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Mon, May 19, 2003

ADs: Rolls Royce

Rolls Royce Engines

Applicability: Rolls-Royce plc (RR) model RB211-535E4-37, RB211-535E4-B-37, and RB211-535E4-B-75 turbofan engines.

Requirement: removal from service of certain high pressure (HP) turbine discs before they reach newly established life limits.

Background: This amendment is prompted by the manufacturer's inspections and analysis of HP turbine discs that have accumulated high cycles. The actions specified by this AD are intended to prevent machining-induced cracking of the HP turbine disc which could cause an uncontained HP turbine disc failure and damage to the airplane.

FMI: http://ftp.atp.com/ADs/pdf/031003.pdf

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