CL350 Recurrent Oral Flashcards
Power ON HYD pumps order
L-ON R-ON Aux-AUTO PTU-AUTO L-AUTO R-AUTO
ENG switch to RUN
Fuel pump ON
FADEC initialized
PMA’s role
Permanent Magnet Alternator
Above 45%N2 it powers FADEC
Oxygen system
EPAV
2 bottles located in the lav.
Full 1850psi, 5439 liters.
Electro Pneumatic Actuating Valve.
EMER BRAKES
Pressure to all 4 wheels, no Anti-skid protection available.
Radar altimeter failure indication.
Red RA on PFD
When connecting external power to ship, to get ext pwr light AVAIL
Must have voltage and polarity
Multi function spoilers
MFS
Roll spoilers + flight spoilers
Panels 1,8 deploy up to 45deg
Emergency spoilers 1,2,7,8
Max positive pressure differential
9.4 Psid
Max negative pressure differential
-0.5 psid
FMS Appch prohibited w/o
APPR displayed
Ground spoilers
Panels 3,4,5,6
Deploy to 60 degree
Can only deploy on the ground
When they deploy the flight spoilers deploy also ( all 8 panels are up)
Dual fire detector loops feeds:
FIREX-CU
Pushing fire switch
Arms squib Shuts: FADEC Fuel Air Hydraulic Electric
Primary method of checking oil:
Secondary:
At the refuel panel
ROLS:Remote Oil Level Sensor
Between 5 and 30’ after shutdown.
Sec: sight gauge
AUX HYD pump pressure
2500-3350 psi
Cycles on and off to maintain pressure.
Radar:Collins multi-scan
Works best in auto mode.
Above FL200 you have 6000’ storm overflight protection
Underwater beacon for
CVR and FDR
Pax oxygen masks in auto:
Deploy at 14,500ft+/-500
Flow until cabin altitude is 9500 ft +/-500
Tick mark on the cabin manual rate is approximately:
300 fpm
Minimum fuel
2800lbs
With less than 1,000lbs per side, do not operate engines for more than 30’.
Oil cooler gets uncovered.
To/To on FD
Must have:
Vspeeds for T/O
Flaps for T/O
Engines on?
Total hydraulic failure
PCU’s lock so the cable connects to PCU and moves the flight control ( rudder + elevator only)
Surge tanks function
They allow for expansion of fuel without venting overboard
CABIN ALT
CAUTION
RED CAS
CAUTION @ 8500ft
RED CAS @ 9400ft
Mach trim available
In primary trim only.
Hydraulic Qty
Right
Left
Right 9 qts
Left 13 qts
DCMP Flaps out of 0
The DCMP HYD PUMPS will always run ( when in AUTO) @ 2800 psi.
Collector fuel tanks capacity.
500lbs each.
Min fuel for go around
IP AIR use
Intermediate pressure
Engine start
Environmental
Pressurization
Max 50 psi
HP air use
Anti-ice only
36psi
Gasper ceiling
All cold air
Cabin leak rate
800fpm
2 safety valves
1 underpressure (-0.5 psid) 1 overpressure (9.4 psid)
1 outflow valve
Located on belly of the plane ( unlocked for flight)
BUS TIE
You can FORCE OPEN a bus tie when you want.
You cannot FORCE CLOSE a bus tie manually if computer opened it.
Ships batteries
2 x 24V NiCad
44 Ahr
1 hr on Essential battery power.
Standby instrument duration
3.5 hrs
DOORS
Amber in air or ground.
Main Emergency exit Cargo Aft equipment bay Battery
DOORS
White or amber on ground.
Main entrance and cargo door.
Changes when Left engine switch to run.
HOT battery bus
Left batt: lights
Right batt: fuel panel
Failure of 1 generator
Aux buses shed in the air. Loose: Foot warmer R window heat A/C+D/C in the back
STBY INST
Recharged by RIGHT ESS BUS
Rudder limiter
Limits travel in relation to airspeed to not rip it.
Icing temp
OAT on the ground
TAT to use it
SAT not to use it
Cross bleed start the left engine above
9,000ft
APU won’t make enough pressure
If fire is detected
Fire switch illuminates Master warning light comes ON 3 chimes L(R) ENGINE FIRE CAS Red FIRE in the N1 indicator Aural L(R) ENGINE FIRE
Synoptic pages RED AMBER GREEN WHITE MAGENTA CYAN
Red:exceedance Amber: no flow or pressure Green: normal ops with flow White: no flow and operation normal Magenta: unknown data Cyan : advisory