NPRM 2003-CE-55-AD

Became AD 2004-06-05

Proposed airworthiness directive · Pilatus

Published
January 9, 2004 · 69 FR 1551
Comments due
February 19, 2004
Action
Notice of proposed rulemaking (NPRM)
Docket
2003-CE-55-AD
FR document
04-476
Products
Aircraft

A proposal is not in force. If adopted, it becomes an AD, usually with changes. Only the Federal Register edition is official.

Summary

The FAA proposes to adopt a new airworthiness directive (AD) for all Pilatus Aircraft Ltd. (Pilatus) Models PC-12 and PC-12/45 airplanes. This proposed AD would require you to determine whether certain main landing gear shock absorber attachment bolts have been replaced and, if not replaced would require you to replace shock absorber attachment bolts on main landing gear assemblies that had a serial number beginning with AM. This proposed AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. We are issuing this proposed AD to detect and correct hydrogen embrittlement in the main landing gear shock absorber attachment bolts, which could result in failure of the main landing gear. This failure could lead to main landing gear collapse during operation with consequent loss of airplane control.

The resulting AD

Notices in this docket · 1