Ch: 12 Flashcards
(131 cards)
1
Q
Crosswind Dry or Wet T/O
A
30
2
Q
Crosswind Contaminated >/= 150
A
15
3
Q
Crosswind Contaminated < 150
A
10
4
Q
Max Tailwind for T/O
A
10
5
Q
Max Ramp / Taxi Weight
A
31,050
6
Q
Max T/O Weight
A
30,800
7
Q
Max Landing Weight
A
27,575
8
Q
Max Operating Altitude
A
45,000
9
Q
Min Altitude Speedbrake Extension
A
500’
10
Q
Turbulent Air Penetration
A
225 / .73
11
Q
Max Landing Gear Operating (V LO)
A
210
12
Q
Max Flaps 1
A
250
13
Q
Max Flaps 2
A
200
14
Q
Max Flaps FULL
A
175
15
Q
Min Holding Icing
A
180
16
Q
APU Starter Operation
A
3 within 30m, 90s cooling
17
Q
Max Airspeed APU Start
A
305
18
Q
Max Altitude APU Start
A
20k
19
Q
Max APU Operating Altitude
A
30k
20
Q
AP min Enroute Altitude
A
1k
21
Q
AP Min ILS LPV Altitude
A
160
22
Q
AP Min Approach Alt
A
200
23
Q
AP T/O / Climb Altitude
A
400
24
Q
If not already engaged during TO, do not engage auto throttle ____ on the ground, and not until ____
A
Above 65
Above 400
25
Disengage auto throttle prior to landing without ____
FULL flaps
26
Voltage for engine start
Displayed Green
27
Max GPU voltage
30
28
Max Fuel Imbalance
400
29
Max time for PITOT/STATIC on ground
2 minutes
30
Approach Category
B
31
Max Tailwind Engine Start
10
32
Max Time TO Thrust AEO
5m
33
Max time TO Thrust OEI
10m
34
Max Time Reverse Thrust
5m
30s APU Running
35
Transient N1
106 for 20s
36
Transient N2
106 for 20s
37
Transient ITT
950 for 20s
38
Transient 20s Oil PSI
0-20 psi
39
Engine Start Attempts and Cooldown
2m, 5m, 30m
40
BAT only motoring limit
20s
41
BAT w/ gen assist or 1000A GPU
15
42
Starter Motoring Limit GPU 1500A
7s
43
Evacuation
Parking Brake - PF - ON
L & R Engine - PF - STOP
44
Start Malfunction On Ground
L/R Engine - LP - Stop
45
Smoke/Fire/Fume
O2 Mask and Goggles - Don/Emer
Crew Communication - Establish
46
Inflight Reverser Deploy
L/R TR Emer Stow - Press
47
Jammed Pitch/ Roll
Stabilizer Trim - Actuate
Yoke - Relax Pressure
Pitch/Roll Disconnect - Pull Until Latched
Operative Yoke - Identify
48
Stab Trim Runaway
AP/Trim/NWS Disc - PF - Press and Hold
49
Cabin Alt - Emer Descent
O2 Mask - Don/100%
Crew Communications - Establish
50
Battery O’Temp
L/R Batt - LP - Off
51
Engine Start Sequence Numbers
ITT Rise - Start
:20 - Oil Pressure Rise
40% N2 - N1 Rise
90s - Stable (57%, N1 Bugs, CAS Message Out)
52
FADEC Abort Start
1000 Degrees
Insufficient ITT
53
“IGN” means ____
Power applied, not necessarily igniting
54
NWS Degrees
81% Tiller
7% Pedals
88% Cumulative
55
Norm sets Bleed to HP ____
Above 37k
Above 25k w/ Anti Ice On
56
Emer Press Source and Conditions
HP Left Engine
ACM bleed leak or over temp
14.5k
57
Crew Brief Trigger
Crew Assembled
58
Arrival and Approach Brief Trigger
FL180 or prior to commencing
59
Departure Briefing Trigger
Cockpit Prep Checklist Complete
60
Takeoff Brief Trigger
Both Pilots seated
61
Acft Acceptance Flow Trigger
Pilot change
First Flight of Duty
Mx
62
Power On Checklist Trigger
Electrical power is established for the purpose of aircraft movement
63
Exterior Preflight Trigger
Acft Acceptance Flow Complete
64
Interior Preflight Flow Trigger
Acft Acceptance Flow completed
65
Cockpit Prep Flow Trigger
Power On Checklist complete (Postflight Flow for next flight)
66
Before Start Flow Trigger
Ready to Start Engines
67
Engine Start Trigger
Completion of Before Start Checklist
68
After Start Flow Trigger
Both Engines Started
69
Taxi Flow Trigger
Clear of obstacles, established on taxi route
70
Before TO Flow
Approaching TO Runway
71
After TO Flow Trigger
PF calls for Flap Retraction
72
10K Flow Trigger
10K
73
Nose Door Open L / R CAS message micro switch is located on?
