AD 93-18-02
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
Reduced directional control due to loss of the nose landing gear wheel during taxiing or landing.
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Required Actions
Modify the nose landing gear wheels in accordance with Airbus Industrie Service Bulletin No. A320-32-1061, Revision 3, dated October 19, 1992. An alternative method of compliance or adjustment of the compliance time may be used if approved by the FAA. Special flight permits may be issued under FAR 21.197 and 21.199 to operate the airplane to a location where the AD requirements can be accomplished.
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Compliance Time
Within 4 months after the effective date of this AD
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Affected Aircraft
AIRBUS INDUSTRIE Model A320-111, -211, and -231 series airplanes listed in Airbus Industrie Service Bulletin No. A320-32-1061, Revision 3, dated October 19, 1992.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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