Challenger 350 Flashcards
Max Tow Limit
120°
which doors are Monitored by the door warning system?
M E C A B Main Emergency Cargo. Aft Equipment Bay Battery
What happens when you turn on the battery switches
All busses are powered. IRS begins aligning. CVR turns on.
What is the function of the APU
Air and Electric
Where does the APU receive it’s fuel
Right collector tank
When will the passenger door caution turn amber
Left engine run switch on.
Max Fuel Load Pressure refueling. Over wing refueling
Pressure -14,150 Over Wing - 13,000
Take off thrust for the HTF7350 engine
7,372
Which EICAS message requires prompt action
Amber
Synoptic Colors: Amber, Green, White, Red
Amber- Component Failure. Green - Normal with flow. White - Normal without flow, Red - Exceedence
When will the FDR begin recording
Beacon on or Weight off Wheels
When will the emergency lights illuminate
Loss of right main bus power.
What is the purpose of the PTU
Gear retraction with loss of pressure in Left hydraulic system; Left Engine driven pump failure.
What controls the Landing gear
PSEU - Proximity Sensing Electronic Unit.
Which Primary flight control surface is not hydraulic
Ailerons
Which spoilers act as Multi- Function Spoilers
1,2 And 7,8
When are EICAS messages inhibited in flight
Takeoff - Airspeed above 80 kts until 400 feet. Landing - Below 400 feet until less than 40 kts.
Hydraulic Pressure for EDP and DCMP
EDP - 3,000 psi. DCMP - 2,800 psi
Standby Indicator battery life
3.5 hours
When will the Buss Tie open
2 or more generators online.
Which busses will remain powered during loss of all generators.
Essential busses and Battery busses.
How long will the Essential Busses and Battery busses last on battery power only
1 hour
When will the Auxiliary busses load shed
Single generator operation in flight.
Engine Fire and APU fire are controlled by what component
FIREX-CU Fire Detection and Extinguishing Control Unit.