STC SA01684WI

Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 1 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate

Number: SA01684WI

This certificate issued to: Rockwell Collins, Inc.

400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498

Part 23 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: Make: See attached FAA Approved Model List (AML), Model: Document No. RCA-0387, Rev (-), or later FAA approved revisions for the list of approved airplane models, applicable installation data requirements and specific limitations.

Description of Type Design Change: Installation of Rockwell Collins, Inc. Aircraft Information Management (AIM) System in accordance with:

(1) FAA Approved Model List (AML) RCA-0387, Revision (-), dated May 18, 2012;

(2) Instructions for Continued Airworthiness as specified by FAA Approved Model List (AML) RCA-0387, Revision (-), or later approved revision for items (1) and (2).

(1) Approval of this change in type design applies to the above model aircraft only;

(2) Compatibility of this design change with previously approved modifications must be determined by the installer;

(3) A copy of this Certificate and FAA Approved Model List (AML) must be maintained as part of the permanent records for the modified aircraft;

(4) 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: February 28, 2012 Date Reissued:

Date of Issuance: May 18, 2012 Date Amended: July 11, 2016; December 11, 2017

Signature ___Original signed by Steve Brune

Title STC ODA Administrator, ODA-500864-CE

Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 2 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate

To (Name and address of transferee)

From (Name and address of grantor)

Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

FAA Form 8110-2 (5/14) Page 3 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01684WI December 11, 2017

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for design changes that are not significant in FAA Order 8110.48, the certification basis for the FAA Approved Model List (AML) No. RCA-0387 is as follows:

(1) The type certification basis for all Models included in AML No. RCA-0387 is included in the applicable TCDS as listed in the FAA approved AML for parts not changed or not affected by the change.

(2) The certification basis for parts changed or affected by this change since the reference date of application, February 28, 2012 is based upon Part 23 as amended by Amendment 23-62.

14 CFR Part Amend. 14 CFR Part Amend.

23.301 (a) 48 23.853 (a)(d) 62

23.303 all Orig. 23.867 all 49

23.305 all 45 23.1301 all 20

23.561 all 48 23.1306 all 61

23.601 all Orig. 23.1309 (a)(b)(e) 49

23.603 all 23 23.1351 (a)(b) 49

23.605 all 23 23.1357 (a)(c) 43

23.607 (b)(c) 48 23.1359 all 49

23.609 all Orig. 23.1365 all 49

23.611 all 48 23.1431 (a)(b) 49

23.613 (a)(b)(c) 45 23.1529 all 26

23.625 all 7

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