STC SE00032EN

This Certificate issued to: Pratt & Whitney 400 Main Street.

East Hartford, CT 06108

Part 33 of the Federal Aviation Regulations.

Installation of Pratt & Whitney (P&W) Global Material Solutions (GMS) CFM56-3 Fan/Booster Module in accordance with P&W GMS Drawing List 880500-01B, Rev: Initial, dated March 14, 2008 or later FAA-approved revision.

1. Life Limits for Parts approved by this Supplemental Type Certificate are published in P&W GMS Engine manual Airworthiness Limitation Section, Pratt & Whitney GMS CFM56-3 STC Engine Manual Document, Part Number PW9325M80-1, Revision 1, dated April 15, 2008, or later FAA-approved revision.

2. Instructions for Continued Airworthiness (ICA), Pratt & Whitney GMS CFM56-3 STC Engine Manual Document, Part Number PW9325M80-1, Revision 1, dated April 15, 2008, or later FAA accepted revision must be made available to the operator at the time of installation.

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If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

surrendered, revoked, or a termination date is other wise established by the Administrator of the Federal Aviation Administration.

E2GL, E21EU Make : CFM INTERNATIONAL (CFMI) Model : CFM56-3, -3B, -3C Date of application August 31, 2006 Date of issuance : March 14, 2008

Date reissued: April 24, 2009 July 27, 2009 Date amended:

(Signature) Thomas A. Boudreau Manager, Engine Certification Office

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