# Proposed AD FAA-2004-19897: Eagle Aircraft (Malaysia) Sdn. Bhd. Model Eagle 150B Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2005-05-14
- Products: Eagle Aircraft Pty.
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: January 12, 2005, 70 FR 2070
- Comments due: February 11, 2005
- Became: [AD 2005-05-14](https://openairdocs.org/ad/2005-05-14)
- Docket: FAA-2004-19897 (https://www.regulations.gov/docket/FAA-2004-19897, where comments are filed)
- Project: 2004-CE-45-AD
- FR document: 05-606
- Official PDF: https://openairdocs.org/files/sha256/a1/3d/a13dc7c5239a85308bfde018f4b67335b44b90f8685732ca05c23fefaef3309a (from https://www.govinfo.gov/content/pkg/FR-2005-01-12/pdf/05-606.pdf)
- Federal Register: https://www.federalregister.gov/documents/2005/01/12/05-606/airworthiness-directives-eagle-aircraft-malaysia-sdn-bhd-model-eagle-150b-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7D356FABF052865586256F87005F3FBC.0001
- Page: https://openairdocs.org/proposed/FAA-2004-19897

## Summary

The FAA proposes to adopt a new airworthiness directive (AD) for certain Eagle Aircraft (Malaysia) Sdn. Bhd. Model Eagle 150B airplanes. This proposed AD would require you to modify or replace the co-pilot rudder pedal assembly. This proposed AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Malaysia. We are issuing this proposed AD to prevent binding of the co-pilot rudder pedal assembly due to premature wear of the bushing, which could result in loss of co-pilot rudder and brake control. This failure could result in loss of control of the airplane.

## Notices in this docket

- Jan 12, 2005: Notice of proposed rulemaking (NPRM). (first notice), FR document 05-606, comments due Feb 11, 2005 (https://www.federalregister.gov/documents/2005/01/12/05-606/airworthiness-directives-eagle-aircraft-malaysia-sdn-bhd-model-eagle-150b-airplanes)

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