1
Q
The minimum taxi strip width for a 180º turn is based on a maximum nose wheel deflection (80º) is
A
62’ (62 feet)
2
Q
Selecting the MASTER LIGHTING CONTROL knob to OFF position sets
A
Cockpit lighting for daylight conditions (Panel backlights off, switchlights full bright)
3
Q
To open the Cabin Door from the inside
A
4
Q
Engine and APU bleeds off and verify cabin is unpressurized.
A
Lift secondary latch release handle (cherry handle) and hold it.
Using the palm of an open hand, push primary handle up and outward.
Let go of both, and the door will open
5
Q
Opening the Baggage Compartment door from the inside you should
A
Rotate door handle up and aft to unlock door, using hand grips, pull door inward and slide upward on tracks
6
Q
Crew and passenger oxygen masks are not approved for use above
A
40,000’ cabin altitude
7
Q
Tire speed limitation will be exceeded if touchdown is made in excess of
A
195 knots groundspeed
8
Q
The total number of aircraft occupants shall not exceed
A
22
9
Q
What is the Maximum Ramp weight
A
91,400 Ibs.
10
Q
The potable water tank can be serviced
A
Internally and externally to 30 US Gallons
11
Q
If any items are missing from the aircraft on pre-flight (external), refer to the
A
CDL
12
Q
WINDSHEAR is active
A
During take-off until 1500’ AGL
During approach from 1500’ to 10’ AGL
During missed approach until 1500’ AGL
13
Q
WINDSHEAR AMBER message on the PFD during take-off
A
Increasing Performance
14
Q
WINDSHEAR RED message on the PFD during take-off
A
Decreasing Performance
15
Q
The Honeywell Planeview CMF (Communication Management Function) communicates by way of
A
Land based ACARS VHF network or Satellite
16
Q
The CMF attempts to send a message or request by way of all available transmission channels and modes for a period of
A
Six Minutes
17
Q
To access the Planeview CMF displays
A
Push the DLK (datalink) function key on the MCDU
18
Q
ATC will forward a PDC (Pre-Departure Clearance) to GDC for storage approximately
A
20 minutes prior to flight plan filed departure time
19
Q
TOLD (Takeoff and Landing data) MCDU (FMS) performance has been evaluated by the FAA for accuracy and is
A
Acceptable for use according to AFM limitations
20
Q
The maximum runway slope approved for take-off and landing operations is
A
+2% (uphill) and 2% downhill
21
Q
Why would you be cautious when maneuvering in tight spaces when turning?
A
Swept wing growth
22
Q
What is the Maximum Take-Off Weight?
A
91,000 Ibs.
23
Q
What is the Maximum ZFW?
A
54,500 Ibs. (52,000 – JAA)
24
Q
What is the Max Landing Weight?
A
75,300 Ibs.
25
What is the Minimum Control Speed Air?
112 KCAS
26
Additional evacuation trained crew member is required when?
10 or more passengers are onboard
27
If you observe ON BAT, on the IRS switch, what does this mean?
IRS is not on its primary electrical source.
28
What is required for “In-Flight” IRS Alignment?
GPS
29
What powers the GPS antenna?
MAU via GPS MAU card
30
How can you make an in-flight alignment go faster?
Make turns, accelerate / decelerate
31
How many GPS’s needed for alignment?
One valid GPS
32
Polar Navigation is approved provided
True heading is selected prior to N73º and S60º Latitude
33
If a RAIM check is required where will you find the MENU?
NAV menu / pos sensors / GPS / LSK 6
34
What is the default display on DU2?
MAP
PRIMARY ENGINE INSTRUMENTS
SECONDARY ENGINE INSTRUMENTS
35
Change DU2 2/3 to ECS/PRESS
Display Controller / 2/3 / DU2 Main / Next / ECS Press
Or CCD Menu ECS/PRESS
36
How do you bring up the CHK LST on DU3 Lower?
Use either DISP Cont / Push CHK LST button
Or CCD Menu CHECKLIST
37
Change DU1 lower to TRAFFIC
Display Conroller / 1/6 / DU1 Lower {2L} / Traffic
Use CCD – DU1 - Menu TRAFFIC
38
What are the power sources for MAU’s?
Check MAU Function / Failure Matrix IN QRH
39
How many power sources does each MAU have?
Four (4)
40
How many CB’s for each MAU
Four (4)
41
If DU1 fails, what happens?
DU2 switches to PFD Display
42
If DU2 and DU3 fail, what do you have?
PFD on DU1 and DU4
43
Assuming DU 2 and DU 3 have failed, how do you get MAP on DU1 or DU4?
On Disp Cont, push and hold the 2/3 button for 3 seconds, push MAP on respective Disp Cont you want the MAP to appear
Synoptic pages may then be accessed using CCD
44
Why are some CB’s red and other CB’s black?
Red circuit breakers indicate ESS DC bus power Black circuit breakers indicate MAIN DC bus power
45
Power Source for DU1 / DU4?
L ESS (DU1)
R ESS (DU4)
46
Power source for DU2 and DU3?
DU2 is (L MAIN / L ESS)
DU3 is (R MAIN / R ESS)
PLANEVIEW (RNP, EPU, LPV, TEMPERATURE COMPENSATION)
47
Place CHECKLIST on DU1 Lower
On the Disp Cont push 1/6 / select DU1 Lower / Next / Checklist {3}
Or CCD - DU1- Menu – CHECKLIST
48
On which display are WX RADAR / and TERRAIN selected by default?
MAP
49
How do you select WX / TER on the PFD / HSI?
Display Cont / PFD / Box WX or TER
50
Can you use CCD to select WX / TER on the PFD?
No
51
On initial power-up what items are boxed by default on MAP?
TERRAIN / OBSTACLES / TRAFFIC / WEATHER
52
The MAP display increases the Pilot’s
Situational Awareness
53
How do you display runway LOCALIZER feathers?
Select AIRPORTS on MAP DATA and scroll down the range until the feathers appear
54
How is FMS active leg displayed on MAP?
Magenta line
55
When the current aircraft position is not on the map, the aircraft symbol changes to
Magenta color and is placed on the edge of the map
56
Auto speeds (V1, VR, V2) display up to what altitude?
1500 feet
57
F/D CMD bar on T/O is at what pitch?
FMS will calculate nose up angle based on V2+10 kts speed (two engine)
Single engine based on V2 to V2+10 kts
58
Using auto throttles on take-off “HOLD” will appear on PFD at what speed?
60 knots
59
What is the Pilot Not Flying callout at 60 knots?
“Power Set” or “EPR low, increase power”
60
Auto throttles (power levers) stay in HOLD mode up to what altitude?
