BOUTONS ! Flashcards
(90 cards)
1
Q
ELT
A
ELT
ELT is transmitting on 121.5, 243 and 406
2
Q
LE DEVICES
A
LE DEVICES AMBER: le in transit EXT: extended FULL ext: fully ext OFF: retracted
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
4
Q
GPS
A
GPS
Both GPS have failed
During recall: 1 has failed / resets with MC
5
Q
ALIGN (steady)
A
ALIGN (steady)
IRS aligning, or
initiating ATT, or
shutting down
6
Q
ALIGN (flashing)
A
ALIGN (flashing)
Cannot align
position missing or unreasonnable
7
Q
ALIGN (off)
A
ALIGN (off)
IRS available in NAV or ATT mode
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
9
Q
irs FAULT
A
irs FAULT
there is a fault
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
11
Q
ENGINE CONTROL
A
ENGINE CONTROL
non dispatchable engine control issue.
inhibited >80kt -> 30sec after touchdown
12
Q
ON (eec)
A
ON (eec)
Normal
rating controlled by EEC from sensed conditions
off (manually selected to alternate mode)
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.
14
Q
PASS OXY ON
A
PASS OXY ON
Masks have dropped
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.
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.
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.
18
Q
YAW DAMPER
A
YAW DAMPER
yaw damper not engaged
19
Q
LOW QUANTITY standby hyd
A
LOW QUANTITY standby hyd
less than 50% in standby hydraulic RSRVR
20
Q
LOW PRESSURE standby Hyd
A
LOW PRESSURE standby Hyd
standby pump is activated (auto or man) and output pressure is low
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
22
Q
? SPAR VALVE CLOSED ?
A
? SPAR VALVE CLOSED ?
bright: in transit or disagree
dim: closed
off: open
23
Q
? FILTER BYPASS ?
A
? FILTER BYPASS ?
impending bypass due contamination
24
Q
? VALVE OPEN ?
A
? VALVE OPEN ?
bright: in transit or disagree
dim: open
off: closed
25
? 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”
26
? 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”
27
? VIDEO ?
? VIDEO ?
une video passe en cabine
elec BAT DISCHARGE
BAT on, and excessive battery discharge
28
TR UNIT (on the ground)
```
TR UNIT (on the ground)
any TR has failed
```
29
TR UNIT (in flight)
```
TR UNIT (in flight)
TR1 or TR2&3 have failed
```
30
ELEC
ELEC
DC or standby system fault
only illuminated on ground
31
STANDBY PWR OFF
```
STANDBY PWR OFF
au moins un des bus est non alimenté:
AC standby
DC standby
batt buss
```
32
DRIVE
```
DRIVE
IDG OIL Low pressure, meaning:
Engine is off
IDG is failed
IDG disconnected (due OIL TEMP or disconnect swith)
```
33
GRD POWER AVAIL
GRD POWER AVAIL
| connected & quality check ok
34
TRANSFER BUSS OFF
TRANSFER BUSS OFF
| Side transfer bus is unpowered
35
SOURCE OFF
SOURCE OFF
| no source has been selected, or source has been disconnected
36
GEN OFF BUS
GEN OFF BUS
| IDG is not powering the buss (mais n’est pas forcément dispo)
37
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.
38
apu LOW OIL PRESSURE (during start)
apu LOW OIL PRESSURE (during start)
| until APU press is normal
39
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)
40
FAULT
FAULT
Fault is causing auto shutdown
disarmed when switch placed in off position. extinguishes 5 min after. (to note defect)
41
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
```
42
ON (4) Window heat
```
ON (4) Window heat
Heating in progress
off
si tempé ok,
overheat detecté,
fault,
switch off
```
43
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
44
LOW PRESSURE (electric pump) (2)
```
LOW PRESSURE (electric pump) (2)
output pressure is low
```
45
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.
46
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.
47
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
48
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.
