STC ST00237BO

Supplemental type certificate · Learjet Inc.

Holder
Learjet Inc. · United States
Status
Current · Issued
Status date
June 9, 2006
Applied
March 10, 2006
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21, Part 25
Data sheet
TCDSA21EA

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of brake control valves.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

85-173 Bradley International Airport Windsor Locks, CT 06096

Part 25 of the Federal Aviation Regulations.

Original Product Type Certificate Number : A21EA Make : Bombardier

Model : CL-600-1A11, -2A12, -2B16 (C1-601-3A&-3R)

Installation of brake control valves in accordance with Bombardier Aerospace Master Document List BAS63017006, Rev. N/C, dated May 10, 2006, or later FAA-approved revision.

1. Installation to be maintained in accordance with Bombardier Aerospace Instructions for Continued Airworthiness BAS63017006- IFCA-1, N/C, dated May 15, 2006, or later approved revisions.

2. Compatibility of this installation with other previously approved modifications must be determined by the installer.

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 that permission.

Date of application : March 10, 2006 Date of issuance : June 9, 2006 Date reissued :

( Signature) Robert G. Mann Manager, Boston Aircraft Certification Office

(Title)

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 4

MakeModelData sheet
Bombardier Inc.CL-600-1A11 (CL-600)A21EA
Bombardier Inc.CL-600-2A12 (CL-601)A21EA
Bombardier Inc.CL-600-2B16 (CL-601-3A)A21EA
Bombardier Inc.CL-600-2B16 (CL-601-3R)A21EA