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AD FAA-2007-0108

Airworthiness Directives; CFM International, S.A. CFM56-5C4/1 Series Turbofan Engines

Summary

The FAA is superseding an existing airworthiness directive (AD) for CFM International, S.A. CFM56-5C4/1 series turbofan engines. That AD currently requires that the low pressure turbine (LPT) conical support, part number (P/N) 337-002-407-0, be removed from service at or before reaching the cyclic life limit of 9,350 cycles-since-new (CSN). This AD requires that the same P/N LPT conical support be removed from service before reaching the new, relaxed cyclic life limit of 20,000 CSN. This AD results from CFM International, S.A. performing a life extension study of the LPT conical support, P/N 337-002-407-0. We are issuing this AD to prevent LPT conical supports from remaining in service beyond their certified cyclic life limit, which could result in an uncontained engine failure and damage to the airplane.

Directive Details

AD Number

FAA-2007-0108

Document Number

E7-22647

Type

Rule

Publication Date

November 21, 2007

Effective Date

December 6, 2007

Affected Manufacturer

CFM International, S.A. CFM56-5C4/1 Series Turbofan

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2007-0108

Topics

Air transportationAircraftAviation safetySafety

Official Documents

View all ADs for CFM International, S.A. CFM56-5C4/1 Series Turbofan →

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