AD 67-14-07

final rule
Data completeness: 70%

Airworthiness Directives; Piper Model PA-25-235 Airplanes

AD Number
67-14-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
Federal Register: April 20, 1967

Applicability

TypeManufacturerModelDetails
aircraft Lavia Argentina S.A. (Laviasa) PA-25-235 Airworthiness Directives; Piper Model PA-25-235 Airplanes

Unsafe Condition

Failure of engine exhaust system components such as cracks, burn-throughs, weld separations, or failed internal baffles.

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

Required Actions

Conduct initial inspections within specified time frames, inspect exhaust system for damage, inspect lower ignition harness, engine mount, rubber bushings, and ducting. Remove damaged parts before further flight. Perform recurrent inspections every 50 hours' time in service. Adjust intervals up to 15 hours for annual or 100-hour inspections. Install Piper Part No. 753-753 to discontinue recurrent inspections.

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

Compliance Time

Within the next 50 hours' time in service after the effective date for aircraft with 150+ hours total time; before 200 hours' total time for aircraft with less than 150 hours. Recurrent inspections every 50 hours' time in service thereafter. Adjustments up to 15 hours allowed.

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

Affected Aircraft

Piper Model PA-25-235 Airplanes, Serial Numbers 25-2000 to 25-4171 inclusive.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.