Airworthiness Directive

AD 2004-06-05 69 FR 13712 Active

Federal Aviation Administration · 14 CFR part 39

FR document
04-6260
Amendment
39-13531
Published
2004-03-24
Effective
2004-05-06
Models covered
1
Last live check
2026-10-01
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AD

2004-06-05

FR doc 04-6260 · 69 FR 13712

AD 2004-06-05Published 2004-03-24Effective 2004-05-06

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires 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…

Full official abstract

The FAA adopts a new airworthiness directive (AD) for all Pilatus Aircraft Ltd. (Pilatus) Models PC-12 and PC-12/45 airplanes. This AD requires 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 have a serial number beginning with AM001 through AM053. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. We are issuing this 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.

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All Pilatus PC-12 directives

Applies to 1 model in our index