STC SA03845NY

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title SA03845NY MT-Propeller Entwicklung GmbH Flugplatzstrasse 1 94348 Atting, Germany Federal Aviation Regulations.

1. The installation of MT-Propeller Entwicklung GmbH's Model# MTV-9-B/200-58 three Blade constant speed propeller and spinner in accordance with the configuration stated in the Master Operation Manual List, Doc. No. E-2641 (GA8), Rev. 0, dated March 16, 2015, or Doc. No. E-2213 (GA8-TC320), Rev. 0, dated November 21, 2012, or later EASA approved revision and Installation Instructions, Doc. No. E-2643 (GA8), Rev. 0, dated March 16, 2015, or Doc. No. E-2215 (GA8-TC320), Rev. 0, dated November 19, 2012, or later EASA approved revision.

(See Description of Type Design Change continued on Page 3 of 3)

1. The aircraft must be operated in accordance with the “Limitations” section of Airplane Flight Manual Supplement, Doc. No E-2642 (GA8) Rev. 1, dated December 5, 2016, or Doc. No E-2214 (GA8-TC320) Rev. 1, dated December 5, 2016 or later EASA approved revisions.

2. The installer must determine whether this design change is compatible with previously approved modifications.

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

Gaetano Sciortino Manager New York Aircraft Certification Office GA 8 Airvan (Pty) Ltd GA8 GA8-TC320 June 20, 2016 December 28, 2016 IMPORT A00011LA 3

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

3 SA03845NY

FAA Form 8110-2 (5/14) Page 3 of

3 Date of Issuance: December 28, 2016

Description of Type Design Change (continued):

2. Operation must be in accordance with Airplane Flight Manual Supplement, Doc. No E-2642 (GA8) Rev. 1, dated December 5, 2016, or Doc. No E-2214 (GA8-TC320) Rev. 1, dated December 5, 2016 or later EASA approved revisions, and is required as part of this installation.

3. Maintenance must be in accordance with Instructions for Continued Airworthiness, Doc. No E-2644 (GA8) Rev.

0, dated March 16, 2015, or Doc. No E-2216 (GA8-TC320) Rev. 0, dated November 21, 2012, or later EASA accepted revision.

Certification Basis:

Based on 14 CFR §21.115 and §21.101, and FAA Order 8110.48, the certification basis for this modification to the GA 8 Airvan (Pty) Ltd Model GA8 and GA8-TC320 aircraft is as follows:

a) The type certification basis for the GA 8 Airvan (Pty) Ltd Model GA8 and GA8-TC320 aircraft as shown on TCDS A00011LA for parts not changed or not affected by the change.

b) The type certification basis for the GA 8 Airvan (Pty) Ltd Model GA8 and GA8-TC320 aircraft as shown on TCDS A00011LA for parts changed or affected by the change with the following exception:

● Compliance with 14 CFR Part §36 at Amendment 36-30.

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SA03845NY