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Airworthiness Directive

AD 98-24-08 63 FR 64598 Active

Federal Aviation Administration · 14 CFR part 39

Requires inspecting the area of the elevator trim tab hinges for cracks and a secure fit, and repairing any elevator trim tab hinges with cracks or where a proper secure fit is not found.

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FR document
98-30896
Amendment
39-10894
Published
1998-11-23
Effective
1998-12-28
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/98-24-08 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

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AD

98-24-08

FR doc 98-30896 · 63 FR 64598

AD 98-24-08Published 1998-11-23Effective 1998-12-28

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 inspecting the area of the elevator trim tab hinges for cracks and a secure fit, and repairing any elevator trim tab hinges with cracks or where a proper secure fit is not found.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all Burkhart Grob Luft-und Raumfahrt (Grob) Models G115, G115A, G115B, G115C, G115C2, G115D, and G115D2 airplanes. This AD requires inspecting the area of the elevator trim tab hinges for cracks and a secure fit, and repairing any elevator trim tab hinges with cracks or where a proper secure fit is not found. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent structural damage of the trim tab hinges caused by cracks, which could result in trim tab failure with consequent loss of control of the airplane.

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Applies to 1 model in our index