STC SA03818NY

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

Part of the

Signature

Title SA03818NY Avmax Aviation Services Inc.

3691-19th Street, N.E.

Calgary, Alberta T2E 6S8 Canada Federal Aviation Regulations.

1. Installation of Honeywell KGP-860 & IHAS in accordance with Transport Canada Civil Aviation (TCCA) approved Avionics Design Services Ltd. (ADS) Master Drawing List MDL05114, Revision A, dated March 14, 2006 or later TCCA approved revision.

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

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.

Michele J. Maurer Acting Manager New York Aircraft Certification Office Beechcraft Corporation 200, B200 June 30, 2016 October 20, 2016 IMPORT A24CE 3

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

To (Name and address of transferee)

From (Name and address of grantor)

3 SA03818NY

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

3 Date of Issuance: October 20, 2016

Description of Type Design Change (continued):

Configuration One:

Operation of the Honeywell KGP-860 & IHAS must be in accordance with TCCA approved Western Avionics Flight Manual Supplement (FMS) FMS05114-1, Revision N/C, dated December 30, 2005 or later TCCA approved revision.

Maintenance of the Honeywell KGP-860 & IHAS must be in accordance with TCCA accepted ADS Instructions for Continued Airworthiness (ICA) ICA05114-1, Revision A, dated February 14, 2006 or later TCCA accepted revision.

Configuration Two:

Operation of the Honeywell KGP-860 & IHAS must be in accordance with TCCA approved Western Avionics FMS FMS05114-2, Revision N/C, dated December 30, 2005 or later TCCA approved revision.

Maintenance of the Honeywell KGP-860 & IHAS must be in accordance with TCCA accepted ADS ICA ICA05114-2, Revision A, dated February 14, 2006 or later TCCA accepted revision.

2. Antenna provisions require separate approval.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Beechcraft Corporation 200, B200 is as follows::

(a) The type certification basis for Beechcraft Corporation 200, B200 as shown on the FAA Type Certificate Data Sheet TCDS A24CE for parts not changed or not affected by the change.

(b) For parts changed or affected by the change: The existing type certification basis for the aircraft model as shown on the FAA Type Certificate Data Sheet A24CE, in addition to:

i) Part 23 including amendments 23-1 through 23-43.

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