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Airworthiness Directive

AD 2002-19-08 67 FR 60114 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-24179
Amendment
39-12888
Published
2002-09-25
Effective
2002-11-08
Models covered
1
Last live check
2026-10-01

Printed from https://aircraftdirectives.com/ad/2002-19-08 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

2002-19-08

FR doc 02-24179 · 67 FR 60114

AD 2002-19-08Published 2002-09-25Effective 2002-11-08

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 flight and engine control systems to ensure that there is correct connecting bolt and linkage installation, no interference, and correct installation of certain components.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Vulcanair S.p.A. (Vulcanair) P 68 series airplanes. This AD requires you to inspect the flight and engine control systems to ensure that there is correct connecting bolt and linkage installation, no interference, and correct installation of certain components. This AD also requires you to make any necessary adjustments and modify and install the split link and full travel limit assembly. 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 primary flight control system caused by certain configurations. Such failure could lead to loss of airplane flight control.

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

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 1 model in our index