Airworthiness Directive

AD 2005-22-13 70 FR 66749 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to inspect the left and right main landing gear (MLG) assemblies for any part number (P/N) 532.

FR document
05-21803
Amendment
39-14357
Published
2005-11-03
Effective
2005-12-19
Models covered
1

Last live check: 2026-08-19

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AD

2005-22-13

FR doc 05-21803 · 70 FR 66749

AD 2005-22-13Published 2005-11-03Effective 2005-12-19

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 inspect the left and right main landing gear (MLG) assemblies for any part number (P/N) 532.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for certain Pilatus Aircraft Ltd. (Pilatus) Models PC-12 and PC-12/45 airplanes. This AD requires you to inspect the left and right main landing gear (MLG) assemblies for any part number (P/N) 532.10.12.077 or FAA- approved equivalent part number bolts that do not have white primed and painted heads; and replace any bolt found with new P/N 532.10.12.077F or FAA-approved equivalent part number bolts in all MLG assemblies. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. We are issuing this AD to detect and correct any P/N 532.10.12.077 or FAA- approved equivalent part number bolts that do not have white primed and painted heads, which could result in corrosion of the bolt and consequent failure of the bolt. This failure could lead to MLG collapse during airplane landing and take-off operations with consequent loss of airplane control.

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All Pilatus PC-12 directives

Applies to 1 model in our index