AD 2000-15-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 747-200 and -300 | Airworthiness Directives; Boeing Model 747-200 and -300 Series Airplanes Equipped with General Electric CF6-80C2 Series Engines |
| engine | General Electric | CF6-80C2 Series | Airworthiness Directives; Boeing Model 747-200 and -300 Series Airplanes Equipped with General Electric CF6-80C2 Series Engines |
Unsafe Condition
Possible failure modes in the thrust reverser control system that can result in inadvertent deployment of a thrust reverser during flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install a terminating modification, perform repetitive functional tests of the installation, and repair if necessary. Retain original requirements of AD 95-06-01, including repetitive tests and inspections of the thrust reverser system components.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 90 days after April 13, 1995, for the original requirements. Compliance for new requirements is not specified.
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Affected Aircraft
Boeing Model 747-200 and -300 series airplanes equipped with General Electric CF6-80C2 series engines with Power Management Control engine controls.
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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