QEAMIPLANE49TRC Field Flyer

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49.860MHz transmitter operational description of mini plane The transmitter send out 49.820MHz ~ 49.900MHz signal of high frequency to control the plane move which supply voltage is 9.0volts with six batteries (size AA). Please consult with added block diagram and schematic. When the user pulls the trigger to up and pulls the trigger run left or right (schematic presents with S2 ~ S5), the IC U1 high voltage enters into GND. these signal is processed by IC and sent out through Q3, X1, Q1, L2, C4 makes up of oscillator, which generated base oscillatory signal .The signal of R, L, F, and B come by T1, C12, L5, C13, C14 and fixed 49.860MHz of high frequency, it is sent out. When the user need charger about RX battery, the U3 and Q2 would adjust out current. When working finish the D3 LED would dies. D1 LED acts as a power ñon indicator, D2 LED is use the charger
All tuning and verifications are performed by the manufacturer and there are no adjustment which can be made by the user. No external ground is required or used with this transmitter.

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TEST REPORT Report No. : AJ009136-001 Date : 2007 May 31 Page 1 of 11 FCC ID: QEAMIPLANE49T This document shall not be reproduced except in full or with written approval by the laboratory. CMA Industrial Development Foundation Limited Room 1302, Yan Hing Centre, 9-13 Wong Chuk Yeung St.., Fo Tan, Shatin, Hong Kong. Tel: (852) 2698 8198 Fax: (852) 2695 4177 E-mail: [email protected] Web Site: http://www.cmatcl.com Application No. : LJ208075(0) Client : Kid Galaxy INC 150 Dow Street, Tower 2, Unit 425B Manchester, NH 03101 Sample Description : One(1) submitted sample(s) stated to be RC Field Flyer of Model No. 10245 Radio Frequency : 49.860MHz Transmitter Rating : 6 x 1.5V AA size batteries No. of submitted sample : Three (3) piece(s) *** Date Received : 2007 April 10 Test Period : 2007 April 12 ñ 2007 April 18 Test Requested : FCC Part 15 Certification. Test Method : 47 CFR Part 15 (10-1-05 Edition) ANSI C63.4 ñ 2003 Test Result : See attached sheet(s) from page 2 to 11. Conclusion : The submitted sample was found to comply with requirement of FCC Part 15 Subpart C. For and on behalf of CMA Industrial Development Foundation Limited Authorized Signature : ____________________________________________________ Danny Chui Deputy Manager - EL. Division TEST REPORT Report No. : AJ009136-001 Date : 2007 May 31 Page 2 of 11 FCC ID: QEAMIPLANE49T This document shall not be reproduced except in full or with written approval by the laboratory. CMA Industrial Development Foundation Limited Room 1302, Yan Hing Centre, 9-13 Wong Chuk Yeung St.., Fo Tan, Shatin, Hong Kong. Tel: (852) 2698 8198 Fax: (852) 2695 4177 E-mail: [email protected] Web Site: http://www.cmatcl.com Table of Contents 1 General Information .............................................................................................................................3 1.1 General Description .....................................................................................................................3 1.2 Location of the test site ................................................................................................................4 1.3 List of measuring equipment........................................................................................................5 2 Description of the radiated emission test .............................................................................................6 2.1 Test Procedure..............................................................................................................................6 2.2 Test Result....................................................................................................................................6 2.3 Radiated Emission Measurement Data ........................................................................................7 3 Description of the Line-conducted Test...............................................................................................8 3.1 Test Procedure..............................................................................................................................8 3.2 Test Result....................................................................................................................................8 3.3 Graph and Table of Conducted Emission Measurement Data .....................................................8 4 Photograph ...........................................................................................................................................9 4.1 Photographs of the Test Setup for Radiated Emission and Conduction Emission ......................9 4.2 Photographs of the External and Internal Configurations of the EUT.........................................9 5 Supplementary document ...................................................................................................................10 5.1 Bandwidth ..................................................................................................................................10 5.2 Duty cycle ..................................................................................................................................10 5.3 Transmission time ......................................................................................................................10 6 Appendices .........................................................................................................................................11 TEST REPORT Report No. : AJ009136-001 Date : 2007 May 31 Page 3 of 11 FCC ID: QEAMIPLANE49T This document shall not be reproduced except in full or with written approval by the laboratory. CMA Industrial Development Foundation Limited Room 1302, Yan Hing Centre, 9-13 Wong Chuk Yeung St.., Fo Tan, Shatin, Hong Kong. Tel: (852) 2698 8198 Fax: (852) 2695 4177 E-mail: [email protected] Web Site: http://www.cmatcl.com 1 General Information 1.1 General Description The equipment under test (EUT) is a transmitter for RC Field Flyer. It operates at 49.860MHz and the oscillation of radio control is generated by a crystal. The EUT is powered by six AA size batteries. There is a control stick on the EUT. When the control stick is pushed to accelerated, decelerated, turn right or turn left direction, the EUT will transmit different radio control signal to the receiver. The brief circuit description is listed as follows: - U3, Q2, Q4 and associated circuit act as a charger for receiver. - D2 and associated circuit act as a voltage regulator. - U1 and associated circuit act as an encoder. - X1, Q1 and associated circuit act as an oscillator. - Q3 and associated circuit act as a RF amplifier. TEST REPORT Report No. : AJ009136-001 Date : 2007 May 31 Page 4 of 11 FCC ID: QEAMIPLANE49T This document shall not be reproduced except in full or with written approval by the laboratory. CMA Industrial Development Foundation Limited Room 1302, Yan Hing Centre, 9-13 Wong Chuk Yeung St.., Fo Tan, Shatin, Hong Kong. Tel: …

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Job No. WF-EL-EMC-15 Edition 1 2006 April 12 Page of Bandwidth Plot Bandwidth 1

Job No. WF-EL-EMC-15 Edition 1 2006 April 12 Page of Duty Cycle Duty Cycle 1 Duty Cycle 2 Job No. WF-EL-EMC-15 Edition 1 2006 April 12 Page of Duty Cycle Duty Cycle 3