AD 92-19-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | DC-9-81 (MD-81) | Airworthiness Directives; MCDONNELL DOUGLAS DC-9-81, -82, -83, and -87 (MD-81, -82, -83, and -87) Series Airplanes, and MD-88 Airplanes |
| aircraft | The Boeing Company | DC-9-82 (MD-82) | Airworthiness Directives; MCDONNELL DOUGLAS DC-9-81, -82, -83, and -87 (MD-81, -82, -83, and -87) Series Airplanes, and MD-88 Airplanes |
| aircraft | The Boeing Company | DC-9-83 (MD-83) | Airworthiness Directives; MCDONNELL DOUGLAS DC-9-81, -82, -83, and -87 (MD-81, -82, -83, and -87) Series Airplanes, and MD-88 Airplanes |
| aircraft | The Boeing Company | DC-9-87 (MD-87) | Airworthiness Directives; MCDONNELL DOUGLAS DC-9-81, -82, -83, and -87 (MD-81, -82, -83, and -87) Series Airplanes, and MD-88 Airplanes |
| aircraft | The Boeing Company | MD-88 | Airworthiness Directives; MCDONNELL DOUGLAS DC-9-81, -82, -83, and -87 (MD-81, -82, -83, and -87) Series Airplanes, and MD-88 Airplanes |
Unsafe Condition
Chafing damage to the galley power feeder wire assemblies could lead to arcing and smoke in the passenger cabin.
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Required Actions
Inspect the galley power feeder wire assemblies per McDonnell Douglas Alert Service Bulletin A24-132, Revision 1. If damage is found, repair the damaged wire insulator with protective sleeving before further flight and modify the assemblies within 6,000 flight hours. If no damage, modify the assemblies within 15,000 total flight hours or 6,000 flight hours after initial inspection, whichever is later.
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Compliance Time
Prior to or upon the accumulation of 9,000 total flight hours or within 6 months after the effective date of this AD, whichever occurs later.
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Affected Aircraft
Model DC-9-81, -82, -83, -87 (MD-81, -82, -83, -87) series airplanes, and Model MD-88 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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