AD 91-02-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320-111 | Airworthiness Directives; AIRBUS INDUSTRIE Model A320-111, -211, and -231 Series Airplanes |
| aircraft | Airbus | A320-211 | Airworthiness Directives; AIRBUS INDUSTRIE Model A320-111, -211, and -231 Series Airplanes |
| aircraft | Airbus | A320-231 | Airworthiness Directives; AIRBUS INDUSTRIE Model A320-111, -211, and -231 Series Airplanes |
Unsafe Condition
Failure of the landing gear to retract following takeoff due to a defect in relay 48GA's energization system.
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Required Actions
Install wiring and electronic components in relay 48GA's energization system per Airbus Service Bulletin A320-32-1035 Rev 2 or A320-32-1048 Rev 1. Alternate compliance may be approved by the FAA's Standardization Branch. Special flight permits under FAR 21.197/21.199 may be issued for AD compliance operations.
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Compliance Time
within 45 days after the effective date of this AD
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Affected Aircraft
All Model A320-111, -211, and -231 series 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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