# STC SA8163NM-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Learjet Inc, United States
- Description: Installation of a Allied Signal Terrain Awareness Warning System
- Applied: September 30, 1999
- Status date: December 23, 2015
- Product: Aircraft, Small/Large Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A10CE](https://openairdocs.org/tcds/A10CE)
- Certificate PDF: https://openairdocs.org/files/sha256/31/7a/317ae3913f69e997ea2e74f39a90c380f9afc7d9573ddb6b3eb0464d34fb1ed6
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DDB08EE13985FD5E8625813F00688E71.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA8163NM-D

## ADs that name it (0)

None.

## Approved models (4)

- Learjet Inc. 35 ([TCDS A10CE](https://openairdocs.org/tcds/A10CE))
- Learjet Inc. 35A (C-21A) ([TCDS A10CE](https://openairdocs.org/tcds/A10CE))
- Learjet Inc. 36 ([TCDS A10CE](https://openairdocs.org/tcds/A10CE))
- Learjet Inc. 36A ([TCDS A10CE](https://openairdocs.org/tcds/A10CE))

## 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: SA8163NM-D This tortifiente issued le Learjet Inc.

One Learjet Way Wichita, Kansas 67209 furt 25* of the Federut twiation Requlations.

*Certification basis is set forth in Tve Certificate Data Sheet A 10CE Original Product Typet ertificate Number: AI0CE Watte: Learjet Model: 35,35A, 36, 36A Description of Type Design Change: . Configuration 1: Installation of a Allied Signal Terrain Awareness Warning System in accordance with FAA Approved Master Drawing List BAS35010048, Revision (D), dated February 14, 2000 or later FAA Approved Revision.

Configuration 2: Installation of a Universal Avionics MFD-640 Multi Function Display, and RP-1008 Radar Control Panel in accordance with FAA Approved Master Drawing List BAS35010048, Revision (D), dated February 14, 2000 or later FAA Approved Revision.

Limitations and Conditions: . 1) This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. 2) The approval of this modification applies to the above noted airplane model series only. 3) A copy of this STC must be included in the permanent records of the modified aircraft. 4) 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.

5) FAA Approved Airplane Flight Manual Supplement Document BAS35040113 Revision (-) FAA Approved on February 21, 2000 or later FAA approved revision, is required as part of configuration 1. 6) FAA Approved Airplane Flight Manual Supplement Document BAS35040114 Revision (-) FAA Approved February 21, 2000 or later FAA approved revision, is required as part of configuration 2.

suspended, rested or a termination date is huwise established by the Administrater of the Federal Aviation Edministration.

Date of Application: September 30, 1999 December 23, 2015 I ate of innernes February 21, 2000 Date Amended:

FEDERAL AVIATION By Direction of the Administrator ( Signature) TOMINISTRATO Keith Johnston ODA administrator ODA-501508-CE. Learjet Inc Wichua, Kansas (Title>

FAA Form 8110 2(10-68)

## Every issue (1)

- December 23, 2015: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/31/7a/317ae3913f69e997ea2e74f39a90c380f9afc7d9573ddb6b3eb0464d34fb1ed6)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.