400 feet
61
Can we change the range on the HSI?
YES, Max in WX / 300 (WX boxed), Max in TERRAIN / 500 (TER boxed)
62
If the abnormal of DU1 and DU4 in PFD mode exists (DU2 & DU3 are blank) can the Left Seat select MAP on DU1 after the Right Seat has selected MAP on DU4?
No, the system must show at least one PFD
63
If you are down to only one DU, what will it display?
PFD
EICAS (Alternate Primary Engine Inst + CAS)
64
When down to only one DU, can you change it to MAP?
No
65
Which DU’s can the Pilot control?
DU’s 1, 2 & 3
66
Which DU’s can the Co-Pilot control?
DU’s 2, 3 & 4
67
Where do you find Check Charts date?
MAP / CHARTS / TOP WORLD CHARTS (upper left)
68
Can you check the charts date in the CMC?
YES
CMC / DB CONFIG / NEXT
69
How do you know your take-off speeds have been calculated?
(MCDU) / FPL / Page 1
T/O SPD and Vertical Performance numbers will be displayed
Display Controller / FLT REF button
70
AUTO VSPD 1 versus AUTO VSPD 2
AUTO VSPD1 indicates auto speeds from FMS 1
AUTO VSPD2 indicates auto speeds from FMS 2
If comparator problem on ground get Amber VSPD on Speed tape and speeds unbox
71
When will FMS auto speeds change after take-off?
When flap position is changed OR
When a new vertical mode (i.e. FLCH, ASEL) is selected
72
An AGM failure will be indicated
As a Red “X” on any Display Unit
73
For take-off, what 5 items are checked on the Guidance Panel / PFD
GUIDANCE PANEL: ALTITUDE SET, LATERAL MODE (HDG, LNAV ETC), V2 SPEED, MAN HEADING / LNAV (After selecting TOGA, for direction control) PFD CMD-L (For left seat take-off)
PFD: V2, Lateral mode: HDG / FMS etc, Performance mode: TO, Vertical mode: TO, ALT
74
When is it a good time to switch to the Electronic Checklist?
BEFORE STARTING ENGINES CHECKLIST
Available after APU start with AC power
75
Can you defer items in the Electronic Checklist?
Yes, option at bottom of checklist synoptic
76
How do you get back to Electronic Checklist deferred item
Recall
77
Can you “undo” a checklist item?
YES…
78
How do you override a checklist?
Select CHECKLIST
Go to bottom
Select CHECKLIST FUNCTION
Select OVERRIDE
79
How do you check that your charts are up to date?
CHARTS (far left drop down menu) / REVISION INFO
CMC / DB CONFIG
80
Heading information to the SFD (Standby Flight Display) is from what source?
Magnetometer
81
What is normal order of heading source information for the EBDI?
IRS1 / IRS2 / Magnetometer
82
What are the STBY instruments called?
SFD and EBDI
83
What is the power source for STBY instruments?
EMER FLT INST BUS (E-BATTS)
84
What does “ooo” presentation mean on the STBY INST menus?
SUBMENUS for that item
85
What HDG Mode should be selected on the EBDI?
HDG 1 / AUTO
86
Which NAV radio(s) send info to EBDI?
NAV 1 / NAV 2
87
Can you take off with a red flag on the EBDI?
Check MEL
88
Where do you perform Radio Tuning?
MCDU’s
RADIO button
PROGRESS button (optional for some VHF NAV frequencies)
89
Auto Speed Schedule?
200 kts. – ATA (Airport Traffic Area)
250 kts. > ATA < 10,000’
300 kts. > 10,000’
90
What is the power logic for autothrottles when using FLCH?
If next altitude is > 6000’ autothrottles uses CLB EPR / IDLE
If next altitude is < 6000’ autothrottles uses less than CLB EPR / more than IDLE
91
MASTER WARNING INHIBIT inhibits all tones except for
RED messages
Couple Data invalid (LATERAL or VERTICAL)
Cat II Invalid
LPV Unavailable
92
MASTER WARNING INHIBIT light will extinguish on take-off when?
400’ RA
93
How do you get to ECS 2/3 Synoptic?
On the Disp Cont push 2/3 / select ECS
CCD –DU2 or DU3 – Menu – ECS/PRESS
94
What should be lower – RNP or EPU?
EPU
95
The RNP value should always be
Greater than or equal to EPU
96
If EPU is greater than RNP what annunciation will you get?
CDI turns amber
TRACK on VSD changes to amber and flashes for 3 seconds
DEGRADE on HSI
97
What is the RNP for APPROACH / TERMINAL / ENROUTE?
0.3 / 1.0 / 2.0
Terminal enhanced goes to 0.3 at initial approach fix
98
How do you manually set RNP?
FMS / PROG / NEXT / 1L (RNP) / MANUAL
99
How do you delete a manually set RNP?
FMS / PROG / NEXT / DELETE / 1L
100
The RNP value for Approach is
0.3
101
If RNP is 1.0, what does full scale deflection of CDI indicate?
One mile of course
102
When does RNP go to Terminal?
Within 30 miles of departure or destination
First fix of a STAR
SID stays in Terminal until last fix of SID
103
The APPROACH annunciation will appear?
2 NM from the FAF (FMS based approach)
104
RNP/EPU values display only when used with what color NAV data?
Blue (FMS)
105
When VGP mode is used, vertical guidance will ignore
Altitude pre selector
106
RAIM (Receiver Autonomous Integrity Monitoring)?
A monitor that determines if GPS data is good enough to use – requires 5 satellites with good geometry. Found on NAV – Pos Sensors – GPS Status Page 2
107
RNAV – RNAV(RNP) – AR – SBAS – LPV
RNAV – waypoint to waypoint navigation
RNAV (RNP) – is RNAV with designated Performance Boundaries
AR – Authorization Required
SBAS – Space Based Augmentation System
LPV – Localizer Performance with Vertical Guidance
108
LPV stands for
Localizer Performance with Vertical Guidance
109
Hybrid IRS provides
Integrated GPS data to improve accelerometer and gyro performance
Much lower EPU and drift rate than previous
110
IRS Hybrid IRS is required
To support precision like GPS approaches, such as those flown to LPV
minimums
111
LPV approaches need
SBAS (Space Based Augmentation System) to achieve GPS accuracy and availability
112
When is ACTUAL TRUE ALTITUDE higher than INDICATED BAROMETRIC ALTITUDE?
Actual temperature is HOTTER than ISA temperature
113
When is ACTUAL TRUE ALTITUDE lower than INDICATED BAROMETRIC ALTITUDE?
Actual temperature is COLDER than ISA temperature
114
When would you apply TEMPERATURE COMPENSATION procedure?
