2AFBO3677436774

Exhibit Documentation for 36774 Key Fob User Manual FCC ID: 2AFBO36774 IC ID: 20833‐36774 User Manual RevisionCPage 2of 5 REVISION DESCRIPTION Rev Change Description A Initial Release B Modified to include the actual text in the manuals. C Updated model number User Manual RevisionCPage 3of 5 TABLE OF CONTENTS 1 Text from Cirrus Pilot Operating Handbook ................................................................................................................... 4 2 Text from Cirrus Maintenance Manual .......................................................................................................................... 5 User Manual RevisionCPage 4of 5 1 TEXT FROM CIRRUS PILOT OPERATING HANDBOOK User Manual RevisionCPage 5of 5 2 TEXT FROM CIRRUS MAINTENANCE MANUAL

Exhibit Documentation for 36774 Key Fob Frequency Block Diagram FCC ID: 2AFBO36774 IC: 20833‐36774 Frequency Block Diagram Revision BPage 2of 4 REVISION DESCRIPTION Rev Change Description A Initial Release B Updated frequency from 434.92 to 433.92 in block diagram. Removed unrelated information on bottom of document. Frequency Block Diagram Revision BPage 3of 4 TABLE OF CONTENTS 1 Introduction .................................................................................................................................................................... 4 2 Block Diagram ................................................................................................................................................................. 4 Frequency Block Diagram Revision BPage 4of 4 1 Introduction This file contains block diagrams showing the frequency of all oscillators in the 36774 Key Fob along with the signal path and frequency. Note that this device uses a Silicon Labs Si4010 with an internal oscillator. The tuning range(s) and intermediate frequency(s) shall be indicated at each block (e.g. LO, IF, XMIT Output). 2 Block Diagram Figure 1: Block Diagram with Intermediate Frequencies Shown Figure 2: Example Connection of a Si4010 in a Circuit

Exhibit Documentation for 36774 Key Fob External Photos FCC ID:2AFBO36774 IC:20833‐36774 External Photos Revision CPage 2of 4 REVISION DESCRIPTION Rev Change Description A Initial Release B Added side views. C Update back view with correct text External Photos Revision CPage 3of 4 1 External Photos Figure 1 and Figure 2 contain pictures of the front and back side of the key fob model 36774. Figure 1: External Photo, Front View Figure 2: External Photo, Back View External Photos Revision CPage 4of 4 Figure 3 and Figure 4 contain pictures of the top and bottom side of the key fob model 36774. Figure 3: External Photo, Top View Figure 4: External Photo, Bottom View Figure 5 and Figure 6 contain pictures of the left and right side of the key fob model 36774. Figure 5: External Photo, Left Side View Figure 6: External Photo, Right Side View

Exhibit Documentation for 36774 Key Fob FCC Label and Location FCC ID:2AFBO36774 IC:20833‐36774 Label and Location Revision CPage 2of 4 REVISION DESCRIPTION Rev Change Description A Initial Release B Updated text on back of enclosure C Correct model number Label and Location Revision CPage 3of 4 1 Label and Location (FCC ID) Figure 1 and Figure 2 contain drawings and pictures of the FCC and IC ID on the back of the key fob model 36774. The pilot operating handbook (POH) which is the instruction manual for the product contains the following text: “This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions: (1) This device may not cause harmful interference, and (2) this device must accept any interference received, including interference that may cause undesired operation.” Figure 1: FCC and IC ID Text Drawing Label and Location Revision CPage 4of 4 Text Front side of enclosure -White Text on buttons -White Text Back side of enclosure – Standard Gray FCC ID:2AFBO36774 IC: 20833-36774 MODEL:36774 Figure 2: FCC and IC ID Picture

Exhibit Documentation for 36774 Key Fob Internal Photos FCC ID:2AFBO36774 IC:20833‐36774 Internal Photos Revision BPage 2of 4 REVISION DESCRIPTION Rev Change Description A Initial Release B Updated model number Internal Photos Revision BPage 3of 4 1 Internal Photos Figure 1 and Error! Reference source not found. contain pictures of the front and back interiors of the key fob model 36774 along with the front and back side of the PCB. Figure 1: Internal Photo with Front PCB View Internal Photos Revision BPage 4of 4 Figure 2: Internal Photo with Back PCB View

