AD 80-14-03

final rule
Data completeness: 70%

Airworthiness Directives; Piper Model PA-28-161, PA-28-181, PA-28-201T, PA-28-236, PA-28R-201, PA-28RT-201, PA-28R-201T, PA-28RT-201T, PA-32-260, PA-32-300, PA-32-301, PA-32-301T, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301, PA-32R-301T, PA-34-200T and PA-44-180 Airplanes

AD Number
80-14-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-28-161 Airworthiness Directives; Piper Model PA-28-161, PA-28-181, PA-28-201T, PA-28-236, PA-28R-201, PA-28RT-201, PA-28R-201T, PA-28RT-201T, PA-32-260, PA-32-300, PA-32-301, PA-32-301T, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301, PA-32R-301T, PA-34-200T and PA-44-180 Airplanes
aircraft Piper Aircraft Inc. PA-28-181 Airworthiness Directives; Piper Model PA-28-161, PA-28-181, PA-28-201T, PA-28-236, PA-28R-201, PA-28RT-201, PA-28R-201T, PA-28RT-201T, PA-32-260, PA-32-300, PA-32-301, PA-32-301T, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301, PA-32R-301T, PA-34-200T and PA-44-180 Airplanes
aircraft Piper Aircraft Inc. PA-28-201T Airworthiness Directives; Piper Model PA-28-161, PA-28-181, PA-28-201T, PA-28-236, PA-28R-201, PA-28RT-201, PA-28R-201T, PA-28RT-201T, PA-32-260, PA-32-300, PA-32-301, PA-32-301T, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301, PA-32R-301T, PA-34-200T and PA-44-180 Airplanes
aircraft Piper Aircraft Inc. PA-28-236 Airworthiness Directives; Piper Model PA-28-161, PA-28-181, PA-28-201T, PA-28-236, PA-28R-201, PA-28RT-201, PA-28R-201T, PA-28RT-201T, PA-32-260, PA-32-300, PA-32-301, PA-32-301T, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301, PA-32R-301T, PA-34-200T and PA-44-180 Airplanes
aircraft Piper Aircraft Inc. PA-28R-201 Airworthiness Directives; Piper Model PA-28-161, PA-28-181, PA-28-201T, PA-28-236, PA-28R-201, PA-28RT-201, PA-28R-201T, PA-28RT-201T, PA-32-260, PA-32-300, PA-32-301, PA-32-301T, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301, PA-32R-301T, PA-34-200T and PA-44-180 Airplanes
aircraft Piper Aircraft Inc. PA-28R-201T Airworthiness Directives; Piper Model PA-28-161, PA-28-181, PA-28-201T, PA-28-236, PA-28R-201, PA-28RT-201, PA-28R-201T, PA-28RT-201T, PA-32-260, PA-32-300, PA-32-301, PA-32-301T, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301, PA-32R-301T, PA-34-200T and PA-44-180 Airplanes
aircraft Piper Aircraft Inc. PA-28RT-201 Airworthiness Directives; Piper Model PA-28-161, PA-28-181, PA-28-201T, PA-28-236, PA-28R-201, PA-28RT-201, PA-28R-201T, PA-28RT-201T, PA-32-260, PA-32-300, PA-32-301, PA-32-301T, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301, PA-32R-301T, PA-34-200T and PA-44-180 Airplanes
aircraft Piper Aircraft Inc. PA-28RT-201T Airworthiness Directives; Piper Model PA-28-161, PA-28-181, PA-28-201T, PA-28-236, PA-28R-201, PA-28RT-201, PA-28R-201T, PA-28RT-201T, PA-32-260, PA-32-300, PA-32-301, PA-32-301T, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301, PA-32R-301T, PA-34-200T and PA-44-180 Airplanes
aircraft Piper Aircraft Inc. PA-32-260 Airworthiness Directives; Piper Model PA-28-161, PA-28-181, PA-28-201T, PA-28-236, PA-28R-201, PA-28RT-201, PA-28R-201T, PA-28RT-201T, PA-32-260, PA-32-300, PA-32-301, PA-32-301T, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301, PA-32R-301T, PA-34-200T and PA-44-180 Airplanes
aircraft Piper Aircraft Inc. PA-32-300 Airworthiness Directives; Piper Model PA-28-161, PA-28-181, PA-28-201T, PA-28-236, PA-28R-201, PA-28RT-201, PA-28R-201T, PA-28RT-201T, PA-32-260, PA-32-300, PA-32-301, PA-32-301T, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301, PA-32R-301T, PA-34-200T and PA-44-180 Airplanes

Unsafe Condition

The muting relay plug in the audio adapter connector may become loose, causing disruption of radio communication.

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

Required Actions

Within 10 hours time in service: disconnect the muting relay plug, secure it to the harness, conduct a radio operational check, and record maintenance. Within 100 hours time in service: remove the 22 mfd capacitor, install a diode (except Bendix systems), reconnect the relay plug, and record maintenance.

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

Compliance Time

Within the next 10 hours time in service and within the next 100 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-28-161 through PA-44-180 with specific serial ranges, equipped with Bendix, King or Narco transmitters and factory installed control wheel push-to-talk switches.

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.