When actual temperature is COLDER than ISA
WITH ATC COORDINATION
115
How do you activate Temperature Compensation to COLD on the MCDU?
Nav/Next
Maint/Next
Setup/Config/Next
Confirm Temp Comp Config at LSK 3L set to “COLD”
116
How do you apply Temperature Compensation to APPROACH WAYPOINT values?
Select Landing INIT on MCDU
Enter OAT at LSK 4L
Select Temp Comp at LSK 6L
Select ACTIVATE at LSK 6R
117
How do you calculate the CHART MINIMUM (DA/MDA) to a Temperature Compensation value?
Select Landing INIT on MCDU
Enter OAT at LSK 4L
Select Temp Comp at LSK 6L
Select Next key until MDA appears at LSK 1L
Enter CHART MINIMA VALUE at LSK 1L
Temp Compensation value calculation will appear at LSK 1R
Enter Temp Compensation value on Display Controller FLT REF page
118
The heading sources to the EBDI (Electronic Bearing Distance Indicator) are
IRS 1, IRS 2, Magnetic from the magnetometer
119
When operating single engine only, the TCAS must be RESET to what mode?
“TA” only
120
When flying approaches, the PF should have which page displayed on his Display Controller?
NAV; So that FMS mode maybe re-selected on “go-around”
FMS for Blue Data. Nav for GREEN
121
DEGRADE (amber) is an alert annunciation. It is displayed when?
122
The FMS cannot guarantee the position accuracy for the present phase of flight due to sensor availability (i.e. GPS / VOR / DME)
Example EPU exceeds RNP
123
What would you do if DEGRADE is annunciated during an FMS-based approach (blue data)?
Execute a missed approach
124
For the FMS to autotune the localizer frequency, the
Radios need to be in Autotune
125
Can the FMS be used to fly Localizer approaches?
No, you cannot use the FMS to fly Localizer based approaches
126
If you get a “Traffic-Climb” Alert, and ATC says DESCEND, what would you do?
Climb
127
What is the call to ATC for a TCAS Resolution Advisory?
TCAS RA
128
How do you check TERRAIN DATA BASE date on CMC?
MAP PAGE / MENU / CMC / DB CONFIG
129
WINDSHEAR warning is active
On Take-Off from Ground to 1500’ AGL
On Landing from 1500’ to 10’ AGL
On Missed Approach up to 1500” AGL
130
Can you inhibit WINDSHEAR callout function?
NO
131
Obstacles, when selected for display, must be a minimum of _____ feet to appear on the MAP display
1000’ AGL
132
TAWS ALERT pops up in HSI and changes to what range?
5 mile ½ range (10 Mile Range)
133
When will the ground proximity tape appear on the bottom of the PFD ALTITUDE TAPE?
600 feet AGL (RADIO ALTITUDE)
134
Radio Altitude is active between which altitudes
-20’ to 2500’
RA should read -5 on Ground
135
If flying in LNAV (FMS) mode, will track be displayed on the VSD?
NO
The terrain displayed is UNDER the FLIGHT PLAN ROUTE (solid magenta line)
136
When flying in HEADING mode, the aircraft TRACK is displayed on the MAP as?
A dashed MAGENTA line
137
When flying in HEADING mode, what terrain is displayed on the VSD?
The terrain located under the TRACK LINE (dashed Magenta line)
TRACK will be displayed under the VSD display
138
A dashed MAGENTA line on the VSD depicts the aircraft
Flight path Angle (vertical flight path)
139
What does the word TRACK displayed on the VSD mean?
The terrain displayed is UNDER the MAP TRACK LINE (dashed Magenta line)
140
The maximum demonstrated altitude loss for coupled go-around is
60 feet
141
Actual track from the IRS is displayed on the MAP when the ground speed is greater than
20 knots
142
During the tracking phase of an ILS approach the system uses landing aid flight path information from both the pilot and copilot called ILS DUAL COUPLED APPROACH MODE. This phase is automatically initiated at what altitude?
1200 ft. Radio Altitude
143
What does a BLACK LINE on the VSD mean?
Aircraft not flying the Flight Plan Route
144
If the aircraft experiences GPWS and a TCAS event simultaneously, what takes priority?
GPWS event
145
Can you select Weather on the 360 HSI display on the PFD?
NO
146
The glideslope cancel switch on the Master Warning Panel will cancel glideslope alerts when activated below
2000’ AGL
147
The glideslope cancel switch on the Master Warning Panel when activated, is automatically reset when the aircraft descends below _____feet or climbs above _____feet AGL
30’ / 2000’
148
Can you use the Autothrottle on a Single Engine Approach?
NO
149
Can you use the Autopilot on a Single Engine Approach?
YES, but it must be disconnected for Go-Around
150
TOGA function is available only when the airplane is?
Below 16,500” MSL and
Below 2000’ AGL
Or the airspeed is less than 200 knots
151
The HMG (Hydraulic Motor Generator) provides
AC Power to the AUX TRU and Standby AC Buses
152
What is the normal AC power source for the AUX TRU and ESS AC bus?
L MAIN AC bus
153
If the L MAIN AC bus is unpowered, will the AUX TRU and ESS AC bus automatically switch
154
to another power source?
YES. Both switch to the R MAIN AC bus
155
What is the “DEAD BUS” power logic for the AUX TRU?
ESS bus before MAIN
LEFT side before Right side
156
What is the purpose of the E-inverter?
Provides AC Power for the ESS AC bus (if the ESS AC bus loses power)
157
What is the normal position of the E INV switch?
AUTO
158
How long do you wait between selections of L ESS and R ESS when using HMG?
10 seconds
159
The 60Hz converter can be used to
Power the outlets in the galley and passenger cabin
160
If you lose L MAIN AC BUS power, what happens automatically?
AUX TRU transfers to R MAIN AC BUS
AUX TRU Powers L ESS DC Bus
ESS AC bus transfers to R MAIN AC bus
161
How would you power L MAIN DC BUS for the above situation?
Use the L TRU switch / Push / Observe RAC (switch capsule)
162
What two (2) sources can power ESS DC buses simultaneously?
L / R Main batteries
AUX TRU (when powered by the HMG)
163
When do you push the RESET switch?
CAS MSG / CHECKLIST says to push it
164
The MAIN BATTERY switches illuminate ON when the MAIN BATTERIES are being used
Powering the ESS buses (batteries are being used)
When starting the APU
When AUX pump is operating
165
Describe a BREAK POWER TRANSFER
A momentary interruption of power to one or several busses
166
All automatic power transfers will be NBPT’s except between
External AC power and APU generator
167
What is the function of BUS TIE ISLN SWITCH?
