
Text extracted from the exhibit documents filed with the FCC. Open a document above to read the original.
5 6 IMPORTANT NOTES a. 8 x "AA" alkaline batteries (not included) for transmitter.(Diagram 2a) b. 7.2V 2/3 "A" Ni-MH rechargeable battery pack (included).(Diagram 2b) (A). Check the contents list and parts (Diagram 1): BATTERIES REQUIREMENT 12 8 x 1.5V / 8 x"AA" / 8 x LR6 7.2V 2/3"A"900mAh 3 4 7 89 10 ITEM NO. 0202 CONTENTS Air Knight 7.2V 2/3โAโ 900 mAh FAST CHARGER-OFF-SLOW CHARGER SWITCH FAST-OFF-SLOW CHARGING SIGNAL LIGHT BATTERY POWER SIGNAL LIGHT CAR CHARGER CHARGER PLUG CHARGER'S CONNECTOR 8 x LR6 / 8 x 1.5V / 8 x "AA"8 x LR6 / 8 x 1.5V / 8 x "AA" ON OFF ON OFF ON OFF speed control trims direction control speed up speed down the adjustor of vertical rudder the adjustor of horizontal rudder 2 Main wings 2 Joints 1 Wing cover 1 Fuselage 1 Horizontal wing 1 Vertical wing 1 Plastic sheet 1 Landing gear 1 2 3 4 5 6 7 8 9 10 11 12 13 1 Cross-headed screw driver 1 7.2 V 2/3 "A" rechargeable battery pack screws 1 Antenna 12 Screws 1 Transmitter 16 Rubber bands 1 Car charger 1 2 14 15 3 4 5 6 7 8 9 10 12 11 14 15 13 LET'S GO FLYING b). Take off from the ground. Place the airplane on the ground and switch โONโ the transmitter. Push the left stick to the top on the transmitter and propeller will rotate in the highest speed. The airplane will move forword in full speed and take off from the ground. (Diagram 15) CAUTIONS! The person who holds the airplane should NOT touch the propeller with any parts of his body to avoid injury. 1. Switch to "OFF" position, and plug into the electric power input of car, connecting the rechargeable battery to the charger. 2. Switch to fast charge/slow charge, charging signal light or battery power signal light is "ON" that means started charging. 3. After while(fast charge around 40 mins, slow charge around 80 mins), charging signal light is "OFF" and battery is warm that means fully charged for the rechargeable battery. 4. Switch to "OFF" position, take off the charger. Attention: 1. Please do not charge the same rechargable battery continous two times. 2. Please do not use over 12V electric power or the other kind of battery connect to the charger. 3. After fully charged battery are left over 24 hours, please charge again when use. 4. The charger has build-in fuse, when the circuit or rechargable battery set are overheated, the fuse will off the power for protection and safety used. 5. The situation of the liquid coming out from the battery, overheat of the surface of the battery, smoke coming out from the battery are happened, when it is charging. Please take out the battery and the charger immediately. 1 1 3 2 2 ON OFF ON OFF ON OFF ON OFF Battery indicator Warning light Battery voltage indicators 1. BATTERIES INSTALLATION OF TRANSMITTER 1) Horizontally pull down the battery cover, depending on the polarity of batteries installs batteries to the transmitter. (Diagram 3) 2) Transmitter battery power indicator has 5 LED light. (Red light is battery power, yellow light is warning, green light are voltage indicators) 1. Check the contents list and all parts. 2. Study the instruction manual carefully before assembling. 3. Ensure all required batteries are ready. 