AD 2001-24-14
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | DC-9-10 | Airworthiness Directives; McDonnell Douglas Model DC-9-10, -20, -30, -40, and -50 Series Airplanes; C-9 Airplanes; and Model DC-9-81, -82, -83, and -87 Series Airplanes |
Unsafe Condition
Loose terminal stud connections and consequent damage to the small copper terminals could result in overheating of the wires at the terminal strip, leading to electrical failure and potential smoke and fire in the electrical/electronic compartment.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the power feeder bus cables of the auxiliary power unit (APU) for overheat damage between certain fuselage stations. Take corrective action(s), if necessary, to repair or replace damaged cables.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
McDonnell Douglas Model DC-9-10, -20, -30, -40, and -50 series airplanes; C-9 airplanes; and Model DC-9-81, -82, -83, and -87 series airplanes, as listed in McDonnell Douglas Alert Service Bulletin DC9-24A072, Revision 01, dated May 22, 2000.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.