Prevents / Allows alternate power sources to power failed bus side?
Allows you to isolate buses
168
What is the color of the GEN switch if the generator is turned off?
Black – Grey
169
What appears in the GEN switch if the GEN FAILED?
Amber “OFF”
170
The ground service bus may be powered on the ground by
R MAIN DC BUS, when available
R battery or directly from external DC power receptacle when using one of three switches
171
How can you tell if GND SVC Bus is powered?
Beacon is illuminated
172
Can you look at the Electrical Panel and tell if the GND SVC BUS is powered
GND SVC BUS capsule will have “ON” illuminated
173
Is GND SVC BUS powered in flight? And by what?
YES
R MAIN DC bus
174
How many GND SVC BUS switches are there and where are they located?
3 (three)
Forward External Switch Panel Access Door
Tail compartment
Remote Refuel Panel behind Captain seat in cockpit
175
How do you know the generator has failed if looking at the synoptic?
GEN is outlined in Amber
176
Will GND SVC BUS turn off automatically?
Yes, when main cabin door, forward external switch panel access door and tail compartment door are all closed
177
How many E-Batts are there
Four (4)
178
What do the E-Batts power?
Avionics Power – (2)
Emergency Lighting – (2)
179
What do the Avionics E-Batts Power?
Clocks
STBY INST Panel (SFD / EBDI)
Gear Handle and Indicator
MCDU’s 1 & 3
CAPT Audio Panel
180
Emergency Batteries (E-Batts) when armed will activate when
An ESS DC bus power drops below twenty volts
181
With E-Batts on, what appears on MCDU 1 & MCDU 3?
MCDU 1 – STBY ENG INST & FUEL
MCDU 3 – BACK UP RADIOS (VHF 1 COM / NAV) and ATC 1
182
When the aircraft operates on emergency batteries the crew can only tune
COM 1 / NAV 1 / ATC 1 on MCDU 3
183
In emergency battery mode the
Cockpit speakers are not available
184
ACP on E BATTS – illuminated
Captain – COM 1 / SPKR ICS + Phone + MIC
185
Can you plug in AC & DC External Power at the same time?
Yes
186
Which external power source has priority? AC or DC external power?
AC
187
If you remove AC external power will it Auto Switch to DC external power?
No, you have to deselect EXT PWR switch and RESELECT for DC EXT PWR
188
Why would you use DC EXT PWR?
Start APU with low battery voltage
189
How many lights / items appear during an APU fire test?
Eight (8)
2 OVERHEAD / 4 MASTER CAUTION PANEL / 2 CAS
190
The APU is guaranteed to start at or below
39,000’ (may start up to 43,000’)
191
What is the max operating altitude of the APU?
45,000’
192
The APU generator will come on when it has reached
99% after 2 seconds
193
After APU start and selecting APU BLEED AIR, when does the Isolation Valve automatically open?
APU load control valve is inhibited OFF during APU start and 1 minute after APU is online unless EGT before start > 150º. There is no delay when airborne.
194
What is the difference between ESSENTIAL and NON ESSENTIAL APU mode?
ESSENTIAL – Air
NON ESSENTIAL – Ground(15 minutes after landing)
Not all AUTO shutdowns are active in ESSENTIAL mode
195
If the APU is started in flight what mode is the APU in?
ESSENTIAL mode
196
If started in the air, the APU will remain in ESSENTIAL mode for how long after landing?
Stays in ESSENTIAL mode 15 minutes after landing
197
APU ESSENTIAL and NON ESSENTIAL modes depend upon which system
WOW – weight on wheels
198
What does APU ESSENTIAL CAS message mean?
APU is operating in Essential mode
A Non Essential Shutdown signal is sensed
The APU will continue operating
199
If the APU is operating in essential mode while the aircraft is airborne, the APU will
Continue to operate in Essential mode for 15 minutes after landing
200
What CAS message should not be displayed after APU Fire Test
Fire Bottle Discharged
201
The APU Surge Control Valve operates at what altitude and above?
16,500” and above to prevent high altitude compressor stall
202
The APU Bleed Air Augmentation Valve (BAAV) operates at what altitude?
35,000’ and higher – allows 400ºF air into the APU intake for APU starting
203
The APU Bleed Air Augmentation Valve (BAAV) delays the APU start
For 15 seconds to allow the APU to warm before starting at altitude
204
What temperature range is the APU oil tank heated?
+21ºC to +43ºC regardless of whether the APU is in use
205
Depressing the APU STOP switch causes the APU
Shutdown by simulating an overspeed
206
How do you perform an immediate APU shutdown?
Push Master Switch
207
While flying at 41,000’ an emergency condition requires operation on main batteries only
If the APU is available for use, you should:
Immediately descend to the APU start envelope altitude (39,000 feet or below)
208
What are the APU starter limitations when using aircraft batteries?
3 (three) start attempts
Then 1 (one) hour cool down period
209
What are the APU starter limitations when using DC external power?
3 (three) start attempts
A 15 (fifteen) minute cool down is required between start attempts to protect aircraft wiring. This allows the electrical feeder cable from the external power receptacle to the APU starter to cool
Then 1 (one) hour cool down
210
The engine tailwind start limit is
20 knots
211
How many ignitors are used for normal engine ground start?
One (1)
212
How many ignitors are used with the Continuous Ignition Switch?
Two (2)
213
What does FADEC stand for?
Full Authority Digital Electronic Engine Control
214
FADEC has how many power channels?
2 (Channel A and Channel B)
215
What are the FADEC power sources during engine start prior to its using its own generator at 35% HP RPM?
Channel A – L ESS
Channel B – R ESS
216
The FADEC is powered by
A dedicated generator on the accessory gear box
217
How many FADEC channels per engine?
Two (2) – A/B
218
If the FADAC detects an anomaly during start, the start will be
Aborted
219
If FADEC detects a failure which prevents continued operation in the primary Engine Pressure Ratio (EPR) control mode, it will automatically perform a
Soft reversion to the Alternate (LP) control mode (AMBER ALT)
220
Does the engine have different idle settings? If so, what are they?
Yes LO/HI
221
When is LO idle and HI idle active?
LO idle – Flaps < 22º
HIGH idle – Flaps > 22º
222
What is the Continuous Ignition limitation?
There is no limitation
223
The time limit for Maximum Continuous Power is
Unrestricted
224
If an engine reverts to LP control, what indications will be in view? What procedure must be performed in this situation?
At first. ALT (amber) is displayed. This is a SOFT reversion
You must change both engines to BLUE ALT control. This is a HARD reversion
225
Can you use Auto Throttles in ALT control?
