1-HOW MANY SHAFT ARE THERE ENGINE ROLL ROYS TRENT 1000? 3-(N1-N2-N3) 3-(N1-N2-EGT) 3 (N1-N2-TPR).
2-THE MAIN PARAMETER ENGINE TPR-N1-EGT EPR-N1-EGT N1-N2-N3.
3-WHATS SENSOR IS IN THE INLET AREA FWD OF THE FAN? P20/T20 T20/T20 T20/T50.
4-THE ROTATION CW IS FOR N1 N2 N3.
5-ENGINE THE BY PASS RATIO WILL BE 10/1 10/3 10/2.
6-THE SECONDARY AIR WIL BE PRODUCCER 80% TRUSH 90% TRUSH 100% TRUSH.
7-HOW MANY FAN BLADE ARE THERE? 20 MADE TITANIO HOLLOW 21 MADE TITANIO HOLLOW 22 MADE TITANIO HOLLOW.
8-HOW MANY STAGE HAVE IPC? 6 8 ONLY 1.
9-HOW MANY STAGE HAVE HPC? 6 8 1.
10 HOW MANY STAGE HAVE HPT AND IPT? 1 STAGE 8 STAGE 6 STAGE.
11-WHATS ABOUT THESE ARE ONLY THE SECONDARY PARAMETER OF ENGINE? EPR-N1 TPR-N1- EGT N2-N3 ,FF, OIL PRESS,OIL TEMP,OIL QTY VIB.
1-THE TRUSH IS SUPPORT BY FWD MOUNT REAR MOUNT PYLON ONLY THIS ENGINE.
THE FWD MOUNT SUPPORT LOADS LATERAL VERTICAL BOTH ARE CORRECT.
14-WHAT BAND SHOULD BE IN SIGHT WHEN THE ROD OF COWL IS INSURED GREEN YELOW RED.
15 THE SYSTEM PDOS USE ELECTRICAL MOTOR AND PRESSURIZED OIL MECHANIC MOTOR AND PRESSURIZED OIL ONLY MANUAL PUMP.
16 WHO RECEIVE INFORMATION OF ENGINE VIBRATION? EMU EVMU EEC.
17- HOW MANY BEARING HAVE ENGINE TREND 1000? 08 88 80.
PDOS SYSTEM IS MONITORED BY
THIS IS NOT MONITORED EMU EEC.
WHATS TYPE OF BEARING ARE THERE ? ROLLER-BALL ROLLER ONLY ROLLER-CONICAL.
HOW MANY CHANNEL ARE THERE EEC? 4- (2 PROTECCION 2 INDICACION) 4 (2 PROTECCION 2 CONTROL) 8-(4 CONTROL 4 INDICACION).
WHATS CHANNELS WORKS ALWAYS? EEC BOTH 2 PROTECTION 2 CONTROL.
ROTATION LPT IS CCW CW BOTH ARE CORRECT LOOK FROM BACK.
ROTATION IPC IS CCW CW BOTH ARE CORRECT LOOK FROM BACK.
24- HPC SYSTEM ROTATION IS CCW CW BOTH ARE CORRECT LOOK FROM BACK.
HOW MANY MODULES ASSEMBLED FORM THE ENGINE 8 7 9.
26-THE PAINTING OF THE SPINNER BEGINS AND ENDS WITH THE FAN BLADE ONE TRUE FALSE IT CAN BE ANY BLADE.
27-EEC IS POWERED OVER 6% BY PMA PMG HOT BATTERY BUS.
27-HOW MANY SPEED PROBE ARE THERE IN LPT? 4 2 1.
28-INFORMATION OF PRESSION AND TEMPERATURE IS SENT... EEC BOTH CHANNEL EEC ONLY CHANNEL A EEC ONLY CHHANEL B.
29-INFORMATION OF VIBRATION IS SEND EEC EMU AMU.
