# STC SA6003NM-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Learjet Inc, United States
- Description: Interior Installation/Modification
- Applied: January 20, 1992
- Status date: December 23, 2015
- Product: Aircraft, Large Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A21EA](https://openairdocs.org/tcds/A21EA)
- Certificate PDF: https://openairdocs.org/files/sha256/fa/00/fa00f5582e4e3bba018cdb65f68772330a50c852979665981fed40ec0eae4058
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/47A0E597E1247D1486258314005DA9FE.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA6003NM-D

## ADs that name it (1)

- [AD 97-25-11](https://openairdocs.org/ad/97-25-11): Modification IAW Document List CA-1000-TUC, Rev H (Learjet STC SA6003NM or SA6003NM-D). Effective Dec 23, 1997. Named in the applicability

## 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.

SA6003NM-D

Learjet Inc.

One Learjet Way Wichita, Kansas 67209 25*

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

A21AE Canadair CL-600-2A12 / 2B16

: Interior Installation / Modification in accordance with DAS approved Learjet Master Document List No. CA-1000-TUC, Revision “N”, dated January 05, 1995 or later DAS Approved Revision. FAA Approved Learjet Airplane Manual Supplement: C1002, Original Release, dated March 5, 1993; C1003, Original Release, dated February 23, 1993; C1004, Original Release, dated February 23, 1993; and C1005, Original Release, dated March 10, 1993; C1011, Original Release, dated October 12, 1993 or later DAS Approved Revision, is required as part of this modification.

: 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 the permission.

January 20, 1992

March 19, 1993

December 19, 2005;

December 23, 2015 January 05, 1995; May 3, 2002

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.**

## Every issue (2)

- December 23, 2015: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/fa/00/fa00f5582e4e3bba018cdb65f68772330a50c852979665981fed40ec0eae4058)
- December 19, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/4c/19/4c19b4f1fffdb1eb700532ab0c9bc1690f704119c46627cce789e8aa6499aeb6)

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