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Airworthiness Directive

AD 2003-09-01 68 FR 22582 Superseded

Federal Aviation Administration · 14 CFR part 39

Requires you to inspect and correct, as necessary, the aileron control bellcrank assemblies at the wing and fuselage locations.

Superseded by AD 2006-15-02Federal Register (opens in a new tab)

FR document
03-10237
Amendment
39-13130
Published
2003-04-29
Effective
2003-06-17
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2003-09-01 · 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

2003-09-01

FR doc 03-10237 · 68 FR 22582

AD 2003-09-01Published 2003-04-29Effective 2003-06-17

Superseded by 2006-15-02

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 and correct, as necessary, the aileron control bellcrank assemblies at the wing and fuselage locations.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all Pilatus Aircraft Ltd. (Pilatus) Model PC-6 airplanes. This AD requires you to inspect and correct, as necessary, the aileron control bellcrank assemblies at the wing and fuselage locations. 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 detect and correct increased friction in the aileron control bellcrank assemblies, which could result in failure of the aileron flight-control system. Such failure could lead to problems in controlling flight.

More directives for Pilatus PC-6 Porter

  1. AD 2021-24-22 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes Effective 2022-01-25
  2. AD 2021-11-08 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes Effective 2021-07-12
  3. AD 2020-16-02 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes Effective 2020-09-09
  4. AD 2020-11-06 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes Effective 2020-06-30
  5. AD 2019-10-07 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes Effective 2019-07-10

All Pilatus PC-6 Porter directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 2003-09-01 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index