# STC SA01458LA

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Universal Avionics Systems Corp, United States
- Description: Installation of Universal Avionics Unilink 60X/70X Airborne Communications System.
- Applied: February 6, 2002
- Status date: August 31, 2004
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/ca/c9/cac942c7dfa87f57dbaa846a50620d393ae5787fb904cdff624963871883cb93
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B0BE20B245FEF9DD86256F3400722598.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01458LA

## ADs that name it (0)

None.

## Approved models (1)

- Raytheon Aircraft Company B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))

## 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(10-68) Page 1 of 2 Number SA01458LA This Certificate issued to Universal Avionics Systems Corporation 3260 East Universal Way Tucson, Arizona 85706

Part *23 of the Federal Aviation Regulations. (*Certification basis is set forth in Type Certificate Data Sheet A24CE)

Original Product Type Certificate Number : A24CE Make : Raytheon Aircraft Company

B300 King Air Series Model :

Description of Type Design Change: Installation of the Universal Avionics Unilink 60X/70X Airborne Communications System in accordance with FAA Approved Master Installation Drawing List, Drawing No.

MDL-1004, Revision “E”, dated January 16, 2003 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.

The Unilink 60X/70X integrates with separately approved system installations. Adherence to the limitations in the appropriate Airplane Flight Manual Supplements for those systems is mandatory.

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.

Date of application : February 6, 2002

Date of issuance : June 6, 2003 Date reissued:

Date amended : August 31, 2004

( Signature) Manager, Flight Test Branch Los Angeles Aircraft Certification Office

(Title)

Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street)

(City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street)

(City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

FAA Form 8110-2-1(10-69) Page 2 of 2

## Every issue (1)

- August 31, 2004: Amended, Current. [certificate](https://openairdocs.org/files/sha256/ca/c9/cac942c7dfa87f57dbaa846a50620d393ae5787fb904cdff624963871883cb93)

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