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737 > BOUTONS ! > Flashcards

BOUTONS ! Flashcards

1
Q

ELT

A

ELT

ELT is transmitting on 121.5, 243 and 406

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2
Q

LE DEVICES

A 
LE DEVICES
AMBER: le in transit
EXT: extended
FULL ext: fully ext
OFF: retracted
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3
Q

PSEU

A 
PSEU
PSEU fault (proximity switch electronic unit)
or if &OVERWING, overwing flight lock failed to disengage
inhibited inflight
monitors
t/o config warning
ldg confwarning
ldg gear warning
air/ground sensors
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4
Q

GPS

A

GPS
Both GPS have failed
During recall: 1 has failed / resets with MC

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5
Q

ALIGN (steady)

A

ALIGN (steady)
IRS aligning, or
initiating ATT, or
shutting down

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6
Q

ALIGN (flashing)

A

ALIGN (flashing)
Cannot align
position missing or unreasonnable

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7
Q

ALIGN (off)

A

ALIGN (off)

IRS available in NAV or ATT mode

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8
Q

irs ON DC

A

irs ON DC
AC power not normal, IRS on switched Hot battery bus (ground horn sounds)
illuminates normally during self test

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9
Q

irs FAULT

A

irs FAULT

there is a fault

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10
Q

irs DC FAIL

A 
irs DC FAIL
DC is not normal
if other light extinguished: operating normally on AC power
Engine REVERSER
auto restow is activated or
control valve not in commended position or
sleeve not in commanded position
failure in synchronization of shaft lock
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11
Q

ENGINE CONTROL

A

ENGINE CONTROL
non dispatchable engine control issue.
inhibited >80kt -> 30sec after touchdown

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12
Q

ON (eec)

A

ON (eec)
Normal
rating controlled by EEC from sensed conditions
off (manually selected to alternate mode)

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13
Q

ALTN

A

ALTN
auto switch to soft alternate (ON still displayed) or
man swicth to hard alternate
EEC provides rated thrust or higher.

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14
Q

PASS OXY ON

A

PASS OXY ON

Masks have dropped

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15
Q

GEAR LIGHTS

A

GEAR LIGHTS
DOWN and LOCKED
as long as one light from this panel or the other is green, down and locked.

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16
Q

OFF (flight recorder)

A

OFF (flight recorder)

recorder is not operating, or test is invalid, or power failure, or loss of data or fail.

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17
Q

FCTL LOW PRESSURE Flight control

A

FCTL LOW PRESSURE Flight control
Low pressure to (Hyd X) aileron, elevator, rudder
deactivated when standby rudder activated and rudder shutoff valve opens.

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18
Q

YAW DAMPER

A

YAW DAMPER

yaw damper not engaged

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19
Q

LOW QUANTITY standby hyd

A

LOW QUANTITY standby hyd

less than 50% in standby hydraulic RSRVR

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20
Q

LOW PRESSURE standby Hyd

A

LOW PRESSURE standby Hyd

standby pump is activated (auto or man) and output pressure is low

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21
Q

STBY RUDDER ON

A 
STBY RUDDER ON
standby system is pressurizing rudder PCU
FUEL ? ENG VALVE CLOSED ?
bright: in transit or disagree
dim: closed
off: open
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22
Q

? SPAR VALVE CLOSED ?

A

? SPAR VALVE CLOSED ?

bright: in transit or disagree
dim: closed
off: open

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23
Q

? FILTER BYPASS ?

A

? FILTER BYPASS ?

impending bypass due contamination

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24
Q

? VALVE OPEN ?

A

? VALVE OPEN ?

bright: in transit or disagree
dim: open
off: closed

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25
Q

? LOW PRESSURE (center pumps) ?

A

? LOW PRESSURE (center pumps) ?
pump on and low press
> if center pump on and low press for 10 sec, “master caution & “Fuel sys”

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26
Q

? LOW PRESSURE (main pumps)?

