# STC SA01177WI-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc, United States
- Description: Installation of Collins Pro Line 21 Avionics System.
- Applied: November 19, 2001
- Status date: December 12, 2016
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/16/a8/16a831f4f49cdc67d1899887e4b9aaa87d55db94ed5277d8f5bdb65f9c205ae5
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3EC99710B62BF9F68625814800664DB4.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01177WI-D

## ADs that name it (0)

None.

## Approved models (2)

- Hawker Beechcraft Corporation B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B300C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))

## 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

Part of the

Signature

Title *Special Conditions 23-131-SC, and Equivalent Level of Safety ACE-02-17 for FAR 23.1305(c)(2), 23.1305(a)(2)(3), and

23.1549(a)(b)(c)(d), for direct reading digital only displays for oil pressure, oil temperature, and fuel flow.

SA01177WI-D Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 23 Federal Aviation Regulations * Raytheon Aircraft Company B300/B300C King Air 2 A24CE Installation of Collins Pro Line 21 Avionics System in accordance with:

1. Collins Drawing Index 130-340634, Revision (--), dated December 2, 2002;

2. Collins Airplane Flight Manual Supplement AAC-0291-001, Revision (--), dated July 7, 2003; and

3. Collins Maintenance Manual Supplement AAC-0292-001, Revision (--), dated July 7, 2003; or later approved revisions of 1, 2 and 3.

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

2. 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.

3. Prior FAA approved installation of the Honeywell Enhanced Ground Proximity System, P/N 965-1206-010, shall be determined by the installer.

4. Prior FAA approved installation of BF Goodrich Skywatch, HP System Model SKY899, shall be determined by the installer.

August 21, 2003; March 26, 2007;

December 12, 2016 November 19, 2001 July 7, 2003 Mark Fuller STC ODA administrator ODA-100129-CE

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

To (Name and address of transferee)

From (Name and address of grantor)

## Every issue (2)

- December 12, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/16/a8/16a831f4f49cdc67d1899887e4b9aaa87d55db94ed5277d8f5bdb65f9c205ae5)
- March 26, 2007: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/5f/ff/5ffff099861dba8c2456fa7b92444919d07413c2bb9d94bae044d72fd0e24efa)

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