# Proposed AD FAA-2006-23786: CTRM Aviation Sdn. Bhd. (Formerly Eagle Aircraft (Malaysia) Sdn. Bhd.) Model Eagle 150B Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2007-04-02
- Products: CTRM Aviation SDN. BHD.
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: July 11, 2006, 71 FR 39020
- Comments due: August 10, 2006
- Became: [AD 2007-04-02](https://openairdocs.org/ad/2007-04-02)
- Docket: FAA-2006-23786 (https://www.regulations.gov/docket/FAA-2006-23786, where comments are filed)
- Project: 2006-CE-11-AD
- FR document: E6-10773
- Official PDF: https://openairdocs.org/files/sha256/e9/0e/e90e5f1f26947269c49348028a1abcda5c6515161b3c27d4d317c6db1fb1a601 (from https://www.govinfo.gov/content/pkg/FR-2006-07-11/pdf/E6-10773.pdf)
- Federal Register: https://www.federalregister.gov/documents/2006/07/11/E6-10773/airworthiness-directives-ctrm-aviation-sdn-bhd-formerly-eagle-aircraft-malaysia-sdn-bhd-model-eagle
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1324621D2E3780BE862571A8005AC3DE.0001
- Page: https://openairdocs.org/proposed/FAA-2006-23786

## Summary

The FAA proposes to supersede Airworthiness Directive (AD) 2004-11-04, which applies to all CTRM Aviation Sdn. Bhd. (Formerly Eagle Aircraft (Malaysia) Sdn. Bhd.) Model Eagle 150B airplanes. AD 2004-11-04 currently requires you to inspect certain canard inboard flap hinge support brackets (initially before further flight and repetitively before the first flight of each day) and perform any necessary follow-up action. This proposed AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Malaysia to require the installation of improved design inboard flap hinge brackets as terminating action for the repetitive inspections. Consequently, this proposed AD would initially retain the requirement that you inspect certain canard inboard flap hinge support brackets (initially before further flight and repetitively before the first flight of each day) and then require that you replace the parts with new design inboard flap hinge brackets as terminating action for the repetitive inspections or if cracks are found. We are issuing this proposed AD to detect and correct cracks in the canard inboard flap hinge support brackets, which could result in loss of retention of controls and consequently, loss of airplane control.

## Notices in this docket

- Jul 11, 2006: Notice of proposed rulemaking (NPRM). (first notice), FR document E6-10773, comments due Aug 10, 2006 (https://www.federalregister.gov/documents/2006/07/11/E6-10773/airworthiness-directives-ctrm-aviation-sdn-bhd-formerly-eagle-aircraft-malaysia-sdn-bhd-model-eagle)

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