IYFTTX600PA2.4G Transmitter

The Tactic TTX600 airplane radio system uses an advanced 2.4GHz spread spectrum technology to prevent unwanted outside interference from interrupting control of the model, ensuring error-free fl ying and eliminating the need to pull frequency pins before every fl ight. Tactic 2.4GHz transmitters and receivers are not compatible with other brands of 2.4GHz equipment. For safe operation and best results, it’s strongly recommended to read this manual in its entirety before use! Also read and understand the instructions included with the model. Damage resulting from misuse or modifi cation will void your warranty. FEATURES Trainer Switch CH5 Switch CH6 Dial LED Power Indicator Power Switch Reversing Switches Neck Strap Eyelet D/R Switch Trim Lever Charge Jack ● Ball-bearing gimbals ● Built-in failsafe & wireless trainer function ● Dual rates for aileron, elevator and rudder ● Analog & digital trims with servo reversing ● Transmitter binds to multiple Tactic 2.4GHz receivers ● Power status LED & built-in charge jack INSTRUCTION MANUAL 2.4GHz 6-Channel Spread Spectrum Radio ™ 2 TTX600 TRANSMITTER ( Tx ) The TTX600 airplane transmitter is available in either a “Mode 2” confi guration with throttle on the left and elevator on the right, or “Mode 1” confi guration with throttle on the right and elevator on the left. Mode 2 radios are most commonly used in the U.S., whereas Mode 1 radios are popular in other countries. Be sure the radio purchased is of the correct mode. Four “AA” batteries are required to power the Tx (not included). Non-rechargeable 1.5V alkaline, or 1.2V rechargeable nickel-cadmium (NiCd) or nickel-metal hydride (NiMH) cells, can be used. Do not mix cell types, or old and new cells, etc. See the SERVOS AND ACCESSORIES section on page 17 for optional batteries available at local hobby retailers. To install the batteries, slide the battery door down. Insert the cells as shown in the diagram, making sure to note proper polarity for each cell. Close the battery door. POWER SWITCH, LED, and LOW BATTERY ALARM The red power LED should light when the power switch is moved upwards to the “ON” position. The 3 Tx should have adequate power for fl ight when the LED is on constantly. Anytime the LED begins to fl ash, accompanied by the sounding of an audible tone, the Tx battery voltage has dropped too low and operation of the model should NOT be attempted! WARNING! Never operate an R/C model with weak Tx batteries! Reduced operational range and/or possible loss of control of the aircraft could result. Replace weak alkaline batteries, or re-charge NiCd or NiMH batteries, before attempting a fl ight! If during a fl ight the Tx LED starts to fl ash, accompanied by the sounding of audible tones, it’s a warning that the Tx batteries have become weak and the aircraft should be landed as soon as possible! AILERON (CH1) Controls the moveable surfaces at the end of both main wings to rotate the airplane about the “roll” axis (an imaginary line which extends from the airplane’s nose to the tail). Since every airplane is different, the aileron reversing switch must be set so that moving the aileron stick to the right will cause the airplane’s right aileron to defl ect up, thus causing the right wing to drop and the airplane to bank right. Moving the aileron stick to the left will cause the airplane’s left wing to drop and the airplane to bank left. This is one important method for turning the aircraft. ELEVATOR (CH2) Controls the moveable horizontal surfaces on the airplane’s tail to rotate the airplane about the “pitch” axis (an imaginary line extending through the center of both main wings, from one wing tip to the other wing tip). Position the elevator reversing switch so that pulling the elevator stick back (towards you) will cause the elevators to defl ect up, thus causing the nose of the airplane to rise. Pushing the elevator stick forwards (away from you) will cause the nose of the airplane to drop. When using the ailerons to bank the airplane’s wings, pulling the elevator stick back will help the aircraft maintain altitude and turn the aircraft more quickly. THROTTLE (CH3) Controls the speed (R.P.M.) at which the engine or electric motor operates. With the throttle reversing switch in the NOR position, pulling the throttle stick back will cause the engine’s speed to decrease. Pushing the throttle stick forward will cause the engine’s speed to increase. RUDDER (CH4) Controls the sideways movement of the airplane’s tail and will rotate the airplane about the “yaw axis” (an imaginary line from the top of the airplane’s fuselage to the bottom of the fuselage, located near the center-point of the fuselage). Position the rudder reversing switch so that moving the rudder stick to the right causes the rudder to defl ect to the right, thus causing the nose of the airplane to point to the right. Moving the rudder stick to the left will cause the nose of the airplane to turn 4 left. When using the rudder in conjunction with the ailerons, the airplane’s nose can point into a turn (instead of pointing up and “skidding” through the turn), allowing the airplane to perform tighter, more coordinated turns. RETRACTABLE LANDING GEAR (CH5) Channel 5 offers non-proportional control of a servo, and is typically used to control retractable landing gear. Servo movement is limited to rotating the servo’s output arm to the end of clockwise movement, and the end of counter-clockwise movement. The switch for channel 5 is located on the top-left of the transmitter. FLAPS (CH6) Channel 6 offers proportional control of a servo anywhere throughout the rotational range of the servo’s output arm. This control is normally used to adjust the position of an airplane’s fl aps. The dial for channel 6 is located above the left stick. TRIMS A “trim” lever is included for each of the main controls, located adjacent to the respective stick. The aileron, elevator, and rudder trim levers are digital in function, and always rest at center…

