AD 82-23-01 R1

final rule
Data completeness: 70%

Airworthiness Directives; Piper Model PA-24, PA-24-250, PA-24-260, PA-30 and PA-39 Airplanes

AD Number
82-23-01 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-24 Airworthiness Directives; Piper Model PA-24, PA-24-250, PA-24-260, PA-30 and PA-39 Airplanes
aircraft Piper Aircraft Inc. PA-24-250 Airworthiness Directives; Piper Model PA-24, PA-24-250, PA-24-260, PA-30 and PA-39 Airplanes
aircraft Piper Aircraft Inc. PA-24-260 Airworthiness Directives; Piper Model PA-24, PA-24-250, PA-24-260, PA-30 and PA-39 Airplanes
aircraft Piper Aircraft Inc. PA-30 Airworthiness Directives; Piper Model PA-24, PA-24-250, PA-24-260, PA-30 and PA-39 Airplanes
aircraft Piper Aircraft Inc. PA-39 Airworthiness Directives; Piper Model PA-24, PA-24-250, PA-24-260, PA-30 and PA-39 Airplanes

Unsafe Condition

Possible loss of airplane control due to asymmetrical flap extension or retraction.

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

Required Actions

Install a temporary placard near the flap actuator stating 'DO NOT EXTEND FLAPS BEYOND 15 DEGREES (TAKEOFF POSITION)', insert Figure 1 of this AD dated March 3, 1983, into the Airplane Flight Manual, and make a maintenance record entry. Compliance may be removed upon installation of a positive flap retraction system per Robertson Service Bulletin 19.

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

Compliance Time

within 25 hours time-in-service after the effective date of this AD unless already accomplished

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

Affected Aircraft

Piper Models PA-24, PA-24-250, PA-24-260, PA-30, and PA-39 airplanes modified per Robertson STC SA2495WE or SA2312WE without the positive flap retraction system.

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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