Exhibit Documentation for 36774 Key Fob Antenna Information FCC ID: 2AFBO36774 IC ID: 20833‐36774 Antenna Information Revision BPage 2of 4 REVISION DESCRIPTION Rev Change Description A Initial Release B Updated model # on cover page. Change frequency from 432.92 MHz to 433.93 MHz Antenna Information Revision BPage 3of 4 TABLE OF CONTENTS 1 Introduction .................................................................................................................................................................... 4 1.1 Antenna Type .......................................................................................................................................................... 4 1.2 Antenna Image ........................................................................................................................................................ 4 1.3 Compliance to FCC 15.203 ...................................................................................................................................... 4 1.4 Dimensional Description ......................................................................................................................................... 4 Antenna Information Revision BPage 4of 4 1 Introduction This file will provide the following information: 1. A list of antennas to be used with the transmitter. Include manufacturer, model number, gain (dBi), and description (e.g. dipole, yagi, patch, etc.) 2. Drawing or photograph unless clear photos appear in the external photos exhibit 3. For FCC Part 15 transmitters, describe compliance with FCC 15.203 4. For transmitters below 30 MHz, instead of the gain, please provide the dimensions of the loop antenna and / or a ruler in the photograph of the loop. The size of the loop, the dimensions, and the number of turns should be documented. 1.1 Antenna Type The antenna used on the key fob circuit card assembly (CCA) is a differential loop antenna implemented in copper as part of the printed circuit board (PCB). The antenna has ‐5dBi gain 1.2 Antenna Image Figure 1 has an image of the PCB implemented differential loop antenna Figure 1: View of Differential Loop PCB Antenna 1.3 Compliance to FCC 15.203 This assembly complies to FCC 15.203 because the antenna is a part of the PCB and the PCB is an integral part of the assembly. There are no provisions to re‐populate components and use another antenna. 1.4 Dimensional Description The assembly transmits at 433.92MHz so a dimensional description of the antenna is not required.

1 2 3 A B C 4 A B C D 12 3 4 D UNLESS OTHERWISE SPECIFIED: DO NOT SCALE DRAWING. DIMENSIONS ARE IN INCHES. GENERAL TOLERANCES: ANGLE: LINEAR: .X =
# 0.1 .XX =
# 0.03 .XXX =
# 0.010 SPECIFICATION PER CDC 90000 DRAWING PER DRM CDEP 309. Cirrus Design Corporation 4515 Taylor Circle Duluth, MN 55811 THE INFORMATION CONTAINED IN OR DISCLOSED IN THIS DOCUMENT IS CONSIDERED PROPRIETARY BY CIRRUS DESIGN CORPORATION. THIS DOCUMENT AND THE ITEMS AND INFORMATION CONTAINED OR DISCLOSED HEREIN SHALL NOT BE USED,COPIED,OR REPRODUCED IN WHOLE OR IN PART, NOR SHALL THE CONTENTS BE REVEALED IN ANY MANNER TO ANY PERSON UNLESS WRITTEN PERMISSION IS OBTAINED FROM CIRRUS DESIGN CORPORATION. SHEET SCALE SIZE REV DRAWING NO. TITLE LAST MODIFIED BY: LAST MODIFIED ON: ORIGINATED BY: ORIGINATED ON: LATEST REVISION DESCRIPTION ECOZONESHTLTR 1. INITIAL RELEASE. A ASSEMBLY, CIRCUIT CARD, KEY FOB CNTS1 OF 336775 A 09-Oct-15 08:46:44 AM Will Kessler 16-Oct-15 11:12:08 AM Will Kessler SEE SEPARATE PARTS LIST (TOP VIEW) NOTES: 1. SOLDERING PER 90014. 2. REF: DEVICE TO COMPLY WITH E00000729. 3. LOAD SOFTWARE (ITEM 2) AND TEST PER ATP E00000677. 4. LABLE WITH PART NUMBER, SOFTWARE PART NUMBER AND DATE CODE. -001 CDC Document Control Released To: Prototype - Revision: A.9 Release Date: 10/16/2015 12:45PM CIRRUS DESIGN CORPORATION 1 2 3 A B C 4 A B C D 12 3 4 D 4515 Taylor Circle Duluth, MN 55811 THE INFORMATION CONTAINED IN OR DISCLOSED IN THIS DOCUMENT IS CONSIDERED PROPRIETARY BY CIRRUS DESIGN CORPORATION. THIS DOCUMENT AND THE ITEMS AND INFORMATION CONTAINED OR DISCLOSED HEREIN SHALL NOT BE USED,COPIED,OR REPRODUCED IN WHOLE OR IN PART, NOR SHALL THE CONTENTS BE REVEALED IN ANY MANNER TO ANY PERSON UNLESS WRITTEN PERMISSION IS OBTAINED FROM CIRRUS DESIGN CORPORATION. SHEET SCALE SIZE REV DRAWING NO. ASSEMBLY, CIRCUIT CARD, KEY FOB CNTS2 OF 336775 A (BOTTOM VIEW) -001 CDC Document Control Released To: Prototype - Revision: A.9 Release Date: 10/16/2015 12:45PM CIRRUS DESIGN CORPORATION 1 2 3 A B C 4 A B C D 12 3 4 D 4515 Taylor Circle Duluth, MN 55811 THE INFORMATION CONTAINED IN OR DISCLOSED IN THIS DOCUMENT IS CONSIDERED PROPRIETARY BY CIRRUS DESIGN CORPORATION. THIS DOCUMENT AND THE ITEMS AND INFORMATION CONTAINED OR DISCLOSED HEREIN SHALL NOT BE USED,COPIED,OR REPRODUCED IN WHOLE OR IN PART, NOR SHALL THE CONTENTS BE REVEALED IN ANY MANNER TO ANY PERSON UNLESS WRITTEN PERMISSION IS OBTAINED FROM CIRRUS DESIGN CORPORATION. SHEET SCALE SIZE REV DRAWING NO. ASSEMBLY, CIRCUIT CARD, KEY FOB CNTS3 OF 336775 A -001 CDC Document Control Released To: Prototype - Revision: A.9 Release Date: 10/16/2015 12:45PM Drawing NumberRevision Date Released 36775.drwA 10/16/2015 12:45PM Approval Release NumberChange ClassModel NumberProject NumberType Certificate 138272Not Applicable Not ApplicableNot ApplicableA00009CH Release Authorizations Approver Roles (Tasks Name)ApproverDate Approved CheckerArthur Smith10/16/2015 11:28AM Cog EngScott Jardine10/16/2015 11:49AM Eng ManagerTim Timmerman10/16/2015 12:45PM CDC Document Control Released To: Prototype - Revision: A.9 Release Date: 10/16/2015 12:45PM

