STC ST521CH

Supplemental type certificate · Canard Aerospace Corporation

Holder
Canard Aerospace Corporation · United States
Status
Current · Reissued
Status date
April 18, 2007
Applied
February 22, 1996
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21, Part 25
Data sheet
TCDSA1NM

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of a Teledyne Controls Aircraft Communication Addressing and Reporting System (ACARS) Management Unit (MU), a Teledyne Controls Interactive Display Unit (IDU), and a Miltope Thermal Printer. Installation of a Communications Management Unit and pprinter.

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.

FAA FORM 8110-2(10-68) PAGE 1 of 3 PAGES Number ST521CH This certificate issued to Canard Aerospace 250 South Fuller Street Shakopee, MN 55347

Part 25 of the Federal Regulations.

(See Type Certificate Data Sheet A1NM for complete certification basis.)

Original Product--Type Certificate Number : A1NM Make : Boeing Model : 767-200 Series, 767-300 Series, 767-300F Series, and 767-400ER Series Description of Type Design Change:

Option 1: Applies to 767-300 series aircraft. Installation of a Teledyne Controls Aircraft Communication Addressing and Reporting System (ACARS) Management Unit (MU), a Teledyne Controls Interactive Display Unit (IDU) and a Miltope Thermal Printer, in accordance with Canard Aerospace Corporation Top Level Document Control Drawing No. 30009, Revision D, dated September 18, 2003, Appendix A, or later FAA approved revision.

Option 2: Applies to 767-200 series, 767-300 series, 767-300F series and 767-400ER series aircraft. Installation of a Communications Management Unit and pprinter in accordance with Canard Aerospace Corporation Top Level Document Control Drawing No. 30009, Revision D, dated September 18, 2003, Appendix B, or later FAA approved revision.

1. Compatibility of this design change with previously approved modifications must be determined by the installer.

Date of application : February 22, 1996

Date of issuance : June 20, 1996 Date reissued : April 18, 2007

Date amended : June 21, 2000, September 30, 2003

( Signature) Charles L. Smalley Manager, Systems & Flight Test Branch Chicago Aircraft Certification Office

( Title)

FAA FORM 8110-2-1(10-69) PAGE 2 of 3 PAGES

Number

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES

Number ST521CH Date of Issuance: February 22, 1996 Date Amended: April 18, 2007

2. Option 2: Airplane Flight Manual Supplement, Canard Aerospace Corporation (CDC) Document No. 23-3301-04, Revision NC, FAA approved on September 30, 2003, or later FAA Approved revision, is required on board modified aircraft.

3. 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.

…END…

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
The Boeing Company767-200 SeriesA1NM
The Boeing Company767-300 SeriesA1NM
The Boeing Company767-300F SeriesA1NM
The Boeing Company767-400ER SeriesA1NM