30-EMU IS POWERED BY EEC PMG ALWAYS OF AIRPLANE.
28-FUEL FLOW TRANSMITER SEND DATA : EEC CHANNEL B BOTH CHANNEL EEC CHANNEL A.
30 HOW MANY FUEL SPRAY NOZZLE HAVE THE ENGINE? 18 (16 TUNGTEN-2 STEEL) 20 (16 TUNGTEN 4 STEEL) 16( CROMMEL /ALUMMEL).
HOW MANY SWITCH FOR ENGINE HAVE THE PDOS SYSTEM? 4 SWITCH 2 SWITCH 1 SWITCH.
WHATS DO YOU NEED TO WORK AND OPERATE PDOS SYSTEM? ELECTRICAL POWER HYDRAULIC SYSTEM BOTH ARE CORRECT.
HOW DO YOU KNOW WHEN THE POWER PACK (PDOS SYSTEM) LACK OIL? THE FAN COWL DOORS NOT FULLY COME UP. THE FAN COWL DOORS NOT ASSURE CLOSE POSITION THE FAN COWL DOORS SENSOR DETECT MORE 40 KNOOT.
THE THREE SHAFT ROLL ROYS TREND 1000 ARE ASSOCIATED AS: N1 LOW- N2 INTERMEDIATE- N3 HIGHT N3 LOW- N1 INTERMEDIATE- N2 HIGHT N2 LOW- N3 INTERMEDIATE- N1 HIGHT.
ON ENGINE R/R TREND 1000 HAVE: PROTECTION BY BREAKER OF SHAFT ONLY N1 AND N2 PROTECTION BY BREAKER OF SHAFT ONLY N2 PROTECTION BY BREAKER OF SHAFT ONLY N1 .
THE SENSOR P20 FAIL WHATS HAPPEN WITH ENGINE? THE ENGINE REVERT TO N1 BECAUSE TPR IT GOST LOST. THE ENGINE REVERT TO N1 BECAUSE EPR IT GOST LOST. THE ENGINE REVERT TO N1 BECAUSE EGT IT GOST LOST.
40-HOW MANY SPEED SENSOR ARE THERE FOR N3? 2 4 1.
41-SPEED SENSORs FOR HPC ARE LRU? YES IS LRU NO IS NOT LRU THERE ARE NO SENSORS HPC.
SPEED SENSORs FOR LPC ARE LRU? YES ARE LRU THEY ARE NOT LRU THERE ARE NO SENSORS.
HOW MANY PROVETS EGT ARE THERE? 12 6 4.
44-THE ELECTRICAL CONNECTORS OF EEC HAVE CODE COLOURS CHANNEL A AND B . CHANNEL A YELLOW COLOURS AND CHANNEL B GREEN COLOURS CHANNEL A GREEN COLOURS AND CHANNEL B YELLOW COLOURS CHANNEL A RED COLOURS AND CHANNEL B GREEN COLOURS.
THE CHANNELS (A AND B) OF CONTROL EEC: BOTH CHANNEL OF CONTROL WILL ALTERNATE EACH ENGINE START. BOTH CHANNEL OF CONTROL WILL ALTERNATE EACH ENGINE SHUT DOWN. BOTH CHANNEL OF CONTROL WILL BE ALWAYS ACTIVATE.
THE CHANNELS (A AND B) OF PROTECTION EEC: BOTH CHANNELs OF PROTECCTION WILL BE ALWAYS ACTIVATE. ONE CHANNEL OF CONTROL WILL BE ALWAYS ACTIVATE AND OTHER STAND-BY. ONE CHANNEL OF CONTROL WILL BE ALWAYS ACTIVATE AND OTHER NO.
47- ENGINE TREND 1000 WHERE THE REMNANT FUEL OF THE LINES IS TAKEN DURING ENGINE SHUT DOWN ON GROUND? TO CAMERA COMBUSTION DIRECTLY FOR THE NEXT ENGINE START . TO DRAIN MAST DIRECTLY TO DRAIN COLECTOR MAST THEN FOR THE NEXT ENGINE START .
