2AS39-AVIATORUAV200Inmarsat SwiftBroadband Class 4 SATCOM system

Template #: 875-A0064 Issue: 2.7 AVIATOR UAV 200 Installation Manual Document number : 677-A0219_IM Issue : 1.4 Date : 02 November 2020 AVIATOR UAV 200 Installation Manual Document: 677-A0219_IM issue 1.4 COBHAM PUBLIC Page 3 of 61 Safety Summary The following general safety precautions must be observed during all phases of operation, service and repair of this equipment. Failure to comply with these precautions or with specific warnings in this manual may violate the safety standards of design, manufacture and intended use of the equipment. Cobham assumes no liability for the customer's failure to comply with these requirements. If the equipment is used in a manner not specified by the manufacturer, the protection may be impaired. During transmission the AVIATOR UAV 200 SATCOM terminal can radiate microwave power in any direction not screened by the aircraft fuselage. High levels of radio frequency radiation are considered harmful to health. Although all countries have not agreed upon a single value, the American National Standards Institute (ANSI/IEEE C95.1-1999) recommends that according to General Public Requirements a person should not be exposed to radiation stronger than 1 mW/cm 2 at the frequencies used in this terminal. Accordingly, the operator of the system should ensure that no person should approach within 50 cm (1.6 ft) of the terminal when it is transmitting. Electrostatic Discharge Caution The terminal contains items that are electrostatic discharge (ESD) sensitive. Use approved industry precautions to keep the risk of damage to a minimum when you touch, remove or insert parts or assemblies. Under extreme heat conditions or prolonged transmission periods, do not touch metal parts of the AVIATOR UAV 200, as this may result in injury. AVIATOR UAV 200 Installation Manual Document: 677-A0219_IM issue 1.4 COBHAM PUBLIC Page 4 of 61 FCC REGULATORY INFORMATION EQUIPMENT IDENTIFICATION: Model FCC ID AVIATOR UAV 200 2AS39-AVIATORUAV200 RADIOFREQUENCY RADIATION EXPOSURE INFORMATION: This equipment complies with FCC radiation exposure limits set forth for an uncontrolled environment. This equipment should be installed and operated with minimum distance of 50 cm between the radiator and your body. This transmitter must not be co-located or operating in conjunction with any other antenna or transmitter. NOTICES: 1) This device complies with Part 15 of the FCC Rules. Operation is subject to the following two conditions: a) this device may not cause harmful interference, and b) this device must accept any interference received, including interference that may cause undesired operation. 2) Changes or modifications made to this equipment not expressly approved by Omnipless Manufacturing (PTY) Ltd may void the FCC authorization to operate this equipment. 3) This equipment has been tested and found to comply with the limits for a Class A digital device, pursuant to Part 15 of the FCC Rules. These limits are designed to provide reasonable protection against harmful interference when the equipment is operated in a commercial environment. This equipment generates, uses, and can radiate radio frequency energy and, if not installed and used in accordance with the instruction manual, may cause harmful interference to radio communications. Operation of this equipment in a residential area is likely to cause harmful interference in which case the user will be required to correct the interference at his own expense. AVIATOR UAV 200 Installation Manual Document: 677-A0219_IM issue 1.4 COBHAM PUBLIC Page 5 of 61 TABLE OF CONTENTS PAGE 1. ABOUT THIS MANUAL ......................................................................................................... 10 1.1 INTRODUCTION ........................................................................................................................... 10 1.2 PURPOSE ................................................................................................................................... 10 2. APPLICABLE & REFERENCE DOCUMENTS ........................................................................... 11 2.1 APPLICABLE DOCUMENTS ............................................................................................................... 