AD 2008-23-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Embraer | Various | Airworthiness Directives; Empresa Brasileira de Aeronautica S. A. (EMBRAER) Models EMB-110P1 and EMB-110P2 Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Empresa Brasileira de Aeronautica S. A. (EMBRAER) Models EMB-110P1 and EMB-110P2 Airplanes |
Unsafe Condition
Corrosion at the regions of Wings-to-Fuselage attachments, Vertical Stabilizer to Fuselage attachments, Rib 1 Half-wing, and Passenger Seat Tracks may lead to cracking of the affected parts, compromising aircraft structural integrity, which may result in structural failure and/or loss of some control surface.
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Required Actions
Within 30 days or 100 flight hours after the effective date, carry out a general visual inspection for corrosion at specified regions, following Embraer Service Bulletin S.B. No.: 110-00-0007, Revision No.: 01. Remove detected corrosion before further flight.
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Compliance Time
Within 30 days or 100 flight hours after December 22, 2008, whichever occurs first.
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Affected Aircraft
EMBRAER Models EMB-110P1 and EMB-110P2 airplanes, all serial numbers, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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