NO
226
What are four (4) ways to open the Bleed AIR Isolation valve?
Start Master selected ON
Crank Master selected ON
APU Bleed Air switch selected ON
Manually select the Isolation Valve ON
227
The Temperature Scale on the Engine Start Synoptic switches from what to what after engine start?
From 800º to 1000º temperature scale
228
What is the basic function of the Crank Master Switch?
Motor Engine
229
What is the Engine Starter Duty Cycle?
Three (3) attempts
Wait 15 seconds between start attempts
Wait 15 minutes after 3 start attempts
230
Which AC pack shuts off automatically with the Master Crank or Master Start switch?
Right AC Pack
231
Which AC pack shuts off automatically with the Individual Engine Start Switch?
Left AC Pack
232
What does “Start Switch Configuration” CAS message mean?
Both Crank and Start Master switches selected ON simultaneously
233
What does “SAV Maintenance” CAS message mean?
AMBER CAS message (QRH)
Can occur if start is attempted without air source, or if start switch is not pressed for sufficient time
234
What does “Throttle Configuration” CAS message mean?
AMBER CAS message (QRH)
Power lever is not at idle position prior to engine start
235
What two (2) system sources are required to unlock the T / R?
Hydraulic
Electric
236
When you push the ENG START switch, what indication do you look for?
SVO ICON on Primary Engine Instruments and ENG START synoptic
237
Fuel Control switch is selected ON, what indication do you look for?
IGN ICON on primary engine instruments
238
The preferred Engine Airstart procedure and limitations are?
AIRSTART Automatic and at or below 25,000’
239
When do the Auto Throttles retard (RTD) on landing?
50 feet RA
240
What does “L / R Throttle Configuration” CAS message indicate?
AMBER CAS message (QRH)
Power lever is not at IDLE position during engine start
241
Will the engine start with a “L / R Throttle Configuration” CAS message?
Yes, but it will accelerate to power lever setting immediately upon start
242
How do you display STBY engine information?
MCDU 1 / MENU / STBY ENG
243
The reversers should be at idle Reverse by what speed?
60 knots
244
MAXIMUM REVERSE time limit is
30 seconds
245
FADEC keeps the engine at high idle for _____ seconds on landing to facilitate the use of thrust reversers on touchdown?
5 (five) seconds
246
If an engine maintenance message “LTD” is present and if the cause of the fault is an EEC / P30 fault, this should be considered a
No Dispatch condition
247
What is the procedure for a Fire Detect Loop A Fault on the Right engine?
Disable (turn off) LOOP A on the right engine
Perform a RIGHT ENGINE FIRE TEST to verify remaining LOOP B is functioning
248
The pilot would be alerted to single activated fire loop by a
LOOP switch segment illuminated red on the Fire Test Switch coupled with a red ENGINE
FIRE LOOP ALERT warning message displayed on the CAS
249
How many items are there for a Fire Test?
Eight (8)
250
How many items are there for a Fire Detection Fault Test?
Eight (8)
251
Which bottle is the APU Fire bottle?
Left(#2) FIRE BOTTLE
252
Why do you use Fire Bottle 1 for fire?
To save no 2 FIRE BOTTLE for possible APU FIRE
253
If a fire is detected in the APU enclosure, what will happen automatically?
FUEL is automatically shut off at the APU fuel control and at the fuel tank
254
If a fire is detected in the APU enclosure, will the FIRE Bottle automatically discharge?
NO, the crew must discharge the FIRE BOTTLE using the APU discharge switch located on the APU Control Panel
255
Pulling the ENG FIRE HANDLE shuts off
FUEL
HYDRAULICS
ELECTRICS (ENG IDG Generator)
256
What does a red “RED PYLON HOT” CAS message indicate?
Bleed Air Leak
250º F
257
What does the amber “HOT” CAS message indicate? What temperature causes indication?
Electrical Overheat
150º F
258
What control would be used to evacuate smoke from the baggage compartment?
The EMERGENCY SMOKE EVACUATION valve
259
Rotating the EMERGENCY SMOKE EVACUATION valve to EVAC smoke position performs what action?
Deflates the baggage door seal allowing smoke to exit around the baggage door
260
What extinguisher is most effective against electrical fires
Halon extinguisher
261
Once smoke is evacuated from the baggage compartment, can the baggage door seal be reinflated?
YES, by rotating handle to the NORMAL OPS position
262
Do the lavatory / lavatories have fire protection?
Yes, each cabin lavatory is equipped with an integrated fire detector and extinguisher unit mounted over lavatory trash bins. The unit consists of a container holding extinguishing agent and discharge tubes capped with a fusible alloy.
The discharge tube caps will melt (170 - 177°F), and the extinguishing agent will be directed into the trash bin
263
Which fuel Hopper L / R has the APU fuel supply line?
Left
264
Which fuel Hopper L / R has the fuel tank temperature sensor?
Both for HFRS
265
A fuel quantity system test results in the following indications
7000 / 7000 / 14000 in amber inverse video on all synoptic pages displaying fuel information and an amber “L – R FUEL LEVEL LOW” CAS message is displayed
266
How do you preset the quantity of fuel being added to the aircraft?
Remote Fuel Panel cockpit, set total quantity of desired fuel load
267
If electrical power is lost to the fuel pumps, will the engines still run?
Suction Feed is available below 20,000’
268
If automatic refuelling has been accomplished since the last flight you should check that the
Auto refuel switch on the Remote Refuelling Panel is selected off
269
On Emergency Batteries (E-BATTS) the pilot can determine the fuel quantity on
MCDU 1 (Multi Function Display Unit No.1)
270
How do you use the Remote Fuel Panel?
Set fuel quantity desired
Select AUTO
Asterisk (*) displays next to amount to be added
271
Which manual describes FUELING PROCEDURES?
AOM Chapter 9 Handling & Servicing Procedures
09-02-10 Fuel Servicing
272
How do you transfer fuel from tank to tank?
User Inter Tank Valve
273
How do you balance fuel using the INTER TANK VALVE?
Rotate Rudder Trim in direction of HEAVY WING, resulting in ½ trapezoid displacement, then open INTER TANK VALVE
274
During pressure refueling, the FQSC (Fuel Quantity Signal Conditioner) monitors intertank quantities. What happens if an imbalance of 500 lbs. / 226 Kg occurs?
The FQSC interrupts fueling to the HEAVY wing until the imbalance is reduced to 100 lbs. / 45 kg. a fuel level low probe is installed in each fuel hopper.
275
At what fuel level will a “FUEL LEVEL LOW” CAS message appear?
650 Ibs. / 295 kg
276
How much fuel does each fuel hopper contain?
