Intial / Recurrent CE650 GS Flashcards
As you are lining up on the runway for takeoff what light will be illuminated on the annunciator panel assuming everything is normal.
PAC HP Valve Open
Ground Idle
Electronic memory aid
DC _______ and AC ________
lies
doesn’t not share
how long does it take to extend the flaps from:
0 - 7
7 - 20
12-14 seconds
4 secsonds
Before starting the second engine
Ground Idle switch in HIGH
and
Amps less then 200
Min fuel
700 lbs, 350 in each wing
How many drain valves and where are they located
12
5 - lt
4 - Rh
3 empennage
if the brakes stop working on touchdown
recycle Anti Skid switch
The Ailerons are ________ boosted like power steering
The captains control wheel is connected to the ailerons via _______ The copilot is connected to the ______
Hydraulic
Captain - cable
Copilot - Hyd Assist (Roll Spoilers)
Total number of vortex generators and how many are on each wing.
How many can be missing
22
11
1
Total number of static wicks and how many can be missing
Which static wick can not be missing as per the MEL
23
2, not adjacent
On the singer
On Landing how many annunciators lights will be illuminated when TR are deployed assuming everything is normal
6 + 1
ARM, UNLOCK, DEPLOY
RUDDER BIAS
TR are to be tested ______ at a time
1
Max rev thrust is _______%
91%
All switches are ______ activated
DC
Pneumatic bleed valves are held closed, when they loose power the valves _______
open
when using pneumatic bleed air for A/I, PAC in HIGH or HP Bleed air is _________
prohibited
what 3 gauges can be seen in the left nose equipment area?
- Emergency Gear and brake
- NWS accumulator
- W/S Alcolhol
Leave gen ______ for GPU starts
GPU starts count as ______ battery starts
OFF
0
How do you know if the generator field relay is open
Volt indicate 0
Landing lights may cause up to ______ of magnetic variation
10 deg
what makes up Passenger lights
Overhead
Reading
Footwell
min fuel in left tank to fill fus tank during overwing fueling
175 gallons - 1,100 lbs
Engine start can be aborted anytime by pressing the __________
starter disengage switch
Reasons to shut down engine start
HOT, ITT limit
HUNG, no N1 20 seconds
No light off, 10 seconds
APR will increase N1 by
1%
the EEC requires ___V
14 - 30 V
The mechanical N2 governor in the FCU is at ______% N2 to provide overspeed protection
105%
X-gen start in flight is
inhibited
Landing Gear locks PAC Bleed select to
LP
If svc air is lost pressure in the cabin
increases
max alt with a hydraulic issue
45,000
OFV sequence after landing
60 sec 300 fpm
60 fully open
Flap setting for Takeoff Alt above 8,000
7
Engine Fuel burn both engines
10 lbs/min
Average taxi time and fuel burn
20 min, 200 lobs
Rt and LT P/S switch control
LT - P/S, AOA
RT - P/S, Rudder bias
max quantity of w/s alcohol and time limit
2 quarts
15 min
roll spoilers move after _____” of control movement
3.5”
Vref is _____Vs0
1.3
N2 Lights
Green
Red
48 - 99.9%
> 99.9%
use_________ in the III with W/S bleed air on, on ground, due to lack of ram air
Caution
Actions to take if both batteries overheat
Batt sw off
Rotary test is required on the ________
Start with ______ to check all lights are working
VII - Rotary test requires w/s heat switch to be selected ______ during Rotary w/s temp test
first flight of day
ANNUN
ON
AP basic mode consist of
Hdg select and alt hold
AP _____ be tested before use
must
if PRI Trim is INOP, AP is
Inop
Flap up speed
v2 + 25
Vref + 25
STBY GYRO switch must be _____ for automatic transfer to emergency battery pack
ON
Gyro slave in manual moves LH and RH at _____ per min
30 deg
VERT GYRO switch to FAST acts as a _______
timer for AHRS
Attempting to override the feedback cable “snatcher” or advance throttles prior to unlock extingushing light requires _______
Mx inspection
Engine start, test flood lights ________
backup, dedicated emergency, battery
When the aileron boost looses pressure a ______ horn will sound and the _____ trips off
warning
AP
On A/C without INV ON/OFF switch
Avionics switch turns on _____ and _____ equipment
AC and DC equipment
the Red gun in the display is the ________ to fail
1st
TFE 731, 731 means
731 lbs
N2 produces _______
N1 Produces ________
Power
Thrust
engine holds _______ qts of oil
oil breather closes at _________
1 sensor for the __________
1 sensor for the _______
11.6
27,000 - 30,000
annunciator
gauge
APU produces ______ amps and _____ volts
150
28
________ batteries need to be charged at the same time
both
Junction box connects heaver ______amp wire to smaller _____ amp wire
365
75
if one batter is 24 volts and the second is 19 volts the second battery is
faulty
with the generators online switch the batt switch to ______ to read battery voltage from the HBB
off
Engine fire bottle _______ oxygen
displaces
smoke detector is next to the OFV where air is the ________
thickest
wing fuel tanks are _______
fus fuel tank is a _______
wet tanks, fuel on metal
bladder
Fuel flow pressure to the engine is _________
1450 psi
wing fuel tanks are not ______
pressurized
fuel transfers at a rate of approx ______ lbs a min
25
the aft vanity FUS FUEL Transfer T handle ________ the transfer valve, pushing the handle in does NOT ______ the valve and pulling the T handle does ______ trigger the light
opens
close
does not
NWS accumulator provides
3-4 90deg turns
spoiler hold down accumulator _______ pressure and does ______ loose fluid
provides
not
when does the AUX HYD PUMP turn on
Low Pressure -1200 PSI
SPoiler Hold down is on
HYD Accumulators do what 3 things
- Store fluid under pressure
- Absorb system shock
- Instant Pressure Available to components
HYD fluid is _____ compressible
not
explain Venturi effect
Bernoulli’s principle
as fluid travels thru a smaller cross section the pressure decreases and velocity increases
Gen is limited to _____ amps on takeoff
365 amps
receiving wing tank boost pump must be ______ during fuel transfer
off
SPPR must be accomplished in accordance to the ______
Placard
red light on rotary test _______ when out of off
illuminates
Pri Trim may need to be ________ to for Rotary test to illuminate PRI TRIM Fail light
actuated
On models 0-178 with automatic transfer of Inverters
The left switc” AKA Avionics Master controls the ____ components of the avionics equipment. The INV switch controls the ____ components of the avionics equipment.
