# STC SA8054NM-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Learjet Inc, United States
- Description: Installation of a Honeywell TCAS II.
- Applied: August 1, 1994
- Status date: December 23, 2015
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A21EA](https://openairdocs.org/tcds/A21EA)
- Certificate PDF: https://openairdocs.org/files/sha256/ca/d7/cad78070cbf73cd81e895de55602aace42dadbebe84dded86944a3f3774d0ad4
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2B08A126ACB23EE8862583140064A220.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA8054NM-D

## ADs that name it (0)

None.

## Approved models (4)

- 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.

Learjet Inc.

One Learjet Way Wichita, Kansas 67209 25*

(*For Certification Basis see T.C.D.S. A21EA)

A21EA Canadair CL600-2A12 / 2B16 : Installation of a Honeywell TCAS II in accordance with DAS Approved Learjet Master Document List No. CA-1024b-TUC, Revision (B), dated February 06, 1995, or later DAS Approved Revision. DAS Approved Learjet Airplane Flight Manual Supplement Document C1028, DAS Approved on February 07, 1995, or later DAS Approved Revision, is required as part of this modification. FAA Accepted Maintenance Instructions for Continued Airworthiness (ICA) are contained in Document Number TE-MMS-1024b, Revision (B), dated August 18, 2008, or later FAA Accepted Revision.

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 n ot introduce any adverse effect upon the airworthiness of the aircraft. 2) A copy of this STC must be included in the permanent records of the modified aircraft. 3) If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

August 01, 1994

February 09, 1995

December 23, 2015

August 26, 2008

Original signed by Keith Johnston

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

Wichita, Kansas (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.**

SA8054NM-D Date of Issuance: February 09, 1995 Date Amended: August 26, 2008

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## Every issue (2)

- December 23, 2015: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ca/d7/cad78070cbf73cd81e895de55602aace42dadbebe84dded86944a3f3774d0ad4)
- August 26, 2008: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/4d/67/4d676de3dbcab3234ef1a312e006fb3f99f37273bb3673afbd78fc8bf855e1a0)

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