49
RAM DOOR FULL OPEN (2)
```
RAM DOOR FULL OPEN (2)
#
```
50
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
```
51
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
52
BLEED TRIP OFF (2)
BLEED TRIP OFF (2)
bleed press or temp has been excessed
bleed valve closed automatically,
Reset possible with *TRIP RESET.
53
AUTO FAIL
AUTO FAIL
Alone: Dual controller fault, automatic pressurisation failed
ALTN illuminated: single controller failure
54
OFF SHED DESCENT
OFF SHED DESCENT
| descent initiated before *FLT ALT was reached
55
ALTN
ALTN
Mode selector is in alternate or
if ALTN & AUTO FAIL, a single controller has fail
56
MANUAL (press)
MANUAL (press)
| pressurisation is in manual mode
57
Front Panel OPL side FMC P/RESET
Front Panel OPL side FMC P/RESET
Check CDU !
test switch
(some matricules) FAIL illuminated on CDU
58
AT P/RESET (FLASHING RED) (2)
AT P/RESET (FLASHING RED) (2)
| AT has disengaged
59
A/P P/RESET (FLASHING RED) (2)
A/P P/RESET (FLASHING RED) (2)
| AP disconnect
60
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
61
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
62
CABIN ALTITUDE (2)
CABIN ALTITUDE (2)
Alt > 10.000,
concomitant with horn for CABIN ALT ALERT
63
TAKEOFF CONFIG (2)
TAKEOFF CONFIG (2)
lever advance with conf not for T/O
concomitant with horn for T/O Config alert
64
SPEEDBRAKE EXTENDED (in flight) (1)
```
SPEEDBRAKE EXTENDED (in flight) (1)
LEVER beyond ARM, with Flaps more than 10 or RA<800ftRA
```
65
SPEEDBRAKE EXTENDED (On the ground) (1)
SPEEDBRAKE EXTENDED (On the ground) (1)
Lever in the Down detent, or
Ground spoiler not stowed
66
BELOW G/SP-Inhibit (2)
BELOW G/SP-Inhibit (2)
#
push to inhibit below 1000 RA
67
INOP (GPWS) (1)
```
INOP (GPWS) (1)
#
Front Panel CDB side SPEEDBRAKE ARMED (1)
valid auto speedbrake inputs
deactivated in down detent
```
68
SPEEDBRAKE DO NOT ARM (1)
SPEEDBRAKE DO NOT ARM (1)
invalid auto speedbrake inputs
deactivated in down detent
69
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
```
70
XXX GEAR (3)
```
XXX GEAR (3)
down and locked
```
71
LE FLAPS EXT
LE FLAPS EXT
ALL LE Flaps EXT and
ALL LE SLATs in EXT (F1-2-5) or FULLY EXT (F10->40)
72
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
73
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
```
74
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
```
75
*Bell cuttout
*Bell cuttout
| stops FIRE WARN, cuts bell, silence ground APU FIRE horn, resets
76
*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
77
*Eng ext test
*Eng ext test
| test dish circuits for Eng & APU
78
*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.
```
79
*APU FIRE (dwn/up/rotate)
*APU FIRE (dwn/up/rotate)
Fire detected, lever unlocked
UP
Arms
80
ENG X OVERHEAT
```
ENG X OVERHEAT
#
```
81
WHEEL WELL FIRE
```
WHEEL WELL FIRE
#
```
82
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
83
APU DET INOP
```
APU DET INOP
#
```
84
XXX BOTTLE DISCHARGED
XXX BOTTLE DISCHARGED
#
CARGO DET *test
test foward and aft, fire detect loops and suppression system
85
*det select A/B/NORM (fwd and aft)
*det select A/B/NORM (fwd and aft)
| A&B or A or B Active
86
DETECTOR FAULT
DETECTOR FAULT
| both loops in one or both cargo compartiment have failed
87
*ARMED (2)
```
*ARMED (2)
#
```
88
FWD
FWD
1 detector in each loop detects smoke
with one loop failed: 1 detector detects smoke
89
*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)
90
#N/A
#N/A
