AD 97-09-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A310-203 | Airworthiness Directives; Airbus Model A310 Series Airplanes |
| aircraft | Airbus | A310-221 | Airworthiness Directives; Airbus Model A310 Series Airplanes |
| aircraft | Airbus | A310-222 | Airworthiness Directives; Airbus Model A310 Series Airplanes |
| aircraft | Airbus | A310-304 | Airworthiness Directives; Airbus Model A310 Series Airplanes |
| aircraft | Airbus | A310-322 | Airworthiness Directives; Airbus Model A310 Series Airplanes |
| aircraft | Airbus | A310-324 | Airworthiness Directives; Airbus Model A310 Series Airplanes |
| aircraft | Airbus | A310-325 | Airworthiness Directives; Airbus Model A310 Series Airplanes |
Unsafe Condition
Chafing of wire bundles 626VB, 628VB, and 632VB for the hydraulic fire shutoff valves to the right engine could lead to short circuiting and inability to close these valves in the event of fire.
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Required Actions
Modify the wiring for hydraulic fire shutoff valves in wire bundles 626VB, 628VB, and 632VB according to Airbus Service Bulletin A310-24-2065 or Revision 1. Submit alternative compliance requests through an FAA Principal Maintenance Inspector.
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Compliance Time
Within 60 days after the effective date of this AD (May 29, 1997).
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Affected Aircraft
Airbus Model A310 series airplanes listed in Airbus Service Bulletin A310-24-2065, dated November 30, 1995, and Revision 1, dated April 19, 1996.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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