Tesla TI2000GPU-24

3-6

CAUTION

Unit damage may occur if inlet and outlet vent ports are obstructed

and/or cooling air flow is restricted.

3-13. UNIT OPERATION DURING AIRCRAFT FUELING/DEFUELING

Power output is restricted to 24 VDC power cell output only. DO

NOT CONNECT 120 or 240 VAC POWER SUPPLY. 120-240 VAC power

(charger or AC-DC converter) functions of unit shall not be oper-

ated during any aircraft fuel handling operation.

WARNING

*******FIRE/EXPLOSION HAZARD POTENTIAL********

Severe injury, or Death, may occur from fire or explosion, as a

result of electrical sparks produced near fuel vapors.

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