AD 2006-26-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 777-200 and -300 | Airworthiness Directives; Boeing Model 777-200 and -300 Series Airplanes Equipped with Rolls-Royce Engines |
| engine | Rolls-Royce | engines | Airworthiness Directives; Boeing Model 777-200 and -300 Series Airplanes Equipped with Rolls-Royce Engines |
Unsafe Condition
Cracks in the outer V-blades of the thrust reverser, which could lead to separation of the thrust reverser from the airplane during normal reverse thrust or refused takeoff, potentially causing impact damage to other airplane areas and unexpected thrust asymmetry.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the outer V-blades of the thrust reverser for cracks, replace cracked V-blades with serviceable parts, and send inspection results to Boeing. Repetitive inspections are required with intervals not exceeding 2,000 flight cycles from the last detailed inspection. Optional terminating action is provided to eliminate repetitive inspections.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 250 to 6,000 flight cycles after the effective date of the AD, depending on the number of flight cycles on the V-blade.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Boeing Model 777-200 and -300 series airplanes equipped with Rolls-Royce engines.
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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