AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 2003-19-07 68 FR 55191 Active

Federal Aviation Administration · 14 CFR part 39

FR document
03-23677
Amendment
39-13310
Published
2003-09-23
Effective
2003-11-03
Models covered
1
Last live check
2026-10-02

Printed from https://aircraftdirectives.com/ad/2003-19-07 · 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.

Opens your browser's print dialog. Choose “Save as PDF” to export a file. Keyboard: Ctrl+P or Cmd+P.

AD

2003-19-07

FR doc 03-23677 · 68 FR 55191

AD 2003-19-07Published 2003-09-23Effective 2003-11-03

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 canard rear spar and the rear spar attachment bracket.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Eagle Aircraft (Malaysia) Sdn. Bhd. (Eagle) Model 150B airplanes. This AD requires you to modify the canard rear spar and the rear spar attachment bracket. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Australia. The type design responsibility has been transferred from Australia to Malaysia since the release of the MCAI. The actions specified by this AD are intended to prevent detachment of the rear spar bracket from the canard rear spar, which could result in failure of the canard rear spar. Such failure could lead to 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 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

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 1 model in our index