# STC SA01170LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Sandel Avionics LLC, United States
- Description: :   Installation of Sandel Avionics SN3308 Navigation Display Unit in accordance with FAA Approved Sandel Avionics Master Drawing List, Document No. ST8691LA-A-01, Revision "B", dated May 14, 2001, or later FAA approved revision.  FAA Approved Airplane Flight Manual Supplement, Document No. ST8691LA-A-09, Revision "N/C", dated June 01, 2001, or later FAA approved revision.
- Applied: January 4, 2011
- Status date: June 23, 2021
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A00009CH](https://openairdocs.org/tcds/A00009CH)
- Certificate PDF: https://openairdocs.org/files/sha256/de/23/de2364244792a0d833685dd9a7b365375c4bda38ecc11e2e42124273edeb32e0
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A7B3AA1DD853AD0D8625875D006C9F83.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01170LA

## ADs that name it (0)

None.

## Approved models (1)

- Cirrus Design Corporation SR20 ([TCDS A00009CH](https://openairdocs.org/tcds/A00009CH))

## 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 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Part of .

SA01170LA Sandel Avionics, Inc.

1370 Decision Street, Suite D Vista, CA 92081 23 the Federal Aviation Regulations A00009CH Cirrus Design Corporation SR20 Series

Installation of Sandel Avionics SN3308 Navigation Display Unit in accordance with FAA Approved Sandel Avionics Master Drawing List, Document No.

ST8691LA-A-01, Revision "B", dated May 14, 2001, or later FAA approved revision. FAA Approved Airplane Flight Manual Supplement, Document No. ST8691LA-A-09, Revision "N/C", dated June 01, 2001, or later FAA approved revision.

This approval should not be incorporated in an 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 pennit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

January 4, 2001

June 23, 2021 June 6, 2001

Manager, Technical & Administrative Support Section Los Angeles ACO Branch 2

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___

SA01170LA 2

## Every issue (3)

- June 23, 2021: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/de/23/de2364244792a0d833685dd9a7b365375c4bda38ecc11e2e42124273edeb32e0)
- November 10, 2011: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/93/87/9387378b39dd97151947412c77d9b08ee2db36b1a76bab0e130b26719c497c25)
- June 6, 2011: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/00/a9/00a9c7d7836c6897402947c16cb057f44746048f8fdcb78ac4ad147b68d675e6)

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