# STC SA2358CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc, United States
- Description: Category II certification.
- 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/sha256/0b/af/0baf464be637b00d612e430410a5a448223d8710ab5f6b4adf34eeed697905fa
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FB7B2D68736664658625814D0044ABD1.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2358CE

## ADs that name it (0)

None.

## Approved models (2)

- Hawker Beechcraft Corporation 400 ([TCDS A16SW](https://openairdocs.org/tcds/A16SW))
- Hawker Beechcraft Corporation 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 SA2358CE Federal Aviation Regulations * 25 A16SW 400; MU-300-10 Category II certification, in accordance with:

1. OMNI-Tech, Inc. Top Drawing No. 25C2000, Revision A, dated February 4, 1988; and

2. FAA approved Airplane Flight Manual Supplement No. 25C2900, Revision None, dated February 11, 1988, or later FAA approved revisions of 1 or 2.

Beech Aircraft Corporation *effective February 1, 1965, Amendments 25-1 thru 25-40 with specific paragraphs of Amendments 25-41 and 25-46 as delineated on Type Certificate Data Sheet A16SW.

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 those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane. This installation requires prior or concurrent installation of STC SA2218CE, Second Flight Director, and STC SA2338CE, Three Tube EFIS. 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.

April 15, 1996; March 26, 2007;

December 13, 2016 August 24, 1987 February 11, 1988 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/sha256/0b/af/0baf464be637b00d612e430410a5a448223d8710ab5f6b4adf34eeed697905fa)
- March 26, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/cf/8f/cf8fc1db552c8a10cb73c528dda05d96af63cbf27ad67930bdd0b329839c2e01)

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