A

? LOW PRESSURE (main pumps)?
pump off or low press
> one low press in a tank & RECALL > “master caution & “Fuel sys”
> two low press in a tank > “master caution & “Fuel sys”

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27
Q

? VIDEO ?

A

? VIDEO ?
une video passe en cabine
elec BAT DISCHARGE
BAT on, and excessive battery discharge

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28
Q

TR UNIT (on the ground)

A 
TR UNIT (on the ground)
any TR has failed
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29
Q

TR UNIT (in flight)

A 
TR UNIT (in flight)
TR1 or TR2&3 have failed
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30
Q

ELEC

A

ELEC
DC or standby system fault
only illuminated on ground

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31
Q

STANDBY PWR OFF

A 
STANDBY PWR OFF
au moins un des bus est non alimenté:
AC standby
DC standby
batt buss
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32
Q

DRIVE

A 
DRIVE
IDG OIL Low pressure, meaning:
Engine is off
IDG is failed
IDG disconnected (due OIL TEMP or disconnect swith)
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33
Q

GRD POWER AVAIL

A

GRD POWER AVAIL

connected & quality check ok

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34
Q

TRANSFER BUSS OFF

A

TRANSFER BUSS OFF

Side transfer bus is unpowered

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35
Q

SOURCE OFF

A

SOURCE OFF

no source has been selected, or source has been disconnected

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36
Q

GEN OFF BUS

A

GEN OFF BUS

IDG is not powering the buss (mais n’est pas forcément dispo)

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37
Q

APU GEN OFF BUS

A

APU GEN OFF BUS
APU is not powering the bus and is available
APU MAINT
APU may be operated but needs maintenance
disarmed when apu switch off.

38
Q

apu LOW OIL PRESSURE (during start)

A

apu LOW OIL PRESSURE (during start)

until APU press is normal

39
Q

LOW OIL PRESSURE (after start cycle)

A

LOW OIL PRESSURE (after start cycle)
low oil press is causing auto shutdown
disarmed when switch placed in off position. extinguishes 5 min after. (to note defect)

40
Q

FAULT

A

FAULT
Fault is causing auto shutdown
disarmed when switch placed in off position. extinguishes 5 min after. (to note defect)

41
Q

OVERSPEED

A 
OVERSPEED
Overspeed is causing auto shutdown, or
During shut down, and overspeed test has failed.
Disarmed when switch placed in off position. extinguishes 5 min after. (to note defect)
Equip cooling
OFF (2)
No airflow is detected from cooling fan
Emer Exit Light NOT ARMED
Switch not in armed position
Window heat OVERHEAT (4)
Overheat detected
ou power interrompu
42
Q

ON (4) Window heat

A 
ON (4) Window heat
Heating in progress
off
si tempé ok,
overheat detecté,
fault,
switch off
43
Q

Probe Heat “PROBE NAME” (8) eg CAPT PITOT

A

Probe Heat “PROBE NAME” (8) eg CAPT PITOT
not heated
note:: on standby power, does not indicate status
Hydraulic LOW PRESSURE (engine pump) (2)
output pressure is low
!!! deactivated when engine fire warning is pulled

44
Q

LOW PRESSURE (electric pump) (2)

A 
LOW PRESSURE (electric pump) (2)
output pressure is low
45
Q

OVERHEAT (2) (elec pump)

A

OVERHEAT (2) (elec pump)
pump or fluid cooling the pump has overheated
Anti Ice_ VALVE OPEN (2) or COWL VALVE OPEN (2)
Bright: in transit, or disagree with switch
Dim: open
off: closed.

46
Q

COWL ANTI-ICE (2)

A

COWL ANTI-ICE (2)
Overpressure in duct downstream of cowl anti-ice valve
Doors “DOOR NAME” (11)
not closed and lock
or flight lock fail to engage (overwing)
or fails to unlock OVERWING &PSEU
Air ZONE TEMP (LEFT)
Duct overheat
or failure of primary and standby cockpit temp control
During recall: one failed. Off when Master caution reset.

