AD 91-12-05

final rule
Data completeness: 70%

Airworthiness Directives; General Dynamics (CONVAIR) Model 340, 440, and C131, B, C, D, E, and F (Military) Series Airplanes

AD Number
91-12-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
90-NM-289-AD
FR Citation
This information is not available

Applicability

TypeManufacturerModelDetails
aircraft Kelowna Flightcraft R & D Ltd. 340 Airworthiness Directives; General Dynamics (CONVAIR) Model 340, 440, and C131, B, C, D, E, and F (Military) Series Airplanes
aircraft Kelowna Flightcraft R & D Ltd. 440 Airworthiness Directives; General Dynamics (CONVAIR) Model 340, 440, and C131, B, C, D, E, and F (Military) Series Airplanes
aircraft Kelowna Flightcraft R & D Ltd. Military C-131B Airworthiness Directives; General Dynamics (CONVAIR) Model 340, 440, and C131, B, C, D, E, and F (Military) Series Airplanes
aircraft Kelowna Flightcraft R & D Ltd. Military C-131D Airworthiness Directives; General Dynamics (CONVAIR) Model 340, 440, and C131, B, C, D, E, and F (Military) Series Airplanes
aircraft Kelowna Flightcraft R & D Ltd. Military C-131E Airworthiness Directives; General Dynamics (CONVAIR) Model 340, 440, and C131, B, C, D, E, and F (Military) Series Airplanes
aircraft Kelowna Flightcraft R & D Ltd. Military C-131F/R4Y-1 Airworthiness Directives; General Dynamics (CONVAIR) Model 340, 440, and C131, B, C, D, E, and F (Military) Series Airplanes

Unsafe Condition

Loss of the elevator hinge pins due to non-conforming dimensions, cracked bearing plate assemblies, or loose, chattering, dry, or seized bearings (P/N AN201KP1A).

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

Required Actions

Within 50 hours time-in-service or 60 days after the effective date, remove the elevator and inspect hinge pins and bearings per SB 55-5. Replace non-conforming pins, bushings, or tapered bushings; replace cracked bearing plates, loose/chattering/dry/seized bearings. Ensure proper mating of tapered bushing and pin surfaces during reinstallation; rework pins if needed per SB 55-5.

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

Compliance Time

Within 50 hours time-in-service or 60 days after the effective date of this AD, whichever occurs first

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

Affected Aircraft

General Dynamics (CONVAIR) Model 340, 440, and C131, B, C, D, E, and F (Military) series airplanes, including all airplanes converted to turbopropeller power, certificated in any category.

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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