# STC SA00674WI-D

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Rockwell Collins Inc, United States
- Description: Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II system installation.
- Applied: May 22, 1998
- Status date: July 23, 2012
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A17EU](https://openairdocs.org/tcds/A17EU), [TCDS A21EU](https://openairdocs.org/tcds/A21EU), [TCDS A56EU](https://openairdocs.org/tcds/A56EU), [TCDS A28CE](https://openairdocs.org/tcds/A28CE), [TCDS A7CE](https://openairdocs.org/tcds/A7CE), [TCDS A16EU](https://openairdocs.org/tcds/A16EU), [TCDS 3A20](https://openairdocs.org/tcds/3A20), [TCDS A23CE](https://openairdocs.org/tcds/A23CE), [TCDS A24CE](https://openairdocs.org/tcds/A24CE), [TCDS A31CE](https://openairdocs.org/tcds/A31CE), [TCDS A18SW](https://openairdocs.org/tcds/A18SW), [TCDS A5SW](https://openairdocs.org/tcds/A5SW), [TCDS A8SW](https://openairdocs.org/tcds/A8SW), [TCDS A10SW](https://openairdocs.org/tcds/A10SW), [TCDS A2PC](https://openairdocs.org/tcds/A2PC), [TCDS A7PC](https://openairdocs.org/tcds/A7PC), [TCDS A59EU](https://openairdocs.org/tcds/A59EU), [TCDS A50EU](https://openairdocs.org/tcds/A50EU), [TCDS 1A10](https://openairdocs.org/tcds/1A10), [TCDS A23SO](https://openairdocs.org/tcds/A23SO) and 3 more
- Certificate PDF: https://openairdocs.org/files/sha256/d2/d7/d2d7f64894b1e2a0115b06478d08a64eae9a3c36435f7e098586a82ecbc9e126
- Approved model list and other attachments: [SA00674WI-D_AML.pdf](https://openairdocs.org/files/sha256/68/ad/68ad328e8fcdcdd6b87872984ceec8d25f4138fa4c9f4270e0f091000263818f)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2C70A73B46DD8A2786257A8D00699BB7.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00674WI-D

## ADs that name it (0)

None.

## Approved models (101, first 50)

- B-N Group Ltd. BN-2 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-2 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-20 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-21 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-26 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-27 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-3 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-6 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-8 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-9 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2B-20 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2B-21 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2B-26 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2B-27 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2T ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2T-4R ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- British Aerospace Regional Aircraft Jetstream 3201 ([TCDS A56EU](https://openairdocs.org/tcds/A56EU))
- British Aerospace Regional Aircraft Jetstream Series 3101 ([TCDS A21EU](https://openairdocs.org/tcds/A21EU))
- Cessna Aircraft Company 425 ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 441 ([TCDS A28CE](https://openairdocs.org/tcds/A28CE))
- Dornier Luftfahrt GmbH Dornier 228-100 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Dornier Luftfahrt GmbH Dornier 228-101 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Dornier Luftfahrt GmbH Dornier 228-200 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Dornier Luftfahrt GmbH Dornier 228-201 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Dornier Luftfahrt GmbH Dornier 228-202 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Dornier Luftfahrt GmbH Dornier 228-212 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Hawker Beechcraft Corporation 1900C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 1900C (C-12J) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 1900D ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 300LW ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 58P ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))
- Hawker Beechcraft Corporation 58PA ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))
- Hawker Beechcraft Corporation 58TC ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))
- Hawker Beechcraft Corporation 58TCA ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))
- Hawker Beechcraft Corporation A200 (C-12A) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200 (C-12C) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200C (UC-12B) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200CT (C-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200CT (C-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200CT (FWC-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200CT (RC-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200CT (RC-12G) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200CT (RC-12H) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200CT (RC-12K) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))

All 101: https://openairdocs.org/stc/SA00674WI-D/models.md

## 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.

Part * of the * Regulations.

Original Product--Type Certificate Number : * *See attached FAA Approved Model List (AML) Make : * No. SA00674WI-D for list of approved airplane models Model : * and applicable airworthiness regulations.

Description of Type Design Change: Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation in accordance with Collins Installation Instructions as listed on AML No. SA00674WI-D, Revision -, or later FAA approved revisions.

