Ground School Study Questions Flashcards
The aircraft may be towed up to a limit of _______ degrees of nose wheel center with the torque like connected and the nose wheel steering control disconnected
120*
Which doors are monitored by the door warning system
M - main door
E - emergency exit
C - cargo door
A - aft equipment door
B - battery door
What happens when you turn the batteries on?
CVR starts recording
BIT test
IRS alignment
All busses powered
What is the primary function of the APU
Provide electric power for the aircraft
Where does the APU receive its fuel
Right collector tank
Under what condition does a passenger door caution (amber) CAS message display when the aircraft is on the ground and the door is not fully secured
When the left engine run switch is set to run
What is the maximum fuel quantity with pressure fueling
14150 lbs
What is normal TO thrust flat rated to ISA 15* C at sea level
7372
Which EICAS messages require prompt action
Amber
What color CAS message denotes failure of component or no flow, energy or pressure
Amber
What engines does the 350 have
HTF7350
(Honeywell turbofan 7000 series on the 350)
What is the max cabin altitude
7850 @FL450
What happens if nosewheel is turned to 120*
CAS message
What happens if the nosewheel is turned to 123*
Damage to sheer pin
What is the aircraft dimensions
W 69ft
L 69ft
H 20 ft
What is connected to the right battery?
Fuel panel
What is connected to the left battery
Lights
How many way are there to close the main door
2
Buttons
Hand crack/Lully
What must be done if baggage door is closed from the inside
Verify the button is popped back out and flush on the handle on the exterior
What are you looking for in the stall rudder limiter test
Red STALL on both PFDs
L/R stick shaker
Pusher is activated
White CAS RUDDER LIMITER IN TEST
red LSC on both PFDs
Flashing red AOA
How long does the standby instrument back up battery last for
3.5 hours
How long does the IRS aligning take
A few minutes depends on location in the world; the farther north/south from the equator you are
Why is the right battery selected first when powering the aircraft
Prevent inadvertent APU start
Red CAS message require _____ action
Immediate
Amber CAS message require _______ action
Prompt
What does cyan CAS message mean
Aircraft has automatically done something for you
What does a white CAS message mean
You have manually done something to the aircraft
How can you tell the difference between the taxi and landing light
Taxi light is fogged
Landing light is clear
What are the doors by the right wing root
Refueling panel
Single point connection door
Outflow valves door
What are the large fin like antennas on top/bottom of the aircraft for
VHF
top = com1 & 3
Bottom = com2
How many static wicks can be missing from each group
1
What is apart of the right aileron? The left aileron
Right - balance anti servo tab
Left - balance anti servo tab and trim tab
What doors must remain unlocked during flight
CABO
Cargo
Aft equipment
Battery
Outflow value
When does the emergency lights turn on
When power to the right main bus is lost
Where would you look to find the required oxygen quantities for a flight
QRH Volume 1
What causes the FDR to start recording
When the STROBE BCN is selected to any position or WOW
When the emergency lights are armed, when will they illuminate
Right main bus power is lost
Which fuel tanks supply fuel to the engine
The collector tanks
What is the purpose of the PTU
Retracts the landing gear when the left EDP (engine driven hydraulic pump) system fails
What electronically controls the landing gear system
The proximity sensing electronic unit PSEU
What is the only primary flight control system that is not hydraulically assisted
Ailerons
Which spoilers operates as multi function spoilers
The 2 outbound spoilers on each wing
Select EICAS messages are inhibited when
TO above 80kts until 400ft agl
Landing below 400ft agl and lower then then 40kts
Max operating speeds of flaps
10 - 210
20 - 210
30 - 175
When will the bus tie open
3 gens operating
2 gens operating
Forced open
When will the auxiliary busses load shed
In flight with only one generator operative
Dual fire protection loops in the engine and APU provide info to what component
FIREX-CU
Fire detection and extinguishing control unit
During climb out what is the correct button sequence to transfer to the engine bleeds from the APU bleeds
X bleed
Left bleed
APU bleed
Right bleed
When the air source selector switch is selected to trim air only which valves open and which valves close
right FCV opens
Left FCV closes
PCV closes
What does the CABIN DELTA P warning CAS message indicate
Cabin differential pressure is greater then 9.2 or less then -0.5
Until what point is the TO and return to base sequence active in the pressurization system
Until 1 of the following occurs
• aircraft reaches 6000ft above TO elevation
•10 mins elapse
What is the maximum delta p permitted for landing
1.0
When crossing the holding fix for a hold manually entered into the FMS what would be displayed at the bottom of the legs page
