# STC SA2217CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc, United States
- Description: Installation of Sperry Instrument monitor system, Model CM-400.
- Status date: December 13, 2016
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A16SW](https://openairdocs.org/tcds/A16SW)
- Certificate PDF: https://openairdocs.org/files/sha256/a1/50/a15011d622fed3ee8e9ce96bb68ce8c87bed1dc233d148defb7d3ad699ae1298
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/644654A2003C26748625814C006F2B97.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2217CE

## ADs that name it (0)

None.

## Approved models (2)

- Raytheon Aircraft Company 400 ([TCDS A16SW](https://openairdocs.org/tcds/A16SW))
- Raytheon Aircraft Company MU-300-10 ([TCDS A16SW](https://openairdocs.org/tcds/A16SW))

## 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 Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 2 SA2217CE Federal Aviation Regulations * 25 Beech Aircraft Corporation A16SW 400; MU-300-10 *effective February 1, 1965, Amendments 25-1 through 25-40, with specific paragraphs of Amendments 25-41 and 25-46 as delineated on Type Certificate Data Sheet A16SW.

Installation of Sperry Instrument Monitor System, Model CM-400, in accordance with:

1. Omni Tech, Inc. Top Drawing No. BJCM000, Revision D, dated December 12, 1986; and

2. FAA approved Airplane Flight Manual Supplement BJCM900, Revision None, dated December 17, 1986; or later FAA approved revisions of 1 or 2.

This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of these other previously approved modifications will introduce no adverse effect upon the airworthiness of the airplane. 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.

February 17, 1987; April 15, 1996;

March 26, 2007; December 13, 2016 September 5, 1986 December 17, 1986 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 13, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a1/50/a15011d622fed3ee8e9ce96bb68ce8c87bed1dc233d148defb7d3ad699ae1298)
- March 26, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/9b/b0/9bb029d551389a4c727f598d9f399a3986ee150159b7dd1fa68adc189724d4b7)

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