# STC SA642NE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Bombardier Completion Center Inc
- Description: Installation of a passenger interior and avionics.
- Status date: February 4, 2000
- Data sheets: A21EA
- Certificate PDF: https://openairdocs.org/files/sha256/88/08/88086befd45338fc4c609ddc4b24a4e6ff49a77b535a139b28495f4ffb4e8710
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/99D07FC3B063115586257D15006BC4C1.0001
- Page: https://openairdocs.org/stc/SA642NE

## ADs that name it

None.

## Approved models (1)

- Bombardier Inc. CL-600-2B16 (CL-601-3A) (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.

Par t 25 of the Federal Aviation R egulations.

Original Product Type Certificate N umber:

M ake:

M odel:

Configuration 1: Installation of a Passenger Interior and Avionics in accordance with I.A.E.L. Modification List ML 14367 Revision C, dated February 17, 1989.

Configuration 2: Installation of a Passenger Interior and Avionics in accordance with I.A.E.L. Modification List ML 14467 Revision A, dated May 4, 1989.

Configuration 3: Installation of a Passenger Interior and Avionics in accordance with I.A.E.L. Modification List ML 100004 Re vision B, dated February 23, 1990.

1. For Configuration 1: The Canadian Department of Transport approved Flight Manual Supplement CL-600-IAEL-125 Installation of Single Stand Alone Global GNS-X Navigation Management System (NMS)/ Airborne Flight Information System (AFIS), Original Issue, dated March 17, 1989, is required.

Bombardier Completion Center Inc.

200 Cote Vertu West Dorval, Quebec H4S 2A3 Canada

A21EA Bombardier, Inc.

CL–600–2B16 (601-3A), S/N 5028, 5032, 5049 Date reis sued: February 4, 2000

Date amended : June 12, 1989, March 30, 1990

B y direction of the A dministrator

(Signature) Gaetano Sciortino Manager New York Aircraft Certification Office

(Title)

Date of application : February 21, 1989

Date of issuance : March 22, 1989

FAA Form 8110-2-1(10-69) Page 3 of 3

N umber SA642NE Date Reissued: February 4, 2000

2. For Configuration 1: The Canadian Department of Transport approved Flight Manual Supplement CL-601-IAEL-104, Installation of Scott Gaseous Oxygen System, Original Issue, dated July 10, 1987, is required.

3. For Configuration 1, 2 and 3: The Canadian Department of Transport approved Flight Manual Supplement CL-600-IAEL-

119. Baggage Compartment Smoke Detector System, Original Issue dated August 4, 1988, is required.

4. For Configuration 1, 2 and 3: The Canadian Department of Transport approved Flight Manual Supplement CL-600-IAEL- 126, Installation of a Sundstrand MKV, GPWS, Original Issue dated March 17, 1989, is required.

Note: Mod 7 of the Sundstrand MK V GPWS is not operative in Canada.

5. For Configuration 2 and 3: The Canadian Department of Transport approved Flight Manual Supplement CL-600-IAEL- 110, Installation of Honeywell Lasertrak Navigation Display Unit, Original Issue, dated December 2, 1987 is required.

6. For Configuration 2: The Canadian Department of Transport approved Flight Manual Supplement CL-600-IAEL-127, Installation of Solid State Passenger Oxygen System, Original Issue, dated May 29, 1989 is required.

7. For Configuration 2: The Canadian Department of Transport approved Flight Manual Supplement CL-600-IAEL-128, Installation of a Honeywell Primus 870 Coloradar System with Honeywell LSZ-850 Lightning Sensor System, Original Issue, dated May 29, 1989 is required.

8. For Configurations 3: The Canadian Department of Transport approved Flight Manual Supplement CL-600-IAEL-128, Installation of a Honeywell Primus 870 Coloradar System with Honeywell LSZ-850 Lightning Sensor System, Rev. A, dated June 12, 1989 is required.

9. For Configuration 3: The Canadian Department of Transport approved Flight Manual Supplement CL-600-IAEL-134, Installation of a Scott Gaseous Oxygen System, Original Issue dated September 11, 1989.

10. The following Maintenance and Inspections must be complied with:

a. Maintenance Procedures Gaseous Oxygen System, Report No. TM-601-874, issue A, dated June 13, 1986 for configuration 1.

b. Maintenance Instructions for Scott Solid State Oxygen System, Report No. MEC0566-0140, Revision A, dated November 28, 1988 for configuration 2.

c. Inspection of AFT overboard servicing report No. TM0375-0010, issue NC, dated June 28, 1988, is required with configuration 1, 2, and 3.

d. Operational Instructions for Scott Solid State Passenger Oxygen, Report No. TM0375-0200, issue NC, dated May 4, 1989 is required with configuration 2.

e. Maintenance Procedures Gaseous Oxygen System, Report No. TM0706-0004 Issue B, dated September 14, 1989 for configuration 3.

11. Configuration 1 is eligible only on airplane Serial Number 5028.

Configuration 2 is eligible only on airplane Serial Number 5032.

Configuration 3 is eligible only on airplane Serial Number 5049.

12. You cannot use descriptive data about this design change to duplicate other products. This approval is limited to only the installation made in Bombardier, Inc. Model CL–600–2B16 (601-3A), S/N 5028, 5032, 5049. This STC does not permit manufacturing of parts for multiple installations.

----END----

## Every issue (1)

- February 4, 2000: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/88/08/88086befd45338fc4c609ddc4b24a4e6ff49a77b535a139b28495f4ffb4e8710)

---
From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.
