AD 93-05-10

final rule
Data completeness: 70%

Airworthiness Directives; PIPER AIRCRAFT CORPORATION Model PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301 and PA-32R-301T Airplanes

AD Number
93-05-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
92-CE-37-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-32R-300 Airworthiness Directives; PIPER AIRCRAFT CORPORATION Model PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301 and PA-32R-301T Airplanes
aircraft Piper Aircraft Inc. PA-32R-301 (HP) Airworthiness Directives; PIPER AIRCRAFT CORPORATION Model PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301 and PA-32R-301T Airplanes
aircraft Piper Aircraft Inc. PA-32R-301 (SP) Airworthiness Directives; PIPER AIRCRAFT CORPORATION Model PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301 and PA-32R-301T Airplanes
aircraft Piper Aircraft Inc. PA-32R-301T Airworthiness Directives; PIPER AIRCRAFT CORPORATION Model PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301 and PA-32R-301T Airplanes
aircraft Piper Aircraft Inc. PA-32RT-300 Airworthiness Directives; PIPER AIRCRAFT CORPORATION Model PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301 and PA-32R-301T Airplanes
aircraft Piper Aircraft Inc. PA-32RT-300T Airworthiness Directives; PIPER AIRCRAFT CORPORATION Model PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301 and PA-32R-301T Airplanes

Unsafe Condition

Cracks in the engine mount could result in inability to retract or extend the nose landing gear, leading to substantial damage or loss of control of the airplane.

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

Required Actions

Inspect the engine mount per Piper SB No. 955 and repair cracks; modify airframe structure with Engine Mount Drag Link Installation Kit (Piper Part No. 766-252 for turbocharged, 766-253 for normally aspirated models); inspect nose gear actuator attachment bracket rivets per SB No. 955 and reinforce if rivets are not correct dimensions. If modification parts are unavailable, reinspect engine mount every 100 hours TIS until parts are available.

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

Compliance Time

within the next 100 hours time-in-service (TIS) 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 Aircraft Corporation models PA-32R-300 (serial 32R-7680001-32R-7880068), PA-32RT-300 (32R-7885001-32R-7985105), PA-32RT-300T (32R-7887001-32R-7987126), PA-32R-301 (32R-8013001-32R-8613005 and 3213001-3213037), PA-32R-301T (32R-8029001-32R-8629006 and 3229001-3229003)

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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