11 2.2 REFERENCE DOCUMENTS ............................................................................................................... 11 3. INTRODUCTION .................................................................................................................. 12 3.1 SCOPE ...................................................................................................................................... 12 3.2 SYSTEM OVERVIEW ...................................................................................................................... 12 3.3 EXTERNAL INTERFACES ................................................................................................................. 13 4. INSTALLATION ................................................................................................................... 15 4.1 GENERAL INFORMATION AND OVERVIEW ............................................................................................ 15 4.2 STORAGE AND TRANSPORTATION ..................................................................................................... 15 4.3 UNPACKING & INITIAL INSPECTION .................................................................................................. 15 4.4 INSTALLING THE USIM ................................................................................................................. 15 4.5 INSTALLATION CONSIDERATIONS ..................................................................................................... 16 4.5.1 Terminal Mass and CG ....................................................................................................... 16 4.5.2 Terminal Cooling Considerations ..........................................…

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PROJECT: AVIATOR UAV 200 Date: Issue: Author: Page: 02/12/2019 A.0 Spammer, Fanus 1 OF 3 Form #: 875-A0067 iss 2.0 Addendum to Confidentiality Request: FCC rules 47 CFR 0.457 and 0.459 FCC ID: 2AS39-AVIATORUAV200 Cobham Cape Town submitted a request for long-term confidential treatment of all of the information accompanying the FCC application as listed below, i.e.: 1) Block Diagrams 2) Schematic Diagrams 3) Part Lists 4) Internal Photos of the sealed antenna feed board subassembly affixed to the AVIATOR UAV 200 5) Operational Description These materials contain trade secrets and proprietary information not customarily released to public and the public disclosure of these matters might be harmful to the Applicant and provide unjustified benefit to its competitors. The antenna feed board contains the integral antenna. Its design is an essential part of our intellectual property. We keep information on its design confidential. Thus, the information is not available in the public domain. As such, the details are not shown in marketing materials nor in manuals associated with the radio transceiver. This subassembly is attached to a mechanical part (the midplane) by means of screws. The midplane is a solid aluminium part except for four connector holes. The radome for the antenna subassembly is then bonded to the midplane with an epoxy. The radome that covers the antenna subassembly is optically opaque and can only be removed at the factory by cutting it off. The radome completely covers the antenna feed board. We are not seeking long-term confidentiality for the internal photographs of the other two circuit boards that make up the device (i.e. the modem board and the RF board) as those boards are accessible without destroying a portion of the device, unlike the antenna feed board. As such, we submit that the antenna feed board presents the sort of exceptional case discussed in KDB Publication 726920, Confidentiality Request Procedures, pertaining to long-term confidentiality for certain internal photos if the information shown on the photo is a circuit board or internal component not accessible to users. PROJECT: AVIATOR UAV 200 Date: Issue: Author: Page: 02/12/2019 A.0 Spammer, Fanus 2 OF 3 Form #: 875-A0067 iss 2.0 The subsequent correspondence with the FCC following the submission for Confidentiality Request was limited to the issue of keeping the internal photographs of the antenna array assembly confidential. Reference for this correspondence was done under inquiry