AD 2001-17-19
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | DC-10 | Airworthiness Directives; McDonnell Douglas Model DC-10 Series Airplanes, and KC-10A and KDC-10 (Military) Airplanes |
Unsafe Condition
Current thrust reverser systems do not adequately preclude unwanted deployment of a thrust reverser, which could significantly jeopardize continued safety of flight and landing of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the thrust reverser control and indication system and wiring on each engine. Install an additional locking system for the thrust reverser control system.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 5 years after the effective date of this AD for the thrust reverser wiring modification and installation of an additional locking system. Within 24 months or 12,000 flight hours after the effective date of this AD for the thrust reverser health checks and other modifications specified in paragraph (a).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All McDonnell Douglas Model DC-10 series airplanes, and KC-10A and KDC-10 (military) airplanes.
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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