Airworthiness Directive

AD 2007-04-02 72 FR 6928 Active

Federal Aviation Administration · 14 CFR part 39

FR document
E7-2319
Amendment
39-14933
Published
2007-02-14
Effective
2007-03-21
Models covered
1
Last live check
2026-10-02
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AD

2007-04-02

FR doc E7-2319 · 72 FR 6928

AD 2007-04-02Published 2007-02-14Effective 2007-03-21

Supersedes 2004-11-04

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 before 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) to supersede 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 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 AD retains 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 requires 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 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.

More directives for Eagle 150B

  1. AD 2007-23-06 Airworthiness Directives; CTRM Aviation Sdn. Bhd. (Formerly Eagle Aircra... 2007-11-06
  2. AD 2005-05-14 Airworthiness Directives; Eagle Aircraft (Malaysia) Sdn. Bhd. Model Eagl... 2005-03-10
  3. AD 2004-26-01 Airworthiness Directives; Eagle Aircraft (Malaysia) Sdn. Bhd. Model Eagl... 2004-12-22
  4. AD 2004-11-04 Airworthiness Directives; Eagle Aircraft (Malaysia) Sdn. Bhd Model Eagle... 2004-05-27
  5. AD 2003-19-07 Airworthiness Directives; Eagle Aircraft (Malaysia) Sdn. Bhd. Model 150B... 2003-09-23

All Eagle 150B directives

Applies to 1 model in our index