Ch: 12 Flashcards
Crosswind Dry or Wet T/O
30
Crosswind Contaminated >/= 150
15
Crosswind Contaminated < 150
10
Max Tailwind for T/O
10
Max Ramp / Taxi Weight
31,050
Max T/O Weight
30,800
Max Landing Weight
27,575
Max Operating Altitude
45,000
Min Altitude Speedbrake Extension
500’
Turbulent Air Penetration
225 / .73
Max Landing Gear Operating (V LO)
210
Max Flaps 1
250
Max Flaps 2
200
Max Flaps FULL
175
Min Holding Icing
180
APU Starter Operation
3 within 30m, 90s cooling
Max Airspeed APU Start
305
Max Altitude APU Start
20k
Max APU Operating Altitude
30k
AP min Enroute Altitude
1k
AP Min ILS LPV Altitude
160
AP Min Approach Alt
200
AP T/O / Climb Altitude
400
If not already engaged during TO, do not engage auto throttle ____ on the ground, and not until ____
Above 65
Above 400
Disengage auto throttle prior to landing without ____
FULL flaps
Voltage for engine start
Displayed Green
Max GPU voltage
30
Max Fuel Imbalance
400
Max time for PITOT/STATIC on ground
2 minutes
Approach Category
B
Max Tailwind Engine Start
10
Max Time TO Thrust AEO
5m
Max time TO Thrust OEI
10m
Max Time Reverse Thrust
5m
30s APU Running
Transient N1
106 for 20s
Transient N2
106 for 20s
Transient ITT
950 for 20s
Transient 20s Oil PSI
0-20 psi
Engine Start Attempts and Cooldown
2m, 5m, 30m
BAT only motoring limit
20s
BAT w/ gen assist or 1000A GPU
15
Starter Motoring Limit GPU 1500A
7s
Evacuation
Parking Brake - PF - ON
L & R Engine - PF - STOP
Start Malfunction On Ground
L/R Engine - LP - Stop
Smoke/Fire/Fume
O2 Mask and Goggles - Don/Emer
Crew Communication - Establish
Inflight Reverser Deploy
L/R TR Emer Stow - Press
Jammed Pitch/ Roll
Stabilizer Trim - Actuate
Yoke - Relax Pressure
Pitch/Roll Disconnect - Pull Until Latched
Operative Yoke - Identify
Stab Trim Runaway
AP/Trim/NWS Disc - PF - Press and Hold
Cabin Alt - Emer Descent
O2 Mask - Don/100%
Crew Communications - Establish
Battery O’Temp
L/R Batt - LP - Off
Engine Start Sequence Numbers
ITT Rise - Start
:20 - Oil Pressure Rise
40% N2 - N1 Rise
90s - Stable (57%, N1 Bugs, CAS Message Out)
FADEC Abort Start
1000 Degrees
Insufficient ITT
“IGN” means ____
Power applied, not necessarily igniting
NWS Degrees
81% Tiller
7% Pedals
88% Cumulative
Norm sets Bleed to HP ____
Above 37k
Above 25k w/ Anti Ice On
Emer Press Source and Conditions
HP Left Engine
ACM bleed leak or over temp
14.5k
Crew Brief Trigger
Crew Assembled
Arrival and Approach Brief Trigger
FL180 or prior to commencing
Departure Briefing Trigger
Cockpit Prep Checklist Complete
Takeoff Brief Trigger
Both Pilots seated
Acft Acceptance Flow Trigger
Pilot change
First Flight of Duty
Mx
Power On Checklist Trigger
Electrical power is established for the purpose of aircraft movement
Exterior Preflight Trigger
Acft Acceptance Flow Complete
Interior Preflight Flow Trigger
Acft Acceptance Flow completed
Cockpit Prep Flow Trigger
Power On Checklist complete (Postflight Flow for next flight)
Before Start Flow Trigger
Ready to Start Engines
Engine Start Trigger
Completion of Before Start Checklist
After Start Flow Trigger
Both Engines Started
Taxi Flow Trigger
Clear of obstacles, established on taxi route
Before TO Flow
Approaching TO Runway
After TO Flow Trigger
PF calls for Flap Retraction
10K Flow Trigger
10K
Nose Door Open L / R CAS message micro switch is located on?
4 mechanical latches
Cabin entry door lift motor is powered by?
Left Battery Bus
How long is the door held close by the motor?
10s
The emergency exit can be removed from inside or outside the aircraft?
Both
Baggage compartment heated or pressurized?
Not heated, not pressurized
1 battery turned off with generators online?