tracking number 322827. In conclusion, the FCC granted long term confidentiality of all documents listed above including internal photographs of the antenna array. A copy of this latest response from the FCC staff with the request for confidential treatment is given below: ---------------------------------------------------------------------------- From: [email protected] <[email protected]> Sent: Wednesday, August 7, 2019 2:28 PM To: Hilliard, David <[email protected]> Subject: Response to Inquiry to FCC (Tracking Number 322827) Inquiry on 06/12/2019 : Inquiry: On behalf of Omnipless Manufacturing (PTY) Ltd, this is to request pre-approval guidance to accord long- term confidentiality with respect to the internal photograph of the sealed circuit board described in the attached request. If you have questions or require additional information, please contact David Hilliard as noted above. The device referred to in the attachment has not yet been submitted to a TCB. FCC response on 06/13/2019 The long term confidentiality request is acceptable. However, there should be a non-disclosure agreement as an example, does not require signature between the two parties in question. This non-disclosure agreement is required in FCC Publication No. 726290 dated April 8, 2016. ---Reply from Customer on 06/20/2019--- The documentation associated with the device will make clear that the use of the equipment is subject to a confidentiality condition associated with the sealed cover that obscures viewing of the confidential information and that removal of the cover is prohibited. Please see attachment to this reply. FCC response on 07/02/2019 The FCC is requesting the following information before we make a response to this request: questing : Photo’s of the part that is requested to be confidential. Photo’s of the cover/enlcosure and the epoxy enclosing the confidential part to determine if the confidential part would be destroyed if someone tried to open the cover and take photo’s of the confidential part. ---Reply from Customer on 08/02/2019--- Please see attached confidential information responsive to the July 2, 2019, FCC response. Confidential treatment for the attached information is requested pursuant to Sections 0.457 and 0.459 of the FCC rules. FCC response on 08/07/2019 Information submitted is acceptable. ------------------------------------------------------------------------ PROJECT: AVIATOR UAV 200 Date: Issue: Author: Page: 02/12/2019 A.0 Spammer, Fanus 3 OF 3 Form #: 875-A0067 iss 2.0 The non-disclosure agreement as suggested by the FCC in their response of 06/13/2019 has been included in the updated AVIATOR UAV 200 Installation Manual and is also given below: --------------------------------------------------------------------- Attachment Details: Documentation Excerpt re Nondisclosure https://apps.fcc.gov/kdb/GetAttachment.html?id=5mOxtKRGIEOCl6yrl7tlHg%3D%3D

Cobham Aerospace Communications www.cobham.com COBHAM PRIVATE Omnipless Manufacturing (Pty) Ltd. 2002/009019/07 Directors: NJ Jansen van Rensburg, W Kasselman, E Kawaishi (French), M Ermeneux (French) Template #: 875-A0416 Issue 1.13 Omnipless Manufacturing (Pty) Ltd. 2 Westlake Drive Westlake 7945 PO Box 31093 Tokai, 7966 Cape Town, South Africa T: +27 (0)21 700 7000 F: +27 (0)21 700 7199 22 nd October 2019 CTC Advanced Untertürkheimer Straße 6-10 66117 Saarbrücken Germany Re: Company structure and name of Omnipless Manufacturing (Pty) Ltd. To whom it may concern, Omnipless Manufacturing (Pty) Ltd is a company located in Cape Town, South Africa and registered in South Africa with Company Number: 2002/009019/07. Omnipless Manufacturing is a wholly owned subsidiary of Cobham PLC, and forms part of the Cobham Aerospace Communications Business Unit. Before a recent restructuring the company used to operate under the Cobham SATCOM Business Unit. In South African legal jurisdiction, we trade as Omnipless Manufacturing (Pty) Ltd. In European parlance we are Omnipless Manufacturing, trading as Cobham Aerospace Communications (formerly Cobham SATCOM) Should you have any questions you are more than welcome to contact the undersigned. Andrew de Pomeroy-Legg Regional Sales Director Omnipless Manufacturing (Pty) Ltd. Cobham Aerospace Communications T: +27 21 700 7131 M: +27 83 628 8163 [email protected] www.cobham.com

