Bombardier-Challenger_01-Electrical庞巴迪挑战者电气

航空发表于 2010-5-9 08:56:38

Bombardier-Challenger_01-Electrical
 
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航空发表于 2010-5-9 08:56:56

canaetair ctiaiientyer OPERATING MANUAL PSP 601A-6 SECTION 7 ELECTRICAL TABLE OF CONTENTS Page 1. GENERAL 1 2. AC GENERATION SYSTEMS 1 A. Primary Generating System 1 B. Auxiliary Generating System 1 C. Emergency Generating System 2 3. DC GENERATION SYSTEMS 2 A. Static Conversion System 2 B. Battery System 3 4. EXTERNAL POWER 3 5. ELECTRICAL LOAD DISTRIBUTION 4 LIST OF ILLUSTRATIONS Figure Number Title Page 1 AC Generation Systems - Layout 5 2 DC Generation Systems - Layout 6 3 Electrical Power Generation and Distribution System - 7/8 Basic Configuration 4 Primary AC Power Control 9 5 Auxiliary AC Power Control 10 6 Main DC Power Control 11 7 Essential AC Power and ADG Control 12 8 External Power and Battery Control 13 9 AC and DC Metering 14 7-CONTENTS Page 1 Apr 02/87 OPERATING MANUAL PSP 601A-6 Figure Title Page Number 10 Main AC No. 1 and DC No. 1 Circuit Breaker Panel 15 11 Battery Bus - Left Circuit Breaker Panel 16 12 Main AC No. 2 and DC No. 2 Circuit Breaker Panel 17 13 Battery Bus - Right Circuit Breaker Panel 18 14 AC Essential Bus Circuit Breaker Panel 19 15 DC Essential Bus Circuit Breaker Panel 20 16 Aft Electrical Distribution Box Circuit Breaker Panel (2 Sheets) 21 7 - CONTENTS Page 2 Apr 10/95 chauenaer OPERATING KANUAL PSP 6 0 U -6 SECTION 7 ELECTRICAL GENERAL The electrical power generating system consists of the AC generation systems, the DC generation systems, the external power system and the electrical load distribution. AC GENERATION SYSTEMS (Figures 1 and 2) A. Primary Generating System The primary generating system normally supplies all i n - f l i g h t aircraft electrical power requirements- The system consists of two engine-driven integrated drive gpnerators (IDG), GEN 1 and GEN 2. Each generator provides a 115/200-volt, 400-Hz output, with a maximum power rating of 30 kVA. Each generator normally supplies power to the associated distribution system. GEN 1 supplies power to ac main bus No. 1, the ac essential bus, TRU 1 and ac utility bus No. 1. The ac essential bus supplies the essential loads and ESS TRU 1. GEN 2 supplies power to ac main bus No. 2, TRU 2 , ESS TRU 2, ac u t i l i t y bus No. 2 and the main battery charger. If either generator f a i l s , the associated bus is transferred automatically to the other generator and both ac u t i l i t y busses are disconnected. The automatic transfer circuit can be inhibited using the AUTO OFF/FAIL switch/lights. To restore the services of the ac u t i l i t y busses, the APU generator must be brought on line (refer to paragraph B.). Under bus tie conditions, if an overload occurs in the bus t i e , the generator control circuit de-energizes the transfer contactors, removing power from the failed side distribution panels. If power i s lost from ac main bus No. 1, the essential transfer contactor automatically transfers the ac essential bus to ac main essential bus No. 2. When both IDGs are operating, the ac essential bus can be manually transferred to the ac main bus No. 2 (refer to Figure 7). The GEN 1 and GEN 2 operation can be monitored on the power management panel (refer to Figures 4 and 9). B. Auxiliary Generating System The auxiliary generating system supplies aircraft electrical power on ground in lieu of external power and can also supply power in flight if