Limitations and Conditions: (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) No. SA00674WI-D issued November 17, 1998, or later FAA approved revision, must be maintained as part of the permanent records for the modified aircraft. (4) A VHF-22C unit can be installed to replace either an existing VHF-22A or VHF-22B unit. A VHF-22D unit can only be installed to replace an existing VHF-22B unit. (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.

Rockwell Collins, Inc.

400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498 Date of application : May 22, 1998

Date of issuance : November 17, 1998

Date reissued : May 14, 1999

( Signature) Dale R. Koonts

Manager, DAS-3CE

( Title)

FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES

Number

**TABLE 1**

Collins Drawing Index

Configuration Airplane Flight Manual Supplement (AFMS)

### SA00674WI-D_AML.pdf

Rockwell Collins, Inc.

1 of 10

APPROVED MODEL LIST (AML) PRO LINE II 8.33 KHZ COM RADIO WITH CSDB CONTROL FOR PART 23 AIRCRAFT

**STC SA00674WI-D**

RCA-0436 Revision: C July 23, 2012

FAA APPROVED BY:

Steven P. Brune STC ODA Administrator, ODA-500864-CE

Approved Model List

Rockwell Collins Proprietary Information RCA-0436, Revision C 2 of 10

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: D. W. Jessen Checked by: V. J. Humphrey Approved by: C. J. Terrington

Approved Model List

Rockwell Collins Proprietary Information RCA-0436, Revision C 3 of 10

1. AML REVISION LOG Rev Page(s) ECO Description Date

- All N/A Original release 11/17/1998 A 10 N/A Amended AML to include Hawker Beechcraft Corporation Model 1900C (C-12J).

05/14/1999 B 1 - 8 N/A Revised AML to update aircraft make column.

Amended AML aircraft model A200CT (FWC-11D) to read (FWC-12D).

01/25/2011 C 1 - 10 INU321 Revised AML document to better align with AC 23-22 dated 01/27/05. Updated aircraft make and TCDS to latest revision.

Amended AML to include Hawker Beechcraft Corporation Model 1900C.

07/23/2012

Approved Model List

Rockwell Collins Proprietary Information RCA-0436, Revision C 4 of 10

2. INTRODUCTION This document is the FAA Approved Model List for STC No. SA00674WI-D for the modification of Rockwell Collins VHF-22A/VHF-22B VHF Comm Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Rockwell Collins VHF-22C/VHF-22D VHF Comm Receiver Transmitter with a CTL-22C Control 8.33 KHz Pro Line II System Installation in 14 CFR Part 23 Aircraft.

3. IMPORTANT NOTE The existing equipment specified within the Installation Instructions is a prerequisite to this STC for each airplane eligible for this proposed modification. It is the responsibility of the installer to ensure this prerequisite equipment is properly linked to meet the intended function for the system, as certified under this AML approval.

4. APPROVED MODEL LIST Item Aircraft Make Aircraft Model Type Certificate Number Required Approved Data and Added Model Specific Limitations AML Amdt Date 1 Nomad TC Pty Ltd.

N22B N22S A7PC Revision 5 05/28/2010 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A 2 Beech 58P 58PA 58TC 58TCA A23CE Revision 15 11/20/2007 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A

Approved Model List

Rockwell Collins Proprietary Information RCA-0436, Revision C 5 of 10

Item Aircraft Make Aircraft Model Type Certificate Number Required Approved Data and Added Model Specific Limitations AML Amdt Date 3 Hawker Beechcraft F90 A31CE Revision 8 03/26/2007 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A 4 Viking Air Limited (Twin Otter) DHC-6-100 DHC-6-200 DHC-6-300

A9EA Revision 14 09/08/2011 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A 5 British Aerospace (Operations) Limited Jetstream Series 3101 A21EU Revision 18 03/31/2008 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A 6 Jetstream Aircraft Limited (British Aerospace) Jetstream Model 3201 A56EU Revision 7 03/02/2007 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A

Approved Model List

Rockwell Collins Proprietary Information RCA-0436, Revision C 6 of 10

Item Aircraft Make Aircraft Model Type Certificate Number Required Approved Data and Added Model Specific Limitations AML Amdt Date 7 Cessna 425 A7CE Revision 48 03/01/2010 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A 8 Cessna 441 A28CE Revision 12 09/22/2003 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A 9 Dornier Luftfahrt GmbH Dornier 228-100 Dornier 228-101 Dornier 228-200 Dornier 228-201 Dornier 228-202 Dornier 228-212

