# STC SA00228WI-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Rockwell Collins Inc, United States
- Description: Installation of Collins EFIS-84 Electronic Flight Instrument System (4 tube), Collins Dual MCS-65 Compass System, and Collins Dual 332D-11T Vertical Gryo System.
- Applied: November 13, 1995
- Status date: November 7, 1997
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A18SW](https://openairdocs.org/tcds/A18SW)
- Certificate PDF: https://openairdocs.org/files/sha256/a4/c0/a4c000bfb3194b597cfd5b7b553c8d85368d908f75631bc4921c795a566c914a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/83275D4D48DE6B0B862572D600551693.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00228WI-D

## ADs that name it (0)

None.

## Approved models (2)

- M7 Aerospace LP SA227-CC ([TCDS A18SW](https://openairdocs.org/tcds/A18SW))
- M7 Aerospace LP SA227-DC (C-26B) ([TCDS A18SW](https://openairdocs.org/tcds/A18SW))

## 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: SA00228WI-D This certificate issued to: Rockwell Collins, Inc.

400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498 Purt 23 of the Federal Aviation ¡Regulations, and Special Conditions 23-CE-85.

Original Product Type Fertificate Number: A18SW Make: Fairchild Aircraft Incorporated Model: SA227-CC, SA227-DC Lescrip/ion c/ Type Laiya CAnge: Installation of Collins EFIS-84 Electronic Flight Instrument System (4 tube), Collins Dual MCS-65 Compass System, and Collins Dual 332D-11T Vertical Gyro System in accordance with:

(1) Collins Drawing Index 992-1998-001, Revision A, dated January 29, 1996; (2) Collins Airplane Flight Manual Supplement (AFMS) ACC-95-98, no revision, dated January 29, 1996; and (3) Maintenance Manual Supplement, ACC-96-4, no revision, dated January 29, 1996, or later FAA Approved revisions to (1), (2) or (3).

Limitations and Conditions: (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.

Administruter of the Federal Aviation Administration , Lute c/ appfiretion : November 13, 1995 Date Reissued: April 8, 1996; November 7, 1997 Dule of idamunce : January 29, 1996 Dule untended: February 29, 1996 FEDERAL AVIATIO By Direction of the Administrator (Signature) Dale R. Koonts

TOMINISTRATO Manager, DAS-3CE (Title) f this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding ) years, or both.

## Every issue (1)

- November 7, 1997: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a4/c0/a4c000bfb3194b597cfd5b7b553c8d85368d908f75631bc4921c795a566c914a)

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