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SYSTEMS Flashcards

1
Q

APU BLEED AIR VALVE POWERED BY

A

DC BATT BUS

OPENS AT 95% RPM

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2
Q

BLEED TRIP OFF LIGHT

A

OVER PRESSURE

OVER TEMP

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3
Q

ISOLATION VALVE POWERED BY/WHEN OPENS

A

AC

AUTO OPENS WHEN ANY CORNER SWITCHES ARE OFF

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4
Q

PNEUMATIC PRESSURE GAUGE POWERED BY

A

AC PWR

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5
Q

WING BODY OVERHEAT

A 
LE DUCT
LEADING EDEGES
A/C BAYS
KEEL BEAM
APU BLEED AIR DUCT

CANNOT BE RESET, ESTINGUISH WHEN TEMP BACK TO NORMAL

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6
Q

DUAL BLEED

A

MONITORS APU BLEED, ISOLATION VALVE AND BLEED AIR SWITCHES POSITION

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7
Q

RAM AIR DOORS FULL OPEN WHEN

A

FLAPS EXTENDED

MAX COOLING IS REQUIRED

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8
Q

FAN TO HEAT EXCHANGE

A

PNEUMATICALLY OPERATED . DRAWS AIR TO THE HEAT EXCHANGER TO HELP COOLING WHEN
AIR/GROUND SWITCH ON
FLAPS ARE NOT RETRACTED

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9
Q

PACK TRIP OFF LIGHT WHEN

A

DUCT OVERHEAT

HIGH TEMP ON THE PACK

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10
Q

PACKS AUTO OPERATIONS

A

BOTH AUTO……LOW FLOW RATE
1 OFF 1 AUTO….HIGH FLOW IN FLGTH FLAPS UP

ON HIGH +APU BLEED OPEN….WILL CAUSE THE APU TO PROVIDE HIGH FLOW. IF BOTH PACKS HIGH AND APU BLEED ON WILL GIVE MAX COOLING ON GROUND

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11
Q

FLOW CONTROL VALVE

A

CONTROL AIR FROM RECIRC FAN TO FWD CARGO OVERBOARD.
OPEN : GND OR PRESS<2.5PSI
CLOSE: IN FLIGHT OR PRESS >2.5PSI

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12
Q

RELIEF VALVES

A

2 TOTAL. MAIN ONE MAINTAIN MAX CAB PRESSURE TO 8.65 PSI

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13
Q

PRESSURIZAION ON GROUND

A
  1. 25 PSI

- 200FT AFE

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14
Q

MANUAL OPERATION OUTFLOW VALVE TIME

A

AC:4”
DC:8”

