STC SA00858DE

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

Part 23 of the Federal Aviation Regulations.

5A6; 3A13; 3A24; A9CE Model:

Installation of inspection panels on the left and right side of the aft fuselage in accordance with Aeropod, Inc. Master Drawing List, Document No. AP-0005-MDL, Revision IR, dated January 20, 2017, FAA approved March 10, 2017, or later FAA approved revisions.

1. The 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.

2. Instructions for Continued Airworthiness (ICA), Aeropod, Inc. Document No. AP0712057-ICA, Revision IR, dated January 19, 2017, FAA accepted February 27, 2017, or later FAA accepted revision is required.

3. 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.

Date of Application: May 18, 2016 Date Reissued:

Date of Issuance: March 10, 2017 Date Amended:

Signature

SA00858DE

Aeropod, Inc. 18961 East Kent Circle Aurora, CO 80013

Textron Aviation Inc.

180 Series, 182, 182A, 182B, 182C, 182D, 185 Series, and 188 Series Todd G. Dixon Manager, Denver Aircraft Certification Office Northwest Mountain Region

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: SA00858DE FAA Form 8110-2 (5/14) Page 3 of 3

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 design change to the Textron Aviation Model 180 is as follows:

• The type certification basis for Textron Aviation Model 180 is shown on TCDS 5A6 for parts not changed or not affected by the change.

• The certification basis for parts changed or affected by the change is 14 CFR § 23 dated February 01, 1965 as amended by Amendment 23-0 except as noted: 14 CFR § 23.1529 Amdt 23-8

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 design change to the Textron Aviation Model 182 is as follows:

• The type certification basis for Textron Aviation Model 182 is shown on TCDS 3A13 for parts not changed or not affected by the change.

• The certification basis for parts changed or affected by the change is 14 CFR § 23 dated September 28, 1964 as amended by Amendment 23-0 except as noted: 14 CFR § 23.1529 Amdt 23-8.

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 design change to the Textron Aviation Model 185 is as follows:

• The type certification basis for Textron Aviation Model 185 is shown on TCDS 3A24 for parts not changed or not affected by the change.

• The certification basis for parts changed or affected by the change is 14 CFR § 23 dated September 28, 1964 as amended by Amendment 23-0 except as noted: 14 CFR § 23.1529 Amdt 23-8.

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 design change to the Textron Aviation Model 188 is as follows:

• The type certification basis for Textron Aviation Model 188 is shown on TCDS A9CE for parts not changed or not affected by the change.

• The certification basis for parts changed or affected by the change is 14 CFR § 23 dated September 28, 1964 as amended by Amendment 23-0 except as noted: 14 CFR § 23.1529 Amdt 23-8.

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(Ref. 14 CFR 21.1

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00858DE

FAA Form 8110-2 (5/14) Page 4 of