AD 96-21-03

final rule
Data completeness: 70%

Airworthiness Directives; The New Piper Aircraft, Inc. PA31, PA31P, PA31T, and PA42 Series Airplanes

AD Number
96-21-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
95-CE-84-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-31 Airworthiness Directives; The New Piper Aircraft, Inc. PA31, PA31P, PA31T, and PA42 Series Airplanes
aircraft Piper Aircraft Inc. PA-31-300 Airworthiness Directives; The New Piper Aircraft, Inc. PA31, PA31P, PA31T, and PA42 Series Airplanes
aircraft Piper Aircraft Inc. PA-31-325 Airworthiness Directives; The New Piper Aircraft, Inc. PA31, PA31P, PA31T, and PA42 Series Airplanes
aircraft Piper Aircraft Inc. PA-31-350 Airworthiness Directives; The New Piper Aircraft, Inc. PA31, PA31P, PA31T, and PA42 Series Airplanes
aircraft Piper Aircraft Inc. PA-31P Airworthiness Directives; The New Piper Aircraft, Inc. PA31, PA31P, PA31T, and PA42 Series Airplanes
aircraft Piper Aircraft Inc. PA-31P-350 Airworthiness Directives; The New Piper Aircraft, Inc. PA31, PA31P, PA31T, and PA42 Series Airplanes
aircraft Piper Aircraft Inc. PA-31T Airworthiness Directives; The New Piper Aircraft, Inc. PA31, PA31P, PA31T, and PA42 Series Airplanes
aircraft Piper Aircraft Inc. PA-31T1 Airworthiness Directives; The New Piper Aircraft, Inc. PA31, PA31P, PA31T, and PA42 Series Airplanes
aircraft Piper Aircraft Inc. PA-31T2 Airworthiness Directives; The New Piper Aircraft, Inc. PA31, PA31P, PA31T, and PA42 Series Airplanes
aircraft Piper Aircraft Inc. PA-31T3 Airworthiness Directives; The New Piper Aircraft, Inc. PA31, PA31P, PA31T, and PA42 Series Airplanes

Unsafe Condition

Cracks beneath and in the area of the inboard aileron hinge bracket on the aileron spar and rib could result in structural failure of the aileron and loss of control of the airplane.

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

Required Actions

Inspect for cracks beneath and in the area of the inboard aileron hinge bracket on the aileron spar and rib using methods acceptable to the FAA. Repair cracks as necessary. Install part numbers 74461-02 (left) and 74461-03 (right) inboard aileron hinge brackets if not already equipped. Comply with applicable service bulletins (SB) 967 or 974.

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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