Skip to content

Emergency ADRule

AD FAA-2008-0975

Airworthiness Directives; Rolls-Royce Corporation (RRC) AE 3007A Series Turbofan Engines

Summary

This document publishes in the Federal Register an amendment adopting emergency airworthiness directive (AD) 2009-08-51 that was sent previously to all known U.S. owners and operators of RRC AE 3007A series turbofan engines. This AD requires performing an eddy current inspection (ECI) or surface wave ultrasonic test (SWUT) inspection on each affected high-pressure turbine wheel. This AD results from additional reports of cracks in the high-pressure turbine (HPT) stage 2 wheels identified from the required inspections in AD 2008-26-06. A revised risk assessment that includes these additional reports indicates we need to require a higher inspection rate. We are issuing this AD to prevent an uncontained failure of the HPT stage 2 wheel and damage to the airplane.

Directive Details

AD Number

FAA-2008-0975

Document Number

E9-11126

Type

Rule

Publication Date

May 12, 2009

Effective Date

May 27, 2009

Affected Manufacturer

Rolls-Royce Corporation (RRC) AE 3007A Series Turbofan

Criticality

critical

Emergency

Yes

Docket ID

Docket No. FAA-2008-0975

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Rolls-Royce Corporation (RRC) AE 3007A Series Turbofan →

Automated AD compliance tracking

AeroCopilot matches ADs to your aircraft and tracks compliance status. Included in every plan from $9.99 monthly.

3 sections gated

Unlock AD-to-aircraft matching, compliance tracking, recurrence schedule with a free AeroCopilot account.

Sign up free to unlock AD-to-aircraft matching, compliance tracking, recurrence schedule

Free forever · No credit card · Sourced directly from FAA & NOAA pipelines