David E. Hilliard 202.719.7058 [email protected] VIA ELECTRONIC FILING May 28,2019 Roger Noel Chief, Mobility Division Wlreless.Felecommunlcatlcns Bureau Federal Communications Commission 445 12th st SW Washington, DC 20554 RANTE ~-~~v/7S~ G11311~ Re: Omnipless Manufacturing (PTY) ltd. Request for Waiver of Part 87 Rules to Allow Equipment Authorization of an Aeronautical Mobile Satellite Service Transceiver (AVIATOR UAV 200) . Dear Mr. Noel: Pursuant to Section 1.925 of the Commission's Rules, Omnipless Manufacturing (PTY) Ltd. trading as Cobham Aerospace Communication Cape Town ("Omnipless") hereby requests waiver of Sections 87.131,87.137., 87.139(i}{1) Note 2, and 87.141(j) ofthe Commission's Rules to permit certification of its next-generation aeronautical-mobile satellite service ("AMSS") transceiver, the AVIATOR UAV 200 ("UAV 200"). The transceiver will support the Inmarsat SwiftBroadband aircraft communications service as used with unmanned aircraft. Under Section 1.925, the FCC may grant waiver if "[tlhe underlying purpose ofthe rule(s) would not be served or would be frustrated by application to the instant case, and that a grant of the waiver would be in the public interest or; liln view of unique or unusual factual circumstances of the instant case, application ofthe rule(s) would be inequitable, unduly burdensome or contrary to the public interest, or the applicant has no reasonable alternative.'? The FCC granted similar waivers of the Part 87 rules to Thrane & Thrane in September 2018 to permit authorization of similar equipment." Indeed, the UAV 200 utilizes the same radio module as specified for the radios described in the September 2018 waiver requests. There, the Commission agreed that grant served the public interest to allow provision of "high-speed data and voice capabilities on aircraft."? The agency has also granted similar waivers to EMS, 47 C.F.R. § 1.925(b)(3). See Letter dated September 13, 2018, for the Aviator 700D, from David E. Hilliard to Roger Noel, Mobility Division, Wireless Telecommunications Bureau (Stamp Grant, Sept. 21 2018 "for the reasons set forth herein"); Letter dated September 13, 2018, for the Aviator 200/300/350 Series, from David E. Hilliard to Roger Noel, Mobility Division, Wireless Telecommunications Bureau (Stamp Grant, Sept. 21, 2018 "for the reasons set forth herein"). 'd. 1776 K Street NW I Washington, DC 20'00'6 I 20'2.719.70'0'0' wileyrein.com Roger Noel May 28,2019 Page 2 Honeywell International, Inc. and Rockwell Collins, tnc.," finding "waiver would be in the public interest" because "current Part 87 rules do not allow for the wider bandwidth, higher transmission speeds and-more efficient modulation techniques of newer AMSS systems." Grant here would provide the same public interest benefits and allow Omnipless's next- generation transceiver to deliver high-speed data in support of aircraft. Description 0/ the Equipment The UAV200 supports Inmarsat Swiftbroadband signals using QPSK as well as 16-point and 4- point Quadrature Amplitude Modulation (16QAM, 4QAM). The UAV200 transceiver provides one baseband communication channel capable of supporting simultaneous full-duplex of SwiftBroadband nonvoice data functionality. The System functions in the 1525-1559 MHz receive band and 1626.5-1.660.5 MHz transmit band. The UAV200 transceiver will meet the technical requirement of Part 87 AMSS rules with respect to output power, spurious emissions, intermodulation and frequency stability. As the FCC has acknowledged, Inmarsat's Swlftfsroadband service "offers higher data rates by utilizing more efficient modulation techniques.:" Grant of the instant waiver request would serve the public interest because the Part 87 rules have not yet been updated to reflect the Inmarsat SwiftBroadband emission types and bandwidths. A more detailed description of the equipment and the specific rules for which waiver is requested is attached under the company's letterhead. Please contact me with any questions. Respectfully, David E. Hilliard See Letter dated April 9, 2010, from Bruce A. Olcott to James Shaffer, Mobility Division, Wireless Telecommunications Bureau (Stamp Grant Apr. 29, 2010) ("EMS Stamp Grant"); Rockwell Collins, Inc. equipment authorization for the HST·2110B and HST·2120B transceivers, FCC 10 AJK8222232 and AJK8222234 (2008); Honeywell International, Inc. equipment authorization for the HD·128 transceiver, FCC 10 GB8HD·128 (2007). Request of EMS Technologies Canada, Ltd. for Waiver of Part 87 Emission Mask to Allow Certification and Use of Aeronautical Mobile Satellite Service Transceiver, 26 FCC Red 8824 (WTB 2011). 