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15
Q

PRESSURIZATION FLT/GRD SWITCH

A

GRD: DEPRESSURIZE
FLT:FOLLOW SYSTEM LOGIC

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16
Q

AUTO FAIL LIGHT

A

FAIL OF PRESS.CONTROLLER
LOSS OF ELECTRICAL PWR>15”
CAB ALT>14000FT
ROC >1800 FPM

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17
Q

OFF SCHEDULE DESCENT LIGHT

A

START DESC BEFORE REACHING SET FLT ALT

PLANE WILL PRESSURIZE TO DEP AIRPORT ALT

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18
Q

ALTITUDES/DIFF PRESSURE

A

<28000FT…….7.45PSI

>28000FT…….7.80PSI

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19
Q

PRESSURIZATION SBY MODE

A

WHEN ON INDEX=300FPM

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20
Q

ANTI ICE COWL VALVE OPERATED

A

ELECTRICALLY CONTROLLED
PNEUMAICALLY OPERATED
FAIL CLOSED

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21
Q

ANTI ICE COWL ANTI ICE AMBER LIGHT

A

OVER PRESS

OVER TEMP

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22
Q

ICING CONDITIONS

A

<10C+ VIS MOISTURE OR <1SM

IN FLGHT NO IF CRZ/CLB AND <40C SAT

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23
Q

WING ANTI ICE

A

AC POWER
3 OUTBOARD LE SLATS
IF ONLY 1 BLEED ISOL VALVE OPENS
HOT AIR EXHAUSTED OVERBOARD

CLOSES ON GROUND IF TL ADVANCE ABOVE TAKE OFF WARNING POSITION. PRESSING TEST WILL BYPASS THIS FUNCTION

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24
Q

HYD EMDP PUMPS POWERED BY

A

SYS A …….AC 2

SYS B………AC 1

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25
HYD EDP VALVE POWERED BY
OPERATED BY DC SOLENOID . IF LOSS OF DC PWR SOLENOID WILL LEAVE VALVE OPEN
26
EDP+EMDP OUTPUT PSI
3000PSI
27
FUEL QTY NEEDED TO COOL EDP+EMDP
1700 LBS
28
HYD REFILL BLW
88% ONLY ON GROUND
29
HYD SBY PUMP
AC BUS 1 AC BUS 2 (SBY) 3000PSI BUT ONLY 1/2 VOLUME
30
HYD SBY PUMP AUOMATIC OPS
PROVIDES BACK UP TO RUDDER DURING CRITICAL PHASES SYS A+B LOW PRESS IN FLIGHT.....T/E FLAPS EXENDED ON GROUND.......WHEEL SPEED >60 KIAS STOPS FLAPS RETRACTED WHEEL SPEED <60 KIAS
31
PTU
IN FLIGHT EDP B LOW PRESS FLAPS >0 <15 OPERATES LE DEVICES (AUTOSLATS TOO)
32
LANDING GEAR SAFETY FEATURES
SAFEY LOCK ....NO RETR ON GRD OVERRIDE TRIGGER...BYPASS LEVER LOCK LGTU
33
LANDING GEAR TRANSFER UNIT (LGTU)
NGN#1 N1 BELOW VALUE LG NOT UP LG LEVER UP AIRBORNE
34
LANDING GEAR WARNING HORN
F1-10+TL NEAR IDLE.....OK CANCEL F15+TL NEAR IDLE........NO CANCEL (ADV TL) F>15..................................NO CANCEL
35
ANTISKID
EACH WHEEL HAVE TRANSDUCER THAT SEND INFO TO ANTISKID/AUTBRAKE UNIT IF ALT ANTI SKID ON ....ONLY PAIR OF WHEELS OPS TOUCHDOWN PROTECTION....NO BRAKES APPLICATION BEFORE TD
36
ANTISKID INOP LIGHT WHEN
SWITCHED OFF FAULT IN THE AS/AB SYS LOSS OF POWER INBD/OUTBD AS LIGHT IS ONLY POWERED WITH LG DOWN
