# STC SA01472WI-D

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Rockwell Collins Inc, United States
- Description: Modification of a Rockwell Collins Weather Radar System installation
- Applied: January 18, 2008
- Status date: October 14, 2011
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A1WI](https://openairdocs.org/tcds/A1WI), [TCDS 3A20](https://openairdocs.org/tcds/3A20), [TCDS A00010WI](https://openairdocs.org/tcds/A00010WI), [TCDS A24CE](https://openairdocs.org/tcds/A24CE), [TCDS A59EU](https://openairdocs.org/tcds/A59EU)
- Certificate PDF: https://openairdocs.org/files/sha256/ad/f5/adf5905cd9aab669e6622d5e8699edd09554a2a2ead9d8d8ffc3b4169ab589ef
- Approved model list and other attachments: [SA01472WI-D_AML.pdf](https://openairdocs.org/files/sha256/a5/08/a50811988d02a4d9e2e58279373c7257d366a069913f414f3e6bd0434ec11159)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5F475F3C1E77E71E86257A8D0069708F.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01472WI-D

## ADs that name it (0)

None.

## Approved models (33)

- Cessna Aircraft Company 525 ([TCDS A1WI](https://openairdocs.org/tcds/A1WI))
- Cessna Aircraft Company 525A ([TCDS A1WI](https://openairdocs.org/tcds/A1WI))
- Cessna Aircraft Company 525B ([TCDS A1WI](https://openairdocs.org/tcds/A1WI))
- Hawker Beechcraft Corporation 1900 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- 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 390 ([TCDS A00010WI](https://openairdocs.org/tcds/A00010WI))
- Hawker Beechcraft Corporation B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C (C-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C (C-12R) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C (UC-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C (UC-12M) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B300C (MC-12W) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B300C (UC-12W) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation C90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation C90A ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation C90GT ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation C90GTi ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation E90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation H90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Piaggio Aero Industries S.p.A. P-180 ([TCDS A59EU](https://openairdocs.org/tcds/A59EU))

## What the certificate says

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA01472WI-D This certificate issued to: Rockwell Collins, Inc.

400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498 Burt "of the " Requations.

Criqiant Preduct Type Certificate Vinter: * *See attached FAA Approved Model List (AML) Make: No. SA01472WI-D for list of approved airplane models Model: and applicable airworthiness regulations.

deseriplion of Type Lestyn Chunge: Modification of a Rockwell Collins Weather Radar System installation in accordance with Rockwell Collins Master Drawing List as listed on AML No. SA01472WI-D, Revision -, dated March 31, 2008, or later FAA approved revision.

(1) Prior FAA approved installation of a Rockwell Collins Weather Radar Receiver/Transmitter/Antenna as listed in Table 1 of Rockwell Collins Aircraft Equipment Matrix document number RCA-2462, Revision -, dated January 7, 2008, or later FAA approved revision, is a prerequisite to this STC.

(2) Installer shali verify that the existing airplane radome is compliant with RTCA Minimum Operation Performance Standards (MOPS) for nose mounted radomes DO-213 Class A Category 1 or equivalent.

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

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

(5) A copy of this Certificate and FAA Approved Model List (AML) No. SA01472WI-D issued March 31, 2008, or later FAA approved revision, must be maintained as part of the permanent records for the modified aircraft.

(6) 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.

Administrater of the Federal Aviation Administration .

But of upficuirn: January January 2008 Jut risined:

Let o/ Ence : March 31, 2008 Date Amended:

FEDERAL AVIATION By directica c/ Uhr. Astavinistruter Quites Boter (Signature) TOMNISTRATO John S. Bohn Administrator, DAS-500864-CE (Title)

**PAA FOR ST**

### SA01472WI-D_AML.pdf

**FAA APPROVED MODEL LIST (AML) NO. SA01472WI-D**

**ROCKWELL COLLINS, INC.**

FOR

MODIFICATION OF A ROCKWELL COLLINS WEATHER RADAR SYSTEM INSTALLATION IN 14 CFR PART 23 AIRCRAFT Issue Date: March 31, 2008 Page 1 of 2 ITEM

