STC SA04234AT

FAA Form 8110-2 (5/14) Page 1 of 3

Number: SA04234AT

This certificate issued to: Avenger Aerospace Solutions, Inc.

103 N. Main Street, Suite 106 Greenville, SC 29601

Part 23 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: A7CE Make: Textron Aviation Inc.

Model: 402C

Installation of redesigned Nose Landing Gear Drag Brace Assembly in accordance with Avenger Aerospace Solutions drawing A013LM5142002 Revision C dated October 15, 2015 or later FAA approved drawing revisions.

1. For maintenance and inspections, apply Avenger Aerospace Solutions, Inc. engineering report Cape Air Cessna 402 C Instructions for Continued Airworthiness AAS-ICA-15-001, Revision C, dated September 7, 2015, or later FAA accepted 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 this certificate to alter the product, the holder must give the other person written evidence of that permission.

Date of Application: March 4, 2015 Date Reissued:

Date of Issuance: September 9, 2016 Date Amended:

Signature

Title Melvin D. Taylor, Manager Atlanta Aircraft Certification Office

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

To (Name and address of transferee)

From (Name and address of grantor)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR04200AT

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

Date of Issuance: September 9, 2016 Date Amended:

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, for the Cessna 402C, the Certification Basis is as follows:

• The type certification basis for the Cessna 402C aircraft is shown on TCDS A7CE for parts not changed or not affected by the change.

• The certification basis for parts changed or affected by the change since the reference date of application, March 4, 2015, is based upon part 23 as amended by amendment 23-62. Based on 14 CFR §§ 21.115 and 21.101, and FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment 23-0 through 23-62

23.301 Amdt 23-48, 23.303 Amdt 23-0, 23.305 Amdt 23-45, 23.307(a) Amdt 23-0, 23.471 Amdt 23-0, 23.473 Amdt 23-48,

23.477 Amdt 23-0, 23.479 Amdt 23-45, 23.483 Amdt 23-0, 23.493 Amdt 23-0, 23.499 Amdt 23-48, 23-507 Amdt 23-14,

23.509 Amdt 23-14, 23.511 Amdt 23-7, 23.573 (b) Amdt 23-48, 23.601 Amdt 23-0, 23.603 Amdt 23-23, 23.605 Amdt 23- 23, 23.607 Amdt 23-48, 23.609 Amdt 23-0, 23.613 Amdt 23-45, 23.729 Amdt 23-49, 23.1529 Amdt 23-26

Regulations at an intermediate amendment None

Regulations at the amendment level in TCDS A7CE None

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