AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 2000-01-10 65 FR 1767 Active

Federal Aviation Administration · 14 CFR part 39

FR document
00-498
Amendment
39-11508
Published
2000-01-12
Effective
2000-03-03
Models covered
1
Last live check
2026-10-03

Printed from https://aircraftdirectives.com/ad/2000-01-10 · 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.

Opens your browser's print dialog. Choose “Save as PDF” to export a file. Keyboard: Ctrl+P or Cmd+P.

AD

2000-01-10

FR doc 00-498 · 65 FR 1767

AD 2000-01-10Published 2000-01-12Effective 2000-03-03

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 replacing the rudder and elevator pivot arms with parts of improved design on certain Pilatus Aircraft Ltd.

Full official abstract

This amendment supersedes Airworthiness Directive (AD) 98-08- 07, which currently requires replacing the rudder and elevator pivot arms with parts of improved design on certain Pilatus Aircraft Ltd. (Pilatus) Model PC-7 airplanes. This AD requires replacing the rudder and elevator pivot arms with parts that have been improved since issuance of AD 98-08-07. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. The actions specified by this AD are intended to prevent failure of the elevator and rudder caused by fatigue cracking of the pivot arms, which could result in reduced airplane controllability and possible loss of control of the airplane.

More directives for Pilatus PC-7

  1. AD 2020-26-19 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2021-02-22
  2. AD 2021-04-06 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2021-02-12
  3. AD 2019-05-15 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2019-04-03
  4. AD 2018-04-10 Airworthiness Directives; Pilatus Aircraft Limited Airplanes 2018-03-08
  5. AD 2016-17-07 Airworthiness Directives; PILATUS Aircraft Ltd. Airplanes 2016-08-26

All Pilatus PC-7 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