# STC SA01848WI

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Rockwell Collins Inc., United States
- Description: Modification of a Rockwell Collins Global Positioning System (GPS)
- Applied: December 2, 2016
- Status date: September 20, 2024
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A59EU](https://openairdocs.org/tcds/A59EU), [TCDS 3A20](https://openairdocs.org/tcds/3A20), [TCDS A00010WI](https://openairdocs.org/tcds/A00010WI), [TCDS A1WI](https://openairdocs.org/tcds/A1WI), [TCDS A24CE](https://openairdocs.org/tcds/A24CE), [TCDS A18SW](https://openairdocs.org/tcds/A18SW)
- Certificate PDF: https://openairdocs.org/files/sha256/4e/8d/4e8def7f4036d10d0ff00878bc9b3b989446abcd30206707ac2442249cff84e8
- Approved model list and other attachments: [SA01848WI_AML.pdf](https://openairdocs.org/files/sha256/67/9d/679d91704a79395a4bed89f70ba5690301a7cd606b254904fb19c4b29c463efa)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165564192720240925135252.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01848WI

## ADs that name it (0)

None.

## Approved models (15)

- Ontic Engineering and Manufacturing Inc. SA227-DC (C-26B) ([TCDS A18SW](https://openairdocs.org/tcds/A18SW))
- Piaggio Aero Industries S.p.A. P-180 ([TCDS A59EU](https://openairdocs.org/tcds/A59EU))
- Textron Aviation Inc. 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. 390 ([TCDS A00010WI](https://openairdocs.org/tcds/A00010WI))
- Textron Aviation Inc. 525 ([TCDS A1WI](https://openairdocs.org/tcds/A1WI))
- Textron Aviation Inc. 525A ([TCDS A1WI](https://openairdocs.org/tcds/A1WI))
- Textron Aviation Inc. 525B ([TCDS A1WI](https://openairdocs.org/tcds/A1WI))
- Textron Aviation Inc. 525C ([TCDS A1WI](https://openairdocs.org/tcds/A1WI))
- Textron Aviation Inc. B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. B200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. B200GT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. B300C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. C90GTi ([TCDS 3A20](https://openairdocs.org/tcds/3A20))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

FAA Form 8110-2 (5/14) Page 1 of 4 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate

Number: SA01848WI

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-0392, Rev B, or later FAA approved revisions for the list of approved airplane models, applicable installation data requirements, and model specific limitations.

Description of Type Design Change: Modification of a Rockwell Collins Global Positioning System (GPS) installation in accordance with:

(1) AML RCA-0392, Revision B, dated July 3, 2024;

(2) Instructions for Continued Airworthiness (ICA) RCA-0 394, Revision B as specified by AML RCA-0392, Revision B; or later FAA approved/accepted revision for items (1) and (2).

(1) Prior FAA approved installation of a Rockwell Collins GPS-4000S, P/N: 822-2189-001/-002/-003/-004/-005/-006/ -007/-010/-011/-100/-101, is a prerequisite to this STC;

(2) Approval of this change in type design applies to only the aircraft models listed on AML RCA-0392, Revision B, or later FAA approved revisions;

(3) Compatibility of this design change with previously appr oved modifications must be determined by the installer;

(4) If the holder agrees to permit another person to use this ce rtificate to alter the product, the holder shall give the other person written evidence of that permission;

(5) A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft.

Note: This modification has been determined to be a no acoustical change in accordance with 14 CFR 21.93(b).

This certificate and the supporting data which is the basi s for approval shall remain in effect until surrendered, suspended, and revoked or a te rmination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of Application: December 2, 2016 Date Reissued: September 20, 2024

Date of Issuance: September 27, 2017 Date Amended: June 24, 2020; July 3, 2024

Signature ___Original signed by Jeremy L. Crittenden Jeremy L. Crittenden

Title: STC ODA Administrator, ODA-500864-CE

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

FAA Form 8110-2 (5/14) Page 3 of 4 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01848WI September 20, 2024 Certification Basis:

Based on 14 CFR § 21.115, § 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-0392 is as follows:

a. The type certification basis for all Models included in AML No. RCA-0392 is included in the applicable TCDS as listed in the FAA approved AML for parts not changed or not affected by the change;

b. The certification basis for parts changed or affected by this change since the reference date of application, December 2, 2016, is based upon part 23 as amended by Amendment 23-61.

Data Pertinent to Piaggio Aviation S.p.A. P-180 14 CFR Part Amend. 14 CFR Part Amend.

23.301 48 23.1306 (b) 61

23.303 Orig. 23.1308 (b) 57

23.305 (a)(b) 45 23.1309 (a)(b)(c)(d)(e) 34*

23.601 Orig. 23.1309 (a)(b)(c)(d)(e) 49**

23.611 48 23.1351 (a)(1)(2)(i)(ii) 49

23.867 (a)(b) 49 23.1431 Orig.

