BOUTONS ! Flashcards
ELT
ELT
ELT is transmitting on 121.5, 243 and 406
LE DEVICES
LE DEVICES AMBER: le in transit EXT: extended FULL ext: fully ext OFF: retracted
PSEU
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
GPS
GPS
Both GPS have failed
During recall: 1 has failed / resets with MC
ALIGN (steady)
ALIGN (steady)
IRS aligning, or
initiating ATT, or
shutting down
ALIGN (flashing)
ALIGN (flashing)
Cannot align
position missing or unreasonnable
ALIGN (off)
ALIGN (off)
IRS available in NAV or ATT mode
irs ON DC
irs ON DC
AC power not normal, IRS on switched Hot battery bus (ground horn sounds)
illuminates normally during self test
irs FAULT
irs FAULT
there is a fault
irs DC FAIL
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
ENGINE CONTROL
ENGINE CONTROL
non dispatchable engine control issue.
inhibited >80kt -> 30sec after touchdown
ON (eec)
ON (eec)
Normal
rating controlled by EEC from sensed conditions
off (manually selected to alternate mode)
ALTN
ALTN
auto switch to soft alternate (ON still displayed) or
man swicth to hard alternate
EEC provides rated thrust or higher.
PASS OXY ON
PASS OXY ON
Masks have dropped
GEAR LIGHTS
GEAR LIGHTS
DOWN and LOCKED
as long as one light from this panel or the other is green, down and locked.
OFF (flight recorder)
OFF (flight recorder)
recorder is not operating, or test is invalid, or power failure, or loss of data or fail.
FCTL LOW PRESSURE Flight control
FCTL LOW PRESSURE Flight control
Low pressure to (Hyd X) aileron, elevator, rudder
deactivated when standby rudder activated and rudder shutoff valve opens.
YAW DAMPER
YAW DAMPER
yaw damper not engaged
LOW QUANTITY standby hyd
LOW QUANTITY standby hyd
less than 50% in standby hydraulic RSRVR
LOW PRESSURE standby Hyd
LOW PRESSURE standby Hyd
standby pump is activated (auto or man) and output pressure is low
STBY RUDDER ON
STBY RUDDER ON standby system is pressurizing rudder PCU FUEL ? ENG VALVE CLOSED ? bright: in transit or disagree dim: closed off: open
? SPAR VALVE CLOSED ?
? SPAR VALVE CLOSED ?
bright: in transit or disagree
dim: closed
off: open
? FILTER BYPASS ?
? FILTER BYPASS ?
impending bypass due contamination
? VALVE OPEN ?
? VALVE OPEN ?
bright: in transit or disagree
dim: open
off: closed
? LOW PRESSURE (center pumps) ?
? LOW PRESSURE (center pumps) ?
pump on and low press
> if center pump on and low press for 10 sec, “master caution & “Fuel sys”
? LOW PRESSURE (main pumps)?
? 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”
? VIDEO ?
? VIDEO ?
une video passe en cabine
elec BAT DISCHARGE
BAT on, and excessive battery discharge
TR UNIT (on the ground)
TR UNIT (on the ground) any TR has failed
TR UNIT (in flight)
TR UNIT (in flight) TR1 or TR2&3 have failed
ELEC
ELEC
DC or standby system fault
only illuminated on ground
STANDBY PWR OFF
STANDBY PWR OFF au moins un des bus est non alimenté: AC standby DC standby batt buss
DRIVE
DRIVE IDG OIL Low pressure, meaning: Engine is off IDG is failed IDG disconnected (due OIL TEMP or disconnect swith)
GRD POWER AVAIL
GRD POWER AVAIL
connected & quality check ok
TRANSFER BUSS OFF
TRANSFER BUSS OFF
Side transfer bus is unpowered
SOURCE OFF
SOURCE OFF
no source has been selected, or source has been disconnected
GEN OFF BUS
GEN OFF BUS
IDG is not powering the buss (mais n’est pas forcément dispo)
APU GEN OFF BUS
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.
apu LOW OIL PRESSURE (during start)
apu LOW OIL PRESSURE (during start)
until APU press is normal
LOW OIL PRESSURE (after start cycle)
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)
FAULT
FAULT
Fault is causing auto shutdown
disarmed when switch placed in off position. extinguishes 5 min after. (to note defect)
OVERSPEED
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
ON (4) Window heat
ON (4) Window heat Heating in progress off si tempé ok, overheat detecté, fault, switch off
Probe Heat “PROBE NAME” (8) eg CAPT PITOT
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
LOW PRESSURE (electric pump) (2)
LOW PRESSURE (electric pump) (2) output pressure is low
OVERHEAT (2) (elec pump)
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.
COWL ANTI-ICE (2)
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.
ZONE TEMP (Mid and Right)
ZONE TEMP (Mid and Right)
Duct overheat
During recall: Zone temp control failed. Off when Master caution reset.
