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Airworthiness Directive

AD 2004-11-04 69 FR 30189 Superseded

Federal Aviation Administration · 14 CFR part 39

Requires you to inspect certain canard inboard flap hinge support brackets (initially prior to further flight and repetitively before the first flight of each day) and perform any necessary follow-up action.

Superseded by AD 2007-04-02Federal Register (opens in a new tab)

FR document
04-11876
Amendment
39-13649
Published
2004-05-27
Effective
2004-06-04
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2004-11-04 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

2004-11-04

FR doc 04-11876 · 69 FR 30189

AD 2004-11-04Published 2004-05-27Effective 2004-06-04

Superseded by 2007-04-02

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires you to inspect certain canard inboard flap hinge support brackets (initially prior to further flight and repetitively before the first flight of each day) and perform any necessary follow-up action.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for all Eagle Aircraft (Malaysia) Sdn. Bhd (Eagle Aircraft) Model Eagle 150B airplanes. This AD requires you to inspect certain canard inboard flap hinge support brackets (initially prior to further flight and repetitively before the first flight of each day) and perform any necessary follow-up action. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authorities for Australia and Malaysia. We are issuing this AD to prevent failure of the canard inboard flap hinge support brackets caused by undetected cracks. This failure could result in asymmetric flap deployment and the inability to lower or raise the flaps with consequent loss of control of the airplane.

More directives for Eagle 150B

  1. AD 2007-23-06 Airworthiness Directives; CTRM Aviation Sdn. Bhd. (Formerly Eagle Aircra... Effective 2007-12-11
  2. AD 2007-04-02 Airworthiness Directives; CTRM Aviation Sdn. Bhd. (Formerly Eagle Aircra... Effective 2007-03-21
  3. AD 2005-05-14 Airworthiness Directives; Eagle Aircraft (Malaysia) Sdn. Bhd. Model Eagl... Effective 2005-04-22
  4. AD 2004-26-01 Airworthiness Directives; Eagle Aircraft (Malaysia) Sdn. Bhd. Model Eagl... Effective 2005-01-31
  5. AD 2003-19-07 Airworthiness Directives; Eagle Aircraft (Malaysia) Sdn. Bhd. Model 150B... Effective 2003-11-03

All Eagle 150B directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 2004-11-04 (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index