AD 74-13-04

final rule
Data completeness: 70%

Airworthiness Directives; Piper Model PA-28-140 Airplanes

AD Number
74-13-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-28-140 Airworthiness Directives; Piper Model PA-28-140 Airplanes

Unsafe Condition

Loss of power due to a failed ball joint assembly in the throttle control cable.

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

Required Actions

Remove the throttle control cable ball joint assembly and install an alignment bracket and spherical rod end bearing as per Piper Kit 760 780V or approved procedure. Adjust throttle closure and check inspection hole for visible threads.

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

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

Affected Aircraft

Piper Model PA-28-140 airplanes with serial numbers 28-25001 to 28-26331 inclusive; 28-26401 to 28-26946 inclusive; 28-7125001 to 28-7125641 inclusive, and 28-7225001 to 28-7425354 inclusive.

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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