AD 2010-11-14
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Embraer | Various | Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 190-100 STD, -100 LR, -100 IGW, -200 STD, -200 LR, and -200 IGW Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 190-100 STD, -100 LR, -100 IGW, -200 STD, -200 LR, and -200 IGW Airplanes |
Unsafe Condition
Cracks were found in some structural components during full-scale fatigue testing of ERJ 190 airplanes. Failure to inspect these components according to new tasks, thresholds, and intervals could lead to undetected fatigue cracks, adversely affecting structural integrity.
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Required Actions
Revise the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness (ICA) to include new and modified structural inspections as specified in EMBRAER Temporary Revisions (TR) 2-5 and 2-6. Insert these revisions within 90 days after the effective date of the AD.
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Compliance Time
Within 90 days after the effective date of the AD.
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Affected Aircraft
Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 190-100 STD, -100 LR, -100 IGW, -200 STD, -200 LR, and -200 IGW airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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