AD 2005-04-03

final rule
Data completeness: 80%

Airworthiness Directives; Boeing Model 747-400, -400D, and -400F Series Airplanes

AD Number
2005-04-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2004-18999
FR Citation
70 FR 8239

Applicability

TypeManufacturerModelDetails
aircraft Boeing 747-400 Airworthiness Directives; Boeing Model 747-400, -400D, and -400F Series Airplanes

Unsafe Condition

Disengagement of all three flap control units (FCUs) at the same time, leading to loss of primary flaps control and flaps indication display.

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

Required Actions

Replace at least one flap control unit (FCU) in the main equipment center with a new or modified FCU, in accordance with Boeing Alert Service Bulletin 747-27A2386, dated March 13, 2003. Concurrently, perform actions specified in Boeing Service Bulletin 747-27-2319, dated January 24, 1991.

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

Compliance Time

Within 60 months after the effective date of the final rule (March 25, 2005).

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

Affected Aircraft

Boeing Model 747-400, -400D, and -400F series airplanes.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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