37
ALTERNATE BRAKES/ANTISKID DON'T PROVIDE
LOCKED WHEEL PROTECTION TOUCH DOWN PROTECTION AUTO BRAKES AS ONLY WORKS ON PAIR OF WHEELS
38
HYD ACCUMULATOR
PRESSURIZED BY SYSTEM B 3000PSI SHOWS 1000PSI WHEN DEPLETED ABOUT 6 BRAKES APPLICATIONS IF SYS B LOSS PRESS THAN SYS A WILL CLOSE ACCUMULATOR ISOL VALVE SO PRESSURE IS TRAPPED INSIDE IF BOTH SYS A AND B LOSS THE ISOL VALVE WILL OPEN SO TO GO ON NORMAL BRAKES LINE AND PARKING BRAKES
39
AUTOBRAKES
SYSTEM B ACTIVE: TL IDLE WHEEL SPIN UP ``` DE-ACTIVE: MANUAL BRAKING TL MOVE FORWARD SPD BRAKE DOWN SWITCH OFF ```
40
RTO
ACTIVE : TL IDLE >90 KNOTS RTO ON IF FORGOT RTO ON LANDING, WILL BE DEACTIVATED AND AFTER 2' SHOWS A/B DISARMED LIGHT
41
AUTO BRAKE DISARMED AMBER LIGHT
``` AB MALFUNCTION MANUALLY DISARMED REJECTED T/O >60<90 KNOTS FAIL SELF TEST ON LANDING IS ON AND PASS 2' ```
42
SPOILERS MOVES ON YOKE ANGLE
10 DEGREES
43
AILERONS TRIM NEED
SYS A + SYS B
44
YOKE SEPARATION FLT CTRLS OPERATED BY
CAPT .....AILERONS | FO.....SPOILERS
45
LOSS SYS A AND SYS B EFFECT ON FLT CTRL
DIRECT MODE ON AILERONS | NO SPOILERS
46
MACH TRIM ACTUATES AT WHICH SPEED
>M 0.615 | MINOR CHANGES IN CASE OF FAILURE
47
STAB TRIM POWERED BY
MAIN ELECTRICAL TRIM ONLY ELECTRICAL PWR | AUTOPILOT TRIM NEED ELECTR.+HYD
48
STAB OUT OF TRIM AMBER LIGHT
A/P NOT TRIMMING PROPERLY
49
SPEED TRIM WHEN
``` LOW SPEED LOW GROSS WEIGHT AFT CG HIGH THRUST FLAPS NOT UP ```
50
Y/D AMBER LIGHT
LOSS PWR >2" | LOSS HYD B+SBY RUDD ON
51
TRAILING EDGES ASSYMMETRY PROTECTION
SENSORS ON FLAPS GAUGE WHEN NEEDLS SPLIT APART
52
LEADING EDGES DEVICES
4 LE FLAPS | 6 LE SLATS
53
LE FLAPS TRANSIT AMBER LIGHT
LE IN TRANSIT | LE DISAGREE WITH SELECTED POSITION
54
LE DEVICES WITH FLAPS LEVER POSITON
F 1..... SLATS INTERM POSITION, LE FLAPS FULL EXT F>5....SLATS FULL EXT
55
FLAPS LOAD LIMITER
F40 SPEED >158KIAS | AUTOMATICALLY F30 UNTIL 153KIAS
56
AUTOSLATS EXTEND WHEN
IN FLIGHT FLAPS 1-5 HIGH ANGLE OF ATTACK EXTENDED UNTIL AOA BACK TO NORMAL VALUES
57
TAKE OFF WARNING HORN
``` STAB TRIM NOT IN T/O RANGE SPEED BRAKE LVR NOT DOWN TE FLAPS NOT IN T/O POSITION LE FLAPS NOT EXTENDED PARKING BRAKES ON ```
58
CSD TEMP IN/RISE
IN ...OIL ENTERING CSD (INNER SCALE) | RISE...OIL OUT-OIL IN , SHOWS WORKLOAD (OUTER SCALE)
59
ELECTRICAL SBY POWER
POWERED BY XFER1 + DC1 BACK UP MAIN2 +T3 OR BATTERY NO AUOSWITCHING ON THE GROUND . IF XFER1 FAIL ON GROUD NO SBY PWR AVAIL
60
SBY POWER OFF AMBER LIGHT
ONLY ACTIVE ON GROUND . SBY BUS ARE UNPOWERED WE CAN POSITION THE SBY POWER SWITCH TO BATT TO POWER IT
61
BUS XFER SWITCHED OFF
NO AUTOSWITCHING IN CASE OF LOSS OF ONE OF THE BUSSES...SYSTEMS ARE ISOLATED
62
GRND PWER BLUE LIGHT
GP AVAILABLE...DOES NOT MEAN THE POWER IS GOOD. | WHEN SWITCHED ON THE BUS PROTECTION PANEL MAKES SURE PWR IS GOOD
