STC SA02358LA

This certificate issued to: NIACC Avitech Technologies 245 W Dakota Ave.

Clovis, CA 93612

This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The approval of this modification applies to the above noted airplane model series only. A copy of this STC must be included in the permanent record of the modified aircraft. 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.

Installation of Main Landing Gear Wire Harness Assemblies, in accordance with FAA approved NIACC Avitech Master Drawing List (MDL) No. NT-MDL-18-001, Rev. L, dated March 23, 2012, or later FAA approved revision.

Part 25 Title 14 Code of Federal Regulations .

SA02358LA

A21EA-1 Bombardier, Inc.

CL-600-2C10, CL-600-2C11, CL-600-2D24 02/09/2009 11/21/2012 07/15/2013 07/01/2011 04/09/2025 for Manager, West Certification Branch 3

SA02358LA 3

SA02358LA 3 3 Add Page Based on 14 CFR §§ 21.115 and 21.101, and FAA order 8110.48, the type certification basis for the Bombardier Inc. Models CL-600-2C10, CL-600-2C11, and CL-600-2D24 aircraft is as shown on TCDS A21EA-1 for parts changed or affected by the change. Based on 14 CFR §§

21.101(g), applicable provisions of 14 CFR part 26 are included in the certification basis. For any future part 26 amendments, the holder of this STC must demonstrate compliance with the applicable sections. As of the issuance date of this STC, compliance has been found for the following regulations 14 CFR §§ 26.11, (Amdt. No. 26-0). The above certification basis is only applicable to NIACC Avitech Master Drawing List (MDL) No. NT-MDL-18-001, Rev. L, dated March 23, 2012 or later FAA approved revisions.

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