Airworthiness Directives; The New Piper Aircraft, Inc., Models PA-46-310P and PA-46-350P Airplanes
airworthiness · Rule · Final rule. · Published 2000-05-25 · Effective 2000-07-28 · 65 FR 33745
Document
Document number
00-13083
Federal Register citation
65 FR 33745
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
The New Piper
Publication date
2000-05-25
Effective date
2000-07-28
FAA docket
Docket No. 98-CE-112-AD
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.