AD 2003-15-09

final rule
Data completeness: 70%

Airworthiness Directives; Rolls-Royce plc Trent 768-60, Trent 772-60, and Trent 772B-60 Turbofan Engines

AD Number
2003-15-09
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2003-NE-28-AD
FR Citation
68 FR 46444

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce plc Trent 768-60 Airworthiness Directives; Rolls-Royce plc Trent 768-60, Trent 772-60, and Trent 772B-60 Turbofan Engines

Unsafe Condition

Reports of low power surges indicate larger than anticipated high pressure compressor (HPC) tip clearances, leading to reduced surge margin and potential dual-engine in-flight surge, which could result in loss of control of the airplane.

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Required Actions

Perform initial surge margin testing using Rolls-Royce plc Service Bulletin No. RB.211-71-D509, Revision 2, for engines with specific cycle counts. Conduct repetitive surge margin testing at intervals not exceeding 130 cycles-since-last test.

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Compliance Time

Before further flight for engines with specified cycle counts; repetitive testing within 130 cycles-since-last test.

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Affected Aircraft

Rolls-Royce plc Trent 768-60, Trent 772-60, and Trent 772B-60 turbofan engines installed on, but not limited to, Airbus 330 series airplanes.

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Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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