AD 2004-14-12

final rule
Data completeness: 80%

Airworthiness Directives; The New Piper Aircraft, Inc., Models PA-28-161, PA-28-181, PA-28R-201, PA-32R-301 (HP), PA-32R-301T, PA-32-301FT, PA-32-301XTC, PA-34-220T, PA-44-180, PA-46-350P, and PA-46-500TP Airplanes

AD Number
2004-14-12
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2004-18032
FR Citation
69 FR 41407

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Airworthiness Directives; The New Piper Aircraft, Inc., Models PA-28-161, PA-28-181, PA-28R-201, PA-32R-301 (HP), PA-32R-301T, PA-32-301FT, PA-32-301XTC, PA-34-220T, PA-44-180, PA-46-350P, and PA-46-500TP Airplanes

Unsafe Condition

could result in loss of control of the ailerons and elevator.

Required Actions

you to inspect the control wheel attaching hardware for proper installation, replace if required, add Loctite thread- locking compound to the screw installation, and install a retainer clip to the control wheel attachment

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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