# STC SA8139NM-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Learjet Inc, United States
- Description: Installation of a Collins VHF-22C Comm System with CTL-22C.
- Applied: November 25, 1998
- Status date: December 23, 2019
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A21EA](https://openairdocs.org/tcds/A21EA)
- Certificate PDF: https://openairdocs.org/files/sha256/fe/77/fe773503fab47472acd5d7af1d23eaa5d062cce3fee07fbf21f829de98f06b06
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/41F55819835D7CBB86258450005093B9.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA8139NM-D

## ADs that name it (0)

None.

## Approved models (5)

- Bombardier Inc. CL-600-1A11 (CL-600) ([TCDS A21EA](https://openairdocs.org/tcds/A21EA))
- Bombardier Inc. CL-600-2A12 (CL-601) ([TCDS A21EA](https://openairdocs.org/tcds/A21EA))
- Bombardier Inc. CL-600-2B16 (CL-601-3A) ([TCDS A21EA](https://openairdocs.org/tcds/A21EA))
- Bombardier Inc. CL-600-2B16 (CL-601-3R) ([TCDS A21EA](https://openairdocs.org/tcds/A21EA))
- Bombardier Inc. CL-600-2B16 (CL-604) ([TCDS A21EA](https://openairdocs.org/tcds/A21EA))

## 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) Number SA8139NM-D

This Certificate issued to Learjet Inc.

One Learjet Way Wichita, Kansas 67209 Part 25* of the Federal Aviation Regulations. *Certification basis is set forth in Type Certificate Data Sheet A21EA

A21EA

**CANADAIR CL-600-1A11, CL-600-2A12, CL-600-2B16**

Description of Type Design Change: Installation of a Collins VHF-22C Comm System with CTL-22C, in accordance with FAA Approved Master Drawing List No. BAS63010060, Revision “-”, dated December 17, 1998, or later FAA Approved Revision. FAA Approved Flight Manual Supplement required for this installation is listed on the approved Master Drawing List.

Limitations and Conditions : 1) This installation should not be incorporated in any aircraft unless it is d the interrelationship between this installation and any previou sly approved configuration will not introdu c effect upon the airworthiness of the aircraft. 2) If the holder agrees to permit another person to use this certific product, the holder shall give the other person written evidence of that permission.

Date of application : November 25, 1998

Date of issuance : December 19, 1998

Date reissued : December 23, 2015

Date amended : February 26, 1999; March 26, 1999; April 12, 1999

Original signed by Keith Johnston

( Signature) Keith Johnston ODA administrator ODA-501508-CE, Learjet Inc.

W i c h i t a , K a n s a s (Title)

NOTE:

**DO NOT DELETE THIS PAGE.**

**DO NOT ADD ANY DATA TO THIS PAGE.**

**THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.**

## Every issue (2)

- December 23, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/fe/77/fe773503fab47472acd5d7af1d23eaa5d062cce3fee07fbf21f829de98f06b06)
- December 23, 2015: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/fe/77/fe773503fab47472acd5d7af1d23eaa5d062cce3fee07fbf21f829de98f06b06)

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