STC ST09652DS

Number: ST09652DS

FAA Form 8110-2 (5/14) Page 1 of 4 This certificate, issued to: Flight Program Operations 6500 S. MacArthur Boulevard Oklahoma City, OK 73169 Part 25 of the Federal Aviation Regulations.

A21EA

Make: Bombardier Inc.

Model: CL-600-2B16 (CL-604 Variant)

Installation of the Identification Friend or Foe (IFF) Mode 5 System. This alteration is to be made in accordance with data list D09652, dated July 22, 2020, or later approved FAA (ODA) revision.

This STC is intended for Military and Public Use only. Installation on commercial aircraft is prohibited.

This STC is for Government use only and is limited to installations completed at the FAA facility in Oklahoma City, Oklahoma.

Date of Application: October 31, 2018 Date Reissued:

Date of Issuance: July 22, 2020 Date Amended:

Signature

Title ODA Administrator-Alternate, ODA-700576-SW

FAA Form 8110-2 (5/14) Page 2 of 4

To (Name and address of transferee)

From (Name and address of grantor)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST09652DS

FAA Form 8110-2 (5/14) Page 3 of 4 Description of Type Design Change (Continued):

Aviation System Standards STC ST09640AC-D, “Installation of AN/AAQ-24(V) Large Aircraft Infrared Countermeasure (LAIRCM) System,” date amended June 12, 2020 must be accomplished prior to this STC.

Midcoast Aviation, Inc. STC ST00838WI, “Installation of the Rockwell Collins TRE-920 Directional Antenna,” date of issuance December 3, 1999 must be accomplished prior to this STC.

Proline 21 Advanced Avionics installation per Bombardier Inc. Canadair Challenger Service Bulletin Number 605-34-019, dated December 15, 2015 or later must be accomplished prior to this STC.

Compatibility of the alteration with other approved alterations is to 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.

A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft.

FAA approved airplane flight manual supplement, “IFF Transponder,” dated July 22, 2020, or later approved FAA (ODA) revision, is required.

Instructions for continued airworthiness, “Installation of the IFF Mode 5 System,” M09652, dated June 17, 2020, or later accepted FAA (AEG) revision, is a required part of this modification.

FAA certification of this installation was limited to the performance requirements for Extended Squitter ADS-B OUT equipment operating on the 1090 MHz RF as defined in 14 CFR §91.227 following the guidance for installation and airworthiness approval in AC 20-165B, and evaluation of the equipment’s effects on the safe operation of the aircraft.

FAA certification of this installation was limited to IFF modes 1 & 2 performance requirements for civil functions only. FAA does not endorse the operation and effectiveness of the military functions of the IFF Mode 5 system.

In addition, the IFF Mode 5 System also requires approval of the operation of military functions by the DoD AIMS Office. The KIV-77 crypto unit which contains a lithium manganese dioxide battery is not part of the FAA certification/airworthiness approvals related to this STC, so installation of the KIV-77 crypto unit is not FAA approved for civilian operational purposes.

The following Raytheon parts are not eligible for FAA Parts Manufacturer Approval:

Nomenclature Part Number Mode 5 Receiver/Transmitter 4079100-0530 Mode 5 Control Panel 4087561-0502 See continuation sheet 4.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST09652DS

FAA Form 8110-2 (5/14) Page 4 of 4 Certification Basis Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis of the Bombardier Model CL-604 variant aircraft is a follows:

a. The type certification basis fo r the Bombardier Model CL-604 variant aircraft is shown on TCDS A21EA for parts not changed or affected by the modification.

b. The certification basis for parts changed or affected by the modification since the reference date of application, October 31, 2018, is based upon the TCDS A21EA. Based on 14 CFR §§ 21.115 and

21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment 25-0 through 25-80

25.23(all), 25.301(a), 25.303, 25.305(a), 25.307(a), 25.561(c), 25.603(all), 25.605(a), 25.609(all),

25.611(a), 25.613(all), 25.777(a)(b)(c), 25.1301(all), 25.1307(c), 25.1309(a)(b)(c)(d)(g), 25.1316(a)(b),

25.1322(all), 25.1351(a), 25.1353(a)(b), 25.1357(a)(c)(d)(e), 25.1359(a)(d), 25.1431(a)(c), 25.1541(all),

25.1555(a), 25.1581(all), 25.1583(all), 25.1585(all)

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