# STC SA8072NM-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Learjet Inc., United States
- Description: Installation of Interior Modification
- Applied: October 25, 1996
- 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/c0/55/c055889b0fbc2e0dc6149c1064c99df2cb1b35e292f4d676db6c15f95ad3357b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/096D09D36B65BEA2862583140064B2C3.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA8072NM-D

## ADs that name it (2)

- [AD 2001-02-05](https://openairdocs.org/ad/2001-02-05): Fuel Service Panel · Bombardier CL-600-2B16 (CL-604) with STC SA8060NM-D or 2 others. Effective Mar 5, 2001. Named in the applicability
- [AD 2000-01-51](https://openairdocs.org/ad/2000-01-51) (historical): Fuel Service Panel Maintenance Light · Bombardier CL-600-2B16 (CL-604) with STC SA8060NM-D or 2 others. Effective Jan 7, 2000. Named in the applicability

## Approved models (3)

- 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.

SA8072NM-D

Learjet Inc.

One Learjet Way Wichita, Kansas 67209 25*

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

A21EA Canadair CL-600-2B16

: Installation of Interior Modification in accordance with DAS Approved Master Document List No. CA-3000b-TUC, Revision (D), dated April 10, 1997, or later DAS Approved Revision. DAS Approved Learjet Airplane Flight Manual Supplement Documents C1051 approved on April 13, 1997, C1052 approved on April 13, 1997, C1053 approved on April 13, 1997, C1055 approved on April 13, 1997, C1070 approved on April 13, 1997 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) This installation declassifies the Type III over wing exit to a Type IV over wing exit, thereby limiting the maximum number of passengers to (9) nine.

October 25, 1996

April 14, 1997

December 23, 2015

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/c0/55/c055889b0fbc2e0dc6149c1064c99df2cb1b35e292f4d676db6c15f95ad3357b)
- April 14, 1997: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/d3/a3/d3a3f7395ca3c40a9eab6b7e1ff2819e9f1f974954728e2d733b41a0b20587be)

---
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.