6 EMS Stamp Grant, at 2. 1776 K Street NW I Washington, DC 20006 I 202.719.7000 wileyrein.com CDBHRm Cobham Aerospace Communications Westlake Drive Westlake 7945 PO Box 31093 Takal,7966 cape Town, South Africa T: + 27 (0}21 700 7000 F: +27 (0)21 700 7190/2/3/9 May 27,2019 Mr. Roger Noel Chief, Mobility Division Wireless Telecommunications Bureau Federal Communications Commission 445 12th St SW Washington, DC 20554 Re: Omnipless Manufacturing (PTY) Ltd. Request for Waiver of Part 87 Rules to Allow Equipment Authorization of an Aeronautical Mobile Satellite Service Transceiver (AVIATOR UAV 200) Dear Mr. Noel: Pursuant,to Section 1.925 of the Commission's Rules, Omnipless Manufacturing (PTY) Ltd. trading as Cobham Aerospace Communication Cape Town ("Omnipless'') hereby requests waiver of Sections 87.131,87.137, 87.139(i)(1) Note 2, and 87.141(j) of the Commission's Rules to permit certification of its next-generation aeronautical-mobile satellite service (,'AMSS',) transceiver, the AVIATOR UAV 200 ("UAV 200''). The transceiver will support the Inmarsat SwiftBroadband aircraft communications service as used with unmanned aircraft. Under Section 1.925, the FCC may grant waiver if "[t]he underlying purpose of the rule(s) would not be served or would be frustrated by application to the instant case, and that a grant of the waiver…

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Template #: 875-A0064 Issue: 2.7 AVIATOR UAV 200 External Pictures Document number : 870-A0867 Issue : 1.4 Date : 10 November 2020 AVIATOR UAV 200 External Pictures Document: 870-A0867 issue 1.4 COBHAM PUBLIC Page 3 of 6 TABLE OF CONTENTS PAGE 1 SCOPE ...................................................................................................................................... 4 2 APPLICABLE DOCUMENTS ....................................................................................................... 4 3 AVIATOR UAV 200 (677-A0219) .............................................................................................. 4 LIST OF FIGURES PAGE Figure 1: AVIATOR UAV 200 .................................................................................................................... 4 Figure 2: Bottom View ............................................................................................................................. 5 Figure 3: FCC label location and text ........................................................................................................ 5 Figure 4: Top View .................................................................................................................................. 6 Figure 5: Front View ................................................................................................................................ 6 Figure 6: Side View ................................................................................................................................. 6 AVIATOR UAV 200 External Pictures Document: 870-A0867 issue 1.4 COBHAM PUBLIC Page 4 of 6 1 SCOPE This document contains external pictures of the AVIATOR UAV 200 as part of FCC certification:  FCC: 2AS39-AVIATORUAV200 2 APPLICABLE DOCUMENTS [1] None. 3 AVIATOR UAV 200 (677-A0219) Figure 1: AVIATOR UAV 200 AVIATOR UAV 200 External Pictures Document: 870-A0867 issue 1.4 COBHAM PUBLIC Page 5 of 6 Figure 2: Bottom View Figure 3: FCC label location and text AVIATOR UAV 200 External Pictures Document: 870-A0867 issue 1.4 COBHAM PUBLIC Page 6 of 6 Figure 4: Top View Figure 5: Front View Figure 6: Side View