48-DRAIN COLECTOR MAST IT CAN RECEVER FUEL DURING ONE ENGINE SHUT DOWN OR UNTIL THREE ATTEMPTED ENGINE START. THREE ENGINE SHUT DOWN OR UNTIL THREE ATTEMPTED ENGINE START. FIVE ENGINE SHUT DOWN OR UNTIL THREE ATTEMPTED ENGINE START.
49-WICH IS THE AIR WITH MAJOR COMPRESSION ON ENGINE TREND 1000? AT THE EXIT HPC (STAGE 6) AT THE INLET HPC (STAGE 6) AT THE EXIT HPT (STAGE 6).
THE GEAR BOX WILL BE MOVED : N2 N1 N3.
51-FOR TRIM BALANCE PORPUSE... DO YOU HAVE INTERROGATE? EEC EMU AMU.
52-THE WORK OF ENGINE MONITORING UNIT (EMU) IS: MONITORIG CRITICAL PARAMETER OF ENGINE AS N1 MONITORING NO CRITICAL PARAMETER OF ENGINE AS CALCULATE VIBRATIONS MONITORING N3.
53- WHEN YOU MOVE THE FUEL CONTROL SWITCH TO CUT OFF POSITION; WHATS VALVE IN THE ENGINE FUEL SYSTEM CLOSE? THE PRSOV IN THE HMU AND FUEL SPARE VALVE. THE FUEL SHUT DOWN MODULE INTERMEDIATE N3.
54-CAN YOU MANUALLY TURN SHAFT N2 AND N3 SAME TIME? YES ,FROM THE SAME PLACE . YOU CAN BUT FROM DIFFERENT POINTS. BOTH ARE CORRECT.
55-WHAS IS THE REGARDING FUEL OIL HEAT EXCHANGUER (FOHE)? OF FUEL SYSTEM ABOUT ENGINE RR TREND 1000? RISE FUEL TEMPERATURE AND LOWER OIL TEMPERATURE LOWER FUEL TEMPERATURE AND LOWER AIR TEMPERATURE RISE OIL TEMPERATURE AND LOWER FUEL TEMPERATURE.
56-WHEN THE ENGINE IS LOWER POWER AND OR CRUISE ,WHATS PUMP WILL GO FUEL DIRECTLY TO BE BURN (CC). FROM PRIMARY FUEL PUMP ONLY FROM PRIMARY AND SECONDARY FUEL PUMP SECONDARY PUMP ALWAYS.
57-WHEN THE ENGINE IS HIGHT POWER (AS TAKE-OFF ),WHATS PUMP WILL GO FUEL DIRECTLY TO BE BURN (CC) PRIMARY AND SECONDARY FUEL PUMP SECONDARY FUEL PUMP ALWAYS PRIMARY FUEL PUMP ONLY.
58-FUEL METERING SERVO VALVE IS CONTROLED BY EEC EMU HMU.
59-WHO CONTROL THE FMV? EEC FUEL METEERING SERVO VALVE. EMU.
60-WHO DOSIFIES THE AMOUNT OF FUEL TO WILL GO CHAMBER COMBUSTION? HMU FUEL METERING VALVE (INSIDE HMU) THRUST CONTROL MODULE.
61-ENGINE RR TREND 1000 CAN YOU DO MANUAL START? IT IS NOT POSSIBLE YES, YOU CAN ONLY IF YOU HAVE START VALVE OPERATIVE.
62-WHEN THE ENGINE HAVE FUEL FROM PRIMARY PUMP GIVING TO SYSTEM? WHEN NON-RETOURN VALVE IS CLOSED (SETTING IDLE OR CRUISE) WHEN NON-RETOURN VALVE IS STAND-BY (SETTING IDLE OR CRUISE) WHEN NON-RETOURN VALVE IS OPEN (SETTING IDLE OR CRUISE).
