# Proposed AD 2003-CE-26-AD: GROB-WERKE Model G120A Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2003-19-13
- Products: Grob-Werke
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: July 15, 2003, 68 FR 41760
- Comments due: August 18, 2003
- Became: [AD 2003-19-13](https://openairdocs.org/ad/2003-19-13)
- Docket: 2003-CE-26-AD
- FR document: 03-17818
- Official PDF: https://openairdocs.org/files/sha256/e0/24/e0240b7bf4ddd5bae639613a04b7350bf894fdceacc58c56b84d095a4201d198 (from https://www.govinfo.gov/content/pkg/FR-2003-07-15/pdf/03-17818.pdf)
- Federal Register: https://www.federalregister.gov/documents/2003/07/15/03-17818/airworthiness-directives-grob-werke-model-g120a-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/533D918FBC367B1586256D64004C55BE.0001
- Page: https://openairdocs.org/proposed/2003-CE-26-AD

## Summary

This document proposes to adopt a new airworthiness directive (AD) that would apply to all GROB-WERKE (GROB) Model G120A airplanes. This proposed AD would require you to modify the flight control system operating levers. This proposed AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this proposed AD are intended to prevent failure of a ball bearing in flight control system operating levers. Such failure could lead to reduced control or loss of control of the airplane.

## Notices in this docket

- Jul 15, 2003: Notice of proposed rulemaking (NPRM). (first notice), FR document 03-17818, comments due Aug 18, 2003 (https://www.federalregister.gov/documents/2003/07/15/03-17818/airworthiness-directives-grob-werke-model-g120a-airplanes)

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