**AIRCRAFT MAKE**

**AIRCRAFT MODEL**

**ORIGINAL TYPE**

**CERTIFICATE NUMBER**

**CERTIFICATION BASIS FOR**

**ALTERATION**

**INSTALLATION**

**INSTRUCTIONS AFM**

**SUPPLEMENT**

**NUMBER/DATE AML**

**AMENDMENT DATE MASTER**

**DRAWING LIST NO.**

**REVISION NO.**

AND DATE[1]

1 Cessna Aircraft Company 525 (CJ1) 525A (CJ2) 525B (CJ3) A1WI TCDS A1WI Revision 19 March 1, 2011 RCA-0161-001 Rev C, 10/14/11 RCA-0167 Rev A, 04/04/09 10/14/11

2 Hawker Beechcraft Corporation 390 (Premier I) A00010WI TCDS A00010WI Revision 8 March 26, 2007 RCA-0161-001 Rev C, 10/14/11 RCA-0167 Rev A, 04/04/09 10/14/11

3 Hawker Beechcraft Corporation 200 200C 200CT 200T B200 B200C B200CT B200T 300 300LW B300 B300C 1900 1900C 1900D A24CE TCDS A24CE Revision 101 September 14, 2011 RCA-0161-001 Rev C, 10/14/11 RCA-0167 Rev A, 04/04/09 10/14/11

[1] Or later FAA approved revision

**FAA APPROVED MODEL LIST (AML) NO. SA01472WI-D**

**ROCKWELL COLLINS, INC.**

FOR

MODIFICATION OF A ROCKWELL COLLINS WEATHER RADAR SYSTEM INSTALLATION IN 14 CFR PART 23 AIRCRAFT Issue Date: March 31, 2008 Page 2 of 2 ITEM

**AIRCRAFT MAKE**

**AIRCRAFT MODEL**

**ORIGINAL TYPE**

**CERTIFICATE NUMBER**

**CERTIFICATION BASIS FOR**

**ALTERATION**

**INSTALLATION**

**INSTRUCTIONS AFM**

**SUPPLEMENT**

**NUMBER/DATE AML**

**AMENDMENT DATE MASTER**

**DRAWING LIST NO.**

**REVISION NO.**

AND DATE[1]

4 Piaggio Aero Industries S.p.A Piaggio P-180 A59EU TCDS A59EU Revision 20 March 21, 2011 RCA-0161-001 Rev C, 10/14/11 RCA-0167 Rev A, 04/04/09 10/14/11

5 Hawker Beechcraft Corporation B90 C90 C90A C90GT C90GTi E90 H90 3A20 TCDS 3A20 Revision 70 June 2, 2011 RCA-0161-001 Rev C, 10/14/11 RCA-0167 Rev A, 04/04/09 10/14/11

[1] Or later FAA approved revision

FAA Approved: Original signed by Steve Brune

STC ODA Administrator, ODA-500864-CE Amended: September 19, 2008, April 4, 2009, October 14, 2011

## Every issue (2)

- October 14, 2011: Amended, Current. [certificate](https://openairdocs.org/files/sha256/ad/f5/adf5905cd9aab669e6622d5e8699edd09554a2a2ead9d8d8ffc3b4169ab589ef), [SA01472WI-D_AML.pdf](https://openairdocs.org/files/sha256/a5/08/a50811988d02a4d9e2e58279373c7257d366a069913f414f3e6bd0434ec11159)
- March 31, 2008: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/60/d6/60d6079e45e7f4dfe736f91b8b58ad4c98d3b3b6887cdba2964800a5c1c3cdea), [SA01472WI-D_.Rockwell Collins.pdf](https://openairdocs.org/files/sha256/d0/b7/d0b718255a4119230adca9baac68bbb2d9d1e6c1af8b8b71de8f90ebb7df8208)

---
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.
