Airworthiness Directive

AD 2002-02-01 67 FR 5043 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-2318
Amendment
39-12629
Published
2002-02-04
Effective
2002-03-21
Models covered
1
Last live check
2026-10-02
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AD

2002-02-01

FR doc 02-2318 · 67 FR 5043

AD 2002-02-01Published 2002-02-04Effective 2002-03-21

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 the attachment of the port and starboard throttle arms, and the starboard bushing of the throttle torque tube.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Eagle Aircraft Pty. Ltd. (Eagle) Model 150B airplanes. This AD requires you to modify the attachment of the port and starboard throttle arms, and the starboard bushing of the throttle torque tube. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Australia. The actions specified by this AD are intended to prevent failure of the throttle control assembly caused by rivets of the wrong size. Such failure could lead to reduced 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 2005-05-14 Airworthiness Directives; Eagle Aircraft (Malaysia) Sdn. Bhd. Model Eagl... 2005-03-10
  4. AD 2004-26-01 Airworthiness Directives; Eagle Aircraft (Malaysia) Sdn. Bhd. Model Eagl... 2004-12-22
  5. AD 2004-11-04 Airworthiness Directives; Eagle Aircraft (Malaysia) Sdn. Bhd Model Eagle... 2004-05-27

All Eagle 150B directives

Applies to 1 model in our index