AD 83-14-08

final rule
Data completeness: 70%

Airworthiness Directives; Piper Model PA-38-112 Airplanes

AD Number
83-14-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-38-112 Airworthiness Directives; Piper Model PA-38-112 Airplanes

Unsafe Condition

The stall characteristics of the Piper Model PA-38-112 airplanes are not standardized or adequate, posing a safety risk during stall conditions.

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

Required Actions

Install Piper Flow Strip Installation Kit Part No. 763-930, replace the airspeed indicator with Piper Part No. 61906-02 or 61905-02 (or remark original instrument with specified markings), insert Piper Part No. 761-658 Rev 3 into the Pilot's Operating Handbook, and ensure any remarking is done by a certificated instrument repair station.

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

Compliance Time

within the next 100 hours time-in-service 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 Model PA-38-112 airplanes with serial numbers 38-78A0001 through 38-79A0582

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.