Airworthiness Directive

AD 2000-24-05 65 FR 75599 Active

Federal Aviation Administration · 14 CFR part 39

FR document
00-30317
Amendment
39-12012
Published
2000-12-04
Effective
2001-01-05
Models covered
1
Last live check
2026-10-01
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AD

2000-24-05

FR doc 00-30317 · 65 FR 75599

AD 2000-24-05Published 2000-12-04Effective 2001-01-05

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 nose landing gear (NLG) upper strut for evidence of cracking (cracks or crack beginnings), and replace the NLG upper strut if you find evidence of cracking.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Vulcanair S.p.A. (Vulcanair) Models P 68 "OBSERVER", P68 "OBSERVER 2", and P68TC "OBSERVER" airplanes. This AD requires you to inspect the nose landing gear (NLG) upper strut for evidence of cracking (cracks or crack beginnings), and replace the NLG upper strut if you find evidence of cracking. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. The actions specified by this AD are intended to prevent failure of the NLG upper strut caused by cracking in the area of the seeger retaining ring groove, which could result in loss of control of the airplane.

More directives for Vulcanair / Partenavia P68

  1. AD 2022-20-10 Airworthiness Directives; Vulcanair S.p.A. Airplanes 2022-10-24
  2. AD 2021-26-15 Airworthiness Directives; Vulcanair S.p.A. Airplanes 2022-01-11
  3. AD 2019-06-10 Airworthiness Directives; Vulcanair S.p.A. Airplanes 2019-04-09
  4. AD 2015-18-01 Airworthiness Directives; Vulcanair S.p.A. Airplanes 2015-09-02
  5. AD 2014-10-01 Airworthiness Directives; Vulcanair S.p.A. Airplanes 2014-05-14

All Vulcanair / Partenavia P68 directives

Applies to 1 model in our index