B757 AMM - DC GENERATION - ADJUSTMENT/TEST

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1 1. General DC GENERATION - ADJUSTMENT/TEST A. This procedure has these tasks: (1) An Operational Test of the DC Generation System and Battery Charger Failure Detection Circuit. (2) An Operational Test of the Battery Charger and Current Monitor. (3) An Operational Test of the DC Tie Control Unit and DC Tie Relay. TASK Operational Test - DC Generation System and Battery Charger Failure Detection Circuit A. References Reference Ref P/ Ref P/ Ref P/ B. Location Zones Zone Area 211 ControlCabin, Left 212 ControlCabin, Right Title CONTROL (SUPPLY POWER) - MAINTENANCE PRACTICES SPOILER/SPEEDBRAKE CONTROL SYSTEM - MAINTENANCE PRACTICES ENGINE INDICATION AND CREW ALERTING SYSTEM - MAINTENANCE PRACTICES C. Prepare for the Operational Test SUBTASK (1) Do the deactivation procedure for the spoilers ( Ref. PAGEBLOCK /201 ) or remove all the persons and equipment from the spoiler area. SUBTASK WARNING : MAKE SURE THE SPOILERS ARE DEACTIVATED OR THAT ALL PERSONS AND EQUIPMENT ARE REMOVED FROM THE SPOILER AREA. POWER SOURCES ARE CHANGED AS SWITCHES ARE PUSHED OR CIRCUIT BREAKERS ARE OPENED, WHICH CAN CAUSE THE SPOILERS TO MOVE. ACCIDENTAL MOVEMENT OF THE P.Blk EFFECTIVITY: Page 1 of 13

2 SPOILERS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT. (2) Supply electrical power ( Ref. PAGEBLOCK /201 ). D. Do the Operational Test of the DC Generation System SUBTASK (1) Push the ELEC HYD switch on the EICAS MAINT panel on the right side panel, P61. SUBTASK (2) Do these steps at the standby power control panel on the pilots' overhead panel (P5): (a) Make sure the STBY POWER switch is in the AUTO position. (b) Make sure the ON light in the BAT switch is on. (c) Make sure the DISCH light is off. (d) Make sure the standby bus OFF light is off. SUBTASK (3) Make sure these DC-V values show on the bottom EICAS display: (a) L = 28 ±2 (b) R = 28 ±2 (c) STBY/BAT = 28 ±2 (d) APU/BAT = 28 ±2 SUBTASK (4) Make sure these DC-A values show as positive and not zero on the bottom EICAS display: (a) L (b) R SUBTASK P.Blk EFFECTIVITY: Page 2 of 13

3 (5) Make sure these values show below STBY/BAT on the bottom EICAS display: (a) AC-V = 115 ±5 (b) FREQ = 400 ±5 SUBTASK (6) Make sure these EICAS messages do not show on the top EICAS display: (a) STANDBY BUS OFF (b) BATTERY OFF (c) MAIN BAT DISCH SUBTASK (7) Make sure the EICAS messages do not show on the lower display: (a) STBY INVERTER (b) MAIN BAT CHGR SUBTASK (8) Turn the STBY POWER switch on the P5 panel to the OFF position and do a check as follows: (a) Make sure the EICAS message, STANDBY BUS OFF, shows on the upper display. (b) Make sure the standby bus OFF light on the P5 panel is on. SUBTASK (9) Push the BAT switch on the P5 panel to the OFF position and do a check as follows: (a) Make sure the amber OFF light in the switch is on. (b) Make sure the EICAS message, BATTERY OFF, shows on the upper display. SUBTASK P.Blk EFFECTIVITY: Page 3 of 13

4 (10) Turn the STBY POWER switch on the P5 panel to the AUTO position. SUBTASK (11) Push the BAT switch on the P5 panel to the ON position and do a check as follows: (a) Make sure the amber OFF light in the switch is off. (b) Make sure the EICAS message, BATTERY OFF, does not show on the upper display. SUBTASK (12) Open this circuit breaker: D 10 C00885 INV PWR TRU SUBTASK (13) Make sure the EICAS message, STBY INVERTER, shows on the lower display. SUBTASK (14) Close this circuit breaker: D 10 C00885 INV PWR TRU SUBTASK (15) Make sure the EICAS message, STBY INVERTER, stays shown on the lower display. SUBTASK (16) Do the Maintenance Message Erase procedure ( Ref. PAGEBLOCK /201 ). SUBTASK (17) Make sure the EICAS message, STBY INVERTER, does not show on the lower display. P.Blk EFFECTIVITY: Page 4 of 13