51 13 R2 2.1 2.2 3 2.4 2.3 NOTES: MATERIAL: 630-A01041. FONT: ARIAL, BLACK2. 7 POINT, REGULAR1. 6 POINT, REGULAR2. 4 POINT, REGULAR3. 6 POINT, REGULAR4. SOFTWARE MOD STRIKE 3. 1.4 DRAFT 161513141211109876543 L B C D E F A G H J K 21 M L A B C D E F G H J K 2 DEC PLACE= ±0.2 ANGLES= ±0.5° GENERAL= ±0.5 3 DEC PLACE= ±0.1 PART No: SHEET 1 OF 1 TOLERANCES: UNLESS OTHERWISE STATED IN ACCORDANCE WITH OMNIPLESS SPEC: 862-A0006 THIS DOCUMENT MUST NOT BE USED FOR ANY OTHER PURPOSE THAN THAT FOR WHICH IT WAS SUPPLIED. UNAUTHORISED COPYING OR REDISTRIBUTION IS PROHIBITED. 470-A0841 DIMENSIONS IN MM[IN] INDUSTRIALISATION DESIGN AUTHORITY DRAWN MATERIAL FINISH LATEST ASSOCIATED DOCS A JACOBS L v WYK J CONRADIE NEXT ASSY 2016 COBHAM Plc. © INSPECTION METHOD SIGN ECP#DATEISS DESCRIPTION OF CHANGE M QA APPROVED 677-A0219 FCC CERTIFICATION NUMBER ADDED. 20/264 30.SEP.20201.4 DRAFT DIMENSIONS LABEL, AVIATOR UAV 200 SW & HW MODSTRIKE DETAIL DRAWING - L NGUBANE CAGE CODE (CAPE TOWN): SV658 DWG No: 470-A0841_DD PART DESCRIPTION: LABEL, AVIATOR UAV 200 SW & HW MODSTRIKE COBHAM PROPRIETARY, COMMERCIAL IN CONFIDENCE REVIEWED R STEEL SEE FOR LATEST DRAWING CHANGES 1.4 DRAFT TEMPLATE 875-A0776 ISSUE 2.1 R STEEL 4 DEC PLACE= ±0.05 AMDT: - SEE NOTES -

AVIATOR UAV 200 FCC ID label placement Sept 2020 Commercial in Confidence 0 Cobham plcCobham plc FCC ID Label location on bottom of product 1 Commercial in Confidence AVIATOR UAV 200 Outline Drawing FCC ID label Product Info label Cobham plcCobham plc Location of FCC label (large) 2 Commercial in Confidence AVIATOR UAV 200

Template #: 875-A0064 Issue: 2.7 AVIATOR UAV 200 Internal Pictures Document number : 870-A0866 Issue : 1.1 Date : 9 November 2020 AVIATOR UAV 200 Internal Pictures Document: 870-A0866 issue 1.1 COBHAM PUBLIC Page 3 of 5 TABLE OF CONTENTS PAGE 1 SCOPE ...................................................................................................................................... 4 2 APPLICABLE DOCUMENTS ....................................................................................................... 4 3 MODEM BOARD (654-A0544) .................................................................................................. 4 4 RF BOARD (654-A0539) .......................................................................................................... 5 LIST OF FIGURES PAGE Figure 1: Modem Board (Top) .................................................................................................................. 4 Figure 2: Modem Board (Bottom) ............................................................................................................. 4 Figure 3: RF Board (Top) ......................................................................................................................... 5 Figure 4: RF Board (Bottom) .................................................................................................................... 5 AVIATOR UAV 200 Internal Pictures Document: 870-A0866 issue 1.1 COBHAM PUBLIC Page 4 of 5 1 SCOPE This document contains internal pictures of the AVIATOR UAV 200 PCBs as part of FCC certification:  FCC: 2AS39-AVIATORUAV200 2 APPLICABLE DOCUMENTS [1] None 3 MODEM BOARD (654-A0544) Figure 1: Modem Board (Top) Figure 2: Modem Board (Bottom) AVIATOR UAV 200 Internal Pictures Document: 870-A0866 issue 1.1 COBHAM PUBLIC Page 5 of 5 4 RF BOARD (654-A0539) Figure 3: RF Board (Top) Figure 4: RF Board (Bottom)

AVIATOR UAV 200 RF Safe Distance (FCC) AuthorF Spammer Date 28-10-2020 Product:AVIATOR UAV 200 FCC ID:2AS39-AVIATORUAV200 Reference: RF Safety Calculations Exposure Limits FCC Minimum Safe RF Distance Calculation FCC OET Bulletin 65 - Evaluating Compliance with FCC Guidelines for Human Exposure to Radiofrequency Electromagnetic Fields FCC Maximum Permissible Exposure based on whole body averaged SAR of 4W/kg Cobham Confidential AVIATOR UAV 200 RF Safe Distance (FCC) For AVIATOR UAV 200 operating in the L-Band (1626.5 to 1660.5 MHz), MPE limit = FCC General Public (Uncontrolled Exposure): S =1 mW/cm 2 RF Field Prediction EIRPEquivalent Isotropic Radiated Power SPower Density limit PPower input to the antenna GNumerical Antenna Gain (in direction of interest relative to isotropic antenna) RDistance to the center of radiation of the antenna UAV 200 Parameters Power calculation: Power3,1dBW2,04W Tune accuracy (EIRP accuracy) 0,3dB1,07W P total 3,4dBW2,19W Antenna Gain8dBiC6,31Numerical Gain NOM_EIRP11,1dBW12,88W MAX_EIRP11,4dBW13,80W Safe Distance: R0,5m50,00cm Power Density Calculation MAX_EIRP11,4dBW13804mW R50cm S(calc)0,44 mW/cm 2 The Safe Distance of 50 cm results in a Power Density of 0,44 mW/cm 2 which is less than the required maximum of 1 mW/cm 2 Summary: FCC General Public Cobham Confidential AVIATOR UAV 200 RF Safe Distance (FCC) FCC OET Bulletin 65 - Evaluating Compliance with FCC Guidelines for Human Exposure to Radiofrequency Electromagnetic Fields Cobham Confidential