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Operational description

Report No: CCIS13100042201 Shenzhen Zhongjian Nanfang Testing Co., Ltd. Project No.: CCIS131000422RF No.B-C, 1/F., Building 2, Laodong No.2 Industrial Park, Xixiang Road, Bao’an District, Shenzhen, Guangdong, China Telephone: +86 (0) 755 23118282 Fax: +86 (0) 755 23116366 Page 37 of 43 8 EUT Constructional Details Exterior photo Report No: CCIS13100042201 Shenzhen Zhongjian Nanfang Testing Co., Ltd. Project No.: CCIS131000422RF No.B-C, 1/F., Building 2, Laodong No.2 Industrial Park, Xixiang Road, Bao’an District, Shenzhen, Guangdong, China Telephone: +86 (0) 755 23118282 Fax: +86 (0) 755 23116366 Page 38 of 43 Report No: CCIS13100042201 Shenzhen Zhongjian Nanfang Testing Co., Ltd. Project No.: CCIS131000422RF No.B-C, 1/F., Building 2, Laodong No.2 Industrial Park, Xixiang Road, Bao’an District, Shenzhen, Guangdong, China Telephone: +86 (0) 755 23118282 Fax: +86 (0) 755 23116366 Page 39 of 43

Size：20mmX15mm Label location

Report No: CCIS13100042201 Shenzhen Zhongjian Nanfang Testing Co., Ltd. Project No.: CCIS131000422RF No.B-C, 1/F., Building 2, Laodong No.2 Industrial Park, Xixiang Road, Bao’an District, Shenzhen, Guangdong, China Telephone: +86 (0) 755 23118282 Fax: +86 (0) 755 23116366 Page 40 of 43 Interior photo Report No: CCIS13100042201 Shenzhen Zhongjian Nanfang Testing Co., Ltd. Project No.: CCIS131000422RF No.B-C, 1/F., Building 2, Laodong No.2 Industrial Park, Xixiang Road, Bao’an District, Shenzhen, Guangdong, China Telephone: +86 (0) 755 23118282 Fax: +86 (0) 755 23116366 Page 41 of 43 Report No: CCIS13100042201 Shenzhen Zhongjian Nanfang Testing Co., Ltd. Project No.: CCIS131000422RF No.B-C, 1/F., Building 2, Laodong No.2 Industrial Park, Xixiang Road, Bao’an District, Shenzhen, Guangdong, China Telephone: +86 (0) 755 23118282 Fax: +86 (0) 755 23116366 Page 42 of 43 Report No: CCIS13100042201 Shenzhen Zhongjian Nanfang Testing Co., Ltd. Project No.: CCIS131000422RF No.B-C, 1/F., Building 2, Laodong No.2 Industrial Park, Xixiang Road, Bao’an District, Shenzhen, Guangdong, China Telephone: +86 (0) 755 23118282 Fax: +86 (0) 755 23116366 Page 43 of 43 ------End of report------

