AD 88-15-05

final rule
Data completeness: 70%

Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -10F, -15, -30, -30F, -40, and KC-10A (Military) Series Airplanes

AD Number
88-15-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-10-10 Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -10F, -15, -30, -30F, -40, and KC-10A (Military) Series Airplanes
aircraft The Boeing Company DC-10-10F Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -10F, -15, -30, -30F, -40, and KC-10A (Military) Series Airplanes
aircraft The Boeing Company DC-10-15 Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -10F, -15, -30, -30F, -40, and KC-10A (Military) Series Airplanes
aircraft The Boeing Company DC-10-30 Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -10F, -15, -30, -30F, -40, and KC-10A (Military) Series Airplanes
aircraft The Boeing Company DC-10-30F (KC-10A, KDC-10) Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -10F, -15, -30, -30F, -40, and KC-10A (Military) Series Airplanes
aircraft The Boeing Company DC-10-40 Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -10F, -15, -30, -30F, -40, and KC-10A (Military) Series Airplanes

Unsafe Condition

Fire in the Center Accessory Compartment (CAC) due to arcing and/or corrosion of the battery ground stud installation or improper operation of the CAC drain valves.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect the battery ground stud installation for arcing/corrosion and check CAC drain valves for proper operation within 30 days after AD effective date, and every 60 days thereafter. Replace burnt/corroded ground stud parts and repair/replace non-functional drain valves before further flight. Replace main battery ground cable bracket within 90 days if Service Bulletin 24-73 not incorporated.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 30 days after the effective date of this AD, and thereafter at intervals not to exceed 60 days for inspections. Within 90 days after the effective date for replacing the main battery ground cable bracket if applicable.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

McDonnell Douglas DC-10-10, -10F, -15, -30, -30F, -40, and KC-10A (Military) series airplanes listed in Service Bulletin A24-141, Revision 1.

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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