63-THE PRIMARY MANIFOLD IS AROUND THE CORE ENGINE? TRUE. FALSE ARE 18 KNOW PIG-TAIL.
64-WHATS POSITION ARE THERE FUEL NOZZLE DIFFERENT? POSITION 8 AND 12 ARE NEAR THE IGNITER PLUG AND GIVE BETTER PERFORMANCE DURING ENG START OR RE-LIGHT. POSITION 4 AND 8 ARE NEAR THE IGNITER PLUG AND GIVE BETTER PERFORMANCE DURING ENG START OR RE-LIGHT. POSITION 1 AND 4 ARE NEAR THE IGNITER PLUG AND GIVE BETTER PERFORMANCE DURING ENG START OR RE-LIGHT.
65-CAUTION :EACH TIME YOU CHANGE MANIFUL SECUNDARY FUEL NOZZLE (PIG-TAIL)? YOU WILL HAVE TO OCCUPY AN IMMOBILIZING TOOL YOU WILL HAVE TO OCCUPY AN TOOL PNEUMATIC. SWITCH OVERHEAD P5 PANEL ON POSITION .
66-HOW CAN YOU IDENTIFICATE FUEL SPRAY NOZZLE TUNGSTEN? TUNGSTEN WEIGHTS ARE IDENTIFICATED BY X ON THE END ON THE WEIGHT TUNGSTEN WEIGHTS ARE IDENTIFICATED BY T ON THE END ON THE WEIGHT TUNGSTEN WEIGHTS ARE IDENTIFICATED BY (-) ON THE END ON THE WEIGHT.
66-HOW CAN YOU IDENTIFICATE FUEL SPRAY NOZZLE STEEL? STEEL WEIGHTS ARE IDENTIFICATED BY (-) ON THE END ON THE WEIGHT STEEL WEIGHTS ARE IDENTIFICATED BY (S) ON THE END ON THE WEIGHT STEEL WEIGHTS ARE IDENTIFICATED BY (Y) ON THE END ON THE WEIGHT.
67-THE CHANNEL OF PROTECCTION EEC IS FOR MONITORING: BREAKER SHAFT N1-N2,OVERSPEED,TCMA BREAKER SHAFT N3,OVERSPEED,TCMA BREAKER SHAFT N1-N2,UNDER SPEED,TCMA.
68-TRHUST CONTROL MALFUNCTION ACOMODATION (TCMA) IS ONLY GROUND TRHUST ASYMMETRIC CRUISE TAKE-OFF.
69-WERE IS LOCATED TCMF? AUTOMATIC SOFTWARE GPM AUTOMATIC SOFTWARE EEC CHANNELs AUTO FLIGHT FUNCTION FCE.
WITH THE ENGINE RUNNING AND N2 OVER 6% EEC IS POWERED BY: PMG PMA AIRPLANE 115 VAC.
72- WITH THE ENGINE RUNNING AND PMA FAIL EEC WILL BE POWERED BY: 115 VAC AIRPLANE 28 VAC AIRPLANE RPDU.
73-WHICH ARE THE THREE WAY GIVE POWER TO GO TO EEC? MISCELANEO PAGE MODE TEST, FUEL CONTROL SWITCH RUN POSITION, ROTARY SELECTOR START. MISCELANEO PAGE MODE TEST, FUEL CONTROL SWITCH RUN POSITION, EXTERNAL POWER ON MISCELANEO PAGE MODE TEST, FUEL CONTROL SWITCH OFF POSITION, ROTARY SELECTOR START.
74-WHERE IS LOCATED THE PMA? GEAR BOX EEC SHAFT N3.
75-WHATS PARAMETER CAN YOU SEE ON EICAS WITH ONLY EXTERNAL POWER AVAILABLE WITHOUT EEC? N2 TPR EPR.