SAR Evaluation for extremity conditions 1. Extremity exposure conditions Devices that are designed or intended for use on extremities or mainly operated in extremity only exposure conditions; i.e., hands, wrists, feet and ankles, may require extremity SAR evaluation. When the device also operates in close proximity to the user’s body, SAR compliance for the body is also required. The 1-g body and 10-g extremity SAR Test Exclusion Thresholds should be applied to determine SAR test requirements. 2. Standalone SAR test exclusion considerations 1) The 1-g and 10-g SAR test exclusion thresholds for 100 MHz to 6 GHz at test separation distances 50 mm are determined by: [(max. power of channel, including tune-up tolerance, mW)/(min. test separation distance, mm)] · )(GHz f ≤ 3.0 for 1-g SAR and ≤ 7.5 for 10-g extremity SAR, where  f (GHz) is the RF channel transmit frequency in GHz  Power and distance are rounded to the nearest mW and mm before calculation  The result is rounded to one decimal place for comparison  3.0 and 7.5 are referred to as the numeric thresholds in the step 2 below The test exclusions are applicable only when the minimum test separation distance ≤ 50 mm and for transmission frequencies between 100 MHz and 6 GHz 2) At 100 MHz to 6 GHz and for test separation distances > 50 mm, the SAR test exclusion threshold is determined according to the following, and as illustrated in Appendix B of KDB 447498 D01 v05r01  [Power allowed at numeric threshold for 50 mm in step 1) + (test separation distance - 50 mm)·(f(MHz)/150)] mW, at 100 MHz to 1500 MHz  [Power allowed at numeric threshold for 50 mm in step 1) + (test separation distance – 50 mm)·10] mW at > 1500 MHz and ≤ 6 GHz 3. EUT Description The Tactic TTX600 handheld airplane radio system uses an advanced 2.4GHz spread spectrum technology to prevent unwanted outside interference from interrupting control of the model, ensuring error-free flying and eliminating the need to pull frequency pins before every flight. Tactic 2.4GHz transmitters and receivers are not compatible with other brands of 2.4GHz equipment. EUT Front view Antenna Location Top Bottom Left Ri ght Distance of antenna to extremity exposure positions(mm) Top Bottom Left Right 55 117 69 71 Table 1 Conducted power of EUT Frequency(MHz) Power in dBm Power in mW Tune-up power (dBm) Tune-up power (mW) 2403 14.26 26.67 15 31.62 2441 14.18 26.18 15 31.62 2480 14.19 26.24 15 31.62 Table 2 4. Extremity SAR test exclusion calculation According to appendix B of KDB 447498 D01v05r01, Power allowed at numeric threshold for 50 mm for 2450 MHz is 96 mW for 1-g SAR, 242 mW for 10-g extremity SAR, so the SAR exclusion threshold for Top position (worst case) is 146 mW for 1-g SAR, and 272mW for 10-g extremity SAR, and the maximum tune-up power of EUT is 36.62 mW, so the 1-g SAR and 10-g extremity SAR test is exclusion. 5. Conclusion SAR test for 1-g and 10-g extremity is exclusion.

