STC ST09640AC-D

United States of America Department of Transportatio n Federal Aviation Administration Supplemental Type Certificate

Number: ST09640AC-D

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-601-3R, CL-604 and CL-604 Variant) Description of Type Design Change:

Installation of AN/AAQ-24(V) Large Aircraft Infrared Countermeasure (LAIRCM) System. This alteration is to be made in accordance with data list D09640, dated June 12, 2020, or later approved FAA (ODA) revision. Amendment 1 adds CL-604 variant. Amendment 2 adds limitations (use and installation).

Amendment 3 locates the LAIRCM Control Indicator Unit (CIU) from the Mission Specialist Station to the flight deck center pedestal for CL-604 variant aircraft.

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

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

Date of Application: April 11, 2006 Date Reissued: February 27, 2008 Date of Issuance: February 14, 2007 Date Amended: February 17, 2009, March 8, 2010, June 12, 2020

Signature

TitleODA Administrator-Alternate, ODA-700576-SW

..ST09640AC-D

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: ST09640AC-D

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

FAA Flight Program Operations Engineering Order Part B-I No. 19-05-04, “RH Aft Equipment Bay Shelf LAIRCM Preparation”, date 12/9/19 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, “Installation of the Northrop Grumman Large Aircraft Infrared Countermeasure (LAIRCM) System, AN/AAQ-24(v) Missile Defense System,” dated June 12, 2020, or later approved FAA (ODA) revision, is required.

Instructions for continued airworthiness, “Installation of the Large Aircraft Infrared Countermeasure (LAIRCM) System, AN/AAQ-24(V),” M09640, dated March 20, 2020, or later accepted FAA (AEG) revision, is a required part of this modification.

FAA certification of this installation was limited to the evaluation of the electronic countermeasure equipment’s effects on the safe operation of the aircraft, and does not connote FAA endorsement of the effectiveness of the equipment in countering a Man Portable Air Defense System (MANPADS) threat.

In addition, the FAA has not evaluated the safety of the IR laser for use on the ground or in the air.

Operation of the IR laser, to include appropriate laser training for flight crew and maintenance personnel, should be in accordance with the intent of American National Standards Institute (ANSI) Standards Z136.1, Safe Use of Lasers, and Z136.6, Use of Lasers Outdoors.

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

Nomenclature Part Number Countermeasure Signal Processor 001-007722-3061 Control Indicator Unit 001-007678-103 Infrared Countermeasure Sensor 001-007671-009 Small Laser-Transmitter 001-007915A0301 Smart Card 152-001478-002

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 for the Bombardier Model CL-604 variant aircraft is shown on TCDS A21EA for parts not changed or affected by the modification.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST09640AC-D

FAA Form 8110-2 (5/14) Page 4 of 4 Certification Basis (Continued):

b. The certification basis for parts changed or affected by the modification since the reference date of application, January 1, 2006, is based upon the Original STC part 25 Amendment levels. 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 25-116

25.23(all), 25.1301(a), 25.1309(b)(c)(d), 25.1321(a)(e), 25.1322(all), 25.1353(a)(d), 25.1357(a)(b)(c),

25.1359(d), 23.1365(a)(b)(d)(e), 25.1381(all), 25.1431(a)(c)(d), 25.1529(all), 25.1541(all), 25.1555(a),

25.1581(all), 25.1583(all), 25.1585(all)

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