Battery is isolated, DC is powered by generators
REMOTE CB TRIPPED
CB not accessible by crew has tripped
Primary DC Sources
APU, GEN, EPU
Batteries during engine start?
Both batteries for every start (except windmilling)
Bus tie opens and closes?
Auto on ground, manually in flight
DC GEN OFF L / R
QRH
APU power is supplied to?
Bus if respective GEN is unavailable
BUS TIE CLOSED CAS displays?
In flight if bus tie button is selected closed, both GENs are online, and 5 minutes has elapsed.
When is the BUS TIE auto in flight?
Closed to Open if overcurrent
BATTERY O’ TEMP L / R temp?
63
ACFT main electrical system is?
Split bus system, 2 DC GENs, 2 DC Batteries (25V / 44A)
White AVAIL on the EPU switch means?
Connected and correct voltage (not necessarily correct amperage)
BAT voltage before engine start?
Indicate green digits
GEN switches for ENG start?
ON (off is checklist driven, normally ON)
INTERIOR button?
Adds or removes all cabin power except EMER ARM lights (3 overhead, 5 floor, 6 exit)
Will the APU come online (be used) with the L GEN on?
No, L GEN will take priority and power the system (will power left side if R GEN is online)
TRU selected on means?
Windshield loses AC power so ALT can provide DC power (via TRU)
Will the interior lights illuminate on battery power?
Yes
The cabin entry light button is on which bus?
Right battery, 15 minute timer
PAX SAFETY with EMER ARM illuminates?
Interior and Exterior Emergency Lights
EMER lights, when ARMED, come on with?
Loss of DC power (ARM before BAT on)
5G impact
PAX SAFETY on
Red CAS messages do what when posted?
Flash until acknowledged by Master Warning button
Amber CAS messages do what when posted?
Flash amber and illuminate the steady amber Master Caution
How does the NO TAKEOFF message act
White CAS, then red w/ aural NO TAKEOFF when throttles are moved to TO
Engine Shutdown Inhibit (ESDI)
Activated when a pilot shuts down the engine or white ENGINE SHUTDOWN CAS posts
Deactivated when engine reaches idle
Max Fuel Capacity Over Wing and SPPR
11,390 / 10,720
SPPR Precheck must be completed?
Before every SPPR operation
CAS message for L ENG low fuel pressure?
FUEL BOOST PUMP ON L (amber)
Crossfeed from left tank to right engine may not occur if what CAS is displayed?
FUEL MOTIVE VALVE R (amber)
Boost Pump in NORM comes on?
Low fuel pressure
APU w/ R ENG off
Cross feed
Engine Start
APU Fire Light sequence
APU shuts down
BAG/APU fire bottle is discharged after 8s if APU FIRE button is not pressed
APU provides?
DC power
Bleed Air (service air, environmental/ pressurization)
APU oil level is monitored by?
CAS message (no gauge)
Check engine oil by?
OIL LEVEL LOW L / R CAS (amber)
N1 gauge inward pointing line indicates
FADEC setting for CRU
FADEC will abort start when stabilized IDLE is not achieved by?
90s
If the engine does not start, but the QRH has you dry motor, how long before you try another start?
2 minutes before the dry motor, 5 minutes before the start
Prior to shutdown, the engine must be at idle power for ____ prior to shutdown
2 minutes
Generator cooling times
Eng idle with load < 75 amps for 4 minutes
Or
Wait 35 minutes before restart
____ squat switches must indicated on ground for TRs to deploy
All 3
TRs at idle by what speed?
65
Type of fire sensor in baggage
2 optical smoke sensors
FIRE DETECT FAIL L
Failure of the fire detect loop on left engine
Areas monitored by fire detection system
Engines (heat)
APU (heat)
Baggage Compartment (smoke)
L ENG FIRE button shuts off?
Fuel
Hyd
GEN
Bottles (armed)
TR
BAGGAGE FIRE button causes?
BAG-APU fire bottle in the tail cone, and the low discharge function of the fire bottle in the nose, to discharge
PRESS SOURCE controls bleed air
From engines for environmental/ pressurization
L/R ENG BLD AIR NORM selects HP and LP when?
HP - low throttle setting, > 14500, 25k w/ anti-ice, 37k anytime, wing XFLOW, default if input signals are invalid
TAIL BLD LEAK
Only overtemp that won’t automatically close associated bleed air valve
ENG BLD AIR first enters
Pylor precooler
EMER PRESS auto when?
ACM Bleed air leak
ACM Overtemp
Cabin > 14500
IFR Fuel Reserve
1464
Emergency Fuel
1100
Runway length, width and slope
4k, 70, 2%
