AD 78-23-01

final rule
Data completeness: 70%

Airworthiness Directives; Piper Models PA-28-235, PA-32-260, PA-32-300, PA-32S-300, PA-32R-300, PA-32RT-300 and PA- 32RT-300T Airplanes

AD Number
78-23-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-28-235 Airworthiness Directives; Piper Models PA-28-235, PA-32-260, PA-32-300, PA-32S-300, PA-32R-300, PA-32RT-300 and PA- 32RT-300T Airplanes
aircraft Piper Aircraft Inc. PA-32-260 Airworthiness Directives; Piper Models PA-28-235, PA-32-260, PA-32-300, PA-32S-300, PA-32R-300, PA-32RT-300 and PA- 32RT-300T Airplanes
aircraft Piper Aircraft Inc. PA-32-300 Airworthiness Directives; Piper Models PA-28-235, PA-32-260, PA-32-300, PA-32S-300, PA-32R-300, PA-32RT-300 and PA- 32RT-300T Airplanes
aircraft Piper Aircraft Inc. PA-32R-300 Airworthiness Directives; Piper Models PA-28-235, PA-32-260, PA-32-300, PA-32S-300, PA-32R-300, PA-32RT-300 and PA- 32RT-300T Airplanes
aircraft Piper Aircraft Inc. PA-32RT-300 Airworthiness Directives; Piper Models PA-28-235, PA-32-260, PA-32-300, PA-32S-300, PA-32R-300, PA-32RT-300 and PA- 32RT-300T Airplanes
aircraft Piper Aircraft Inc. PA-32RT-300T Airworthiness Directives; Piper Models PA-28-235, PA-32-260, PA-32-300, PA-32S-300, PA-32R-300, PA-32RT-300 and PA- 32RT-300T Airplanes
aircraft Piper Aircraft Inc. PA-32S-300 Airworthiness Directives; Piper Models PA-28-235, PA-32-260, PA-32-300, PA-32S-300, PA-32R-300, PA-32RT-300 and PA- 32RT-300T Airplanes

Unsafe Condition

Inadvertent fuel drain lever actuation due to improper functioning of the fuel drain lever cover assembly door, which may not prevent access to the lever when closed.

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

Required Actions

Remove and replace the fuel drain lever cover assembly with Piper Kit 763 883V, check door operation for free movement and proper lever access prevention, and record maintenance entries. For affected models, inspections must be done within 50 hours time in service after the effective date, with subsequent checks every 100 hours.

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, and at intervals not to exceed 100 hours time in service from the last check.

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

Affected Aircraft

Piper Models PA-28-235 (serial numbers 28-10003 through 28-10660), PA-32-260, PA-32-300, PA-32S-300, PA-32R-300, PA-32RT-300, and PA-32RT-300T, all serial numbers.

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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