190 US gallons / 1283 Ibs.
277
If you are balancing fuel what is the CAS message displayed when you open X-FLOW Valve
Blue “FUEL X-FLOW VALVE OPEN”
After 5 minutes the CAS changes to an AMBER “FUEL X-FLOW VALVE OPEN”
278
If fuel is allowed to go out of balance by more than 1000 Ibs. in flight how will the crew be notified?
Blue “FUEL IMBALANCE” CAS
279
What are the in flight and ground imbalance limits?
Ground - 1,000 lbs.
In Flight - 2,000 Ibs.
280
What is the maximum fuel load at normal fuel density?
41,300 Ibs.
281
The Heated Fuel Return System (HFRS) opens at 0º C and stops at +10ºC. What else is the FADEC monitoring to open the Fuel Return to Tank Valve (FRTT)?
The cockpit overhead switch is selected to AUTO
The engine fire handle stowed (not pulled)
Engine LOW Fuel Pressure not indicated
Engine LOW Fuel Quantity not indicated
Engine FUEL FLOW is less than 2,250 Ibs. per engine
Fuel Filter not blocked
Fuel X-Flow valve closed
Fuel temperature should be at or below 0ºC
Electrical Power to the FRTT valve available
282
What are the electrical power sources for the Fuel Pumps?
L MAIN – Left ESS DC
L ALTERNATE – Left MAIN DC
R MAIN – Right ESS DC
R ALTERNATE – Right MAIN DC
283
Display the HYDRAULICS 2/3 Synoptic. What systems can power the following components
GEAR – L / PTU / EMERGENCY BOTTLE
BRAKES – L / PTU / AUX / BRAKE ACCUMULATOR
FLAPS – L / PTU / AUX
NOSE STEERING – L / PTU / AUX
GROUND SPOILERS – L / R
GROUND SPOILER Pop Up (electro-hydraulic servo valves) – L / PTU / AUX
284
When ARMED, the PTU operates automatically ON when?
L HYD pressure drops below 1500 psi
285
Operation of the PTU assumes loss of the
Left hydraulic system pressure
286
The motor side of the Power Transfer Unit (PTU) is driven by
Right hydraulic system pressure
287
When ARMED, the AUX pump comes on automatically when
L HYD and PTU pressure is below 1500 psi, and
Brake pedals depressed 10º (pump locks on)
288
What is the Brake Accumulator pre charge?
1200psi
289
If L HYD SYSTEM fluid is depleted but AUX fluid remains in the L HYD reservoir, what system can provide braking?
AUX Pump
290
What is the GEAR EMERGENCY BLOWDOWN accumulator pressure charge?
3100 psi
291
How do you turn off the L / R Hydraulic system to get zero (0) hydraulic pressure?
Pull L / R Fire handle
292
Pulling the Engine Fire Handle will shut off
Fuel
Hydraulic pressure
Engine Generator (IDG)
293
What are the fluid quantities of the L / R Hydraulic system reservoirs?
Left – 4.8 gallons on the Synoptic page
Right – 1.6 gallons on the Synoptic page
294
What is lost if you lose the Left Hydraulic system?
Left Thrust Reverser
295
If no other means of pressurizing the LEFT HYD system (L HYD pump and PTU inop) are available, the AUX pump can provide hydraulic pressure to operate the following components
Flaps, Brakes and Nose Wheel Steering
296
Can you change the Yaw Damper from the LEFT to the RIGHT?
Yes
Use DISP CONT / SENSORS / BOX FGC 2
297
What is lost if you loose the RIGHT HYDRAULIC SYSTEM pressure?
Right Thrust Reverser
298
What will prevent automatic PTU operation when PTU is ARMED?
L HYD system fluid quantity less than 1.0 gallons
R HYD system fluid temperature 104.4ºC or more
299
If the PTU shuts of automatically, can you manually select ON?
YES
Push “ON” legend
300
Can you replenish the hydraulic quantity?
YES
Hydraulic replenish reservoir in the tail compartment
301
Where do you find Manual Operations for the Main Entrance Door?
AOM Chapter 9 (09-03-20: Manually Opening and Closing Main Entrance Door)
302
How is the auto turn-on feature of the AUX pump checked during PRE-FLIGHT?
ARM the AUX pump on the overhead panel
Depress brake pedals more than 10º
The AUX pump will latch ON
303
In the above scenario how is the AUX pump turned OFF?
Select AUX pump ARM / NOT ARM switch to NOT ARM and back to ARM
304
If the PTU is operating automatically, how do stop the operation?
Select PTU ARM / NOT ARM switch to NOT ARM
305
The Landing Gear Emergency Bottle during pre-flight shows 1800psi, the bottle should be serviced at
3100psi at 70ºF (21ºC)
306
How many pins are removed before flight from the landing gear and door system?
Six (6); three (3) Gear; three (3) Gear Door
307
Do not lower the landing gear utilizing the alternate system at speeds in excess of
175 knots
308
What are the Gear Extension Speeds?
Gear – 225 (extension) 250 KCAS once down
309
During preflight, a gear uplock is closed. What action should you perform?
Pin the gear door valve OPEN
Turn on external battery switch at Left Front Access panel
Actuate the Aux pump at the Right Front access panel until the gear door and uplocks open
Remove gear door pin
Actuate the Aux pump again until the gear door closes
Turn off external battery switch at the Left Front Access panel
310
If the landing gear fails to retract, you should
NOT RETARD the throttles to IDLE in flight
UNARM the Ground Spoilers
311
If the landing gear fails to extend, what action may reset the extension mode of operation?
Verify the Emergency Landing Gear handle is fully down
Pressing the DUMP valve switch to provide an alternate electrical path for the gear extension control circuit
312
If the landing gear fails to retract, what action must be performed to prevent landing with 400 pounds of applied brake pressure (Wheel despin brakes)?
Press and Hold the DUMP valve for three (3) seconds
313
Which “Down and Locked Indication” has precedence over the other, The Landing Gear Control Panel OR the Landing Gear indication on the Flight Control Synoptic?
The Landing Gear Control Panel
314
Is there an Alternate Landing Gear Extension procedure?
YES, Using the Emergency Landing Gear Handle (EMERGENCY BLOWDOWN)
315
What is the Emergency Landing Gear Nitrogen Bottle Pressure?
3100 PSI
316
What does an illuminated GEAR HANDLE light mean during gear retraction?
The Landing Gear and/or Gear Doors are NOT retracted (up and locked)
317
When will the GEAR HANDLE light extinguish during gear extension?
When the landing gear is down and locked (gear door position is NOT considered)
318
If the LANDING GEAR IS NOT EXTENDED, when will the Landing Gear Warning HORN sound?
