AD 83-04-03 R1
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Embraer S.A. | EMB-110P1 | Airworthiness Directives; EMBRAER Models EMB-110P1 and EMB-110P2 Airplanes |
| aircraft | Embraer S.A. | EMB-110P2 | Airworthiness Directives; EMBRAER Models EMB-110P1 and EMB-110P2 Airplanes |
Unsafe Condition
Loss of airplane control in the event of a control wheel failure
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Required Actions
Operate with a minimum flight crew of two immediately. Within 10 hours time-in-service after the effective date, insert a temporary AFM revision in the Limitations Section, paragraph 2-19, specifying two pilots for all operations. Conduct an inspection of the control wheel installation per EMBRAER Alert Service Bulletin No. 110-027-A070 to verify part numbers 111A-500-10-01-10-01 or 110-500-10-01-10-04 are installed at both crew stations, which may exempt paragraphs a) and b).
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Compliance Time
Effective immediately for paragraph a), and within 10 hours time-in-service after the effective date for paragraph b)
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Affected Aircraft
Embraer S.A. Models EMB-110P1 and EMB-110P2 airplanes certificated in any category
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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