AD 82-02-01

final rule
Data completeness: 70%

Airworthiness Directives; Piper Model PA-38-112 Airplanes

AD Number
82-02-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-38-112 Airworthiness Directives; Piper Model PA-38-112 Airplanes

Unsafe Condition

Cracks in the Aileron Balance Weight Rib P/N's 77342-16 and -17 could cause possible hazards in flight.

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

Required Actions

Inspect the aileron balance weight rib flange area using a minimum 10 power magnifier within the next 100 hours in service. If cracks are found, replace the cracked ribs with undamaged ribs of the same part numbers and incorporate the Aileron Balance Weight Rib Reinforcement Kit (Piper Part No. 764140).

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

Compliance Time

within the next 100 hours in service

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

Affected Aircraft

Piper Model PA-38-112, Serial Nos. 38-78A0001 thru 38-81A0051 and 38-81A0105 certificated in all categories except aircraft incorporating Aileron Balance Weight Rib Reinforcement Kit, Piper Part No. 764140.

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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