both IDGs fail. The system consists of an APU-driven generator with the same power capability as a single IDG. When the aircraft i s on the ground with the flaps at zero degrees, and the APU-driven generator is on line, SECTION 7 Page 1 Apr 02/87 OPERATING MANUAL PSP 601A-6 all busses receive electrical power, with the exception of the ADG bus. In flight or with the flaps greater than zero degrees, the u t i l i ty busses are disconnected, The APU-driven generator operation can be monitored on the power management panel (refer to Figures 5 and 9). Emergency Generating System (Figure 7) The emergency generating system supplies emergency electrical power for limited distribution to essential ac services. The system consists of an automatically deployed, air-driven generator (ADG). The generator provides a 115/200-volt, 400-Hz output with a maximum power rating of 15 kVA at or above airspeeds of 160 knots. If all ac power is lost, the ADG i s deployed automatically. If automatic deployment fails, the ADG can be deployed manually by operating the ADG manual deploy handle located on the centre pedestal. When the ADG comes on line, the ADG ac emergency transfer contactor transfers the ac essential bus to the battery bus. The ADG bus receives power only when the ADG is operating. The ADG operation can be monitored on the AC METERING section of the power management panel (refer to Figure 9). DC GENERATION SYSTEMS (Figures 2 and 3) A. Static Conversion System The dc static conversion system converts the output of the ac generating system into unregulated 28-volt main dc power. The system consists of four transformer rectifier units (TRU). TRU 1, TRU 2 and ESS TRU 2 receive primary ac power from the main ac busses and ESS TRU 1 receives this power from the ac essential bus. The TRU 1 and TRU 2 supply the dc bus No. 1 and dc bus No. 2 respectively. ESS TRU 1 and ESS TRU 2 supply the dc essential bus. If TRU 1 or TRU 2 f a i l s , the affected bus can be transferred to the operating TRU, using the bus t i e switch/lights on the power managment panel (refer to Figure 6). When the bus tie function is selected, the dc utility bus No. 1 and dc u t i l i t y bus No. 2 are disconnected. The ESS TRU 1 and ESS TRU 2 are dedicated to the dc essential bus and cannot be used to supply either the dc bus No. 1 or dc bus No. 2. If ESS TRU 1 or ESS TRU 2 fails, the dc essential bus can be supplied from the operating ESS TRU, or in an emergency condition (all ac power l o s t ) , by deploying the ADG. During ADG operation, the battery bus and the dc essential bus are connected. During transfer to ADG, when the aircraft is in a weight-off-wheels condition and the battery bus i s unpowered, the dc essential bus is supplied from the battery direct bus via the DC EMER TIE CONTROL 2 contactor. SECTION 7 Page 2 Apr 02/87 OPERATING MANUAL PSP 601A-6 B. Battery System The battery system consists of the main battery and the auxiliary battery. The main battery system provides emergency dc power to the battery bus and the battery direct bus when primary dc power is lost due to a complete ac power failure (TRU 1, TRU 2, ESS TRU 1 and ESS TRU 2 are unavailable). The main battery provides a nominal output of 25 volts and has a capacity of 43 ampere-hours at the 1-hour rate. A battery charger is connected directly to the battery and operates automatically, when ac power is available, to maintain the battery in a fully charged condition. The main battery system supplies