Anytime the Flaps are selected more than 22º (FLAPS >22º)
Aircraft Altitude < 350 feet AGL and either throttle positioned to IDLE (may be muted)
319
ANTI SKID braking is available from which hydraulic system/systems?
L HYD SYS / PTU/ AUX SYS
320
Is ANTI SKID protection available when using the PARK/EMER BRAKE?
NO
321
What is the MINIMUM ACCUMULATOR PRESSURE to set the PARKING brake?
1700 PSI, It is recommended the ACCUMULATOR be pressurized to 3000 PSI
322
The MAXIMUM BRAKE PRESSURE when using the PARK/EMER BRAKE or during NO ANTISKID BRAKING is
400 PSI
323
What change occurs to the BRAKE PRESSURE display on the BRAKE synoptic when ANTISKID is selected OFF?
The PRESSURE scale changes to a MAX 800 PSI AND an AMBER LINE appears at 400 PSI
324
In order to obtain a valid BRAKE WEAR INDICATION
The PARKING BRAKE MUST be SET
325
The DIGITAL ANTISKID CONTROL UNIT (DACU) ALSO supplies wheel speed input of knots to which items for operation?
GROUND SPOILERS AND THRUST REVERSER
326
What is the proper position of the OVERTRAVEL indicator on the Nose Strut during PREFLIGHT?
FLUSH with the steering collar
327
Below 18 knots ground speed, TILLER STEERING can provide how many degrees of steering?
80º left and right
328
RUDDER PEDAL STEERING normally provides how many degrees of steering?
7º left and right
If TILLER STEERING FAIL CAS message is displayed, rudder pedal authority increases to 16°
329
If you experience an AMBER WOW FAULT message during flight, you should
SELECT GROUND SPOILER SWITCH OFF and refer to the CHECKLIST
330
An AMBER WOW FAULT message displayed during flight is an indication of
BOTH MAIN GEAR WOW switches being in the GROUND mode
331
If you experience a BLUE WOW FAULT message during flight, you should
REFER to BLUE WOW FAULT message
332
What is required of the combined WOW to be in the AIR mode?
ONE MAIN GEAR WOW in AIR mode
333
If the GEAR HANDLE will NOT move to the UP position after takeoff, you should
SELECT GROUND SPOILER SWITCH OFF
REFER TO QRH CHECKLIST for LANDING GEAR FAILURE TO RETRACT
334
The following conditions will sound the landing gear warning horn
The aircraft is on the ground (WOW switches compressed), the Air Data System (ADS) indicates less than sixty knots (60kts), and the gear handle is in the retract position
335
What does an amber “X” on a flight control on the Flight Control Synoptic Page indicate?
Flight control RVDT has failed
336
If LATERAL HOPS occur, hydraulic power is turned off to
Both Ailerons
337
What can you do in case of a jammed aileron?
Pull disconnect handle for aileron
338
What can you do in case of a jammed elevator?
Pull disconnect handle for elevators
339
What is the maximum deflection of the Speed Brakes when you use the handle?
Maximum deflection is 30º
340
What is the maximum deflection of the Ground Spoilers?
55º
Note: the control pressure is from Left, PTU or AUX system
341
What system does the Standby Rudder use following the loss of Left/Right systems?
Standby Rudder will use AUX pump to YD1. May need to select FGC1.
It uses the AUX pump to power the Rudder through the Left systems port and only works while airborne (WOW in FLIGHT)
342
How are the Flaps controlled?
The flaps are electrically requested and hydraulically powered by the Left, PTU or AUX pressure.
Flap control in the Flap/Stab computer is DC
343
How is AILERON HOPS reset?
Use QRH and PULL / RESET CB’s
344
What happens with a HOPS?
The Aileron HOPS shuts of both actuators whereas Elevators and Rudder only shuts down the affected actuator
345
What must you do to use the mechanical trim wheel?
Select the PITCH TRIM switch light to OFF
346
What does BLUE SINGLE RUDDER CAS message indicate?
Rudder power is down to one (1) hydraulic power source
347
When ON, what does the GRD SPOILER FLAP OVERRIDE switch simulate?
Flaps are actually more than 22º (>22º)
GROUND SPOILERS deploy automatically with Wheel Speed Spin up
348
The reason for selecting the GPWS/GND SPLR ORIDE to ON when landing with flaps less than twenty two degrees (22º) is
To prevent the nuisance TOO LOW FLAPS aural alert and
Deploy the ground spoilers with wheel spin up
349
What does RED GROUND SPOILER CAS message mean?
Failed Ground Spoiler component OR
Deployed Ground Spoiler Panel
350
Loss of one hydraulic system will
Not effect spoiler activation
351
The horizontal stabilizer (STAB) remains operative in the EMER STAB ARM mode, and can be positioned with the
Yoke Trim Switches
352
Selecting the EMER STAB switch ON (ARM)
Illuminates ARM in switch
Enables EMER STAB mode
STABILIZER positioned by using YOKE electric pitch trim wheels
353
Selecting the EMER STAB switch OFF
Switch is dark
EMER STAB mode disabled
STABILIZER now moves corresponding to flap position
354
Selecting STALL BARR switch OFF
OFF illuminates in switch
STALL BARRIER CAS displays
Stick Pusher is disabled
Stall warning stick shaker continues to function
355
Selecting STALL BARR switch ON
Must be selected ON for all flight operations unless a malfunction OR
Procedural reasons require switch to be selected OFF
356
Selecting PITCH TRIM ENG/DISENG switch to ENG
DISENG (AMBER) is extinguished
Pitch Trim is engaged
YOKE pitch trim switch is active for elevator trim
357
Selecting PITCH TRIM ENG/DISENG switch to DISENG
DISENG (AMBER) is illuminated
YOKE pitch trim is disengaged
MANUAL TRIM WHEEL must be used for elevator trim
358
Selecting YAW DAMP ENG/DISENG switch to ENG
DISENG (AMBER) is extinguished
YAW dampers are engaged
359
Selecting YAW DAMP ENG/DISENG switch to DISENG
DISENG (AMBER) is illuminated
YAW dampers are disengaged
360
Selecting the GPWS/GND SPLR switch to ON
ON (AMBER) legend is illuminated
Automatic ground spoiler deployment will occur with flaps <22º and both struts have Wheel Speed Spin up
GPWS voice alarm “TOO LOW FLAPS” is inhibited
361
Selecting the GPWS/GND SPLR switch to OFF
ON (AMBER) legend is extinguished
Automatic ground spoiler deployment will occur with flaps <22º only when Weight On Wheels has occurred
GPWS voice alarm “TOO LOW FLAPS” is not inhibited
362
Selecting the GND SPLR switch to OFF
OFF (AMBER) is illuminated
Ground Spoiler System is not armed to operate
Gear Down the blue “Ground Spoiler Unarm” CAS message will appear
363
What is required for ground spoiler deployment with flaps > 22 degrees?