Cirrus Aircraft Corporation 36774 FCC 15.231:2015 FCC 15.231(b):2015 Report # CIRR0001 NVLAP Lab Code: 200630-0 This report must not be used to claim product certification, approval, or endorsement by NVLAP, NIST, or any agency of the federal government of the United States of America. CERTIFICATE OF TEST 2014-12-10 Product compliance is the responsibility of the client; therefore, the tests and equipment modes of operation represented in this report were agreed upon by the client, prior to testing. The results of this test pertain only to the sample(s) tested. The specific description is noted in each of the individual sections of the test report supporting this certificate of test. This report reflects only those tests from the referenced standards shown in the certificate of test. It does not include inspection or verification of labels, identification, marking or user information. Last Date of Test: December 15, 2015 Cirrus Aircraft Corporation Model: 36774 Radio Equipment Testing Standards Specification Method FCC 15.231:2015 ANSI C63.10:2013 FCC 15.231(b):2015 Results Method Clause Test Description Applied Results Comments 6.5, 6.6 Field Strength of Fundamental Yes Pass 6.5, 6.6 Spurious Radiated Emissions Yes Pass 6.9.2 Occupied Bandwidth Yes Pass 7.5 Duty Cycle Yes N/A Deviations From Test Standards None Approved By: Kyle Holgate, Operations Manager Report No. CIRR00012/20 REVISION HISTORY REV 2014.10.14 Revision Number Description Date Page Number 00 None Report No. CIRR00013/20 ACCREDITATIONS AND AUTHORIZATIONS REV 2015.2.19 United States FCC - Designated by the FCC as a Telecommunications Certification Body (TCB). Certification chambers, Open Area Test Sites, and conducted measurement facilities are listed with the FCC. A2LA - Accredited by A2LA to ISO / IEC 17065 as a product certifier. This allows Northwest EMC to certify transmitters to FCC and IC specifications. NVLAP - Each laboratory is accredited by NVLAP to ISO 17025 Canada IC - Recognized by Industry Canada as a Certification Body (CB). Certification chambers and Open Area Test Sites are filed with IC. European Union European Commission – Validated by the European Commission as a Conformity Assessment Body (CAB) under the EMC directive and as a Notified Body under the R&TTE Directive. Australia/New Zealand ACMA - Recognized by ACMA as a CAB for the acceptance of test data. Korea MSIP / RRA - Recognized by KCC’s RRA as a CAB for the acceptance of test data. Japan VCCI - Associate Member of the VCCI. Conducted and radiated measurement facilities are registered. Taiwan BSMI – Recognized by BSMI as a CAB for the acceptance of test data. NCC - Recognized by NCC as a CAB for the acceptance of test data. Singapore IDA – Recognized by IDA as a CAB for the acceptance of test data. Israel MOC – Recognized by MOC as a CAB for the acceptance of test data. Hong Kong OFCA – Recognized by OFCA as a CAB for the acceptance of test data. Vietnam MIC – Recognized by MIC as a CAB for the acceptance of test data. SCOPE For details on the Scopes of our Accreditations, please visit: http://www.nwemc.com/accreditations/ http://gsi.nist.gov/global/docs/cabs/designations.html Report No. CIRR00014/20 MEASUREMENT UNCERTAINTY TMU.2015.07.10 Measurement Uncertainty When a measurement is made, the result will be different from the true or theoretically correct