BNetzA - CAB - 02/21 - 102 TEST REPORT Test report no.: 1-0834/20-01-02-A Testing laboratory Applicant CTC advanced GmbH Untertuerkheimer Strasse 6 – 10 66117 Saarbruecken / Germany Phone: + 49 681 5 98 - 0 Fax: + 49 681 5 98 - 9075 Internet: https://www.ctcadvanced.com e-mail: [email protected] Accredited Testing Laboratory: The testing laboratory (area of testing) is accredited according to DIN EN ISO/IEC 17025 (2018-03) by the Deutsche Akkreditierungsstelle GmbH (DAkkS) The accreditation is valid for the scope of testing procedures as stated in the accreditation certificate starting with the registration number: D-PL-12076-01. Omnipless Manufacturing (Pty) Limited trading as Cobham Aerospace Communications Westlake Drive 7945 Cape Town / SOUTH AFRICA Phone: +27 21 700 7000 Contact: Fanus Spammer e-mail: [email protected] Phone: +27(0) 21 700 7070 Manufacturer Omnipless Manufacturing (Pty) Limited trading as Cobham Aerospace Communications Westlake Drive 7945 Cape Town / SOUTH AFRICA Test standard/s 47 CFR Part 25 Title 47 of the Code of Federal Regulations; Chapter I; Part 25 - Satellite Communications 47 CFR Part 87 Title 47 of the Code of Federal Regulations; Chapter I; Part 87 - Aviation Services RSS - 170 Issue 3 Mobile Earth Stations (MESs) and Ancillary Terrestrial Component (ATC) Equipment Operating in the Mobile-Satellite Service (MSS) Bands For further applied test standards please refer to section 3 of this test report. Test Item Kind of test item: Aeronautical Inmarsat L-Band Model name: AVIATOR UAV 200 SATCOM TERMINAL FCC ID 2AS39-AVIATORUAV200 IC 24994-AVIAUAV200 Frequency: TX: 1626.5 MHz – 1660.5 MHz Antenna: LGA External Antenna Power supply: 28 V DC from Power Supply Temperature range: -40°C to +55°C This test report is electronically signed and valid without handwritten signature. For verification of the electronic signatures, the public keys can be requested at the testing laboratory. Test report authorized: Test performed: Thomas Vogler Meheza Walla Lab Manager Lab Manager Radio Communications & EMC Radio Communications & EMC Test report no.: 1-0834/20-01-02-A © CTC advanced GmbH Page 2 of 29 1 Table of contents 1 Table of contents ............................................................................................................................................ 2 2 General information ....................................................................................................................................... 3 2.1 Notes and disclaimer .......................................................................................................................... 3 2.2 Application details ............................................................................................................................... 3 2.3 Test laboratories sub-contracted ...................................................................................................... 3 3 Test standard/s and references .................................................................................................................... 4 4 Reporting statements of conformity – decision rule .................................................................................. 5 5 Test environment ............................................................................................................................................ 6 6 Test item .......................................................................................................................................................... 6 6.1 General description ............................................................................................................................. 6 6.2 List of components ............................................................................................................................. 6 6.3 Antenna system(s) ...........................................................................................................................…

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