AD 2001-17-03

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes

AD Number
2001-17-03
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2001-NM-248-AD
FR Citation
66 FR 43766

Applicability

TypeManufacturerModelDetails
aircraft Embraer EMB-135 and -145 Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes

Unsafe Condition

Internal corrosion of the engine thrust reverser stow/transit switches could cause erroneous signals in the Engine Indicating and Crew Alerting System (EICAS), leading to uncommanded loss of engine power in flight or unnecessary aborted takeoffs on the ground.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect the engine thrust reverser stow/transit switches for internal corrosion using a megohmmeter for insulation resistance. Take corrective action if corrosion is found. Repeat inspections every 1,200 flight hours after the initial inspection.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 1,200 flight hours after the initial inspection.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

All EMBRAER Model EMB-135 and -145 series airplanes, certificated in any category.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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