On Models 179 and on the Avionics Power ON switch controls both _____ and _______ components of the avionics.
DC
AC
DC and AC
All equipment on the Emergency buss will ______ if BATT switch is off due to overheat and generators are on
operate
The horizontal stab test will trigger the annunciator light to illuminate for _______
5 seconds
Flight crew non essential CB are located in the _______
J Box
The APU is a ______ stage turb engine the provides _______ , ______ and optional _______
single
Service Air
A/C
Hyd
The APU is controlled by the _______
The APU will ______ shutdown due to failure or fire.
the fie bottle will automatically discharge the fire after _____ seconds
The Fire bell bell will ring ________
ESU, Elec. Seq Unit
automatical
8 seconds
continously
________TR Lights
Arm - a pressure switch, indicating the isolation valve is ______ and hydraulics are _______
Unlock - a Microswitch indicating TR _____ movement
Deploy - a Microswitch indicating _____ deployed
No light means Hydraulic Pressure is _______ from the TR’s and the TR’s are stowed in position by an Over-center condition of the operating _________.
Open
available
Initial
Fully
Isolated
bar mechanism
TR will only deploy when the following 2 conditions are met:
WOW
TL in idle
Pneumatics:
All Systems use _____ air.
The PACs use ____ and ____ air.
HP
HP and LP
III
Caution when using W/S heat on ground as no _____ is mixing with HP air
Ram Air
W/S Bleed Air Switches control the_____ of air
volume
W/S defog does ____ heat the w/s
not
AC/DC Gen Inlet heater is _____ monitored
not
Cycling Engine A/I means
wingroot overheat
min A/S of _____kts in icing conditions to ______ icing build up on a/c
180 kts
prevent
Throttle feed back cable holds the throttle in idle at ______ psi
600 PSI
A/C Dimensions and turning radius
55.2’ in length
53.3 wingtip to tip
17.1’ ht of empennage
Min Turn Radius 33.35’
Green oxygen disc will rupture if the bottle is _______
overpressurized
Pax O2 will not flow until the _______ is pulled to conserve O2
lanyard
Select Pax O2 _____ to conserve O2 for the Crew
OFF
Mic Oxy Mask and Mic Head Set switch is located where
Lt and Rt lower inst panel
the walk around portable O2 is _________cb ft
11 cubic ft
when the aircraft is descending below 8,000’ after a decompression the pax solenoid __________
closes
Turn IGN _____ in heavy rain as a precaution against flamout
ON
with WOW Stab Ht will ______ turn on
not
A stab on light indicates the heating element is ________
stab light cycles on/off indicates ______
Cold
Overheat
W/S Alcohol is dispersed on the _______ window
left
The gear takes approximately ________ to cycle
4-6 seconds
main gear braking is ______. during retraction
automatic
the HYD dump valve is located _________ and pulling the valve relieves landing gear _______ by opening the ______ valve to release blocked fluid to return
in the aft lav
Pressure
Do Not _______ gear after free fall
retract
parking brake _______ fluid return
to use the parking break, if eng are off
_
_
Do not set _____ hot brakes
prevents
- Aux hyd pump on
- pump toe brake
Not
roll spoilers movement begins after _______ of aileron travel
3 - 3.5 deg
Aileron boost needs to be ________ after power interruption
reset
clacker sound when stab trim is moving for more then ______
1 second
Rudder bias provides _________ lbs of rudder pound force
125 - 150
NWS automatically _________ once airborne
Disengages
an indication of a floating spoiler is annun by________ and/or _______
spoiler up lt, speed brake lt
anytime a flap asym is detect the flap control will _______ the flaps
disable
control lock during taxi out in ________ conditions
gusty
when a fault in the left or right AOA probe/transmitter the ________ will illuminate
AOA prob
when their are faulty inputs from the Flap or spoilers to the AOA logic the __________ lt will annunciate
In this cases the stick shaker will will _______ between 0.715 - 0.825 as a fail safe
the AOA gauge, indexer and fast slow indicator will be _____
Flaps/Speedbrake
Activate
Off
both AOA probes have failed when the following light are illuminated
- Probe and Stall warn Lt
During an emergency descent with the AP engaged above 34,275 and bare above 13,500 feet the AP will?
_
_
_
Turn _____ the AP to cancel the Emergency descent mode
- Pitch to maintain Vmo/Mmo
- 35 deg bank left for approx 48 sec
- Level at 15,000
OFF