23.1301 (a)(b)(c)(d) 20 23.1529 26

*For P-180 Aircraft models (S/N 1001-1104) **For P-180 Aircraft models (S/N 1105 and subsequent)

Data Pertinent to Textron Aviation Inc. 390 14 CFR Part Amend. 14 CFR Part Amend.

23.301 48 23.1301 (a)(b)(c)(d) 20

23.303 Orig. 23.1306 (b) 61

23.305 (a)(b) 45 23.1308 (b) 57

23.601 Orig. 23.1309 (a)(b)(c)(d)(e) 49

23.611 48 23.1351 (a)(1)(2)(i)(ii) 49

23.867 (a)(b) 49 23.1431 (a)(b) 49

23.1529 26

FAA Form 8110-2 (5/14) Page 4 of 4 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01848WI September 20, 2024 Data Pertinent to Textron Aviation Inc. 525, 525A, 525B, 525C 14 CFR Part Amend. 14 CFR Part Amend.

23.301 48 23.1306 (b) 61

23.303 Orig. 23.1308 (b) 57

23.305 (a)(b) 45 23.13 09 (a)(b)(c)(d)(e) 34*

23.601 Orig. 23.1309 (a)(b)(c)(d)(e) 49**

23.611 48 23.1351 (a)(1)(2)(i)(ii) 49

23.867 (a)(b) 49 23.1431 Orig.*

23.1301 (a)(b)(c)(d) 20 23.1431 (a)(b) 49**

23.1529 26 *For Model 525B only. **For Models 525, 525A, 525C only

Data Pertinent to Textron Aviation Inc. 300, B200, B200C, B200GT, B200CGT, B300, B300C, C90GTi 14 CFR Part Amend. 14 CFR Part Amend.

23.301 48 23.1301 (a)(b)(c)(d) 20

23.303 Orig. 23.1306 (b) 61

23.305 (a)(b) 45 23.1308 (b) 57

23.601 Orig. 23.1309 (a)(b)(c)(d)(e) 49

23.611 48 23.1351 (a)(1)(2)(i)(ii) 49

23.867 (a)(b) 49 23.1431 (a)(b) 49

23.1529 26

Data Pertinent to Ontic Engineering and Manufacturing, Inc. SA227-DC (C-26B) 14 CFR Part Amend. 14 CFR Part Amend.

23.301 48 23.1301 (a)(b)(c)(d) 20

23.303 Orig. 23.1306 (b) 61

23.305 (a)(b) 45 23.1308 (b) 57

23.601 Orig. 23.1309 (a)(b)(d) 34

23.611 48 23.1351 (a)(1)(2)(ii) 34

23.867 (a)(b) 49 23.1431 (a)(b) 49

23.1529 26 ------------------------------------------------------ END --------------------------------------------------------

### SA01848WI_AML.pdf

© 2017-2020, 2024 Rockwell Collins. All Rights Reserved. 1 of 6

APPROVED MODEL LIST (AML) GPS-4000S GLOBAL POSITIONING SYSTEM (GPS) 14 CFR PART 23 AIRCRAFT

**STC SA01848WI**

RCA-0392 Revision: C September 20, 2024

FAA APPROVED BY:

Original signed by Jeremy L. Crittenden September 27, 2017 Jeremy L. Crittenden FAA Approved Date STC ODA Administrator, ODA-500864-CE

Date Amended: June 24, 2020; July 3, 2024 Date Reissued: September 20, 2024

U.S. Export Classification: NSR

This Document does not contain any export controlled technical data (NSR)

Approved Model List

Rockwell Collins Proprietary Information RCA-0392, Revision C 2 of 6 NOTE(S):

This document is maintained in the Aircraft Certification Center configuration management system.

Paragraphs and/or figures with a vertical line outside the right margin (|) indicate a change to the latest revision.

CAGE Code: 0EFD0

**SIGNATURES**

Name Signature Prepared by: Greggory P. Stutes Checked by: Brian E. Mishmash Approved by: Jeremy L. Crittenden

Approved Model List

Rockwell Collins Proprietary Information RCA-0392, Revision C 3 of 6

1. AML REVISION LOG Rev Page(s) Description Date (-) All Ori ginal Issue 09/27/2017 A 5 Added item 6, M7 Aerospace LLC SA227-DC (C-26B) model 06/24/2020 B 4-5 STC Project SA06934WI-a, amendment to update GPS-4000S. 07/03/2024

Changed the “refer to” Installation Instructions to be generic.

Updated revision of Drawing Index and ICA for all models.

