PASUKAN UDARA TENTERA DARAT REFERENCE A109 LOH ELECTRICAL TRAINING MANUAL CH 24 A109 LOH ROTORCRAFT FLIGHT MANUAL VOL 1 OBJECTIVE AT THE END OF THE LESSON, STUDENT WILL ABLE TO : UNDERSTAND DC POWER SYSTEM MENTION THE COMPONENT AND PART OF DC POWER SYSTEM MENTION THE INDICATION OF DC POWER SYSTEM SCOPE DC GENERATION SYSTEM DC DISTRIBUTION SYSTEM ELECTRICAL MONITORING AND INDICATION DC GENERATION SYSTEM 3 TYPE POWER SOURCE FOR AIRCRAFT EXTERNAL GROUND POWER UNIT INTERNAL POWER PRIMARY POWER GENERATION EXTERNAL GROUND POWER INTERNAL POWER / AIRCRAFT BATERY INTERNAL POWER / AIRCRAFT BATERY BATTERY TYPE (NI-CD) BATTERY RATING (24V-40A/H) PRIMARY POWER GENERATION DC STARTER GENERATOR OUTPUT POWER (6 KVA) OUTPUT VOLTAGE (28V) MAX TRANS LOAD (300A) MAX CONT LOAD (200A) SPEED RANGE (7200RPM TO 12100RPM) DC GENERATION SYSTEM STARTER- GEN 1 AIRCRAFT LOAD EXTERNAL POWER @ BATTERY STARTER-GEN 2 * CHANGE FROM STARTER TO GENERATOR AT 7193 RPM OR 50% NG DC GENERATION CONTROL MSTR AVNX BAT SWITCH GEN SWITCH GEN BUS SWITCH MSTR AVNX SWITCH GND COM GND NORM MSTR AVNX SWITCH MSTR AVNX switch set to GND COM only the following equipment is supplied with electrical power •GCP#1 •GCP#2 •V/UHF #2 & LOGIC UNIT •ADL •CMU •MCDU •NAVM •HF DC GENERATION CONTROL MSTR AVNX switch set to GND, electrical power is removed from •MFD #1 •DF •IFF •DVS •HF transceiver •Observation system •VOR DC DISTRIBUTION SYSTEM DC DISTRIBUTION SYSTEM COMPONENT AND LOCATION AIRCRAFT FEEDER BUSSES MAIN BUS MISSION BUS EMERGENCY BUS ESSENTIAL BUS GROUND BUS BATTERY BUS DC POWER SYSTEM BLOCK DIAGRAM DC POWER SYSTEM BLOCK DIAGRAM DC POWER SYSTEM BLOCK DIAGRAM DC POWER SYSTEM BLOCK DIAGRAM AIRCRAFT BATTERY AIRCRAFT BATTERY AIRCRAFT BATTERY ELECTRICAL MONITORING AND PROTECTION WARNING INDICATION ELECTRICAL BATT DISCH ELECTRICAL MONITORING AND PROTECTION ELECTRICAL WHEN BOTH GENERATORS ARE INOPERATIVE, THE FLIGHT CAN BE CONTINUED ON BATERY POWER FOR A MAXIMUM OF 30 MINUTES IF THE GENERATOR BUSSES ARE NOT DISCONNECTED, THE BATERY IS CAPABLE FOR ONLY 20 MINUTES ELECTRICAL MONITORING AND PROTECTION CAUTION INDICATION #1 DC GEN #2 DC GEN #1 ESS BUS #2 ESS BUS #1 EMER BUS #2 EMER BUS #1 DC CTRL #1 DC CTRL #1 BUS TIE #2 BUSTIE BATT OFF EXT PWR ELECTRICAL MONITORING AND PROTECTION CAUTION INDICATION #1 DC GEN #2 DC GEN #1 ESS BUS #2 ESS BUS #1 EMER BUS #2 EMER BUS #1 DC CTRL #1 DC CTRL #1 BUS TIE #2 BUSTIE BATT OFF EXT PWR ELECTRICAL MONITORING AND PROTECTION CAUTION INDICATION #1 DC GEN #2 DC GEN #1 ESS BUS #2 ESS BUS #1 EMER BUS #2 EMER BUS #1 DC CTRL #1 DC CTRL #1 BUS TIE #2 BUSTIE BATT OFF EXT PWR ELECTRICAL MONITORING AND PROTECTION CAUTION INDICATION #1 DC GEN #2 DC GEN #1 ESS BUS #2 ESS BUS #1 EMER BUS #2 EMER BUS #1 DC CTRL #1 DC CTRL #1 BUS TIE #2 BUSTIE BATT OFF EXT PWR ELECTRICAL MONITORING AND PROTECTION CAUTION INDICATION #1 DC GEN #2 DC GEN #1 ESS BUS #2 ESS BUS #1 EMER BUS #2 EMER BUS #1 DC CTRL #1 DC CTRL #1 BUS TIE #2 BUSTIE BATT OFF EXT PWR ELECTRICAL MONITORING AND PROTECTION CAUTION INDICATION #1 DC GEN #2 DC GEN #1 ESS BUS #2 ESS BUS #1 EMER BUS #2 EMER BUS #1 DC CTRL #1 DC CTRL #1 BUS TIE #2 BUSTIE BATT OFF EXT PWR ELECTRICAL MONITORING AND PROTECTION CAUTION INDICATION #1 DC GEN #2 DC GEN #1 ESS BUS #2 ESS BUS #1 EMER BUS #2 EMER BUS #1 DC CTRL #1 DC CTRL #1 BUS TIE #2 BUSTIE BATT OFF EXT PWR BATTERY POWER GROUND POWER UNIT EXTERNAL GROUND POWER •A DC receptacle located on the right section on the cabin. •Supply power to all DC busses of the aircraft. •Used for engine starting & maintenance purposes. •Rectifier & Power Pack. WARNING,CAUTION & ADVISORY INDICATIONS DC Warning DC Caution DC Advisory - Red - Yellow - Green The EPDGS advices system status and malfunction through the AMS Advisory, Caution and Warning System. Located on screen in instrument console DC POWER SYSTEM CONTROLS & INDICATIONS DC POWER SYSTEM CONTROLS AND INDICATIONS DC POWER SYSTEM CONTROLS AND INDICATOR OVERHEAD CONSOLE PANEL CB CO PILOT OVERHEAD CONSOLE PANEL CB PILOT OVERHEAD CONSOLE PANEL CB