AD 2001-24-14

final rule
Data completeness: 70%

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

AD Number
2001-24-14
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 99-NM-291-AD
FR Citation
66 FR 64135

Applicability

TypeManufacturerModelDetails
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

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