# STC SA00002MC-D

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Rockwell Collins Inc, United States
- Description: Installation of Collins FDS-255 Flight Display System.
- Applied: February 25, 2005
- Status date: May 17, 2006
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/99/f8/99f87d1d6b305c59c9951b611c356a06f590f8b7c8f36f3ccb65f0e01599eb6b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7D135B0F74FEC2C28625717E004D47C3.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00002MC-D

## ADs that name it (0)

None.

## Approved models (1)

- Raytheon Aircraft Company 1900C (C-12J) ([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.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00002MIC-D This certificate issued to: Rockwell Collins, Inc.

400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498 Furt 23 of the Federal Aviation

•Regulutions, and Special Condition 23-115-SC.

Original Product Type Certificate Number : A24CE Make: Raytheon Aircraft Company Model: 1900C (C-12J) Description of Type Design Change: Installation of Collins FDS-255 Flight Display System, TCAS II Traffic Alert and Collision Avoidance System, Collins FMS-3000 Flight Management System, Collins ARC-210 VHF/UHF Communications System, and Allied Signal EGPWS System in accordance with (1) Collins Drawing Index RCA-0092-001, Revision (A) dated March 27, 2006, (2) Collins Airplane Flight Manual Supplement AAC-0341-001, Revision (A) dated March 31, 2006, (3) Collins Maintenance Manual Supplement AAC-8116-001, Revision (A) dated March 27, 2006, or later FAA approved revisions of (1), (2) and (3).

Limitations and Conditions: (1) Prior FAA approved installation of Shadin Air Data Computer, Part Number 962830AR-3-S-1, shall be determined by the installer; it is a prerequisite to this STC installation. (2) Compatibility of this design change with previously approved modifications must be determined by the installer. (3) 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 .

Date of Application: February February 2005 Date Reissued:

Lute of sunce: January 25, 2006 Date Amended: May 17, 2006 FEDERAL AVIATION By Direction of the Administrator JohnS Bohn (Signature) John'S. Bohn TOMINSTRATO Administrator, DAS-500864-CE (Title)

PAA FORM 8110-2 (10-68) PAGE 1 of 1 PAGES

## Every issue (1)

- May 17, 2006: Amended, Current. [certificate](https://openairdocs.org/files/sha256/99/f8/99f87d1d6b305c59c9951b611c356a06f590f8b7c8f36f3ccb65f0e01599eb6b)

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