AD 2003-24-07

final rule
Data completeness: 70%

Airworthiness Directives; The New Piper Aircraft, Inc. Models PA-31, PA-31-300, PA-31-325, PA-31-350, PA-31P, PA-31T, PA-31T1, PA-31T2, PA-31T3, and PA-31P-350 Airplanes

AD Number
2003-24-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2003-CE-03-AD
FR Citation
68 FR 67588

Applicability

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

Unsafe Condition

Corrosion in the rudder torque tube assembly and rudder rib could result in failure of the rudder torque tube, leading to loss of rudder control.

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

Required Actions

Install an inspection hole (or use the existing tooling hole in the rudder bottom rib), conduct a detailed visual inspection of the rudder torque tube and associated ribs for corrosion. If corrosion is found, replace or repair the rib/rudder torque tube assembly. Optionally, repair with an FAA-approved design if corrosion is less than 50% of thickness over an area less than two square inches.

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

Compliance Time

Within 150 flight hours time-in-service (TIS) after the effective date.

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

Affected Aircraft

The New Piper Aircraft, Inc. Models PA-31, PA-31-300, PA-31-325, PA-31-350, PA-31P, PA-31T, PA-31T1, PA-31T2, PA-31T3, and PA-31P-350 airplanes.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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