the battery bus via the battery contactor which is activated when the battery bus is unpowered due to a TRU failure, provided that the BATTERY MASTER switch on the IGNITION/ELECT PWR panel is set to ON (refer to Figure 8)- If an overload condition occurs on the battery bus, the battery RCCB trips and disconnect the battery. When the battery RCCB trips, the BATT CONT circuit breaker also trips. It is necessary to reset the BATT CONT circuit breaker (CBP-E) before resetting the BATT RCCB CONT circuit breaker (CBP-D). The main battery operation can be monitored on the DC METERING section of the power management panel (refer to Figure 9). On aircraft 5001 thru 5134, the auxiliary battery provides dc power to start the APU during cold temperature conditions (refer to SECTION 5). On aircraft 5135 and subsequent and aircraft incorporating Canadair Service Bulletin 601-0418, IRS 2 battery provides dc power to start the APU during cold temperature conditions (refer to SECTION 5). 4. EXTERNAL POWER (Figures 3 and 8) The aircraft can be supplied with electrical power from an external power source through the ac and dc receptacles located on the lower fuselage. External power is an alternative source to the auxiliary generating system power. When the APU generator is running and on line, the external power supply is take off line. The external power supplies all the busses except the ADG bus. When the flaps are greater than zero degrees or the aircraft is in a weight-off-wheels condition, the utility busses are disconnected. SECTION 7 Page 3 Apr 10/95 canadair ctiauencfer OPERATING MANUAL PSP 601A-6 5. ELECTRICAL LOAD DISTRIBUTION The electrical power is distributed through the following circuit breaker panels: - CBP-A i s located on forward bulkhead behind pilot's position and is divided into two sections. One section contains the 115-volt ac main bus No. 1, the 28-volt dc main bus No- 1, the 115-volt ac u t i l i t y bus No. 1 and the 28-volt dc u t i l i t y bus No- 1 circuit breakers. The other section contains the battery bus circuit breakers (refer to Figures 10 and 11). - CBP-B i s located on forward bulkhead behind copilot's position and is divided into two sections. One section contains the 115-volt ac main bus No. 2, the 28-volt dc main bus No. 2, the 28-volt dc u t i l i ty bus No. 2 and the 115-volt ac u t i l i t y bus No. 2 circuit breakers. The other section contains the battery bus, the 26-volt ac bus, and the 115-volt ac main bus No. 2 circuit breakers (refer to Figures 12 and 13). - CBP-C i s located in the flight compartment on pilot's left console and contains the 26-volt ac essential bus, the 115-volt ac essential bus and the 115-volt ac ADG bus circuit breakers. The other section contains the battery bus, the 26-volt ac bus, and the 115-volt ac main bus No. 2 circuit breakers (refer to Figure 14). - CBP-D i s located in the flight compartment on the copilot's right console and contains the 28-volt dc essential bus and the 28-volt dc power control circuit breakers (refer to Figure 15). - CBP-E i s located in the aft electrical distribution box in the battery compartment and contains the battery direct bus and the battery bus circuit breakers (refer to Figure 16). SECTION 7 Page 4 Apr 02/87 canacaatr ctiatienaer OPERATING MANUAL PSP 601A-6 LEGEND - AUXILIARY SYSTEM > MAIN AC SYSTEM »EMERGENCY AC SYSTEM EXTERNAL AC CONNECTION ADG AOG CONTROL UNIT AC ESSENTIAL BUS CBP-C AC Generation Systems - Layout Figure 1 SECTION 7 Page 5 Apr 02/87 OPERATING MANUAL PSP 601A-6 LEGEND • BATT AND EXT PWR •AC STATIC CONVERSION DC AUXILIARY BATTERY EFFECT1V1TY:A/C5001 TO 5134 IRS 2 BATTERY EFFECnVTTY: AJC 5135 AND SUBS AND A/C POST SB 601-0418 BATTSIY BUSRIGHT CBP-B DC ESSENTIAL BUS CBP-D TRANSFORMER RECTIFIER UNITS DC Generation Systems - Layout Figure 2 SECTION 7 Page 6 Apr 10/95 OPERATING MANUAL PSP601A-6 C DC8UST ) Electrical Power Generation and Distribution System - Basic Configuration Figure 3 SECTION 7 Page 7/8 Apr 02/87