47
Q

ZONE TEMP (Mid and Right)

A

ZONE TEMP (Mid and Right)
Duct overheat
During recall: Zone temp control failed. Off when Master caution reset.
Reset possible with *TRIP RESET

48
Q

DUAL BLEED

A

DUAL BLEED
APU bleed open and engine 1 bleed switch on. or
APU bleed open and engine 2 bleed switch on Xvalve open
Means: Possible back pressure on APU: no engine above Idle.

49
Q

RAM DOOR FULL OPEN (2)

A 
RAM DOOR FULL OPEN (2)
#
50
Q

PACK (2)

A 
PACK (2)
Pack trip off or
Failure of both pack controls
During Recall > either primary or secondary pack control failed. Resets with MC
Reset possible with *TRIP RESET
51
Q

WING-BODY OVERHEAT (2)

A

WING-BODY OVERHEAT (2)
Overheat (bleed air leak): engine strut, inboard leading edge, conditioning bay
& keel beam or apu bleed duct

52
Q

BLEED TRIP OFF (2)

A

BLEED TRIP OFF (2)
bleed press or temp has been excessed
bleed valve closed automatically,
Reset possible with *TRIP RESET.

53
Q

AUTO FAIL

A

AUTO FAIL
Alone: Dual controller fault, automatic pressurisation failed
ALTN illuminated: single controller failure

54
Q

OFF SHED DESCENT

A

OFF SHED DESCENT

descent initiated before *FLT ALT was reached

55
Q

ALTN

A

ALTN
Mode selector is in alternate or
if ALTN & AUTO FAIL, a single controller has fail

56
Q

MANUAL (press)

A

MANUAL (press)

pressurisation is in manual mode

57
Q

Front Panel OPL side FMC P/RESET

A

Front Panel OPL side FMC P/RESET
Check CDU !
test switch
(some matricules) FAIL illuminated on CDU

58
Q

AT P/RESET (FLASHING RED) (2)

A

AT P/RESET (FLASHING RED) (2)

AT has disengaged

59
Q

A/P P/RESET (FLASHING RED) (2)

A

A/P P/RESET (FLASHING RED) (2)

AP disconnect

60
Q

A/P P/RESET (FLASHING AMBER) (2)

A

A/P P/RESET (FLASHING AMBER) (2)
mode reversion to CWS when in CMD
test (1) > “STEADY AMBER” AP & AT
test (2) > “STEADY RED” AP & AT

61
Q

A/P P/RESET (STEADY RED) (test, or:) (2)

A

A/P P/RESET (STEADY RED) (test, or:) (2)
Stab out of trim below 800Ft on dual app
ALT ACQ mode in hibit during AP if stab not trimmed for single AP
automatic ground test system fails

62
Q

CABIN ALTITUDE (2)

A

CABIN ALTITUDE (2)
Alt > 10.000,
concomitant with horn for CABIN ALT ALERT

63
Q

TAKEOFF CONFIG (2)

A

TAKEOFF CONFIG (2)
lever advance with conf not for T/O
concomitant with horn for T/O Config alert

64
Q

SPEEDBRAKE EXTENDED (in flight) (1)

A 
SPEEDBRAKE EXTENDED (in flight) (1)
LEVER beyond ARM, with Flaps more than 10 or RA<800ftRA
65
Q

SPEEDBRAKE EXTENDED (On the ground) (1)

A

SPEEDBRAKE EXTENDED (On the ground) (1)
Lever in the Down detent, or
Ground spoiler not stowed

66
Q

BELOW G/SP-Inhibit (2)

A

BELOW G/SP-Inhibit (2)
#
push to inhibit below 1000 RA

67
Q

INOP (GPWS) (1)

A 
INOP (GPWS) (1)
#
Front Panel CDB side SPEEDBRAKE ARMED (1)
valid auto speedbrake inputs
deactivated in down detent
68
Q

