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AD FAA-2013-0143

Airworthiness Directives; Rolls-Royce plc Turbofan Engines

Summary

We are adopting a new airworthiness directive (AD) for certain Rolls-Royce plc (RR) RB211-524B-02; -524B2-19; -524B3-02; -524B4-02; - 524C2-19; -524D4-19; -524D4-B-19; -524D4-39; -535C-37; -535E4-37; - 535E4-B-37, and -535E4-B-75 turbofan engines, and all RB211-524G2-19; - 524G3-19; -524H2-19; and -524H-36 turbofan engines. This AD requires a one-time inspection of the front combustion liner (FCL) metering panel to determine if it is made from N75 material and, if so, replacing it with an FCL made from C263 material. This AD was prompted by the discovery of a cracked and distorted FCL metering panel, which was made from N75 material. We are issuing this AD to prevent hot gases from burning through the engine casing, which could result in an under-cowl fire and damage to the airplane.

Directive Details

AD Number

FAA-2013-0143

Document Number

2013-21109

Type

Rule

Publication Date

September 3, 2013

Effective Date

October 8, 2013

Affected Manufacturer

Rolls-Royce plc Turbofan

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2013-0143

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Rolls-Royce plc Turbofan →

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