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Airworthiness Directive

AD 2003-19-13 68 FR 56154 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to modify the flight control system operating levers.

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FR document
03-24284
Amendment
39-13316
Published
2003-09-30
Effective
2003-11-11
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2003-19-13 · 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

2003-19-13

FR doc 03-24284 · 68 FR 56154

AD 2003-19-13Published 2003-09-30Effective 2003-11-11

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 modify the flight control system operating levers.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for all GROB-WERKE (GROB) Model G120A airplanes. This AD requires you to modify the flight control system operating levers. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to prevent failure of a ball bearing in the flight control system operating levers. Such failure could lead to reduced control or loss of control of the airplane.

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