AD 49-27-02

final rule
Data completeness: 60%

Airworthiness Directives; Piper Model PA-12 and PA-14 Airplanes

AD Number
49-27-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft FS 2002 Corp. | FS 2003 Corp. PA-14 Airworthiness Directives; Piper Model PA-12 and PA-14 Airplanes
aircraft FS 2002 Corp. | FS 2003 Corp. PA-12 Airworthiness Directives; Piper Model PA-12 and PA-14 Airplanes

Unsafe Condition

Cracks across the ears of the forked end of aileron (and flap on Model PA-14) aluminum bellcrank castings (P/N 40092) caused by excessive tightening of the bolt attaching the push rod to the casting.

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

Required Actions

Inspect the forked end of the aileron bellcrank castings (P/N 40092) and replace those found cracked.

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

Compliance Time

not later than October 1, 1949

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

Affected Aircraft

Piper Model PA-12, Serial Numbers 12-1 and up, and Model PA-14, Serial Numbers 14-1 Through 14-193

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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