Tesla TI2000GPU-24

5-3

FIGURE 5-2

TI2000GPU-24 OUTPUT VOLTAGE

OUTPUT VOLTAGE

MINUTES

46 AMP CONSTANT CURRENT LOAD

010 20 30 40 50 60

Contents

Main NONE LIST OF ILLUSTRATIONS Page Page Page 1-3 UNIT DESCRIPTION AND OPERATION Page Page 2-4 Fuse Setting Procedures for Switching Voltages or Changing Blown Fuses CHAPTER 3 OPERATING LIMITS AND RESTRICTIONS FOR MORE INFORMATION ON POWER CORDS SEE APPENDIX A Page without with (C0NTINUED ON NEXT PAGE) without 120 or 240 power cord Horizontal only Page CHAPTER 4 OPERATING PROCEDURES always STATUS CHECK FUSE WINDOW FOR PROPER SETTING (120/240 BEFORE PLUGGING UNIT INTO THE AC POWER SOURCE TO BE USED the unit down horizontally ensuring vent ports are un-blocked. 5. REMOVING DC POWER SUPPLY FROM AIRCRAFT CHECK FUSE WINDOW FOR PROPER SET- TING Unit shall be in horizontal position to ensure units vent ports are free from blockage 6. REMOVING DC POWER SUPPLY FROM AIRCRAFT Page Page FUNCTIONAL CHECK PROCEDURES CHECK FUSE WINDOW FOR PROPER SET- TING Unit shall be in horizontal position to ensure units vent ports are free from blockage Page CHAPTER 5 SECTION 1. INTRODUCTION DATA CRITERIA Derived From Actual Controlled Testing. Variation in Aircraft. Estimated Data Calculated Data. Page Page Page CHAPTER 6 CARE AND MAINTENANCE SECTION I. UNIT CARE CHECK FUSE WINDOW FOR PROPER SETTING Page Chapter 7 Push To Test Modification General Information And Operation Page Page APPENDIX A A-1 A-2 A-3 A-4 UNIVERSAL LINE CORD KIT FOR WORLDWIDE OPERATIONS