AD 2000-24-11

final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model MD-11 Series Airplanes

AD Number
2000-24-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2000-NM-31-AD
FR Citation
65 FR 75612

Applicability

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

Unsafe Condition

Chafing of electrical wire assemblies above the forward passenger doors, which could result in an electrical fire in the passenger compartment.

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

Required Actions

Inspect certain areas around the entry light connector of the sliding ceiling panel above the forward passenger doors for discrepancies and repair if necessary. For certain airplanes, install or modify a flapper door ramp deflector on the forward entry drop ceiling structure. For other airplanes, inspect the wire assembly support installation for evidence of chafing and take corrective actions if necessary. For certain airplanes, modify the support bracket for the ramp deflector assembly.

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

Compliance Time

Within 10 days after December 28, 1998 (effective date of AD 98-25-11), unless previously accomplished.

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

Affected Aircraft

McDonnell Douglas Model MD-11 series airplanes, as listed in McDonnell Douglas Alert Service Bulletin MD11-25A194, Revision 06, dated January 27, 2000, and MD11-24A068, Revision 01, dated March 8, 1999, 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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