Reset possible with *TRIP RESET
DUAL BLEED
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.
RAM DOOR FULL OPEN (2)
RAM DOOR FULL OPEN (2) #
PACK (2)
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
WING-BODY OVERHEAT (2)
WING-BODY OVERHEAT (2)
Overheat (bleed air leak): engine strut, inboard leading edge, conditioning bay
& keel beam or apu bleed duct
BLEED TRIP OFF (2)
BLEED TRIP OFF (2)
bleed press or temp has been excessed
bleed valve closed automatically,
Reset possible with *TRIP RESET.
AUTO FAIL
AUTO FAIL
Alone: Dual controller fault, automatic pressurisation failed
ALTN illuminated: single controller failure
OFF SHED DESCENT
OFF SHED DESCENT
descent initiated before *FLT ALT was reached
ALTN
ALTN
Mode selector is in alternate or
if ALTN & AUTO FAIL, a single controller has fail
MANUAL (press)
MANUAL (press)
pressurisation is in manual mode
Front Panel OPL side FMC P/RESET
Front Panel OPL side FMC P/RESET
Check CDU !
test switch
(some matricules) FAIL illuminated on CDU
AT P/RESET (FLASHING RED) (2)
AT P/RESET (FLASHING RED) (2)
AT has disengaged
A/P P/RESET (FLASHING RED) (2)
A/P P/RESET (FLASHING RED) (2)
AP disconnect
A/P P/RESET (FLASHING AMBER) (2)
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
A/P P/RESET (STEADY RED) (test, or:) (2)
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
CABIN ALTITUDE (2)
CABIN ALTITUDE (2)
Alt > 10.000,
concomitant with horn for CABIN ALT ALERT
TAKEOFF CONFIG (2)
TAKEOFF CONFIG (2)
lever advance with conf not for T/O
concomitant with horn for T/O Config alert
SPEEDBRAKE EXTENDED (in flight) (1)
SPEEDBRAKE EXTENDED (in flight) (1) LEVER beyond ARM, with Flaps more than 10 or RA<800ftRA
SPEEDBRAKE EXTENDED (On the ground) (1)
SPEEDBRAKE EXTENDED (On the ground) (1)
Lever in the Down detent, or
Ground spoiler not stowed
BELOW G/SP-Inhibit (2)
BELOW G/SP-Inhibit (2)
#
push to inhibit below 1000 RA
INOP (GPWS) (1)
INOP (GPWS) (1) # Front Panel CDB side SPEEDBRAKE ARMED (1) valid auto speedbrake inputs deactivated in down detent
SPEEDBRAKE DO NOT ARM (1)
SPEEDBRAKE DO NOT ARM (1)
invalid auto speedbrake inputs
deactivated in down detent
STAB OUT OF TRIM (1)
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
XXX GEAR (3)
XXX GEAR (3) down and locked
LE FLAPS EXT
LE FLAPS EXT
ALL LE Flaps EXT and
ALL LE SLATs in EXT (F1-2-5) or FULLY EXT (F10->40)
LE FLAPS TRANSIT
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
AUTOBRAKE DISARM
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
ANTISKID INOP
ANTISKID INOP # Center Aisle PKBRAKE # ENGINE &APU DET *ovht det A/B/NORM (L and R) A&B or A or B Active
*Bell cuttout
*Bell cuttout
stops FIRE WARN, cuts bell, silence ground APU FIRE horn, resets
*Fautl/inop-Overheat Fire TEST
*Fautl/inop-Overheat Fire TEST
Fautl: test fault detection Eng & APU
Overheat Fire: test overheat fire detection ENG & APU & WhEEL
*Eng ext test
*Eng ext test
test dish circuits for Eng & APU
*ENGINE FIRE (2) (dwn/up/rotate)
*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.
*APU FIRE (dwn/up/rotate)
*APU FIRE (dwn/up/rotate)
Fire detected, lever unlocked
UP
Arms
ENG X OVERHEAT
ENG X OVERHEAT #
WHEEL WELL FIRE
WHEEL WELL FIRE #
FAULT (Engine overheat detection)
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
APU DET INOP
APU DET INOP #
XXX BOTTLE DISCHARGED
XXX BOTTLE DISCHARGED
#
CARGO DET *test
test foward and aft, fire detect loops and suppression system
*det select A/B/NORM (fwd and aft)
*det select A/B/NORM (fwd and aft)
A&B or A or B Active
DETECTOR FAULT
DETECTOR FAULT
both loops in one or both cargo compartiment have failed
*ARMED (2)
*ARMED (2) #
FWD
FWD
1 detector in each loop detects smoke
with one loop failed: 1 detector detects smoke
*DISH (push)
*DISH (push)
has discharged
may take 30 sec to illuminate
(if second bottle, 60 minutes temporisation before second discharge. cancelled if arm is disarmed)
N/A
N/A
