Airworthiness Directive

AD 2005-05-14 70 FR 11846 Active

Federal Aviation Administration · 14 CFR part 39

FR document
05-4554
Amendment
39-14003
Published
2005-03-10
Effective
2005-04-22
Models covered
1
Last live check
2026-10-02
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AD

2005-05-14

FR doc 05-4554 · 70 FR 11846

AD 2005-05-14Published 2005-03-10Effective 2005-04-22

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 modify or replace the co-pilot rudder pedal assembly.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for certain Eagle Aircraft (Malaysia) Sdn. Bhd. Model Eagle 150B airplanes. This AD requires you to modify or replace the co-pilot rudder pedal assembly. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Malaysia. We are issuing this 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.

More directives for Eagle 150B

  1. AD 2007-23-06 Airworthiness Directives; CTRM Aviation Sdn. Bhd. (Formerly Eagle Aircra... 2007-11-06
  2. AD 2007-04-02 Airworthiness Directives; CTRM Aviation Sdn. Bhd. (Formerly Eagle Aircra... 2007-02-14
  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