Airworthiness Directive

AD 2001-22-15 66 FR 56202

Federal Aviation Administration · 14 CFR part 39

FR document
01-27652
Amendment
39-12494
Published
2001-11-07
Models covered
1
Last live check
2026-08-17
AD

2001-22-15

FR doc 01-27652 · 66 FR 56202

AD 2001-22-15Published 2001-11-07Effective 2001-12-26

Requires you to inspect the cargo doors to identify front and rear end frames with plain lightening holes and install reinforcing plates on any frame with plain lightening holes.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all Pilatus Aircraft Ltd. (Pilatus) Models PC-12 and PC-12/ 45 airplanes. This AD requires you to inspect the cargo doors to identify front and rear end frames with plain lightening holes and install reinforcing plates on any frame with plain lightening holes. 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 cracking at the edges of the unflanged lightening holes, which could result in major structural damage to the airplane. Such damage could result in possible loss of control of the airplane.

Applies to 1 model in our index