EXIT HOLD
What kind of batteries does the aircraft have
2 24 volt 44 amp hour nicad batteries
What is normal fuel reserve
1850
What fuel quantity would constitute a fuel emergency
1300
What fuel load is required for inclement wx
6000
What is the hot spare fuel load
6000
When does yaw damp automatically turn on
31,600
When is yaw damp required to be on by
31,000
What is our climb speed schedule
250kts below 10,000
280kts above 10,000
What is Vmo
300 below 8,000
320 above 8,000
When yaw damp is selected ON when will it automatically turn off
Takeoff roll above 60kts to WOW
What is the brains of the landing gear
PSEU
Proximity sensor electronic unit
What hydraulic system controls the gear
The left system
How many quarts of fluid does each hydraulic system hold
L 13
R 9.1
Where does the PTU get its fluid from and provide pressure
Fluid from the right system and provides pressure to the left system
Max alt for APU bleed
20,000
Max alt for APU gen
30,000
Max alt for APU
37,000
Max alt for APU start
30,000
Max airspeed for APU start
285
What is required for any valve to open
Some sort of flow and electrical signal
What happens when the engine run switch is selected to run
Activates ignition system
Turns on DC fuel pump
Position starter control valve to open
What is the fuel imbalances
250 lb imbalance with more then 13,700lbs
600lb imbalance with less then 4000lbs
What are the functions of the primary Stab trim system
Mach trim
Configure trim
* variable rate pitch trim
Which Stab trim does the autopilot not work with
Secondary trim system
What does approach made do
NAV to NAV transfer - auto switch from pink needles to green needles on ILS
Find and follow GS or GP
When shooting an RNAV what also needs to be active for GP to be captured
VNAV
What system doesn’t have hydraulic redundancy
Gear
What is the bulk fuel temp limit
50*C
What are the requirements if fuel temp is between 45c and 49c
Must have at least 2800lbs if fuel
If a tank drops below 1000lbs that engine can only run for 30 more minutes
When will the hydraulic shutoff valves auto close
When hydraulic fluid temp reaches 135*c
What bus powers the right DCMP
Left essential buss
What powers the left DCMP
Right main bus
What are the spoiler limitations
Vref+8
Below 500ft agl
When max spoilers are selected, what spoilers are deployed
1 and 8
What spoilers deploy when EMER spoilers are selected
1,2,7,8
How far do the multi function spoilers deploy
45*
How far do the ground spoilers deploy
60*
What happened if the landing alt is higher then max cabin alt
Caution and warning gates change
What is apart if the TO configuration warning system
Parking break
Roll/pitch disconnect
Any trim out of the green
Flaps not in TO config
Spoilers out
Autopilot on
When does the TO configuration system do it’s logic check
When thrust levers in climb or TO detent
How long can the thrust levers be in TO
5 min
How long can thrust levers be in APR
5 mins
What needs to happen for auto APR to activate
15% N2 split on TO
Gear down
Flaps greater then 27 for single engine go around
What needs to happen for auto APR to arm
Thrust levers in TO detent
When do you get a cabin alt caution
8500
When do you get a cabin alt warning
9400
Max delt p
9.2
-0.5
How many pressurization valves does the aircraft have
3
Outflow
Over pressure
Negative pressure
What is the structural limit for delta P
9.4
What does the manual rate knob control
Cabin rate
Outflow valve
Cabin alt
What is the brains of the pressurization system
Integrated air system controller IASC
What happens when the ditching button is pressed
Depress cabin
Outflow valve closes
Environmental flow control valve closes
When is the ditching button available
Below 15000 ft
If In auto or manual made how does the cabin depress and to what alt
Auto 14000 2500fpm
Manual 14500 3000fpm
Do the tow breaks work if complete loss of hydraulics
Yes one application of toe breaks
What are the breaks made of
Carbon fiber
Does the emergency breaks have anti skid
No
What is the min pavement width required to make a 180 turn with a 5ft safety margin
58 ft
What is the purpose of the scavenger ejectors
Replenish fuel from wing tank to collector tank
Lowest inboard point of each wing
For what system does the pneumatic system use HP air
Wing anti ice
How many ice detectors are required to generate an ICE DETECTED CAS message
1
What do the outboard temp sensors measure
Leading edge for insufficient temperature
What EICAS message will be displayed when the anti ice systems are off and detected
Amber ICE DETECTED
How long must the engine be cranked for after an aborted start
30 sec
At and below what temp must engine anti ice on for ground ops when surface is contaminated
10c or below
When does wing and engine anti ice have to be on while on the ground while on contaminated surfaces
10* C and below Engine anti ice on
5* C and below wing and engine anti ice on
After type 4 application when do you turn in wing anti ice
Right before departure
When is anti ice turned on in flight?
