Airworthiness Directive

AD 99-15-04 R1 65 FR 33745

Federal Aviation Administration · 14 CFR part 39

FR document
00-13083
Amendment
39-11747
Published
2000-05-25
Models covered
1
Last live check
2026-08-19
AD

99-15-04 R1

FR doc 00-13083 · 65 FR 33745

AD 99-15-04 R1Published 2000-05-25Effective 2000-07-28

Requires you to calibrate, inspect, and repair or replace portions of the turbine inlet temperature system on all The New Piper Aircraft, Inc.

Full official abstract

This amendment revises Airworthiness Directive (AD) 99-15-04, which currently requires you to calibrate, inspect, and repair or replace portions of the turbine inlet temperature system on all The New Piper Aircraft, Inc. (New Piper) Models PA-46-310P and PA-46-350P airplanes (different actions for different airplane models). Information reveals that the AD should not apply to airplanes where the factory installed turbine inlet temperature gauge and associated probe have been replaced through supplemental type certificate (STC). This AD retains the actions of AD 99-15-04, and restricts the applicability accordingly. The actions specified by this AD are intended to prevent improper engine operation caused by improperly calibrated turbine inlet temperature indicators or defective turbine inlet temperature probes, which could result in engine damage/failure with consequent loss of control of the airplane.

Applies to 1 model in our index