ctianentjer OPERATING MANUAL PSP 601A-6 GEN 1 GEN "5 AND GEN 2 KVA LOAD METERS indexes the kVA io3fl on the associated gervrattv GEN OFF LIGHT Amber GEN Qfr u$r>z comes or. when the generator ts off line tor any of the following reasons: - Generator treouenry out of tolerance - Generator voJt3ge out of tolerance - No output from the generator. OVLD LIGHT if tne generator output current exceeds 100 A for m c e than 2 seconds, the overload monrtonng circuit m The GCU operates and the amber OVLD light comes on. ON-OFF 'RESET - TEST SWITCH Three-position generator control switch with the following functions: ON - supplies primary power to ac busses OFF - removes primary power f r om the ac busses RESET - respects generator after a fault TEST - checks voltage and freouency of the generator off-load. GlK MAIN BUS 1 OFF T> AUTO OFF FAIL r ^ MAIN BUS 1 OFF UGHT Amber MAIN BUS 1 OFF light comes on when main bus No. 1 is not connected to any generator. AUTO OFF SWITCH LIGHTS When pressed the automatic bus tie operation »s disabled ano the associated amber AUTO OFF light comes on. FAIL LIGHTS Associated amber FAIL light comes on if a bus tie overcurrent or generator overcurrent condition exists. MAIN BUS 2 OFF Z MAIN BUS 2 OFF LIGHT Amber MAIN BUS 2 OFF light comes on when main bus No. 2 is not connected to any generator. CENTRE PEDESTAL Primary AC Power Control SECTION7 Figure 4 Page 9 Apr 02/87 OPERATING MANUAL PSP 601A-6 nSM TOOtCftATE APU KVA LOAD METER Inoicates the kVA load on the APU generator ON-OFF/RESET - TEST SWITCH Three-position generator control switch with the following functions: ON - suppfies power to ac busses. OFF - removes auadiary power from the ac busses. RESET - reseJeets generator after a fault. TEST - checks voltage and frequency of the generator off-load. GEN OFF LIGHT Amber GEN OFF light comes on when the generator is off line for any of the following reasons: - Generator frequency out of tolerance. - Generator voltage out of tolerance. - No output from the generator. If the APU is shut down, the APU GEN OFF light goes out. BUS! BUS 2 OVLD LIGHT If the generator output current exceeds 100 A for more than 2 seconds, the overload monitoring circuit in the GCU operates and the amber OVLD light comes on. CENTRE PEDESTAL Auxiliary AC Power Control SECTION7 F i9"re 5 Page 10 Apr 02/87 "chaueiicrer OPERATING MANUAL PSP 601A-6 MAIN BUS 2 OFF LIGHT Amber MAIN BUS 2 OFF light comes on if the power is lost from the main dc bus No. 2 due to failure of TRU 2 or ac bus No. 2. Power is supplied from main dc bus No. 1 when both BUS TIE CLOSED switch/lights are pressed. MAIN BUS 1 OFF LIGHT Amber MAIN BUS 1 OFF light comes on if power is lost from the main dc bus No. 1 due to failure of TRU 1 or ac bus No. 1. Power is supplied from main dc bus No. 2 when both BUS TIE CLOSED switch/lights are pressed. ESS TRUS 1 OFF LIGHT Amber essential TRUS 1 OFF light comes on rf power is lost from ESS TRU 1 or ac essential bus. In that case, power is