# STC ST00047WI

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Learjet Inc., United States
- Description: Installation of a bulkhead across fuselage station 353 with a hinged swinging door and magazine racks.
- Applied: October 15, 1992
- Status date: May 27, 2021
- Product: Aircraft, Large Airplane
- Certification basis: Part 25
- Data sheets: [TCDS A21EA](https://openairdocs.org/tcds/A21EA)
- Certificate PDF: https://openairdocs.org/files/sha256/a4/e5/a4e505395debcc70ebe8f46b9744735dfd2a9567f1ae9674912d76775309ca03
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F02C808EDA751979862586E7005C4118.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/ST00047WI

## 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.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Original signed by Keith Johnston ST00047WI Learjet Inc.

One Learjet Way Wichita, KS 67209 25 the Federal Aviation Regulations A21EA Bombardier Inc.

CL-600-2A12 CL-600-2B16 Installation of a bulkhead across fuselage station 353 with a hinged swinging door and magazine racks per Precision Pattern Drawing Number CA-1021-TUC stamped “FAA Approved” with a date of March 15, 1993, or later.

October 15, 1992 May 3, 1994; May 27, 2021 March 15, 1993 October 7, 1996 Keith Johnston ODA administrator ODA-501508-CE Learjet Inc.

Wichita, Kansas 2

(1) This approval is for installation of structural provisions only. The installation of the electrical, plumbing and ECS components must be separately approved. (2) This approval should not be extended to other specific airplanes of these models on which previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of those airplanes.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

ST00047WI 2

## Every issue (1)

- May 27, 2021: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a4/e5/a4e505395debcc70ebe8f46b9744735dfd2a9567f1ae9674912d76775309ca03)

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