# STC SA01894LA

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Universal Avionics Systems Corp, United States
- Description: Installation of Universal Avionics Terrain Awareness and Warning System Class A and Class B Displayed on EFI-890
- Applied: December 14, 2004
- Status date: April 14, 2010
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/89/b4/89b4b3adff2231ff4ce1ad19544daf629862f9284ae5069e849943d0a26606c3
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/33219F974573606D862577B30061A6AD.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01894LA

## ADs that name it (0)

None.

## Approved models (21)

- Hawker Beechcraft Corporation 1900 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 1900C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 1900D ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 300LW ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C (C-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C (C-12R) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C (UC-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C (UC-12M) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200CGT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200GT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B300C (C-12W) ([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 SAO1894LA This certificate issued to: Universal Avionics Systems Corporation 3260 East Universal Way Tucson, Arizona 85706-5021 Part *23 of the Federal Joviation Regulations (*Certification basis is set forth in Type Certificate Data Sheet A24CE) Original Product Type Certificate Number: A24CE Hawker Beechcraft Model: King Air Series 200, 200C, 200CT, 200T, B200, B200C, B200CT, B200T, B200GT, B200CGT, 300, 300LW, B300, B300C, 1900, 1900C, 1900D Description of Type Design Change:

Installation of Universal Avionics Terrain Awareness and Warning System Class A and Class B Displayed on EFI-890, in accordance with FAA Approved Master Drawing List, Document No.

MDL-2004-1006, Revision "B", dated December 13, 2005, or later FAA approved revision.

Limitations and Conditions: This approval should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previous approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft.

If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.

This certificate and the supporting data which is the basis for approval shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise estublished by the Administrator Date of Application: December 14, 2004 Date Reissued:

Date of Issuance: April 25, 2006 Date Amended: September 4, 2008, April 14, 2010 FEDERAL AVIATION By Direction of the Administrator lan JOhnse E (Signature) TOMINISTRATIO Angeles Aircraft Certification Office Manager, Systems & Equipment Branch, Los (Title)

## Every issue (1)

- April 14, 2010: Amended, Current. [certificate](https://openairdocs.org/files/sha256/89/b4/89b4b3adff2231ff4ce1ad19544daf629862f9284ae5069e849943d0a26606c3)

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