Clarified Aircraft Make and Model names.

Changed to landscape and adjusted table formatting.

C 4-6 Reissuance to correct make and model names.

Corrected names of all makes and models to match current TCDS.

Deleted revision and date of all referenced TCDS.

Reorganized list of models to be in alphabetical order by make.

09/20/2024

Approved Model List

Rockwell Collins Proprietary Information RCA-0392, Revision C 4 of 6

2. INTRODUCTION This document is the FAA Approved Model List for STC No. SA01848WI for the modification of Rockwell Collins, Inc. Global Positioning System (GPS) installation in 14 CFR Part 23 Aircraft.

It is the responsibility of the installer to ensure the existing aircraft equipment configuration is compatible with this STC. Refer to the Installation Instructions for the approved equipment replacements.

3. APPROVED MODEL LIST Item Make Model Type Certificate Data Sheet Supplemental Type Design Data[1] and Limitations AML Amdt Date 1 Ontic Engineering and Manufacturing, Inc.

SA227-DC (C-26B) A18SW

Installation Instructions:

Drawing Index, RCA-0393, Rev. B Airplane Flight Manual Supplement:

N/A 06/24/20 Instructions for Continued Airworthiness:

RCA-0394, Rev. B

Additional Limitations:

Prior FAA approved installation of GPS- 4000S Part Number, 822-2189-100 or 822-2189-101, is a prerequisite.

2 Piaggio Aviation S.p.A. P-180

A59EU

Installation Instructions:

Drawing Index, RCA-0393, Rev. B

Airplane Flight Manual Supplement:

N/A

Instructions for Continued Airworthiness:

RCA-0394, Rev. B

Additional Limitations:

None

Approved Model List

Rockwell Collins Proprietary Information RCA-0392, Revision C 5 of 6 Item Make Model Type Certificate Data Sheet Supplemental Type Design Data[1] and Limitations AML Amdt Date 3

Textron Aviation Inc.

390 A00010WI Installation Instructions:

Drawing Index, RCA-0393, Rev. B

Airplane Flight Manual Supplement:

N/A

Instructions for Continued Airworthiness:

RCA-0394, Rev. B

Additional Limitations:

None

4 Textron Aviation Inc. 525 525A 525B 525C A1WI

Installation Instructions:

Drawing Index, RCA-0393, Rev. B

Airplane Flight Manual Supplement:

N/A

Instructions for Continued Airworthiness:

RCA-0394, Rev. B

Additional Limitations:

None

5 Textron Aviation Inc. 300 B200 B200C B200GT B200CGT B300 B300C A24CE Installation Instructions:

Drawing Index, RCA-0393, Rev. B

Airplane Flight Manual Supplement:

N/A

Instructions for Continued Airworthiness:

RCA-0394, Rev. B

Additional Limitations:

None

Approved Model List

Rockwell Collins Proprietary Information RCA-0392, Revision C 6 of 6 Item Make Model Type Certificate Data Sheet Supplemental Type Design Data[1] and Limitations AML Amdt Date 6 Textron Aviation Inc. C90GTi

3A20 Installation Instructions:

Drawing Index, RCA-0393, Rev. B

Airplane Flight Manual Supplement:

N/A

Instructions for Continued Airworthiness:

RCA-0394, Rev. B

Additional Limitations:

None

[1] Or later approved revisions

## Every issue (4)

- September 20, 2024: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/4e/8d/4e8def7f4036d10d0ff00878bc9b3b989446abcd30206707ac2442249cff84e8), [SA01848WI_AML.pdf](https://openairdocs.org/files/sha256/67/9d/679d91704a79395a4bed89f70ba5690301a7cd606b254904fb19c4b29c463efa)
- June 24, 2021: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/2f/be/2fbe8310216b95f0fd444a543c6db49239f7d5c8c8d2d02372d61c1bf95aad03), [AML_SA01848WI.pdf](https://openairdocs.org/files/sha256/26/12/2612795d66b670510a89f06d933d602371bb9a817d3088674d55082e7db05f52)
- June 24, 2020: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/2f/be/2fbe8310216b95f0fd444a543c6db49239f7d5c8c8d2d02372d61c1bf95aad03), [AML_SA01848WI.pdf](https://openairdocs.org/files/sha256/26/12/2612795d66b670510a89f06d933d602371bb9a817d3088674d55082e7db05f52)
- September 27, 2017: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/aa/c6/aac68c034fc12756b83f80b57dd949d0f8afe6ad92a024a3635d23bccbc6f150), [SA01848WI_AML.pdf](https://openairdocs.org/files/sha256/da/ee/daee0eba12dae040a7c78c0c194f80824f2e190605246def034a6308a3214786)

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