Select the GND SPLR switch to ARMED (BLUE) legend is illuminated
Both throttles at idle
Wheel spin up or WOW ground on each main gear strut
364
NO GND SPLRS red switch lights on centre windscreen post illuminate if
Operational parameters are satisfied
GND SPLR switch selected to ARMED (BLUE)
Left wing, right wing or both wing ground spoilers did not deploy
365
The flight controls GUST LOCK
Secures the aircraft moveable surfaces in stabilized positions
Prevents damage to surfaces and control linkages from high winds or jet blast
Effective in wind speeds up to 60 knots
366
Ensure hydraulic pressure is depleted prior to engaging the GUST LOCK by
Cycling the flight controls with the control column, yoke, and rudder pedals
AIR CONDITIONING, PRESSURIZATION, PNEUMATICS, & ICE & RAIN
367
How many ways are there to OPEN the Bleed Air Isolation Valve?
CRANK MASTER Switch
START MASTER Switch
APU BLEED AIR Switch
MANUALLY
368
When will the APU Bleed Switch open the Isolation Valve?
60 seconds after the APU reaches 100%
369
The 8th stage bleed air augments the 5th stage. Can you select 8th bleed air ON?
NO – it is opened automatically by the Bleed Air Controller (BAC)
370
14psi, 24psi and 35psi are three set point trigger values in the BAC (Bleed Air Controller) to kick in the 8th stage Bleed Air. What operation mode causes this?
14 psi normal
24 psi (low power settings: descent / holding)
35 psi (single pack operation)
371
What is the minimum pack pressure for single pack operation?
35 psi
372
The BLEED AIR CONFIGURATION CAS messages illuminate for?
APU & ENGINE BLEED AIR selected simultaneously
ISOLATION VALVE OPEN with BOTH ENGINE BLEED AIR switches selected ON
373
What is the temperature range in AUTO?
60º - 90ºF
374
What is the temperature range in MANUAL?
35º - 230ºF
375
If the AUTO TEMP SELECT pushbutton is selected OFF and the TEMP DISPLAY button is Selected to DUCT, the digital temperature readouts reflect the
Actual Temperature in the supply ducts to the air conditioned areas
376
What happens when you select the RAM AIR switch?
Both AC packs turn off
A/C depressurizes at cabin leak rate
377
The TROV is electrically operated in response to the Cabin Pressure Controller (CPC) what are the modes of operation?
AUTO, SEMI and MANUAL
378
During takeoff and departure, climbing to FL410, automatic anti-icing is inhibited
Below 1,500 feet AGL and above 35,000’
379
Automatic anti-ice is available during descent and landing when
From 35,000’ to landing
380
With WING ANTI-ICE operating, the Bleed Air Controller (BAC) maintains the wing leading edge at a temperature of
130ºF
381
When the CABIN WINDOW HEAT switch is pushed on the ground, the switch capsule should
Illuminate OFF (BLUE)
382
The EVS switch on the overhead panel applies heat for
Two (2) minutes until it turns off or when it detects a temperature higher than 14ºC
383
During taxing or holding on the ground at low power settings in temperatures less than +1ºC it is recommended that just prior to take off the engine should be
Accelerated to 40% LP RPM for 10 seconds and at intervals of 1 hour
384
How many motors are available for pressurization TROV operation?
Three (3), 2 for Automatic and 1 manual
385
What are the power sources for the pressurization motors?
Two (2) A/C (AUTO/SEMI)
One (1) D/C (MANUAL)
386
In AUTO, where does the pressurization information come from?
MCDU
387
Maximum cabin pressure differential (psi) permitted for taxi, take-off or landing is
0.3 psi
388
What are the trip points for the Cabin Pressurization Relief Valve?
Cabin Differential 10.28 Amber CAS
Cabin Differential 10.48 Red CAS
Negative differential pressure relief at -0.25 psi
389
The pressurization system will change from LANDING to FLIGHT when
Taxi speed is equal to or greater that 8 knots
Power levers advanced fifteen degrees (15º) forward
390
What are the “Cabin Pressure Low” CAS Trip points?
8000’ - LFE (Landing Field Elevation) less than 7,500
10,000’- LFE greater than 7,500, but less than 9,500
14,500’ – LFE greater than 9,500
10,000’ – Manual Mode
14,750’ (+/-250) Cabin Altitude / Oxygen Masks drop down automatically
391
Activation of the EDM (EMERGENCY DESCENT MODE) will result in the aircraft
Turning left 90º
Descending to 15,000”
At 340 KCAS (MAN)
Once at 15,000’ speed target changes to 250 KCAS (MAN)
Note: Autopilot must be engaged / Autothrottles will engage if disengaged
392
What conditions must exist for EDM mode to activate?
AIRCRAFT ALTITUDE ABOVE 40,000’
AUTOPILOT ENGAGED
393
What airspeed will automatically enter on the GUIDANCE PANEL SPEED window during EDM mode?
340 KCAS (MAN)
250 KCAS (MAN) once level off at 15,000’
394
Can Guidance Panel heading be changed during EDM mode?
NO
395
AUTO ANTI-ICE protection terminates in what sequence after the ice detectors no longer sense the presence of ice
After 1 minute – ICE DETECTED L / R CAS message is removed
After 3 minutes – COWL ANTI-ICE valves close
After 5 minutes – WING ANTI-ICE valves close
396
If the APU is operating when pushing the ICE DET test button, ensure the
WING ANTI-ICE switches are selected OFF
Note: Wing Anti-Ice valve will open and the APU LCV (Load Control Valve) will try to increase APU bleed air output to satisfy WING Anti-Ice demand. Not a good thing for the APU
397
When pushing the ICE DET button, the following CAS messages appear
ICE DETECT FAIL, L/R
ICE DETECTED, L/R
398
What must you do if anti-ice is selected ON for take-off?
Anti-ice must be selected in the MCDU on TAKEOFF INIT page 4/5 in order for the V Speeds to BOX
399
During pre-flight, when the CABIN WDO HT switch is selected ON
OFF (BLUE) legend should illuminate in the switch if OFF (BLUE) legend does not illuminate:
Select the CABIN WDO HT switch to OFF, then
Ensure the CABIN WDW HTRS GROUND BYPASS switch at Observers Seat panel is selected OFF
400
The WSHL BLWR (if installed) operates
Ground only (WOW)
G550
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