4 mechanical latches
74
Cabin entry door lift motor is powered by?
Left Battery Bus
75
How long is the door held close by the motor?
10s
76
The emergency exit can be removed from inside or outside the aircraft?
Both
77
Baggage compartment heated or pressurized?
Not heated, not pressurized
78
1 battery turned off with generators online?
Battery is isolated, DC is powered by generators
79
REMOTE CB TRIPPED
CB not accessible by crew has tripped
80
Primary DC Sources
APU, GEN, EPU
81
Batteries during engine start?
Both batteries for every start (except windmilling)
82
Bus tie opens and closes?
Auto on ground, manually in flight
83
DC GEN OFF L / R
QRH
84
APU power is supplied to?
Bus if respective GEN is unavailable
85
BUS TIE CLOSED CAS displays?
In flight if bus tie button is selected closed, both GENs are online, and 5 minutes has elapsed.
86
When is the BUS TIE auto in flight?
Closed to Open if overcurrent
87
BATTERY O’ TEMP L / R temp?
63
88
ACFT main electrical system is?
Split bus system, 2 DC GENs, 2 DC Batteries (25V / 44A)
89
White AVAIL on the EPU switch means?
Connected and correct voltage (not necessarily correct amperage)
90
BAT voltage before engine start?
Indicate green digits
91
GEN switches for ENG start?
ON (off is checklist driven, normally ON)
92
INTERIOR button?
Adds or removes all cabin power except EMER ARM lights (3 overhead, 5 floor, 6 exit)
93
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)
94
TRU selected on means?
Windshield loses AC power so ALT can provide DC power (via TRU)
95
Will the interior lights illuminate on battery power?
Yes
96
The cabin entry light button is on which bus?
Right battery, 15 minute timer
97
PAX SAFETY with EMER ARM illuminates?
Interior and Exterior Emergency Lights
98
EMER lights, when ARMED, come on with?
Loss of DC power (ARM before BAT on)
5G impact
PAX SAFETY on
99
Red CAS messages do what when posted?
Flash until acknowledged by Master Warning button
100
Amber CAS messages do what when posted?
Flash amber and illuminate the steady amber Master Caution
101
How does the NO TAKEOFF message act
White CAS, then red w/ aural NO TAKEOFF when throttles are moved to TO
102
Engine Shutdown Inhibit (ESDI)
Activated when a pilot shuts down the engine or white ENGINE SHUTDOWN CAS posts
Deactivated when engine reaches idle
103
Max Fuel Capacity Over Wing and SPPR
11,390 / 10,720
104
SPPR Precheck must be completed?
Before every SPPR operation
105
CAS message for L ENG low fuel pressure?
FUEL BOOST PUMP ON L (amber)
106
Crossfeed from left tank to right engine may not occur if what CAS is displayed?
FUEL MOTIVE VALVE R (amber)
107
Boost Pump in NORM comes on?
Low fuel pressure
APU w/ R ENG off
Cross feed
Engine Start
108
APU Fire Light sequence
APU shuts down
BAG/APU fire bottle is discharged after 8s if APU FIRE button is not pressed
109
APU provides?
DC power
Bleed Air (service air, environmental/ pressurization)
110
APU oil level is monitored by?
CAS message (no gauge)
111
Check engine oil by?
OIL LEVEL LOW L / R CAS (amber)
112
N1 gauge inward pointing line indicates
FADEC setting for CRU
113
FADEC will abort start when stabilized IDLE is not achieved by?
90s
114
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
115
Prior to shutdown, the engine must be at idle power for ____ prior to shutdown
2 minutes
116
Generator cooling times
Eng idle with load < 75 amps for 4 minutes
Or
Wait 35 minutes before restart
117
____ squat switches must indicated on ground for TRs to deploy
All 3
118
TRs at idle by what speed?
65
119
Type of fire sensor in baggage
2 optical smoke sensors
120
FIRE DETECT FAIL L
Failure of the fire detect loop on left engine
121
Areas monitored by fire detection system
Engines (heat)
APU (heat)
Baggage Compartment (smoke)
122
L ENG FIRE button shuts off?
Fuel
Hyd
GEN
Bottles (armed)
TR
123
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
124
PRESS SOURCE controls bleed air
From engines for environmental/ pressurization
125
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
126
TAIL BLD LEAK
Only overtemp that won’t automatically close associated bleed air valve
127
ENG BLD AIR first enters
Pylor precooler
128
EMER PRESS auto when?
ACM Bleed air leak
ACM Overtemp
Cabin > 14500
129
IFR Fuel Reserve
1464
130
Emergency Fuel
1100
131
Runway length, width and slope
4k, 70, 2%
