AD 75-02-03

final rule
Data completeness: 60%

Airworthiness Directives; Piper Models PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-32-260 and PA-32-300 Airplanes

AD Number
75-02-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-28-140 Airworthiness Directives; Piper Models PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-32-260 and PA-32-300 Airplanes
aircraft Piper Aircraft Inc. PA-28-150 Airworthiness Directives; Piper Models PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-32-260 and PA-32-300 Airplanes
aircraft Piper Aircraft Inc. PA-28-160 Airworthiness Directives; Piper Models PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-32-260 and PA-32-300 Airplanes
aircraft Piper Aircraft Inc. PA-28-180 Airworthiness Directives; Piper Models PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-32-260 and PA-32-300 Airplanes
aircraft Piper Aircraft Inc. PA-28-235 Airworthiness Directives; Piper Models PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-32-260 and PA-32-300 Airplanes
aircraft Piper Aircraft Inc. PA-32-260 Airworthiness Directives; Piper Models PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-32-260 and PA-32-300 Airplanes
aircraft Piper Aircraft Inc. PA-32-300 Airworthiness Directives; Piper Models PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-32-260 and PA-32-300 Airplanes

Unsafe Condition

Failure of the nose wheel fork assembly due to bends not part of the STC design, cracks in the vicinity of the nose wheel axle holes, or improper material treatment.

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

Required Actions

Visually inspect the nose wheel fork for bends; straighten any bends found; inspect for cracks using penetrant inspection; chamfer and heat treat the fork to Ftu of 180,000 PSI; replace parts with specified equivalents; stamp the fork with 'H'.

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

Compliance Time

prior to the accumulation of 25 landings after the effective date of this AD, unless already accomplished

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

Affected Aircraft

Piper Models PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-32-260, PA-32-300 with Supplemental Type Certificate SA281AL, large nose wheel fork (Tibbetts-Herre Airmotive P/N PA-32-1), and 8.00-6 nose wheel tire.

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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