Airworthiness Directive

AD 96-23-01 Amendment 39-9806

Federal Aviation Administration · 14 CFR part 39

FR document
96-28167
Amendment
39-9806
Published
1996-11-06
Models covered
1
Last live check
Not yet re-verified
AD

96-23-01

FR doc 96-28167

AD 96-23-01Published 1996-11-06Effective 1996-12-11

Requires replacing certain Kratos indicators.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to Bell Helicopter Textron, a Division of Textron Canada, Ltd. (BHTC) Model 206L-1 helicopters that have a Kratos turbine outlet temperature (TOT) indicator (Kratos indicator) installed, that requires replacing certain Kratos indicators. This amendment is prompted by manufacturer's tests and FAA analyses that show certain Kratos indicators may incorrectly provide low-temperature readings when the battery voltage is below 10 volts. The actions specified by this AD are intended to prevent false low-temperature indications, which could result in overheating of the engine turbine (turbine) and subsequent thermal fatigue damage to the turbine wheel.

Applies to 1 model in our index