63
ACCESSORY GEAR BOX
``` DRIVEN BY N2 ROTOR CONTROL FUEL PUMPS HYD PUMPS OIL PUMPS AC GENERATORS ```
64
START VALVE
ELECTRICALLY CONTROLLED PNEUMATICALLY OPERATED SPRING LOADED CLOSED
65
IGNITERS POWERED BY
LEFT ....XFER BUS 1 RIGHT...AC SBY BUS POWERED WHEN ENGING START LEVERS GOES TO IDLE
66
PMC
ELECTRICALLY CONTROLLED SYSTEM . PROVIDEDS AUTOMATIC ADJUSTMENT FOR THE FUEL SCHEDULE PROVIDE NGN OVERSPEED PROTECTION
67
ENGINE LOW/HIGH IDLES
LOW ...22% N1 ON GRD HIGH....30% N1 IN FLIGHT HIGH GOES TO LOW AFTER 4" TD LOW NEEDS AC POWER OTHERWISE ALWAYS HIGH
68
THRUST REVERSERS AVAILABLE WHEN
``` BATT BUS AVAILABLE FIRE HANDLE DOWN ON GRD OR <10FT HYD PRESS AVAIL TR LEVER RAISED ```
69
THRUST REVERSERS AUTO RESTOW
COMPARES TL POS. WITH TR SLEEVE POS
70
LOW OIL PRESSURE AMBER LIGHT IN DESCENT
NORMAL FOR IDLE DESCENT AS OIL PRESSURE PUMP IS UNREGULATED
71
ENGINE START SWITHCES POSITIONS
OFF .......IGN OFF CONT....SELECTED IGNITOR CONT PWRD WHEN START LEVERS IDLE FLT....BOTH IGNITERS CONT PWRD WHEN START LEVERS IDLE
72
REVERSER AMBER LIGHT
ISOLATION VALVE OR TR CTRL VALVE DISAGREE WITH SELECTED POSITION AUTO RESTOW ACTIVATED
73
LOW IDLE AMBER LIGHT
NGN OPERATES AT LOW IDLE WHEN IT SHOULD BE HIGH IDLE
74
ENGINE START LEVER CUTOFF DOES
CLOSES MAIN FUEL SOV CLOSES MEC(MAIN NGN CONTR) SOV DE-ENERGIZE IGNITION
75
FIRE SWITCH PULLED DOES
``` FELTBAG FUEL SOV ENGINE HYD DRIVEN PUMP LOW PRESS EDP THRUST REVERSER BLEED AIR SOV ARM FIRE EXTINGUSHER GENERATOR BRKR/CTRL RELAY TRIP OFF ```
76
APU FIRE SWITCH PULLED DOES
``` FABAG FUEL SOV AIR INLET DOOR CLOSED BLEED AIR VALVE CLOSE ARM SQUIBB GENERATOR BUS TRIPPED ```
77
AUTOTHROTTLE OVERSPEED PROTECTION
FLAPS PLACARD VMO/MMO LG PLACARD
78
A/T LIMITS WITHE LIGHT
N1 LIMITS CALCULATED BY AUTOTHROTTLE COMPUTER INSTEAD OF THE FMC FMC FAIL (N1 SIGNAL) NGN#1OR2 N1 BLW 18%
79
FCC"A"SEPARATED FROM FCC "B"
TAKE OFF GO AROUND <400RA ILS LOC+GS CAPTURED
80
F/D AUTOENGAGE WHEN
PRESS TOGA AFTER 80KTS; BLW 2000' AGL;BEFORE 150" AFTER LIFT OFF
81
GO AROUND MODE
AVAILABLE BLW 2000' AGL 2 NGN: 15 DEG NOSE UP TRACK PRESENT HEADING WILL GIVE 2000 FPM CLIMB THAN PITCH TO MAINTAIN SPEED FOR PRESENT FLAPS POSITION 1NGN: 13 DEG NOSE UP TRACK PRESENT HEADING
82
PERFORMANCE LIMITS REVERSION
IF IN V/S SPEED <5KTS TO MCP SPEED AND NO ACCEL REVERT TO LVL CHANGE "A" WILL SHOW ON SPEED WINDOW
83
MINIMUM SPEED PROTECTION
IF SPEED GOES BELOW VA SPEED (TOP BOTTOM YELLOW LINE) REVERT TO LVL CHNGE "B" WILL SHOW ON SPEED WINDOW
84
RADIO DEGRADED MODE
IF CAPT ....ONLY VHF1 IF F/O..........ONLY VHF2 ``` NO NAV INFO NO INTERPHONE NO PA NO ALT ALERT NO GPWS WARNING NO WS WARNINIGS NO SPEAKERS ```

IJW (4 decks)

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