft Kelowna Flightcraft R & D Ltd. 440 Airworthiness Directives; GENERAL DYNAMICS (Convair) Models 340, 440, and C-131 (Military) Series Airplanes
aircraft Kelowna Flightcraft R & D Ltd. Military C-131B Airworthiness Directives; GENERAL DYNAMICS (Convair) Models 340, 440, and C-131 (Military) Series Airplanes
aircraft Kelowna Flightcraft R & D Ltd. Military C-131D Airworthiness Directives; GENERAL DYNAMICS (Convair) Models 340, 440, and C-131 (Military) Series Airplanes
aircraft Kelowna Flightcraft R & D Ltd. Military C-131E Airworthiness Directives; GENERAL DYNAMICS (Convair) Models 340, 440, and C-131 (Military) Series Airplanes
aircraft Kelowna Flightcraft R & D Ltd. Military C-131F/R4Y-1 Airworthiness Directives; GENERAL DYNAMICS (Convair) Models 340, 440, and C-131 (Military) Series Airplanes

Unsafe Condition

Failure of the main landing gear drag strut pivot bolt and possible subsequent main landing gear collapse.

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

Required Actions

Inspect the main landing gear drag strut pivot bolt assembly using magnetic particle inspection procedures per Service Bulletin 640(340D)32-14. If no cracks are found, reinstall and repeat inspection within 500 hours time-in-service. If cracks are found, replace the bolt assembly with specified part numbers and follow subsequent inspection intervals based on the part number used.

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

Compliance Time

Within 500 hours time-in-service after the effective date of this AD.

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

Affected Aircraft

General Dynamics (Convair) Models 340, 440, and C-131 (Military) series airplanes equipped with main landing gear drag strut pivot bolt assembly Part Numbers 340-5110105, 340-5110105-1, or 340-5110105-3.

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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