AD 80-14-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Piper Aircraft Inc. | PA-28-181 | Airworthiness Directives; Piper Models PA-28-181, PA-32-300 and PA-32R-300 Airplanes |
| aircraft | Piper Aircraft Inc. | PA-32-300 | Airworthiness Directives; Piper Models PA-28-181, PA-32-300 and PA-32R-300 Airplanes |
| aircraft | Piper Aircraft Inc. | PA-32R-300 | Airworthiness Directives; Piper Models PA-28-181, PA-32-300 and PA-32R-300 Airplanes |
Unsafe Condition
Separation of the throttle control cable rod end from the throttle arm on PA-28 and PA-32 airplanes, and rod end binding with possible subsequent throttle cable failure on PA-28 airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the throttle linkage connecting hardware per Piper Service Bulletin No. 537 for PA-32 models, modify the throttle linkage using Piper Part Number 764-009V for PA-28-181 models, and record maintenance.
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 Models PA-28-181 (serial numbers 28-7790032 through 28-8090227), PA-32-300 (serial numbers 32-7640001 through 32-7740032), and PA-32R-300 (serial numbers 32R-7680001 through 32R-7780148)
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.