AD 00-4929

final rule
Data completeness: 60%

Airworthiness Directives; Rolls-Royce plc 524 Series and Trent 768-60 and 772-60 Turbofan Engines

AD Number
00-4929
Status
final_rule
Effective Date
Product Category
engine
FR Citation
65 FR 12084

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce plc 524 Series and Trent 768-60 and 772-60 Airworthiness Directives; Rolls-Royce plc 524 Series and Trent 768-60 and 772-60 Turbofan Engines

Unsafe Condition

Failure of the joint bolt assemblies securing the high-pressure compressor (HPC) to the high-pressure turbine (HPT) could result in a cracked stage 6 HPC disk, possible uncontained engine failure, and damage to the airplane.

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

Required Actions

Replace the joint bolt assemblies that secure the HPC to the HPT. This action must be completed before further flight.

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

Compliance Time

Before further flight

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

Affected Aircraft

Rolls-Royce plc RB211-524G2-T-19, RB211-524G3-T-19, RB211-524H2-T-19, RB211 Trent 768-60, and RB211 Trent 772-60 turbofan engines.

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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