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
