AD 75-12-06

final rule
Data completeness: 70%

Airworthiness Directives; Piper Models PA-24, PA-24-250, PA-24-260 and PA-24-400 Airplanes

AD Number
75-12-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-24 Airworthiness Directives; Piper Models PA-24, PA-24-250, PA-24-260 and PA-24-400 Airplanes
aircraft Piper Aircraft Inc. PA-24-250 Airworthiness Directives; Piper Models PA-24, PA-24-250, PA-24-260 and PA-24-400 Airplanes
aircraft Piper Aircraft Inc. PA-24-260 Airworthiness Directives; Piper Models PA-24, PA-24-250, PA-24-260 and PA-24-400 Airplanes
aircraft Piper Aircraft Inc. PA-24-400 Airworthiness Directives; Piper Models PA-24, PA-24-250, PA-24-260 and PA-24-400 Airplanes

Unsafe Condition

Cracks in the fin forward spar to fuselage attachment assembly channel P/N 20749-0 and straps P/N 20749-5 and -6 in the area of the channel bend relief holes.

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

Required Actions

Inspect the channel and straps for cracks using dye penetrant or approved equivalent inspection within 25 hours' time in service (if not done in last 75 hours). Polish rough edges of bend relief holes. Repeat visual inspections with 5 power magnifying glass or equivalent every 100 hours' time in service. Repair or replace cracked parts with FAA approved methods or equivalent parts before further flight.

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

Compliance Time

Within the next 25 hours' time in service (for initial inspection), and subsequent inspections within 100 hours' time in service from the last inspection.

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

Affected Aircraft

Piper Models PA-24, PA-24-250, PA-24-260, and PA-24-400 certificated in all categories where the fin forward spar uses channel P/N 20749-0 and straps P/N 20749-5 and -6.

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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