AD 79-17-05

Active

Fuel Gauges and Engine Instruments

Key Information
79-17-05
Active
August 22, 1979
August 08, 1979
Unknown
39-3531
Applicability
["Aircraft"]
["Small Airplane"]
Piper Aircraft Inc.
PA-38-112
Regulatory Text

79-17-05 PIPER: Amendment 39-3531. Applies to Model PA-38-112 serial numbers 38-78A0002 thru 38-78A0027, 38-78A0029 thru 38-78A0037, 38-78A0039 thru 38-78A0041, 38-78A0043, 38-78A0045 thru 38-78A0064, 38-78A0066 thru 38-78A0072, and 38-78A0074 thru 38-78A0104.

Compliance required as indicated unless already accomplished.

a. To prevent the occurrence of insufficient or intermittent grounding of the fuel gauges and engine instrument cluster, accomplish the following:

Within the next 25 hours in service after the effective date of this AD, install ground wire harness assembly P/N 77960-400 and connect leads to instruments and terminal ground strip in accordance with Piper Service Bulletin No. 603, or an approved equivalent alteration.

Equivalent alterations must be approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration (FAA), Eastern Region.

b. Aircraft may be flown in accordance with 21.197 to a base where the modification required by this AD can be accomplished.

This amendment is effective August 22, 1979.

AD Assistant

Get AI-powered answers about this AD, check applicability, and find compliance steps.

Sign Up to Unlock
References
This information is not available.
--- - Part 39
--- - _EMPTY_
Issuing Office
["AIR-720: Operational Safety Branch"]
FAA Documents