Tesla TI4676 - page 23

7. CHECK DC VOLTAGE READING AT DC RECEPTACLE TERMINALS. Ensure power

cells are fully charged (see step 6.)

28.5 (±0.57 VDC) with power cells at full state of charge.

8. FUNCTIONAL CHECK COMPLETE - Unit should remain plugged in to AC

power until ready for installtion in aircraft.

4-6

Contents

Main www.teslaind.com TABLE OF CONTENTS LIST OF ILLUSTRATIONS CHAPTER 1 INTRODUCTION Page Page CHAPTER 2 UNIT DESCRIPTION AND OPERATION TI4676: 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) Page without 120 or 240 power cord Page CHAPTER 4 OPERATING AND INSTALLATION PROCEDURES always Capacity % CHECK FUSE WINDOW FOR PROPER SETTING (120/240 BEFORE PLUGGING UNIT INTO THE AC POWER SOURCE TO BE USED Page Page FUNCTIONAL CHECK PROCEDURES AND TROUBLE SHOOTING CHECK FUSE WINDOW FOR PROPER SET- TING Unit shall be in a position to en- sure units vent ports are free from blockage. Page CHAPTER 5 SECTION 1. INTRODUCTION DATA CRITERIA Derived From Actual Controlled Testing. Aircraft Instrument Variations. Variation in Aircraft. Estimated Data Page OUTPUT VOLTAGE * CHAPTER 6 CARE AND MAINTENANCE SECTION I. UNIT CARE CHECK FUSE WINDOW FOR PROPER SETTING MAINTENANCE 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