AD 2000-24-24
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | Rolls-Royce | plc RB211 Trent 768-60 | Airworthiness Directives; Rolls-Royce plc RB211 Trent 768-60, Trent 772-60, and Trent 772B-60 Series Turbofan Engines |
Unsafe Condition
Cracking and detachment of inner skin, and cracks of outer skin on common nozzle assembly part number (P/N) FK16544 or FK16558, due to missing rivets, loose rivets, and high stress levels.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Visually inspect all common nozzle assemblies for cracks, missing rivets, and loose rivets within 500 flight hours after the effective date of this AD. Repeat inspections within 500 flight hours since the last inspection. Repair common nozzle assemblies that exceed allowable limits.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 500 flight hours after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Rolls-Royce plc RB211 Trent 768-60, Trent 772-60, and Trent 772B-60 series turbofan engines with common nozzle assembly part number (P/N) FK16544 or FK16558, installed on but not limited to Airbus A330-341 and A330-342 series 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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