AD 2009-01-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Embraer | Various | Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP Airplanes |
Unsafe Condition
Failure to inspect some structural components, according to the new tasks and intervals for those modified aircraft, could prevent a timely detection of fatigue cracking. Undetected fatigue cracking in these components could adversely affect the structural integrity of these airplanes.
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Required Actions
Revise the Airworthiness Limitations Section, Structural Inspection Requirements Section, and Corrosion Prevention and Control Program Section of the Instructions for Continued Airworthiness to incorporate new structural inspection requirements.
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Compliance Time
Within 200 flight cycles after revising the Airworthiness Limitations Section, or from the initial delivery date of the airplane at the applicable time specified in the tasks, whichever occurs later.
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Affected Aircraft
Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP airplanes that have incorporated Embraer Service Bulletin 145-00-0032, including Revisions 01, 02, 03, and 04.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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