# Proposed AD 2000-CE-23-AD: Eagle Aircraft (Malaysia) Sdn. Bhd. Model 150B Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2003-19-07
- Products: Eagle Aircraft Pty.
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: June 23, 2003, 68 FR 37102
- Comments due: July 25, 2003
- Became: [AD 2003-19-07](https://openairdocs.org/ad/2003-19-07)
- Docket: 2000-CE-23-AD
- FR document: 03-15726
- Official PDF: https://openairdocs.org/files/sha256/f9/ed/f9ed27cca7168d2b1f92097c639f7477d95cd4e69de4b0b5e8acf291bbfd0ab8 (from https://www.govinfo.gov/content/pkg/FR-2003-06-23/pdf/03-15726.pdf)
- Federal Register: https://www.federalregister.gov/documents/2003/06/23/03-15726/airworthiness-directives-eagle-aircraft-malaysia-sdn-bhd-model-150b-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E0B1AB508CFFDA2386256D4E0056743C.0001
- Page: https://openairdocs.org/proposed/2000-CE-23-AD

## Summary

This document proposes to adopt a new airworthiness directive (AD) that would apply to certain Eagle Aircraft (Malaysia) Sdn. Bhd. (Eagle) Model 150B airplanes. This proposed AD would require you to modify the canard rear spar and the rear spar attachment bracket. This proposed AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Australia. The type design responsibility has been transferred from Australia to Malaysia since the release of the MCAI. The actions specified by this proposed AD are intended to prevent detachment of the rear spar bracket from the canard rear spar, which could result in failure of the canard rear spar. Such failure could lead to loss of control of the airplane.

## Notices in this docket

- Jun 23, 2003: Notice of proposed rulemaking (NPRM). (first notice), FR document 03-15726, comments due Jul 25, 2003 (https://www.federalregister.gov/documents/2003/06/23/03-15726/airworthiness-directives-eagle-aircraft-malaysia-sdn-bhd-model-150b-airplanes)

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