supplied to the dc essentia] bus from the ESS TRU 2 or in emergency condition, by deploying the ADG. _ _ _ DC POWER I TRU 1 I ^ t TR U 2 1 T BUS TIE CLOSED SWITCH/LIGHT When both the left and right BUS TIE CLOSED switch/lights are pressed, the dc bus No. 1 and dc bus No. 2 are interconnected and dc utility bus No. 1 and dc utility bus No. 2 are disconnected. ESS TRUS 2 OFF LIGHT Amber essential TRUS 2 OFF light comes on if power is lost from ESS TRU 2 or ac main bus 2. in that case, power is supplied to the dc essential bus from the ESS TRU 1 or in emergency condition, by deploying the ADG. BATT BUS OFF LIGHT Amber BATT BUS OFF light comes on if power is lost from the battery bus due to an ESS TRU 1 and ESS TRU 2 failure. Power is restored to the battery bus by deploying the ADG or by switching on the BATTERY MASTER switch. ESS BUS OFF LIGHT Amber ESS BUS OFF light comes on if power is lost from the dc essential bus due to the failure of ESS TRU 1 and ESS TRU 2. In that case, power is restored to the dc essential bus by deploying the ADG. CENTRE PEDESTAL Main DC Power Control SECTION7 Figure 6 Page 11 Apr 02/87 OPERATING MANUAL PSP 601A-6 FAIL LIGHT Amber FAIL light comes on when the ac essential voltage is less than 90 volts on any phase. ALTN SWITCH/LIGHT When pressed, green ALTN fight comes on and the ac essential bus transfers from ac bus No. 1 to ac bus No. 2- The light comes on automatically if access to ac bus No. 1 is lost. CENTRE INSTRUMENT PANEL AOG LAMP - UNIT TEST SWITCH Two-position switch checks the following: UNIT - Continuity of the uplock squib circuit - Continuity of the three transfer contactors. - Logic circuits LAMP - TEST fight - Weight-on-wheeis circuit. ADG AUTO DEPLOY TEST LIGHT Green fight comes on when the tests performed with the LAMP-UNIT test switch in the UNIT position are correct. On the ground, the fight comes on immediately for 2 seconds. In the air, the light comes on after a delay of 5 seconds and remains on for 2 seconds. A.D.G. MANUAL DEPLOY HANDLE Martuafiy deploys the ADG and energizes the throe transfer contactors. ^ ^ i ADG PWR TXFR OVERRIDE SWITCH When pressed, de-energizes the ac emergency, dc emergency and 38 hydraulic contactors if power has been restored to the main ac bus. CENTRE PEDESTAL Essential AC Power and ADG Control SECTION7 ^gure 7 Page 12 Apr 02/87 cfta/zenaer OPERATING MANUAL PSP 601A-6 ELECT PWR AVAIL LIGHT When external power is connected to the aircraft, the external power monitor checks for: - Correct phase sequence. - Voltage between 106 and 124 volts ac. • Frequency between 370 and 430 Hz. The green AVAIL light comes on if these parameters are met. ELECT PWR IN USE LIGHT When the G PWR switch is on and neither the APU nor any generator is on line, the external contactor energizes. The green AVAIL light goes out and the amber IN USE light comes on. The IN USE light also comes on when external dc power is connected. CHARGER LIGHT The amber CHARGER light comes on if any of the following conditions exist: - Battery charger fail. - Overtemperature of battery. - Loss of ESS TRU 1 and ESS TRU 2 feed to battery bus. - Charger circuit breaker tripped. - AOG deployed. ELECWPWR G PWR CONTROL SWITCH Ground power control switch energizes tne external power contacts of the AP/EPC f (auxiliary power/external power contactor* and if no other generator is on line, the ground power supplies the busses BATTERY LIGHT Amber BATTERY light comes on if any of the following conditions