AD 2004-23-03

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Rolls-Royce plc RB211 Trent 700 Series Turbofan Engines

AD Number
2004-23-03
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2004-19559
FR Citation
69 FR 64653

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce plc RB211 Trent 700 Series Airworthiness Directives; Rolls-Royce plc RB211 Trent 700 Series Turbofan Engines

Unsafe Condition

Internal oil fire in the HP-IP turbine oil vent tubes due to coking and carbon buildup, leading to disk shaft separation, overspeed of the IP turbine rotor, and multiple blade release of IP turbine blades.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Initial and repetitive borescope inspections of the HP-IP turbine oil vent tubes for coking and carbon buildup. Cleaning or replacing the oil vent tubes if they fail the inspection.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 50 flight hours after the effective date of the 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, RB211 Trent 772-60, and RB211 Trent 772B-60 series turbofan engines installed on, but not limited to, Airbus A330-243, -341, -342, and -343 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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