Airworthiness Directives; Pilatus Aircraft Ltd. Models PC-12 and PC-12/45 Airplanes
airworthiness · Rule · Final rule. · Published 1999-08-19 · Effective 1999-10-04 · 64 FR 45149
Document
Document number
99-21016
Federal Register citation
64 FR 45149
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Pilatus
Publication date
1999-08-19
Effective date
1999-10-04
FAA docket
Docket No. 99-CE-10-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that applies to certain Pilatus Aircraft Ltd. (Pilatus) Models PC-12 and PC- 12/45 airplanes. This AD requires modifying the generator 2 excitation by removing certain diodes and installing a new 5-amp circuit breaker and suppression filter. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. The actions specified by this AD are intended to prevent damage to electrical components if the generator 2 is not switched off prior to engine shutdown and it overheats, which could result in loss of electrical power to certain critical airplane components.