SPEEDBRAKE DO NOT ARM (1)

A

SPEEDBRAKE DO NOT ARM (1)
invalid auto speedbrake inputs
deactivated in down detent

69
Q

STAB OUT OF TRIM (1)

A 
STAB OUT OF TRIM (1)
Stab not properly trimmed by PA
Only works with AP/ON
Center Panel XXX GEAR (3)
not down and locked idle below 800ft or
in disagreement with lever position
70
Q

XXX GEAR (3)

A 
XXX GEAR (3)
down and locked
71
Q

LE FLAPS EXT

A

LE FLAPS EXT
ALL LE Flaps EXT and
ALL LE SLATs in EXT (F1-2-5) or FULLY EXT (F10->40)

72
Q

LE FLAPS TRANSIT

A

LE FLAPS TRANSIT
inhibited for autoslats
any LE in transit, not in position, moving
in alternaire, untill flaps 10 and LE device are fully extended

73
Q

AUTOBRAKE DISARM

A 
AUTOBRAKE DISARM
“Disarmed” for
down detent
manual brake
thrust advanced (3sec after touchdown)
landing with RTO
Malfunction
Self test on selection of RTO on the ground
off for autobrake swithc sur off, ou autobrake armed
74
Q

ANTISKID INOP

A 
ANTISKID INOP
#
Center Aisle PKBRAKE
#
ENGINE &APU DET *ovht det A/B/NORM (L and R)
A&B or A or B Active
75
Q

*Bell cuttout

A

*Bell cuttout

stops FIRE WARN, cuts bell, silence ground APU FIRE horn, resets

76
Q

*Fautl/inop-Overheat Fire TEST

A

*Fautl/inop-Overheat Fire TEST
Fautl: test fault detection Eng & APU
Overheat Fire: test overheat fire detection ENG & APU & WhEEL

77
Q

*Eng ext test

A

*Eng ext test

test dish circuits for Eng & APU

78
Q

*ENGINE FIRE (2) (dwn/up/rotate)

A 
*ENGINE FIRE (2) (dwn/up/rotate)
Fire detected, lever unlocked
UP:
arms squib on each 2 bottle & unlock rotation
closes shutoff (hyd, fuel, bleed)
trips generator relay
disable reverser
deactivate Hyd edp LOW PRESS light
rotate: discharge selected bottle.
79
Q

*APU FIRE (dwn/up/rotate)

A

*APU FIRE (dwn/up/rotate)
Fire detected, lever unlocked
UP
Arms

80
Q

ENG X OVERHEAT

A 
ENG X OVERHEAT
#
81
Q

WHEEL WELL FIRE

A 
WHEEL WELL FIRE
#
82
Q

FAULT (Engine overheat detection)

A

FAULT (Engine overheat detection)
DETECTION IS LOST
if ddet normal: both loops on an engine have failed
if det A or B: given loop has failed an engine

83
Q

APU DET INOP

A 
APU DET INOP
#
84
Q

XXX BOTTLE DISCHARGED

A

XXX BOTTLE DISCHARGED
#
CARGO DET *test
test foward and aft, fire detect loops and suppression system

85
Q

*det select A/B/NORM (fwd and aft)

A

*det select A/B/NORM (fwd and aft)

A&B or A or B Active

86
Q

DETECTOR FAULT

A

DETECTOR FAULT

both loops in one or both cargo compartiment have failed

87
Q

*ARMED (2)

A 
*ARMED (2)
#
88
Q

FWD

A

FWD
1 detector in each loop detects smoke
with one loop failed: 1 detector detects smoke

89
Q

*DISH (push)

A

*DISH (push)
has discharged
may take 30 sec to illuminate
(if second bottle, 60 minutes temporisation before second discharge. cancelled if arm is disarmed)

90
Q

N/A

A

N/A

737 (10 decks)

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