AD 93-07-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A310-203 | Airworthiness Directives; AIRBUS INDUSTRIE Model A310 Series Airplanes |
| aircraft | Airbus | A310-221 | Airworthiness Directives; AIRBUS INDUSTRIE Model A310 Series Airplanes |
| aircraft | Airbus | A310-222 | Airworthiness Directives; AIRBUS INDUSTRIE Model A310 Series Airplanes |
| aircraft | Airbus | A310-304 | Airworthiness Directives; AIRBUS INDUSTRIE Model A310 Series Airplanes |
| aircraft | Airbus | A310-322 | Airworthiness Directives; AIRBUS INDUSTRIE Model A310 Series Airplanes |
| aircraft | Airbus | A310-324 | Airworthiness Directives; AIRBUS INDUSTRIE Model A310 Series Airplanes |
| aircraft | Airbus | A310-325 | Airworthiness Directives; AIRBUS INDUSTRIE Model A310 Series Airplanes |
Unsafe Condition
Wing tip brake valve failure, which could lead to reduced controllability of the airplane.
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Required Actions
Conduct an integrity test to detect corrosion of the wing tip brake solenoids within 350 flight hours after the effective date. Repeat the test at intervals not exceeding 350 flight hours. Replace corroded solenoids with part number 500A00003-03 before further flight. Install Modification 6725 as terminating action.
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Compliance Time
Within 350 flight hours after the effective date of this AD
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Affected Aircraft
AIRBUS INDUSTRIE Model A310 series airplanes on which Modification 6725 has not been accomplished, including models A310-203, A310-221, A310-222, A310-304, A310-322, A310-324, A310-325.
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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