# Proposed AD 98-CE-53-AD: EXTRA Flugzeugbau GmbH Models EA-300, EA-300S, and EA-300L Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 98-24-07
- Action: Notice of proposed rulemaking (NPRM).
- Published: September 17, 1998, 63 FR 49675
- Comments due: October 16, 1998
- Became: [AD 98-24-07](https://openairdocs.org/ad/98-24-07)
- Docket: 98-CE-53-AD
- FR document: 98-24874
- Official PDF: https://openairdocs.org/files/sha256/96/62/96622f4c1a2ff5fd5b848e525815f064a278cf36b6627d2254a9a8e23a5bb60d (from https://www.govinfo.gov/content/pkg/FR-1998-09-17/pdf/98-24874.pdf)
- Federal Register: https://www.federalregister.gov/documents/1998/09/17/98-24874/airworthiness-directives-extra-flugzeugbau-gmbh-models-ea-300-ea-300s-and-ea-300l-airplanes
- Page: https://openairdocs.org/proposed/98-CE-53-AD

## Summary

This document proposes to adopt a new airworthiness directive (AD) that would apply to certain EXTRA Flugzeugbau GmbH (EXTRA) Models EA-300, EA-300S, and EA-300L airplanes. The proposed AD would require repetitively inspecting the rudder pedal for proper alignment, the safety control stop for wear and proper clearance, the rudder cables for elongation, and the rudder pedal footrest for cracks. The proposed AD would also require correcting or replacing any discrepant part, as applicable. The proposed AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by the proposed AD are intended to prevent failure of the rudder pedal footrest caused by overloading the rudder pedal safety control stop, which could result in loss of directional control of the airplane.

## Notices in this docket

- Sep 17, 1998: Notice of proposed rulemaking (NPRM). (first notice), FR document 98-24874, comments due Oct 16, 1998 (https://www.federalregister.gov/documents/1998/09/17/98-24874/airworthiness-directives-extra-flugzeugbau-gmbh-models-ea-300-ea-300s-and-ea-300l-airplanes)

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