76-HOW MANY MODES HAVE EEC TO WORK? 2-(ALTERNATE AND NORMAL MODE) 2-(STAND-BY AND NORMAL MODE) 2-(PRIMARY AND NORMAL MODE).
77-THE EEC ALTERNATE MODE IS DIVIDED IN. HARD MODE -SOFT MODE HARD MODE-BACK UP MODE ALTERNATE -EPR MODE.
78 TERMOCUPLA GAS TEMPERATURE (EGT) THERE ARE: 12 18 8.
79-EGT THERMOCUPLES ARE INTERCHANGEABLE? NO, THEY HAVE DIFFERENT SIZED TERMINAL SO THEY CANNNOT BE CONNECTED ICORRECTLY. YES ARE INTERCHANGEABLE. ONLY CROMMEL YOU CAN INTERCHAGEABLE.
80-THE EGT THERMOCUPLE MADE IN CROMMEL/ALUMMEL CROMMEL CROMMEL/VANNADIUM.
81-WHERE IS LOCATED PROBETS TCAF AND TCAR? IPC IPT LPT.
82-TCAF AND TCAR THERMOCUPLE REGARDING IS: MONITORING INDICATION POSSIBLE OIL FIRE IN THE SHAFT SPACE. MONITORING INDICATION POSSIBLE BREAKE SHAFT BOTH ARE CORRECT.
EMU IS POWERED BY: ALWAYS TROUGH AIRPLANE RPDU PMA.
84-HOW MANY VIVRATION SENSORSARE ARE THERE? 3 1 2.
85-WICH IS AIR SERVO? AIR HP 6 AIR IP 8 AIR IP 5.
86-ESS ANTI ICE VALVE PREVENT IT FROM FORMING ICE TO INTAKE IPC TO INTAKE HPC TO INTAKE LPC.
87- WHICH IS FAIL-SAFE POSITION ESS ANTI ICE VALVE WHEN THE ENGINE SHUT DOWN. OPEN CLOSE MIDDLE.
88-WHICH IS FAIL-SAFE POSITION ESS ANTI ICE VALVE WHEN THE ENGINE IS RUNNING? OPEN CLOSE HALF OPEN.
89-HOW MANY BLEED VALVE ARE THERE ENGINE? 5 (3 IPC -2 HPC) 5 (3 LPC -2 HPC) 2 (3 IPC -2 HPC).
90-FAIL-SAFE SECONDARY AIR SYSTEM VALVE (SAS VALVE ) IS: CLOSED OPEN HALF.
91-FAIL-SAFE AIR CONTROL VALVE IS OPEN CLOSED HALF.
92-LP TCC VALVE AND HP/IP TCC VLV FAIL-SAFE WILL BE? PARTIAL OPEN CLOSE.
93-REGARDING LP TCC VALVE AND HP/IPTCC VALVS ARE USED FOR EFFICIENCY PERFORMANCE THRUST CONTROL.
94- ENGINE -THE HP/IP TCC VLV AND LP TCC VALVE( PACKAGE B) WILL BE MOVED BY: FUEL SERVO VALVE AIR SERVO VALVE BOTH ARE CORRECT.
95-ENGINE-HP/IP TCC VALV ARE MOVED BY FUEL SERVO VALVE ONLY PACKAGE C ONLY PACKAGE B ONLY PACKAGE A/B.
96-LP TCC VALVE PACKAGE C WILL BE MOVED BY: FUEL SERVO VALVE OIL SERVO VALVE AIR SERVO VALVE.
97-ESS ANTI ICE VALVE : PREVENT ENGINE ANTI-ICE INLET COWL PREVENT ICE INTAKE INTERMEDIATE PRESSURE COMPRESSOR PREVENT ICE INTAKE INTERMEDIATE PRESSURE TURBINE.