5 E. Do the Operational Test of Battery Charger Failure Detection Circuit SUBTASK (1) Do the Main Battery Charger Failure Detection Circuit as follows: (a) Make sure the lower EICAS display is in the ECS/MSG mode. Push the ECS MSG switch on the P61 panel, if necessary. (b) Open these circuit breakers and install safety tags: APU External Power Panel, P34 AA 16 C04291 MN/APU BAT CHGR DET ENABLE A 4 C04097 BAT CUR MON PWR (c) Approximately 10 seconds after the circuit breakers opened, make sure the EICAS message, MAIN BAT CHGR, shows on the lower display. (d) Remove the safety tags and close these circuit breakers: APU External Power Panel, P34 AA 16 C04291 MN/APU BAT CHGR DET ENABLE A 4 C04097 BAT CUR MON PWR (e) Push the AUTO EVENT READ switch on the P61 panel and make sure the AUTO EVENT page shows on the lower display. (f) Do the Maintenance Message Erase procedure ( PAGEBLOCK /201 ). Ref. (g) Make sure the EICAS message, MAIN BAT CHGR, stays shown on the lower display and cannot be erased. The message can blink when erase is tried, but must remain shown. P.Blk EFFECTIVITY: Page 5 of 13

6 (h) Turn the STBY POWER switch on the P5 panel to the BAT position and permit the switch to stay in this position for at least 5 seconds. (i) Turn the STBY POWER switch on the P5 panel to the AUTO position. (j) Do the Maintenance Message Erase procedure ( PAGEBLOCK /201 ). Ref. (k) Make sure the EICAS message, MAIN BAT CHGR, does not show on the upper display. F. Put the Airplane Back To Its Usual Condition SUBTASK (1) Do the activation procedure for the spoilers if you did the deactivation procedure ( Ref. PAGEBLOCK /201 ). SUBTASK (2) Remove electrical power if it is not necessary ( Ref. PAGEBLOCK /201 ). TASK Operational Test - Battery Charger and Current Monitor A. References Reference Ref P/ Ref P/ Reference SPL-1690 This procedure is a scheduled maintenance task. B. Tools/Equipment Title CONTROL (SUPPLY POWER) - MAINTENANCE PRACTICES SPOILER/SPEEDBRAKE CONTROL SYSTEM - MAINTENANCE PRACTICES When more than one tool part number is listed under the same "Reference" number, the tools shown are alternates to each other within the same airplane series. Tool part numbers that are replaced or non-procurable are preceded by "Opt:", which stands for Optional. Description Actuators/Deactuators Set - ProximitySensor ; , -200ER (Part #: , Supplier: 08748) P.Blk EFFECTIVITY: Page 6 of 13

7 Reference Description (Part #: A , Supplier: 81205) (Part #: KHT , Supplier: 08748) (Opt Part #: A , Supplier: 81205) (Opt Part #: A , Supplier: 81205) (Opt Part #: A , Supplier: 81205) (Opt Part #: KHT , Supplier: 08748) C. Prepare for the Operational Test SUBTASK (1) Do the deactivation procedure for the spoilers ( Ref. PAGEBLOCK /201 ) or remove all the persons and equipment from the spoiler area. SUBTASK WARNING : MAKE SURE THE SPOILERS ARE DEACTIVATED OR THAT ALL PERSONS AND EQUIPMENT ARE REMOVED FROM THE SPOILER AREA. POWER SOURCES ARE CHANGED AS SWITCHES ARE PUSHED OR CIRCUIT BREAKERS ARE OPENED, WHICH CAN CAUSE THE SPOILERS TO MOVE. ACCIDENTAL MOVEMENT OF THE SPOILERS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT. (2) Supply electrical power ( Ref. PAGEBLOCK /201 ). D. Do the operational test SUBTASK (1) Do the Main Battery Charger and Current Monitor test as follows: (a) Make sure the bottom EICAS display is in the ELEC HYD mode. Push the ELEC HYD switch on the EICAS MAINT panel on the right side panel P61 panel, if necessary. (b) Make sure the BAT switch, on the P5 panel, is set to the ON position. (c) Turn the STBY POWER switch, on the P5 panel, to the BAT position. (d) Make sure the DISCH light on the P5 panel comes on. P.Blk EFFECTIVITY: Page 7 of 13

