AD 2003-24-09

final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model MD-11 and -11F Airplanes

AD Number
2003-24-09
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2003-NM-70-AD
FR Citation
68 FR 67796

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas MD-11 and -11F Airworthiness Directives; McDonnell Douglas Model MD-11 and -11F Airplanes

Unsafe Condition

Chafing and arcing of the parallel feeder cables of the number 2 integrated drive generator (IDG), which could result in smoke and/or fire in the right aft galley area.

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

Required Actions

Perform a general visual inspection to detect chafing or damage of the parallel power feeder cables of the number 2 IDG. If no chafing or damage is detected, reposition the cables before further flight. If chafing or damage is detected, repair the chafed cable and damaged structure, and reposition the cables before further flight.

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

Compliance Time

Within 6 months after the effective date of this AD or AD 2001-17-08, depending on the group of affected airplanes.

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

Affected Aircraft

McDonnell Douglas Model MD-11 and -11F airplanes, as listed in Boeing Alert Service Bulletin MD11-24A157, Revision 01, dated March 11, 2003; certificated in any category.

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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