AD 96-06-06

final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 747-100, -200, -300, and SP Series Airplanes

AD Number
96-06-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
95-NM-22-AD
FR Citation
(Federal Register: March 21, 1996 (Volume 61, Number 56))

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 747-100 Series Airworthiness Directives; Boeing Model 747-100, -200, -300, and SP Series Airplanes
aircraft The Boeing Company 747-100B Series Airworthiness Directives; Boeing Model 747-100, -200, -300, and SP Series Airplanes
aircraft The Boeing Company 747-100B SUD Series Airworthiness Directives; Boeing Model 747-100, -200, -300, and SP Series Airplanes
aircraft The Boeing Company 747-200B Series Airworthiness Directives; Boeing Model 747-100, -200, -300, and SP Series Airplanes
aircraft The Boeing Company 747-200C Series Airworthiness Directives; Boeing Model 747-100, -200, -300, and SP Series Airplanes
aircraft The Boeing Company 747-200F Series Airworthiness Directives; Boeing Model 747-100, -200, -300, and SP Series Airplanes
aircraft The Boeing Company 747-300 Series Airworthiness Directives; Boeing Model 747-100, -200, -300, and SP Series Airplanes
aircraft The Boeing Company 747SP Series Airworthiness Directives; Boeing Model 747-100, -200, -300, and SP Series Airplanes

Unsafe Condition

Failure of the flightcrew to be aware of the configuration of the autoland system during landing when a change occurs from fail-operational to fail-passive mode.

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Required Actions

Revise the Airplane Flight Manual (AFM) to include a warning about NAV receiver flags and autopilot disconnection; install a diode and marker on specified shelves and make wiring changes to the flight mode annunciator; perform operational tests after installation and every 20,000 flight hours.

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Compliance Time

Within 3 months after the effective date of this AD for AFM revision, and within 18 months after the effective date for installation and wiring changes. Operational tests must be done before further flight after installation and repeated every 20,000 flight hours.

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Affected Aircraft

Boeing Model 747-100, -200, -300, and SP series airplanes equipped with triple channel autoland autopilots, as listed in Boeing Alert Service Bulletins 747-22A2212 and 747-22A2213.

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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