value. The difference is the result of tolerances in the measurement system that cannot be completely eliminated. To the extent that technology allows us, it has been our aim to minimize this error. Measurement uncertainty is a statistical expression of measurement error qualified by a probability distribution. A measurement uncertainty estimation has been performed for each test per our internal quality document WP 342. The estimation is used to compare the measured result with its "true" or theoretically correct value. The expanded measurement uncertainty (K=2) for each test is on each data sheet. Our measurement data meets or exceeds the measurement uncertainty requirements of the applicable specification; therefore, the test data can be compared directly to the specification limit to determine compliance. The calculations for estimating measurement uncertainty are based upon ETSI TR 100 028 (or CISPR 16-4-2 as applicable), and are available upon request. The following table represents the Measurement Uncertainty (MU) budgets for each of the tests that may be contained in this report. Test + MU - MU Frequency Accuracy (Hz) 0.0007% -0.0007% Amplitude Accuracy (dB) 1.2 dB -1.2 dB Conducted Power (dB) 0.3 dB -0.3 dB Radiated Power via Substitution (dB) 0.7 dB -0.7 dB Temperature (degrees C) 0.7°C -0.7°C Humidity (% RH) 2.5% RH -2.5% RH Voltage (AC) 1.0% -1.0% Voltage (DC) 0.7% -0.7% Field Strength (dB) 5.2 dB -5.2 dB AC Powerline Conducted Emissions (dB) 2.4 dB -2.4 dB Report No. CIRR00015/20 FACILITIES REV 2015.2.19 California Labs OC01-13 41 Tesla Irvine, CA 92618 (949) 861-8918 Minnesota Labs MN01-08, MN10 9349 W Broadway Ave. Brooklyn Park, MN 55445 (612)-638-5136 New York Labs NY01-04 4939 Jordan Rd. Elbridge, NY 13060 (315) 554-8214 Oregon Labs EV01-12 22975 NW Evergreen Pkwy Hillsboro, OR 97124 (503) 844-4066 Texas Labs TX01-09 3801 E Plano Pkwy Plano, TX 75074 (469) 304-5255 Washington Labs NC01-05 19201 120 th Ave NE Bothell, WA 9801 (425)984-6600 NVLAP NVLAP Lab Code: 200676-0 NVLAP Lab Code: 200881-0 NVLAP Lab Code: 200761-0 NVLAP Lab Code: 200630-0 NVLAP Lab Code:201049-0 NVLAP Lab Code: 200629-0 Industry Canada 2834B-1, 2834B-3 2834E-1 N/A 2834D-1, 2834D-2 2834G-1 2834F-1 BSMI SL2-IN-E-1154R SL2-IN-E-1152R N/A SL2-IN-E-1017 SL2-IN-E-1158R SL2-IN-E-1153R VCCI A-0029 A-0109 N/A A-0108 A-0201 A-0110 Recognized Phase I CAB for ACMA, BSMI, IDA, KCC/RRA, MIC, MOC, NCC, OFCA US0158 US0175 N/A US0017 US0191 US0157 Report No. CIRR00016/20 PRODUCT DESCRIPTION 2014-12-10 Client and Equipment Under Test (EUT) Information Company Name: Cirrus Aircraft Corporation Address: 4515 Taylor Circle C…

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XMit 2015.01.14 FCC FF 005.JPG DUTY CYCLE XMit 2015.01.14 FCC FF 005.JPG OCCUPIED BANDWIDTH photo FCC FF 001.JPG FCC FF 002.JPG FIELD STRENGTH OF THE FUNDAMENTAL PSA-ESCI 2015.07.01 photo FCC FF 003.JPG FCC FF 004.JPG FIELD STRENGTH OF THE FUNDAMENTAL PSA-ESCI 2015.07.01 photo FCC FF 005.JPG FIELD STRENGTH OF THE FUNDAMENTAL PSA-ESCI 2015.07.01 photo FCC SRE 001.JPG FCC SRE 002.JPG SPURIOUS RADIATED EMISSIONS PSA-ESCI 2015.07.01 photo FCC SRE 003.JPG FCC SRE 004.JPG SPURIOUS RADIATED EMISSIONS PSA-ESCI 2015.07.01 photo FCC SRE 005.JPG FCC SRE 006.JPG SPURIOUS RADIATED EMISSIONS PSA-ESCI 2015.07.01 photo FCC SRE 007.JPG SPURIOUS RADIATED EMISSIONS PSA-ESCI 2015.07.01