AD 82-05-01 R2
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Embraer S.A. | EMB-110P1 | Airworthiness Directives: EMPRESA BRASILEIRA DE AERONAUTICA S/A (EMBRAER) Models EMB-110P1 and EMB-11OP2 Airplanes |
| aircraft | Embraer S.A. | EMB-110P2 | Airworthiness Directives: EMPRESA BRASILEIRA DE AERONAUTICA S/A (EMBRAER) Models EMB-110P1 and EMB-11OP2 Airplanes |
Unsafe Condition
Failure of wing flap actuators due to wear, damage, or improper lubrication of the threaded shaft, ballscrew/nut assembly, and sealing rings, which could lead to flap malfunction or damage to the mechanism.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect wing flap actuators within 50 hours time-in-service after March 1, 1982, and thereafter at intervals not exceeding 1500 landings or 12 months time-in-service. Replace or overhaul actuators if unsatisfactory, adjust control system to maintain minimum motor stop distances, and replace specific part numbers with updated models by September 30, 1982.
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Compliance Time
Within the next 50 hours time-in-service after March 1, 1982, and thereafter at intervals not to exceed 1500 landings or 12 months time-in-service, whichever occurs first.
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Affected Aircraft
Embraer S.A. Models EMB-110P1 and EMB-110P2 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 8, 2026
Rights: U.S. Government Public Domain
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