STC SA03052NY

Part 23 of the Federal Regulations.

Installation of Model MTV-27-1-E-C-F-R(G)/CFRL250-55b full feathering and reversing 5-bladed propellers in accordance with MT-Propeller document “Installation Instructions,” Doc. No. E-1436, Revision 7, dated September 20, 2010.

The following MT-Propeller documents are required with this installation: EASA approved Airplane Flight Manual Supplement, Doc. No. E-1435, Revision 3, dated February 2, 2009 and Instructions for Continued Airworthiness, Doc. No. E-1437, Revision 2, dated January 10, 2012.

1. The Installer must determine whether this design change is compatible with previously approved modifications.

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

MT- Propeller Entwicklung GmbH FlugplatzstraBe 1 94348 Atting, Germany No. A16EU Make:

Dornier Luftfahrt GmbH Model: Dornier 228-100, -101, -200, -201, -202, -201(K), -202(K), -212 Date of application: April 29, 2009

Date of issuance: January 20, 2012 Date reissued:

( Signature) Timothy Hadsall Acting Manager New York Aircraft Certification Office

( Title)

FAA Form 8110-2-1(10-69) Page 2 of 2

Number SA03052NY Issuance date: January 20, 2012

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for changes that are not significant in FAA Order 8110.48, the certification basis for this modification are as follows:

 The type certification basis for the Dornier Luftfahrt GmbH Dornier 228-100, -101, -200, -201, -202, -201(K), -202(K), and -212 aircraft are type certified under TCDS NO. A16EU for parts not changed or not affected by the change.

 The type certification basis for the Dornier Luftfahrt GmbH Dornier 228-100, -101, -200, -201, -202, -201(K), -202(K), and -212 aircraft are type certified under TCDS NO. A16EU for parts changed or affected by the change with the following 14 CFR exceptions:

14 CFR Section 36 Amendment 36-28 ………………………..END…………………….