exist: -BATTERY MASTER switch se: to off. — Loss of power to the battery direct bus. — Faulty battery direct sensing relay. — 8attery control circuit breaker tnpped. BATTERY MASTER SWITCH ON - Connects the battery to the battery bus when no external power is connected. The battery is automatically connected to the battery bus if ESS TRU 1 and ESS TRU 2 fail. OVERHEAD PANEL External Power and Battery Control SECTION 7 Figure 8 page 13 Apr 02/87 OPERATING MANUAL PSP 601A-6 DC METERING Monitors TRU loads and bus voltages. AC METERING Monitors ac voltages and frequency. AC SELECTOR SWITCH Used to select power source to be monitored. CENTRE PEDESTAL AC and DC Metering SECTION7 Figure 9 Page 14 Apr 02/87 cacnhsacJjiseirri Qer OPERATING MANUAL PSP 601A-6 EFFECTIVITY H A/C POST SB 601 -262 AND 5135 AND SUBS g ] A/C 5001 TO 5134 [§] A/C 5041 AND 5146 0 ] A/C POST SB 601 -0396 AND 5135 AND SUBS g ] A/C POST SB 601-0262 REV.2 AND REV.3 A/C POST SB 601-0355 AND 5135 AND SUBS AR Lyi 110 S3 CONF WARN1 © 80 H CBP-A 2 5s| 5 3 14_ FLAP MOTOR - 1 1 5 V AC BU8 1 - W FAN 115] 1201 31 32 A/C 5067 AND 5087 AND SUBS g] A/C POST SB 601 -0363 ffl A/C 5001 TO 5134 Ly yj iy ii 139 140 141 142 28V DC BATTERY BU8 — STALL PR0T-,, QEN CONT UNITS — , E8S AC , LIGHT8- STICK LH XFR CTR PUSH CHAN 1 2 3 CONT FLOOD DOME WARN LT TE8T -MA8TER CAUTION- 8 CHAN 10 CHAN PILOT ANN 1 ANN 1 LIGHTS 150 151 U71/2J H 7M 152 153 TO2J 154 155 156 157 158 159 160 f3J 161 28V DC BATTERY BU8 WOW I FUELSOV 1 L FUEL | ENQ IQN . L CHAN ' R L ' PUMP ' FUEL 1 ENQ APU ENQ XFLOW CONT A B PUMP -ENQ START- _R L_ 162 163 164 165 © ® ® ® © 166 167 168 169 170 171 172 173 FIRE DETECTORS ENQ ENI APU TEST 28V DC BATTERY BUS - 1 — FIRE EXT—2 ENILQ JEN.Q. JENLQ E±NQ BP FAULT CONT ANN BATT CJD C y CL) C y CEi) CE1 CE1I CE# IE# 174 175 176 177 178 179 180 181 182 xjn_jn_jn_TLj-i_n_n_r 1B3 184 185 Battery Bus - Left Circuit Breaker Panel SECTION 7 Figure.11 Page 16 Aug 14/02 cacnhaadnaeinr Qer OPERATING MANUAL PSP 601A-6 EFFECTIVITY A/C POST SB 601-0262 AND 5135 AND SUBS A/C POST SB 601-0396 AND 5135 AND SUBS A/C 5041 AND 5146 T/0 CONF WARN 2 113 CBP-B 15 14 13 12 10 5 2 TRU E88 2 HYD 8YST FAN -116V AC BUS 2 - 116V AC h% MOTOR 2 30 29 _28 27L 26 25 24 23 22 21 20 19 18 17 16 45 © 44 43 |20j 42 <A href="mailto:§©0@0080080">§©0@0080080</A> 41 40 39 38 37 36 35 34 33 32 31 115VACBU8 2 L/TLT8 1 ICE ADO R R DET DEPLOY WINQ NQ8E 2 SENS 115V AC UTILITY BUS 2 - GALLEY SUPPLY 2 60 59 58 57 I5J 56 55 54 53 52 51 50 49 48 |5J 47 46 wow CH2 10 ST B/AIR PWR SOV R SENS 28VDCBUS2- ICE UTIJL DET BUS 2 CO)NNTT UTIL 28V DC UTILITY BU8 2 FEED JIT TRANS T/T FUEL FEED CONT TRANS PUMP IRU BATT 2 HFCOMM2 CONT • TX/RX- © © © © © © © @ 75 74 73 72 71 70 69 68 _67^/i6_ ; & © 64 63 62 61 PRE88 ' CDU NAV/C ' M/C C/PLT IND 2 2 PWRF -3 •M"A-P A/COLL 2BVDC BU8 2 - 1 CLOCK R RFUEL FLT WINQ 1 FUEL P-;UgMN_P CONT PUMP CONT MON OUTBD INBP NOSE STEER CONT QND 90 f3j 88 87 86 © © © © © © © © © © 85 84 83 82 81 80 79 78 77 76 HTR CONT , R R ADF W8HLD WINDOW 2 AUTO 2 80V R 28VDC BUS 2 RAIR r—CABIN TEMP CONT ir COND ' '~ " CONT AUTO I i\S AC PUMP IND PUMP RENO FAN CONT 1 2 CONT 3A PUMP 80V CONT CP CP CP © © CP CP © CP CP CP CP CP © © 105 104 103 102 101 100 99 98 97 96 95 94 93 92 91 VHF r -AFC8- ADC NAV FQC Y/D ACT SERVO 2 2 2 2 2 CONT 2 28V DC BU8 2 I AURAL HYD SOV VHF I EFIS 2 WARN O/RIDE WXR ATT DME COMM DSPLY EHSI EADI 8 R/H REVRLY 2 2 CONT SQ Q Q Q © ^ 120 119 118 117 116 mrtra $J i£J ^3 <HJ i5J iSJ C5J 112 111 110 109 108 107 106 STATIC