98-WHATS AIR IS OCCUPPIED PREVENT ICE INTAKE IPC? AND WHICH AIR WILL MOVE THE ESS ANTI-ICE VALVE? IP8 AIR IS OCCUPIED ANTI-ICE TO INTAKE IPC AND HP6 AIR IS OCCUPIED TO MOVE THE ESS ANTI-ICE VALVE IP8 AIR IS OCCUPIED ANTI-ICE TO INTAKE IPC AND IP8 AIR IS OCCUPIED TO MOVE THE ESS ANTI-ICE VALVE IP6 AIR IS OCCUPIED ANTI-ICE TO INTAKE IPC AND HP8 AIR IS OCCUPIED TO MOVE THE ESS ANTI-ICE VALVE.
99-REGARDING SECONDARY AIR SYSTEM VALVE (SAS VLV) THIS IS USED FOR: SEAL AND PRESSURIZE THE MAIN BEARING CHAMBERS (SUMP) TAKEN AIR FROM HP 3( LOW POWER) OR IP8 (HIGHT POWER) SEAL AND PRESSURIZE THE MAIN BEARING CHAMBERS (SUMP) TAKEN AIR FROM HP 6 ( LOW POWER) OR IP8 (HIGHT POWER) SEAL AND PRESSURIZE THE MAIN BEARING CHAMBERS (SUMP) TAKEN AIR FROM IP 5 ( LOW POWER) OR IP8 (HIGHT POWER).
100-WHERE IS TAKEN THE AIR WHEN THE SAS VALVE IS CLOSE? IP8 HP3 HP6.
101-WHATS IS THE PURPOSE OF THE THREE AIR CONTROL VALVE? COOLING OF THE LOWER PASSAGES BETWEEN HPT AND IPT THIS PREVENT OVERHEAT DAMAGE TURBINE SECTION COOLING OF THE LOWER PASSAGES BETWEEN HPT AND LPT THIS PREVENT OVERHEAT DAMAGE TURBINE SECTION COOLING OF THE LOWER PASSAGES BETWEEN LPT AND IPT.THIS PREVENT OVERHEAT DAMAGE TURBINE SECTION.
102-WHAT AIR IS OCCUPED TCC VALVE? PRIMARY AIR SECONDARY AIR (BYPASS) HP6.
103-HOW MANY POSITIONS HAVE THE TCC VALVE? 2 (OPEN-PARTIAL) 2 (CLOSE-OPEN) 3 (OPEN PARTIAL CLOSE).
104-WHATS VALVES ARE MODIFICATED PACKAGE C? TCC VALVE HP/IPC BECAUSE WILL BE MODULATED WITH SERVO FUEL TCC VALVE LP/IPC BECAUSE WILL BE MODULATED WITH SERVO FUEL TCC VALVE TC/IPC BECAUSE WILL BE MODULATED WITH SERVO FUEL.
105 THE TWO SOLENOID BANK ARE POWERED BY: EEC VFSG DIFFERENTS RPDUs.
106-IGNITION -- THE EEC ALWAYS USE BOTH CHANNEL IGNITION ON FLIGHT ON GROUND BOTH ARE CORRECT.
107-HOW MANY IGNTION SYSTEM ARE THERE FOR EACH ENGINE. 2-(SYSTEM ONE AND SYSTEM TWO) 3 (SYSTEM ONE,TWO AND SYSTEM THREE) 4 (SYSTEM ONE , TWO,THREE AND FOUR).
108-THE IGNITION SYSTEM IS POWERED BY. 28 VDC CAPTAIN BUS AND F/O BUS 115 VAC VSFG SOLENOID BANK.
109- THE EEC USES TWO IGNITER FOR IN-FLIGHT START OR AUTO-RELIGHT ON GROUND ALWAYS NEVER .
110-THE EEC REMOVE POWER TO IGNITION SYSTEM : APPROXIMATELY 46% N2 APPROXIMATELY 46% N1 APPROXIMATELY 46% TPR.
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