I’m icing conditions TAT 10C to -40C
If airspeed is below 210knts
What happens if ice detected with anti ice on
Cyan ice detected cas message
What happens if Ice detected while anti ice not on
Amber ice detected cas message
When does anti skid provide protection
Above 10 kts
Min OAT for TO
-40c
Min battery temp for TO
-20*C
What does the pack do
Provide cold air
What does the trim air do
Provide warm air
What does the air source selector control
Flow control valves for pack and trim air
What is the auto temperature range
15-35*
What is the auto temp range
3-70*
Is the APU bleed air HP or IP
Ip
What is HP air used for
Wing and engine anti ice
What bleed air source is used for environmental control
IP
If a complete electrical failure occurs how does the anti ice valves fail?
Engine anti ice fails open
All other fail closed
What is the brains of the avionics
IAPS
What is the Brains of the fire detection and extinguishing
FIREX-CU
What happens when engine fire occurs
Aural “engine fire”
L/R fire button lights illuminate
Extinguishing light 1 and 2 illuminate
Triple chime
Fire CAS
“FIRE” in N1 gage
What happens when APU fire occurs
APU fire light
Fire extinguisher 2 light
Triple chime
Aural APU fire
APU fire CAS
Where do we have fire detection
Engine
APU
Cargo compartment
Wheel well
How many handheld fire extinguisher are on the aircraft and where are they
3
Cockpit
Closet
Lav
What happens when L/R fire button is pressed
Squibs are armed
Fuel SOV close
Hydraulic SOV close
Bleed SOV close
Generator turns off
Extinguishing lights illuminate
FADEC command engine shut down
What happens when APU fire button is pressed
Squibs are armed
Fuel SOV close
Bleed SOV close
Generator turns off
Extinguishing 2 light illuminate
ECU commands APU shut down
Do you need both loops of a dual loop fire detection loop to detect a fire for fire signal to be set
2 if both loops are operational
1 if one loop fails
Where do we have dual loop fire protection and where do we have single loop protection
Dual loop in both engines and APU
Wheel well single loop
How many igniters are in each engine
2
When is it recommended to manually select the ignitions switch to ON
During flight through moderate or heavy intensity turbulence
How many ice detectors are installed on the aircraft
2
In what mode is the ditching switch available
Auto mode
Where is the fuel/hydraulic heat exchanger
In the wing fuel tank
What is the power source for left DCMP
Right main bus
How long will the emergency lights remain illuminated at ambient temperature
10 mins at critical ambient temps
What is the purpose of the safety valves
Prevent over pressurization and negative pressures conditions
What is the battery life if the standby instruments
3.5 hours
In what unit is the oxygen quantity displayed to the crew
Liters
At what cabin altitude will the EPAV cause the passenger oxygen masks to automatically deploy
14,500
Auto mode allows flow of oxygen until cabin alt is below 9500
What PSI is a fully charged oxygen system
1850
What is the duration of the batteries in the event of a total loss of generator power
1 hour
When manual mode is selected on the pressurization panel the pilot is controlling what
Manual Control of the outflow valve
Where is the oxygen service point located
Right side of the fuselage, directly forward of the right engine
What is the amp limit while on the ground for APU gen
400
What is the amp limit with 1 gen inflight
500
600 for 5 min
What is the limitation for the air source selector switch
Do not select trim air on the ground
If the aircraft is on the ground powered for 30 min or more when temp is 40*C or higher what must happen
Aircraft must be air condition
When should the igniter’s manually be turned on
TRCT
thunderstorms
Rain/ any moderate precipitation
Turbulence
Contaminated runways
What is the PMA
Permanent magnetic alternator
Provides power to the FADEC system is case of complete electrical failure
When does the PMA provide enough power to the FADEC
At idle thrust
What is the single engine limit APR limitation
10 min
When are the DCMPs automatically turned on
Low hydraulic pressure
Flaps set 10 or greater
When are both igniters on
Manually turned on
Engine flame out
High AOA
How many air data computers the aircraft have?