Shenzhen Zhongjian Nanfang Testing Co., Ltd. Report No: CCIS13100042201 Authorized Signature: Bruce Zhang Laboratory Manager This report details the results of the testing carried out on one sample. The results contained in this test report do not relate to other samples of the same product and does not permit the use of the CCIS product certification mark. The manufacturer should ensure that all products in series production are in conformity with the product sample detailed in this report. This report may only be reproduced and distributed in full. If the product in this report is used in any configuration other than that detailed in the report, the manufacturer must ensure the new system complies with all relevant standards. This document cannot be reproduced except in full, without prior written approval of the Company. Any unauthorized alteration, forgery or falsification of the content or appearance of this document is unlawful and offenders may be prosecuted to the fullest extent of the law. Unless otherwise stated the results shown in this test report refer only to the sample(s) tested and such sample(s) are retained for 90 days only. 1 Cover Page FCC REPORT Applicant: Hobbico, Inc. Address of Applicant: 2904 Research Road Champaign，Illinois，USA Equipment Under Test (EUT) Product Name: 2.4G Transmitter Model No.: TTX600, TTX404,424 FCC ID: IYFTTX600PA Trade Mark: Tower Hobbies, TACTIC Applicable standards: FCC CFR Title 47 Part 15 Subpart C Section 15.247 Date of sample receipt: 18 Oct., 2013 Date of Test: 19 Oct., to 05 Nov., 2013 Date of report issued: 07 Nov., 2013 Test Result : PASS * * In the configuration tested, the EUT complied with the standards specified above. Report No: CCIS13100042201 Shenzhen Zhongjian Nanfang Testing Co., Ltd. Project No.: CCIS131000422RF No.B-C, 1/F., Building 2, Laodong No.2 Industrial Park, Xixiang Road, Bao’an District, Shenzhen, Guangdong, China Telephone: +86 (0) 755 23118282 Fax: +86 (0) 755 23116366 Page 2 of 43 2 Version Version No. Date Description 00 07 Nov., 2013 Original Prepared by: Date: 07 Nov., 2013 Report Clerk Reviewed by: Date: 07 Nov., 2013 Project Engineer Report No: CCIS13100042201 Shenzhen Zhongjian Nanfang Testing Co., Ltd. Project No.: CCIS131000422RF No.B-C, 1/F., Building 2, Laodong No.2 Industrial Park, Xixiang Road, Bao’an District, Shenzhen, Guangdong, China Telephone: +86 (0) 755 23118282 Fax: +86 (0) 755 23116366 Page 3 of 43 3 Contents Page 1 COVER PAGE ................................................................................................................................................... 1 2 VERSION ........................................................................................................................................................... 2 3 CONTENTS ....................................................................................................................................................... 3 4 TEST SUMMARY .............................................................................................................................................. 4 5 GENERAL INFORMATION .............................................................................................................................. 5 5.1 CLIENT INFORMATION ...................................................................................................................................................... 5 5.2 GENERAL DESCRIPTION OF E.U.T. ...................................................................................................................................... 5 5.3 TEST MODE .................................................................................................................................................................... 7 5.4 LABORATORY FACILITY ...................................................................................................................................................... 7 5.5 LABORATORY LOCATION ................................................................................................................................................... 7 5.6 TEST INSTRUMENTS LIST .................................................................................................................................................... 8 6 TEST RESULTS AND MEASUREMENT DATA ............................................................................................. 9 6.1 ANTENNA REQUIREMENT: ................................................................................................................................................. 9 6.2 CONDUCTED OUTPUT POWER .......................................................................................................................................... 10 6.3 20DB OCCUPY BANDWIDTH ............................................................................................................................................ 12 6.4 CARRIER FREQUENCIES SEPARATION .................................................................................................................................. 14 6.5 HOPPING CHANNEL NUMBER .......................................................................................................................................... 17 6.6 DWELL TIME ................................................................................................................................................................. 18 6.7 PSEUDORANDOM FREQUENCY HOPPING SEQUENCE ............................................................................................................. 19 6.8 BAND EDGE .................................................................................................................................................................. 20 6.8.1 Conducted Emission Method ..................................................................................................................... 20 6.8.2 Radiated Emission Meth…

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Report No: CCIS13100042201 Shenzhen Zhongjian Nanfang Testing Co., Ltd. Project No.: CCIS131000422RF No.B-C, 1/F., Building 2, Laodong No.2 Industrial Park, Xixiang Road, Bao’an District, Shenzhen, Guangdong, China Telephone: +86 (0) 755 23118282 Fax: +86 (0) 755 23116366 Page 36 of 43 7 Test Setup Photo Radiated Spurious Emission