8 (e) Make sure the EICAS message, MAIN BAT DISCH, shows on the top display. (f) Make sure these values show below STBY/BAT on the bottom EICAS display: 1) DC-V = 25 ±2 2) DC-A a number larger than 4 in quantity This value will have a minus sign in front of it to show that it is a discharge current. (g) After one minute, turn the STBY POWER switch, on the P5 panel, to the AUTO position. (h) Make sure the DISCH light on the P5 panel goes off. ; AIRPLANES WITH 40-AMP-HOUR BATTERIES (i) Make sure the DC-A value is 38 ±5 below STBY/BAT on the bottom EICAS display. ; AIRPLANES WITH 48-AMP-HOUR BATTERIES (j) Make sure the DC-A value is 50 ±5 below STBY/BAT on the bottom EICAS display. (k) Make sure the DC-V value below STBY/BAT increases to 32 ±4 volts and then decreases to 28 ±2 volts. It will usually take from one to five minutes for the voltage value to increase and then decrease. But a fully discharged battery can extend this time to 75 minutes. (l) After the DC-V value below STBY/BAT decreases to 28 ±2 volts make sure the DC-A value below STBY/BAT is 0 ±5 amps. FED , 775, 776, 779, 780, 783, 787, 788, 904, 905, 907, 909, 913, 914, , 934, 938, 948, 965, 972, 973, 978, 985, 991, 995, 996, 999; FED 087, 774, 777, 778, 781, 782, , , , 906, 908, 910, 912, , 930, 933, (m) Do these steps to do the test in the air mode: 1) Install the proximitysensor test set, SPL-1690 on the proximity sensors S10060 P.Blk EFFECTIVITY: Page 8 of 13

9 and S10062 (System 1 R & L Main Gear Truck Not Tilt). 2) Turn the STBY POWER switch, on the P5 panel, to the BAT position. 3) Make sure the DISCH light on the P5 panel is off. 4) Make sure the DC-V value below STBY/BAT is 28 ±2 volts. 5) Make sure the DC-A value below STBY/BAT is 0 ±5 amps. 6) Turn the STBY POWER switch, on the P5 panel, to the AUTO position. (n) Push the ECS MSG switch on the EICAS MAINT panel on the P61 panel. (o) Make sure the EICAS message, MAIN BAT CHGR, does not show on the top display. E. Put the Airplane Back To Its Usual Condition SUBTASK (1) Do the activation procedure for the spoilers if you did the deactivation procedure ( Ref. PAGEBLOCK /201 ). SUBTASK (2) Remove electrical power if it is not necessary ( Ref. PAGEBLOCK /201 ). TASK Operational Test - DC Tie Control Unit and DC Tie Relay This procedure is a scheduled maintenance task. A. References Reference Ref P/ Ref P/ Title CONTROL (SUPPLY POWER) - MAINTENANCE PRACTICES SPOILER/SPEEDBRAKE CONTROL SYSTEM - MAINTENANCE PRACTICES P.Blk EFFECTIVITY: Page 9 of 13