4. Follow the instructions printed in manual when using the quick charger 5. This product is intended for 14 years and up. (Adult supervision is required if user is below 14 years old) 6. Do not fly over or near people, power pylon, buildings, highways, train rails, vehicles, trees, lake, and airport. 7. Do not fly if wind speed is over 3 M/S(or over 5 mph) 2. PLANE ASSEMBLY 2. THE METHOD OF USING CHARGER AND RECHARGEABLE BATTERY 1) Wing assembly After match left/right wings together, put the wings cover on top of the left/right wings and put 4 pieces of รธ2.0 * 5PWB screws. Installs and put 4 pieces of รธ2.0 * 5PWB screws into the joints.(Diagram 5) 2) Landing gear installation Put the landing gear and plastic sheet together to install into the bottom of the plane. After that, put the รธ2.0 * 5PB screw to fix it.(Diagram 6) 4) Wings and body installation Put wings on top of the plane body and use rubber bangs to fix it, following the picture instruction.(Diagram 8) Switch to โOFFโ position before installing the battery. Motor on/off switch After connecting battery and charger, switch to โFASTโ position for fast charging(40 mins) or switch to โSLOWโ position for slow charging (80mins). The charger will be automatically cut off power. Charging time is around 40 minutes. 1. Insert a fully charged rechargeable battery into the plane body.(Diagram 11a) 2. Follow the direction showed in diagram to tied up the battery inside the plane.(Diagram 11b) 3. Place the cover on top of the body then screw in one screw into both end of the cover holes.(Diagram 11c) 4. BATTERY INSTALLATION 5. USE AND CONTROL OF TRANSMITTER 6. USE OF CONTROL STICK 1. First pull out the antenna to full position, and then switch to โONโ position (all light will switch on). Advised to move trims to middle position. 2. Left control stick on the transmitter is for speed control. Turn over the plane body and then switch โONโ the plane power, then the speed control stick is pushed vertical up/down; the engine will start running and the propeller will also start rotating. The amount of speed will change according to the amount of movement apply to control stick. (Diagram 12) 1. Push the controller stick to right/left, the vertical rudder will respond and move the same direction as the stick. the plane will turn direction during fly according movement of the rudder. 2. Push the controller stick to up/down, the horizontal rudder will respond in moving opposite direction. When the stick is pushed up, the rudder will flip down, in result of that the plane will fly lower. otherwise pushing the stick down will result in the plane fly higher. Note: When all three battery voltage indicators (green lights) are switched off, that indicates the โAAโ battery of the transmitter need renewing. 1. Starting a). Fly by hand. Use left hand to hold the transmitter anโฆ
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FCC ID Label FCC ID: QW70202 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.
