# STC SA01393WI-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Rockwell Collins Inc, United States
- Description: Modification of a Collins CTL-23 or CTL-23C VHF COMM/NAV Control Panel System installation.
- Applied: November 17, 2005
- Status date: July 12, 2006
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A00006WI](https://openairdocs.org/tcds/A00006WI), [TCDS A59EU](https://openairdocs.org/tcds/A59EU), [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/5b/38/5b38d923c61434a88435c30537b89b1d9d165ad64ca75a18e239858c89befb28
- Approved model list and other attachments: [SA01393WI-D.pdf](https://openairdocs.org/files/sha256/49/c3/49c3c10c416cabd3483bb3e7cf32046f5dc18feaf1d429c3788553d607b816ca)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9C0BB14608FD90AA862572340074E898.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01393WI-D

## ADs that name it (0)

None.

## Approved models (7)

- Harbin Aircraft Manufacturing Corporation Y12 IV ([TCDS A00006WI](https://openairdocs.org/tcds/A00006WI))
- Piaggio Aero Industries S.p.A. P-180 ([TCDS A59EU](https://openairdocs.org/tcds/A59EU))
- Raytheon Aircraft Company 1900D ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company 300LW ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Raytheon Aircraft Company B300C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

**FAA APPROVED MODEL LIST (AML) NO. SA01393WI-D ROCKWELL COLLINS, INC.**

FOR MODIFICATION OF A COLLINS CTL-23 OR CTL-23C VHF COMM/NAV CONTROL PANEL SYSTEM INSTALLATION TO A COLLINS CTL-23G OR CTL-23D VHF COMM/NAV CONTROL PANEL SYSTEM INSTALLATION IN PART 23 AIRCRAFT Issue Date: July 12, 2006

**ORIGINAL CERTIFICATION INSTALLATION**

TYPE BASIS INSTRUCTIONS AFM AML AIRCRAFT AIRCRAFT CERTIFICATE FOR DRAWING REVISION NO. SUPPLEMENT AMENDMENT ITEM MAKE MODEL NUMBER ALTERATION INDEX NO AND DATE(") NUMBER/DATE DATE 1 Harbin Aircraft Y12 IV A00006WI TCDS A00006WI RCA-0105 Rev -, 06/12/06 N/A Manufacturing Revision 3 Corporation July 16, 1996 (HAMC) 2 Piaggio Aero P-180 A59EU TCDS A59EU RCA-0105 Rev -, 06/12/06 N/A Industries Revision 13 S.p.A March 24, 2006 Raytheon 1900D (Airliner A24CE TCDS A24CE RCA-0105 Rev -, 06/12/06 N/A Aircraft 300, Super King Revision 91 Company Air) September 1, 300LW (Super 2005 King Air) B300 (Super King Air 350) B300C (Super King Air 350C) [1] Or later FAA approved revision Page 1 of 2

**FAA APPROVED MODEL LIST (AML) NO. SA01393WI-D ROCKWELL COLLINS, INC.**

MODIFICATION OF A COLLINS CTL-23 OR CTL-23C VHF COMM/NAV CONTROL PANEL SYSTEM INSTALLATION TO A COLLINS CTL-23G OR CTL-23D VHF COMM/NAV CONTROL PANEL SYSTEM INSTALLATION IN PART 23 AIRCRAFT Issue Date: July 12, 2006

**ORIGINAL CERTIFICATION INSTALLATION**

TYPE BASIS INSTRUCTIONS AFM AML AIRCRAFT AIRCRAFT CERTIFICATE FOR DRAWING REVISION NO. SUPPLEMENT AMENDMENT ITEM MAKE MODEL NUMBER ALTERATION INDEX NO. AND DATE" NUMBER/DATE DATE 4 Raytheon 390 A00010WI TCDS A00010WI RCA-0105 Rev-, 06/12/06 N/A Aircraft (PREMIER I) Revision 7 Company July 6, 2005 [1] Or later FAA approved revision FAA Approved: / Salind boher Administrator, DAS-500864-CE Amended:

### SA01393WI-D.pdf

This is OCR from the scanned FAA attachment. OCR can misread letters and numbers.

United States of America Department of Transportation - Federal Abiation Administration Supplemental Type Certificate Number SA01393WI-D This certificate, issued to Rockwell Collins, Inc.

400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498 certifies that the change in the type design for the following product with the limitations and conditions therefer as specified hereen meet's the aircorthiness requirments of Part "of the " Regutativas Criginal Product Type Certificate Number: * *See attached FAA Approved Model List (AML) Make : No. SA01393WI-D for list of approved airplane models Model: * and applicable airworthiness regulations.

Description of Type Lesign Chunge: Modification of a Collins CTL-23 or CTL-23C VHF COMMNAV Control Panel System installation to a Collins CTL-23G or CTL-23D VHF COMM/NAV Control Panel System installation in accordance with Collins Drawing Index as listed on AML No. SA01393WI-D, Revision -, or later FAA approved Limitations and Conditions: (1) Prior FAA approved installation of Collins CTL-23 part numbers 622-9851-001/-002/-007/-008 or CTL-23C part numbers 822-1121-001 through -004/-007/-008 is a prerequisite to this STC. (2) Approval of this change in type design applies to the above model aircraft only. (3) Compatibility of this design change with previously approved modifications must be determined by the installer. (4) A copy of this Certificate and FAA Approved Model List (AML) No. SA01393WI-D issued July 12, 2006, or later FAA approved revision, must be maintained as part of the permanent records for the modified aircraft. (5) 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.

This certificate and the supporting data which is the basis for appreval shall remain in effect untit surrendered, suspended, revched, or a termination dute is otherwise established by the Administruter of the Federal Goiation Administration.

Lute of application: November 17, 2005 Lute reissued:

Bute of issuance: July July 2000 Lat unended:

FEDERAL AVIATION By directies of the . Administru poten (Signature) TOMINSTRATO John'S. Bohn Administrator, DAS-500864-CE (Title) Any alteration of this certificate is punishable by a fine of not exceeding s1,000, or imprisonment not exceeding s years, or both FAA FORM 8110-2 (10-68) PAGE 1 This certificate may be transferred in accordance with FAR 21.47.

INSTRUCTIONS: The transfer endorsement below may be used to notify the appropriate FAA Regional Office of the transfer of this Supplemental Type Certificate.

The FAA will reissue the certificate in the name of the transferee and forward it to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number._.

to (Name of transferee) (Address of transferee) (Number and Street) (City, State and ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and Street) (City, State and ZIP code) Extent of Authority (if licensing agreement):

Date of Transfer:

Signature of grantor (In ink):

## Every issue (1)

- July 12, 2006: Issued, Current. [certificate](https://openairdocs.org/files/sha256/5b/38/5b38d923c61434a88435c30537b89b1d9d165ad64ca75a18e239858c89befb28), [SA01393WI-D.pdf](https://openairdocs.org/files/sha256/49/c3/49c3c10c416cabd3483bb3e7cf32046f5dc18feaf1d429c3788553d607b816ca)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