10 B. Prepare for the Operational Test SUBTASK (1) Do the deactivation procedure for the spoilers ( Ref. PAGEBLOCK /201 ) or remove all the persons and equipment from the spoiler area. SUBTASK WARNING : MAKE SURE THE SPOILERS ARE DEACTIVATED OR THAT ALL PERSONS AND EQUIPMENT ARE REMOVED FROM THE SPOILER AREA. POWER SOURCES ARE CHANGED AS SWITCHES ARE PUSHED OR CIRCUIT BREAKERS ARE OPENED, WHICH CAN CAUSE MOVEMENT OF THE SPOILERS. ACCIDENTAL MOVEMENT OF THE SPOILERS CAN INJURE PERSONS OR DAMAGE EQUIPMENT. (2) Supply electrical power ( Ref. PAGEBLOCK /201 ). SUBTASK (3) Do the DC Tie Control Unit and DC Tie Relay Operational Test as follows: (a) Make sure the two BUS TIE switches on the P5 panel are set to the AUTO (latched-in) position. The ISLN light in each switch should be off. (b) Make sure the bottom EICAS display is in the ECS MSG mode. Push the ECS MSG switch on the EICAS MAINT panel on the right side panel P61, if necessary. (c) Make sure the EICAS message, T-R UNIT, does not show on the bottom display. (d) Push the ELEC HYD switch on the EICAS MAINT panel. (e) Make sure these values are below L and R on the bottom EICAS display: 1) DC-V = 28 ±5 2) DC-A = larger than 5 (f) Open these circuit breakers and install safety tags: P.Blk EFFECTIVITY: Page 10 of 13

11 FED 087, , , , 930, , , , 966, 967, 971, , 985, 988, C 23 C00318 R TRU Right Generator Power Panel, P32 FED , , 965, , 972, 986, 987, 989 EE 2 C00318 R TRU (g) Make sure these values are below R on the bottom EICAS display for 11 ±5 seconds: 1) DC-V = 0 ±1 2) DC-A = 0 (h) After 11 ±5 seconds make sure these values are below R on the bottom EICAS display: 1) DC-V = 28 ±5 2) DC-A = 0 (i) Push the ECS MSG switch on the P61 panel. (j) Make sure the EICAS message, T-R UNIT, shows on the bottom display. (k) Remove the safety tags and close these circuit breakers: FED 087, , , , 930, , , , 966, 967, 971, , 985, 988, C 23 C00318 R TRU Right Generator Power Panel, P32 FED , , 965, , 972, 986, 987, 989 EE 2 C00318 R TRU (l) Make sure the EICAS message, T-R UNIT, still shows on the bottom display. (m) Push the left BUS TIE switch on the P5 panel to the ISLN position (out position). P.Blk EFFECTIVITY: Page 11 of 13

12 (n) Make sure the amber ISLN light in the switch comes on. (o) After 3 seconds (minimum), push the left BUS TIE switch on the P5 panel to the AUTO position. (p) Make sure the ISLN light in the switch goes off. (q) Make sure the EICAS message, T-R UNIT, does not show on the bottom display. (r) Push the ELEC HYD switch on the EICAS MAINT panel. (s) Open these circuit breakers: Left Generator Power Panel, P31 FED , , 965, , 972, 986, 987, 989 EE 2 C00312 L TRU FED 087, , , , 930, , , , 966, 967, 971, , 985, 988, C 17 C00312 L TRU (t) Make sure these values are below L on the bottom EICAS display: 1) DC-V = 0 ±1 2) DC-A = 0 (u) After 11 ±5 seconds, make sure these values are below L on the bottom EICAS display: 1) DC-V = 28 ±5 2) DC-A = 0 (v) Push the ECS MSG switch on the EICAS MAINT panel. (w) Make sure the EICAS message, T-R UNIT, shows on the bottom display. (x) Close these circuit breakers: Left Generator Power Panel, P31 FED , , 965, , 972, 986, 987, 989 EE 2 C00312 L TRU P.Blk EFFECTIVITY: Page 12 of 13

13 FED 087, , , , 930, , , , 966, 967, 971, , 985, 988, C 17 C00312 L TRU (y) Make sure the EICAS message, T-R UNIT, still shows on the bottom display. (z) Push the left BUS TIE switch on the P5 panel to the ISLN position (out position). (aa) Make sure the amber ISLN light in the switch comes on. (ab) After 3 seconds (minimum), push the left BUS TIE switch on the P5 panel to the AUTO position. (ac) Make sure the ISLN light in the switch goes out. (ad) Make sure the EICAS message, T-R UNIT, does not show on the bottom display. C. Put the Airplane Back To Its Usual Condition SUBTASK (1) Do the activation procedure for the spoilers if you did the deactivation procedure ( Ref. PAGEBLOCK /201 ). SUBTASK (2) Remove electrical power if it is not necessary ( Ref. PAGEBLOCK /201 ). P.Blk EFFECTIVITY: Page 13 of 13

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