R HEATERS PITOT AOA R R , RIGHT— 1 WSHLD - , 26V AC 1 XFMR — 116V AC BUS 2 CABIN FAN CHAN1 BATT OHQR Main AC No. 2 and DC No. 2 Circuit Breaker Panel SECTION 7 Figure 12 page 17 Aug 14/02 canadair chanenqer OPERATING MANUAL PSP 601A-6 EFFECTIVITY E3 A/C POST SB 601-0262 AND 5135 AND SUBS g] A/C POST SB 601-0225, 5001 AND 5027 AND SUBS A/C 5041 AND 5146 A/C POST SB 601-0359 AND 5100 AND SUBS A/C 5001 TO 5134 A/C POST SB 601-0394 FDR A/P A/P EFIS2 V0LTAQE SYNCH SYNC ADC RMT CQNT Y5L SURF M/ASI Ail PP9B QQO© 139 149 \ 148 147 /l46 145 144 143 142 141 140 139 4 J 2«V DC BATTERY BU8 FLT HYD^BATT i-ADG DEPLOY M/C DOOR \REC S-VYO8TT 3* PDWUIRD ' ftflUT PWR1 WARN \PWR GAUGES SENS AUTO 3 D E P L O Y - T A/ICE • LT CONT ^ VALVE ' 8TBY T/T DUMP T/T P MAN RENQ L ENG CM PS VALVE M7C © CD ® ® CD ® @ @ © @ ® © 161 160 159 158 157 156 155 154 153 152 151\J150 cDt(! 2»V DC BATTERY BUS - m ^JGR NOSE HYD A/ICE C/PLT FUEL PRESS CONT DOOR PUMP MAN FLOOD PUMP FOOT WARM CONT C0NT3B 2 ITS INT MLG BAY WOW LTS OVHT FLAP CHAN DIGITS PET IND 2 <A href="mailto:®®®@o">®®®@o</A>®®®® ""* 9 168 167 166 165 164 163 162 CABIN PRESS — I/COMM — 2 1 - 28V DC BATTERY BUS I ENG JET — 8TBY PIPE OVHT HORIZ R L AURAL FUEL R MAIN ENG WARN X-FEED FUEL INSTR 2 CONT QUANT 8Y8T1 ^3| ( ) (m) | 3 | ( ) ^ 3 | ^zj f^zj ^ y &zj ^zj m^ 185 184 183 182 181 180 179 178 177 /176 175 174 ZTLTLrU Battery Bus - Right Circuit Breaker Panel SECTION 7 Figure 13 page 18 Aug 14/02 OPERATING MANUAL PSP 601A-6 Y7. ffl CBP-C K at <A href="mailto:O©OO@OO§O0OOO">O©OO@OO§O0OOO</A> 1 2 9 4 6 9 7 > » W 11 12 tt ^ iiivACcaaamALSM- « TTwy?? a » <A href="mailto:O@O©0©©©©§@OO">O@O©0©©©©§@OO</A> U t! tl 17 II II 20 21 22 2> 24\ 25 2* K >J qg T ag gg -1UVACI 1 1 O©©©©OOO0©OOU 2 7 2 B 9 3 0 3 1 3 2 3 3 3 4 3 6 37 38 30 r ^ J T •? — CTBCK WtWOH ^QvK^l oooo 48 60 51 52 V. EFFECnVTTY H POST SB 601-0M8.A/C 6100 4.8UBS B PO8TS8601-03W AC Essential Bus Circuit Breaker Panel SECTION 7 Figure 14 page 19 Apr 10/95 OPERATING MANUAL PSP 601A-6 V CBP-D i T r w r r r m ^r'Hi A A re OOO®©®®©©©©®© 12 11 10 7N W4M •A* ABF - J 2— ffi ? f i I £ a y ,«Y_ o » 26 24 23 a 21 20 19 1* 17 II 15 14 ir Y * 1 mfocwmmm \[ )' ^sa% • ~ HfHgTT . '«? MC i t gg «- T 1) ©©©©©©©©©©©©© » 3 e « 7 3 6 J 6 $ 4 » l 2 3 1 3 0 2 1 2 1 27 i rm wrpcptw .__ . _ ii \lf *t jr/JHU'wr ^ • ' f ' J V I . 8£ 11 ®©®©©®©©©®©®© 52 5 1 5 0 4 * 4 8 4 7 4 6 4 5 4 4 4 3 4 2 4 1 40 DC Essential Bus Circuit Breaker Panel SECTION 7 Figure 15 page 20 Apr 10/95 OPERATING MANUAL PSP 601A-6 BFFECTIVJTY: A/C 5001 TO 51S4 CBP-E •ATT son L Sttl stun can CD O UJ cc o >- O c pwro ME omor OVT I MMI IS wm OKI L rwwi O Gs] S3 o £23 o o o ca raD @ @ r" O sc aicar 01 1H7 am UDOS 133 CUD o o GaD O o »—CO CD CD CO CD CO o O> CO Aft Electrical Distribution Box Circuit Breaker Panel Figure 16 (Sheet 1) SECTION 7 Page 21 Apr 10/95 OPERATING MANUAL PSP 601A-6 EFFECnVTTY: A/C 5135 & SUBS r 1ATT r= Em AM ' MM cam [•AM [o^ oi 0 I (§1 ® ® ® ® ® ® j® EM MVft EN •OIL GOUT »TF*A* OIL ® OCT AC 6MT •AT CWT JMASO TtT ® i ® ® I Po o p <•>! I <£>[ 23 CBP-E -J Aft Electrical Distribution Box Circuit Breaker Panel Figure 16 (Sheet 2) SECTION 7 Page 22 Apr 10/95

wwjkankan 发表于 2010-9-11 10:15:57

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dul 发表于 2011-2-11 13:28:28

ding

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ericgyf 发表于 2011-6-28 20:19:42

回复 1# 航空的帖子

谁有CRJ200 Flight Deck Book

bocome 发表于 2011-7-31 07:42:23

庞巴迪挑战者电气

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