# Airworthiness Directives; Burkhart Grob Luft-und Raumfahrt Models G115, G115A, G115B, G115C, G115C2, G115D, and G115D2 Airplanes
> **Rule** · Final rule. · Published 1998-11-23 · Effective 1998-12-28 · 63 FR 64598
## Document
- **Document number:** 98-30896
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 63 FR 64598
- **Publication date:** 1998-11-23
- **Effective date:** 1998-12-28
- **FAA docket:** Docket No. 98-CE-68-AD
## 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.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1998/11/23/98-30896/airworthiness-directives-burkhart-grob-luft-und-raumfahrt-models-g115-g115a-g115b-g115c-g115c2-g115d)
---
*AI Analytics · CC0 1.0*