2
Max oxygen quantity liters and PSI
1850 psi
About 5400 liters
What is the brains of the oxygen system
EPAV
What are some concerns with the therapeutic oxygen
The oxygen is provided by the same bottle as crew O2. Oxygen charts don’t account for its use
What happens to the oxygen system if a complete electrical failure
The crew o2 valve fails open to ensure mask have oxygen flow
Where are the oxygen bottles located
In the lav
What is function of the HF?
It has auto tune
What is needed for an oceanic clearance
Route
Altitude
Mach speed
What are some of the items on the auxiliary bus
Microwave
Cockpit foot heaters
Pax convinces
Where are the safety valves
Rear pressure bulkhead
Where are CB panels 1&2
In the cockpit
Where CB panels 3&4
I’m the galley by the main entrance
Which CB are in the right side of the aircraft
2&4
Which CB panels are on the left side of the aircraft
1&3
What Kind of system does the electrical system prefer
Split bus system
Can you force close bus ties closes
No, can be forced open
What are the generator amp limits
400 on ground
400 inflight more then 1 gen
500 in flight 1 gen
600 max in flight for 5 min 1 gen
What kind of landing gear does the aircraft have
Trailing link landing gear
What happens when the manual gear extension is pulled
Unlocks are released
Accumulator is fired - good for 30 min from time of complete hydraulic failure
Does the anti skid work if complete hydraulic failure
Yes 1 anti skid cycle in normal break accumulator
How many EMER break applications are stored in the accumulator
6
What does a cyan L/R EMGINE FAULT CAS mean
1 of the FADEC channels on that side has failed
What controls the T2 probe heat
Engine A/I
Which spoilers are on the right hydraulic system
1,3,6,8
Which spoilers are on the left hydraulic system
2,4,5,7
What else in the battery compartment
Hydraulic pressure gage
Which tab on the left aileron is the trim tab
Inboard tab
where all does RAM airflow go
Cabin
PAC
Precooler
What are the dangers areas of the aircraft when engines/APU are running
15ft forward of engine intake
200ft aft of engine exhaust at idle
400ft aft of engine exhaust at TO
19 ft aft of APU exhaust
How far can the nose wheel go either side of center with the tiller
65*
When does the main cabin door Motor need to be cooled
After 3 door actuations in 3 mins needs to be cooled for 5 min
Thrust reverser limitations
Ground ops on paved surfaces
Do not deploy inflight
Do not back up the aircraft
Do not deploy in touch and goes
Reverse thrust above idle below 40 knots
How many degrees does the of steering does just the rudder pedals have
7
How May static wicks are on the airplane
26
How is the electrical power distributed through the aircraft
3 DC power controllers
2 secondary power controls
What is shed inflight when you go down to one gen
Aux busses
Will the batteries auto disconnect
Yes at 70 degrees C
What is the HP regulated at
36 psi
What is the IP regulated at
50 psi
After an aborted start, what temp does the engine need to be before attempting another start
350 to start, 250 for FADEC to introduce fuel
What is the purpose of the AUX hydraulic pump
Powers lower PCU in the event of right hydraulic system failure
What cause the DC fuel pumps to come on
Engine switch to run
Primary ejector pump failure
APU running
What holds the landing gear down and locked
The side brace actuator with an internal down locking mechanism
When will you get a gear warning
Flaps 30 gear not down
