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AD FAA-2012-0416

Airworthiness Directives; Pratt & Whitney Canada Corp. Turboprop Engines

Summary

We are superseding an existing airworthiness directive (AD) for all Pratt & Whitney Canada Corp. (P&WC) PW118, PW118A, PW118B, PW119B, PW119C, PW120, PW120A, PW121, PW121A, PW123, PW123B, PW123C, PW123D, PW123E, PW123AF, PW124B, PW125B, PW126A, PW127, PW127E, PW127F, PW127G, and PW127M turboprop engines. That AD currently requires initial and repetitive inspections of certain serial numbers (S/Ns) of propeller shafts for cracks and removal from service if found cracked. This new AD requires the same actions, but requires removal from service of affected propeller shafts as mandatory terminating action to the repetitive inspections. This AD was prompted by reports of two propeller shafts found cracked at time of inspection during maintenance. We are issuing this AD to detect propeller shaft cracks, which could cause failure of the shaft, propeller release, and loss of control of the airplane.

Directive Details

AD Number

FAA-2012-0416

Document Number

2012-31361

Type

Rule

Publication Date

January 11, 2013

Effective Date

February 15, 2013

Affected Manufacturer

Pratt & Whitney Canada Corp. Turboprop

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2012-0416

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Pratt & Whitney Canada Corp. Turboprop →

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