THRU Lab & Engineering. RM1105,11FL, ACE TECHNO TOWER 197-22,GURO-DONG GURO-GU SEOUL KOREA T81221095059F81221095056 email [email protected] APPLICANT: HOBBYENGINE MODEL INDUSTRIAL LTD. FCC ID: QW70202 REPORT #: THRU-404006 COVER SHEET Test Report Product Name: 26.96-27.28 MHz Wireless R/C Toy - TX FCC ID: QW70202 Applicant: HOBBYENGINE MODEL INDUSTRIAL LTD. ROOM 619, 6/F., PENINSULA CENTRE, 67 MODY ROAD, TSIMSHATSUI EAST KOWLOON HONG KONG Date Receipt: 04/20/2004 Date Tested: 04/21/2004 THRU Lab & Engineering. RM1105,11FL, ACE TECHNO TOWER 197-22,GURO-DONG GURO-GU SEOUL KOREA T81221095059F81221095056 email [email protected] APPLICANT: HOBBYENGINE MODEL INDUSTRIAL LTD. FCC ID: QW70202 REPORT #: THRU-404006 COVER SHEET TABLE OF CONTENTS LIST APPLICANT: HOBBYENGINE MODEL INDUSTRIAL LTD. FCC ID: QW70202 TEST REPORT CONTAINING: PAGE 1...............TEST EQUIPMENT LIST PAGE 2...............TEST PROCEDURE PAGE 3-5.............RADIATION INTERFERENCE TEST DATA PAGE 6...............OCCUPIED BANDWIDTH PAGE 7...............OCCUPIED BANDWIDTH PLOT EXHIBITS CONTAINING: BLOCK DIAGRAM SCHEMATIC PARTS LIST INSTRUCTION MANUAL SAMPLE OF FCC ID LABEL LOCATION OF FCC ID LABEL EXTERNAL PHOTO - FRONT SIDE EXTERNAL PHOTO - BACK SIDE INTERNAL PHOTO - COMPONENT SIDE INTERNAL PHOTO - COPPER SIDE CIRCUIT DESCRIPTION THRU Lab & Engineering. RM1105,11FL, ACE TECHNO TOWER 197-22,GURO-DONG GURO-GU SEOUL KOREA T81221095059F81221095056 email [email protected] APPLICANT: HOBBYENGINE MODEL INDUSTRIAL LTD. FCC ID: QW70202 REPORT #: THRU-404006 Page 1 of 7 Test Equipment List DEVICE MODEL MFGR SERNO DUE.CAL EMI Test Receiver ESVS 10 Rohde & Schwarz 830489/001 2005.04.07. Spectrum Analyzer 8566B Hewlett Packard 2311A02394 2005.04.07. Spectrum Display 85662A Hewlett Packard 2542A12429 2005.04.07. Quasi-Peak Adapter 85650A Hewlett Packard 2521A00887 2005.04.07. RF Preselector 85685A Hewlett Packard 2648A00504 2005.04.07. Pre-Amplifier 8449B Hewlett Packard 3008A00375 2005.04.07. Pre-Amplifier 8447F Hewlett Packard 3113A05367 2005.04.07. Spectrum Monitor EZM Rohde & Schwarz 862304/007 2005.04.07. Bico-Antenna 94455-1 Eaton 977 2005.03.17. Log-Periodic Antenna 3146 EMCO 2051 2005.03.17. Dipole Antenna TDA25/1/2 Electro Metrics 176/200/200 2005.03.17. Horn Antenna SAS-571 A.H Systems 414 2005.03.17. Spectrum Analyzer R3261C Advantest 71720189 2005.04.07. LISN KNW-242 Kyoritsu 8-923-2 2004.07.17. LISN 8012-50-R- 24 Solar 8379121 2004.07.17. Loop Ant 6507 EMCO 1435 2004.10.06. Signal Generator SMS Rohde & Schwarz 872165/100 2005.04.07. Modulation Analyzer 8901B Hewlett Packard 3438A05094 2005.04.07. Frequency Counter CMC251 Tektronic CMC-251TW52489 2005.04.07. THRU Lab & Engineering. RM1105,11FL, ACE TECHNO TOWER 197-22,GURO-DONG GURO-GU SEOUL KOREA T81221095059F81221095056 email [email protected] APPLICANT: HOBBYENGINE MODEL INDUSTRIAL LTD. FCC ID: QW70202 REPORT #: THRU-404006 Page 2 of 7 TEST PROCEDURE GENERAL: This report shall NOT be reproduced except in full without the written approval of Thrulab & Engineering. RADIATION INTERFERENCE: The test procedure used was ANSI STANDARD C63.4- 1992 using a HEWLETT PACKARD spectrum analyzer with a preselector. The bandwidth of the spectrum analyzer was 100 kHz with an appropriate sweep speed. The analyzer was calibrated in dB above a microvolt at the output of the antenna. The resolution bandwidth was 100 kHz and the video bandwidth was 300 kHz. The ambient temperature of the UUT was 25ยบC with a humidity of 75%. FORMULA OF CONVERSION FACTORS: The Field Strength at 3m was established by adding the meter reading of the spectrum analyzer (which is set to read in units of dBuV) to the antenna correction factor supplied by the antenna manufacturer. The antenna correction factors are stated in terms of dB. The gain of the Preselector was accounted for in the Spectrum Analyzer Meter Reading. Example: Freq (MHz) METER READING + ACF = FS 33 20 dBuV + 10.36 dB = 30.36 dBuV/m @ 3m ANSI STANDARD C63.4-1992 10.1.7 MEASUREMENT PROCEDURES: The unit under test was placed on a table 80 cm high and with dimensions of 1m by 1.5m. The table used for radiated measurements is capable of continuous rotation. When an emission was found, the table was rotated to produce the maximum signal strength. At this point, the antenna was raised and lowered from 1m to 4m. The antenna was placed in both the horizontal and vertical planes. The situation was similar for the conducted measurement except that the table did not rotate. The EUT was setup as described in ANSIC63.4-1992 with the EUT 40 cm from the vertical ground wall. Not Applicable, battery operated. THRU Lab & Engineering. RM1105,11FL, ACE TECHNO TOWER 197-22,GURO-DONG GURO-GU SEOUL KOREA T81221095059F81221095056 email [email protected] APPLICANT: HOBBYENGINE MODEL INDUSTRIAL LTD. FCC ID: QW70202 REPORT #: THRU-404006 Page 3 of 7 APPLICANT: HOBBYENGINE MODEL INDUSTRIAL LTD. FCC ID: QW70202 NAME OF TEST: RADIATION INTERFERENCE RULES PART NO.: 15.227(a) REQUIREMENTS: CARRIER FREQUENCY SHALL NOT EXCEEDS 10,000 microvolts/meter AT 3M. Frequency (MHz) Meter Reading dBuv/m PK Meter Reading dBuv/m AV Polar Ant Height m Antenna Factor dB Cable Loss dB Result dBuv PK Result dBuv AV Limit dBuv/m PK Limit dBuv/m AV Margin dBuv/m PK Margin dBuv/m AV 27.095 35.3 33.6 H 2.4 16.1 0.9 52.3 50.6 100 80 -47.7 -29.4 27.095 54.4 51.6 V 2.20 16.1 0.9 71.4 68.6 100 80 -28.6 -11.4 SAMPLE CALCULATION: FSdBuV/m = MR (dBuV) + ACFdB. TEST PROCEDURE : The procedure used was ANSI STANDARD C63.4-1992. The spectrum was scanned from 30 MHz to 1000 MHz. When an emission was found, the table was rotated to produce the maximum signal strength. The antenna was placed in both the horizontal and vertical planes and the worse case emissions were reported. The UUT was tested in 3 orthogonal planes. TEST RESULTS: THE UNIT DOES MEET THE FCC REQUIREMENTS. PERFORMED BY: K.M CHOI DATE: 04/21/2004 THRU Lab & Engineering. RM1105,11FL, ACE TECHNO TOWER 197-22,GURO-DONG GURO-GU SEOUL KOREA T81221095โฆ
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THRU Lab & Engineering. RM1105,11FL, ACE TECHNO TOWER 197-22,GURO-DONG GURO-GU SEOUL KOREA T81221095059F81221095056 email [email protected] APPLICANT: HOBBYENGINE MODEL INDUSTRIAL LTD. FCC ID: QW70202 REPORT #: THRU-404006 THRU Lab & Engineering. RM1105,11FL, ACE TECHNO TOWER 197-22,GURO-DONG GURO-GU SEOUL KOREA T81221095059F81221095056 email [email protected] APPLICANT: HOBBYENGINE MODEL INDUSTRIAL LTD. FCC ID: QW70202 REPORT #: THRU-404006 THRU Lab & Engineering. RM1105,11FL, ACE TECHNO TOWER 197-22,GURO-DONG GURO-GU SEOUL KOREA T81221095059F81221095056 email [email protected] APPLICANT: HOBBYENGINE MODEL INDUSTRIAL LTD. FCC ID: QW70202 REPORT #: THRU-404006
| # | Rule Parts | Frequency Range | Power Output |
|---|---|---|---|
| 1 | 15C | 26.96 MHz - 27.28 MHz | - |

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