AD 95-26-06

final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model MD-11 Series Airplanes

AD Number
95-26-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
95-NM-245-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company MD-11 Airworthiness Directives; McDonnell Douglas Model MD-11 Series Airplanes
aircraft The Boeing Company MD-11F Airworthiness Directives; McDonnell Douglas Model MD-11 Series Airplanes

Unsafe Condition

Improper wiring of the fuel system control panel (FSCP) could lead to degradation of the automatic landing system during flight due to a single short of one DC electrical bus affecting the remaining bus.

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

Required Actions

Within 15 days after the effective date, either revise the AFM to prohibit autoland below 100 feet AGL or open/collar circuit breaker B1-458. Conduct a one-time FSCP inspection, and re-identify, modify, or replace the FSCP if needed. Submit inspection results to the FAA.

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

Compliance Time

Within 15 days after the effective date of this AD

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

Affected Aircraft

McDonnell Douglas Model MD-11 series airplanes, manufacturer's fuselage numbers 0447 through 0593 inclusive

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.

View Official Source ↗ Find More ADs for The Boeing Company MD-11

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