AD 2003-08-01

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Rolls-Royce Deutschland Ltd. & Co KG, Model Tay 650-15 Turbofan Engines

AD Number
2003-08-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2003-NE-06-AD
FR Citation
68 FR 18103

Applicability

TypeManufacturerModelDetails
engine Rolls-Royce Deutschland Ltd Airworthiness Directives; Rolls-Royce Deutschland Ltd. & Co KG, Model Tay 650-15 Turbofan Engines

Unsafe Condition

Excessive corrosion on low pressure (LP) turbine stage 2 rotor discs and LP turbine stage 3 rotor discs may lead to uncontained rotor disc failure and damage to the airplane.

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

Required Actions

Initial and repetitive visual inspections of LP turbine stage 2 and stage 3 rotor discs for corrosion are required.

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 Deutschland Ltd. & Co KG Model Tay 650-15 turbofan engines, specific serial numbers as listed in the AD.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.