A16EU Revision 9 03/02/2007 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A 10 M7 Aerospace SA227-AT SA227-TT A5SW Revision 27 03/19/2010 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A

Approved Model List

Rockwell Collins Proprietary Information RCA-0436, Revision C 7 of 10

Item Aircraft Make Aircraft Model Type Certificate Number Required Approved Data and Added Model Specific Limitations AML Amdt Date 11 M7 Aerospace LP SA226-TC SA227-AC (C-26A) SA227-PC SA227-BC (C-26A) A8SW Revision 23 03/28/2012 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A 12 M7 Aerospace LP SA227-CC SA227-DC (C-26B) A18SW Revision 5 03/15/2012 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A 13 Piaggio P-180 A59EU Revision 20 03/21/2011 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A 14 Mitsubishi MU-2B-26 MU-2B-36 A2PC Revision 19 06/18/2012 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A

Approved Model List

Rockwell Collins Proprietary Information RCA-0436, Revision C 8 of 10

Item Aircraft Make Aircraft Model Type Certificate Number Required Approved Data and Added Model Specific Limitations AML Amdt Date 15 Mitsubishi MU-2B-25 MU-2B-26 MU-2B-26A MU-2B-35 MU-2B-36 MU-2B-36A MU-2B-40 MU-2B-60 A10SW Revision 17 10/09/2009 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A 16 Pilatus PC-7 A50EU Revision 2 07/01/1996 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A 17 B-N Group Ltd.

BN-2 BN-2A BN-2A-2 BN-2A-3 BN-2A-6 BN-2A-8 BN-2A-9 BN-2A-20 BN-2A-21 BN-2A-26 BN-2A-27 BN-2B-20 BN-2B-21 BN-2B-26 BN-2B-27 BN-2T BN-2T-4R A17EU Revision 17 03/02/2007 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A 18 Piper Aircraft, Inc.

PA-23 1A10 Revision 52 02/10/2009 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A

Approved Model List

Rockwell Collins Proprietary Information RCA-0436, Revision C 9 of 10

Additional Limitations:

N/A Item Aircraft Make Aircraft Model Type Certificate Number Required Approved Data and Added Model Specific Limitations AML Amdt Date 19 Piper Aircraft, Inc.

PA-31T2 A8EA Revision 24 02/16/2012 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A 20 Piper Aircraft, Inc.

PA-42 PA-42-720 PA-42-1000 A23SO Revision 20 06/24/2010 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A 21 Hawker Beechcraft C90 C90A E90 3A20 Revision 71 12/02/2011 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A

Approved Model List

Rockwell Collins Proprietary Information RCA-0436, Revision C 10 of 10

Item Aircraft Make Aircraft Model Type Certificate Number Required Approved Data and Added Model Specific Limitations AML Amdt Date 22 Hawker Beechcraft 200 200C 200CT 200T 300 300LW 1900C 1900C (C-12J) 1900D A200 (C-12A) (C-12C) A200C (UC-12B) A200CT (C-12D) (C-12F) (FWC-12D) (RC-12D) (RC-12G) (RC-12H) (RC-12K) (RC-12P) B200 B200C (C-12F) (UC-12F) (UC-12M) (UC-12R) B200CT B200T B300 B300C A24CE Revision 103 12/20/2011 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D 07/23/12 Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A 23 Twin Commander 680 690A 690C 690D 695 695A 695B 2A4 Revision 47 11/12/2009 Installation Instructions:

Drawing Index, 992-4307-001, Rev. D

Airplane Flight Manual Supplement:

N/A Instructions for Continued Airworthiness:

N/A Additional Limitations:

N/A

## Every issue (2)

- July 23, 2012: Amended, Current. [certificate](https://openairdocs.org/files/sha256/d2/d7/d2d7f64894b1e2a0115b06478d08a64eae9a3c36435f7e098586a82ecbc9e126), [SA00674WI-D_AML.pdf](https://openairdocs.org/files/sha256/68/ad/68ad328e8fcdcdd6b87872984ceec8d25f4138fa4c9f4270e0f091000263818f)
- January 25, 2011: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/89/fc/89fca57d03587d36c72a4bfc55a6c1d36e29b85615dd8a54905a58d65e1eda44)

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