AD 82-06-11 R1
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Piper Aircraft Inc. | PA-28R-200 | Airworthiness Directives; Piper Model PA-28R-201T, PA-28RT-201T, PA-28R-200, PA-28R-201, and PA-28RT-201 Airplanes |
| aircraft | Piper Aircraft Inc. | PA-28R-201 | Airworthiness Directives; Piper Model PA-28R-201T, PA-28RT-201T, PA-28R-200, PA-28R-201, and PA-28RT-201 Airplanes |
| aircraft | Piper Aircraft Inc. | PA-28R-201T | Airworthiness Directives; Piper Model PA-28R-201T, PA-28RT-201T, PA-28R-200, PA-28R-201, and PA-28RT-201 Airplanes |
| aircraft | Piper Aircraft Inc. | PA-28RT-201 | Airworthiness Directives; Piper Model PA-28R-201T, PA-28RT-201T, PA-28R-200, PA-28R-201, and PA-28RT-201 Airplanes |
| aircraft | Piper Aircraft Inc. | PA-28RT-201T | Airworthiness Directives; Piper Model PA-28R-201T, PA-28RT-201T, PA-28R-200, PA-28R-201, and PA-28RT-201 Airplanes |
Unsafe Condition
Inadvertent retraction of the nose landing gear.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect, rig, and modify the nose landing gear in accordance with Piper Service Bulletin No. 724A, dated April 20, 1982, Parts I and II as applicable, using dye penetrant for crack detection. Record compliance in the airplane maintenance records. Use an equivalent method of compliance if approved by the FAA.
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Compliance Time
Within the next 100 hours time-in-service after the effective date of this AD
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Affected Aircraft
Piper Model PA-28R-201T (serials 28R-7703001 through 28R-7803373), PA-28RT-201T (serials 28R-7931001 through 28R-8131193), PA-28R-200 (serials 28R-7635522 through 28R-7635545), PA-28R-201 (serials 28R-7737001 through 28R-7837317), and PA-28RT-201 (serials 28R-7918001 through 28R-8118082).
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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