Oral Exam Flashcards
(260 cards)
0
Q
Max rudder travel
A
65 degrees w tiller
7 degrees w pedals
1
Q
Max Operating altitude
A
42000
2
Q
What model engines
A
PW2040
3
Q
When is pitot static heat activated
A
Engine start
4
Q
Max altitude for APU bleed air
A
17000
5
Q
What are the 6 power sources
A
L generator R generator APU generator HDG Ext power Batteries. 30 min
6
Q
Aircraft dimensions
A
155’ long
60’ nose gear to main gear
135’ wingspan
7
Q
How much space for 180 degree turn
A
120’
8
Q
Nose gear strut extension
A
0.5” to 5.5”
9
Q
Main gear strut extension
A
3 fingers
10
Q
Passenger oxygen masks last for
A
22 minutes
11
Q
Passenger masks auto deploy at
A
14000’
12
Q
PBE lasts for
A
15 minutes
13
Q
Total fuel in L, R, and C tanks
A
75,600
14
Q
Fuel in forward aux
A
7123
15
Q
Fuel in aft aux
A
9101
16
Q
Total aux fuel
A
16224
17
Q
All fuel tanks total
A
91824
18
Q
Where is DC fuel pump
A
Left wing. For APU. If AC power, L Fwd AC pump runs
19
Q
3 causes Fuel Configuration Light
A
- Imbalance more than 1800
- Useable fuel less than 2200
- More than 1200 in C tank with pumps off
20
Q
Tell me about C fuel pumps
A
Only run w more than 50% N2
2x more power
Run w fueling station door open
21
Q
Can you suction feed from C tank
A
No
22
Q
Where is the SPR
A
Right wing
23
Q
Can I manually fuel the aircraft
A
Wing yes, center no
24
What indicates a fuel leak
More than 1000 imbalance in less than 30 min
25
What is the max fuel temp
49C
26
Min fuel temp
3 degrees above freeze or -45C, whichever is higher
27
Which ILS receiver functions on stby power?
Center
28
What are marker beacons powered by
Stby power
29
How long does IRS alignment take
10 min
30
When do you have to do extended alignment and how long does it take
70 to 78 degrees N or S. 17 min.
31
How long does fast align take? When can I do it?
30 sec. If less than 18 hrs since full alignment.
32
What powers each IRU
L IRU - L AC XFER BUS
R IRU - R AC BUS
C IRU - C AC BUS
HOT BATTERY IS DC BACKUP
33
Which IRU only has 5 min in DC power
R IRU
34
Can I realign IRS in the air
No
35
What is ATT mode on IRS
Fly level 30 sec to align. Provides heading and attitude
36
Max altitude APU generator
42000
37
Max altitude APU bleed air
17000
38
APU fault light
Fuel (valve disagree, blinks on start)
Fire
Fault
**immediate shutdown
39
What is needed to start APU
Aircraft battery
| APU battery
40
APU run light
APU on speed. Blinks twice on start for self test if circuitry.
41
APU starter duty cycle
3 attempts in 60 min. 5 min cooling between each.
42
How long does APU run bleed air cooling automatically during shutdown
60-120 sec
43
Can I cancel APU shutdown if run light still on?
Yes. Select start
44
Does battery switch off turn off APU
Ground- yes. Still does cooldown.
| Flight- no.
45
Why is it bad to kill APU with battery switch
You lose fire protection during cooldown.
46
What model engine
PW 2040
47
What drives engine accessories
N2 rotor
48
What prevents engine limit exceedences
Electric engine control (EEC)
49
What are primary engine indications on upper EICAS
EPR, N1, EGT
50
What are secondary engine indications?
N2, FF, Oil temp press quant, vib
51
Amber engine indications are inhibited on TO or GA for
5 min. 10 min single engine
52
When does stby engine indicator turn on
Both EICAS computers fail
Both EICAS CRTs fail
AC power loss
53
Max thrust reduction for DTO takeoff
25%
54
What operates Spar and Eng valves
Fuel control switches
55
Oil Pressure Relief valve at
425 PSI
56
Starter cuts out at
50% N2
57
Starting fuel flow is
600 lbs/hr
58
Engine starter duty cycle
3 starts less than 2 min run down to 0% N2, then 15 min cooling.
If greater than 2 min, 4 min max once and then 15 min cooling.
59
What is inflight start envelope
It displays on EICAS
60
When will reverse thrust work
On ground in Idle
61
EGT limit for engine start
570C
62
Min N2 on start for ignition and fuel
18%
63
Position fuel control switch to run at
18% N2 below 9500'
| 24% N2 above 9500'
64
Abort start if EGT fails to rise within
20 sec of RUN
65
Abort start if N1
Fails to rise with EGT
66
Abort start if N2
Fails to stabilize at idle within 120 sec
67
Do not advance thrust beyond required for taxi until oil temp reaches
50C
68
Loss of pressure/rapid D boldface
OXYGEN MASKS ON/100%
| CREW COMMUNICATIONS ESTABLISH
69
Dual engine failure boldface
ENGINE START SELECTORS (BOTH) FLT
THRUST LEVERS (BOTH) IDLE
FUEL CONTROL SWITCHES (BOTH) CUTOFF, then RUN
70
Aborted engine start boldface
FUEL CONTROL SWITCH (AFFECTED SIDE) CUTOFF
71
Unscheduled stab trim boldface
STABILIZER TRIM CUTOUT SWITCHES CUTOUT
72
Fuel temp is measured in the
R tank
73
Center tank scavenge system transfers fuel to the
L tank
74
How is fuel transferred from aux tanks
Bleed air pressure from L duct
75
When will Aux fuel transfer start
Less than 39,300 in C tank. Stops if C tank fills to 41600
76
Can the IDG be reset
No
77
DRIVE LIGHT indicates
IDG oil temp high or press low
78
When is HDG activated
Both L and R AC Systems fail
79
What drives HDG
L system or PTU
80
Is it normal to see BATT DISCHARGE with HDG
Yes. Until batt voltage matches HDG output
81
What does HDG power
```
Capt instr transfer bus
L AC transfer bus
R AC transfer bus
AC stby bus
DC stby bus
Batt bus
Hot batt bus
```
82
What does battery power
Batt bus- if switch on
Hot batt bus- all the time
Stby AC bus- thru inverter
Stby DC bus
83
How long does battery power last inflight
90 minutes (or 30 min)
84
What powers each autopilot for auto land
L- L AC bus
C- battery standby system
R-R AC bus
85
3 times load shedding happens
Engine start- when GND selected
Generator loss
Overload
86
What order does load shedding follow
Galley
Utility buses
Individual equipment
87
How long are emergency lights powered for
15 min
88
Passenger masks auto deploy at
14000
89
What powers RAT
Hot Battery Bus
90
When will RAT auto deploy
80 kts ground speed
| With dual engine failure below 50% N2
91
Min speed for RAT
130
92
Engine start Selector held in GND until
50% N2
93
What is load shed for engine start
Utility buses
| R recirc fan
94
Is there a time limit for igniters
No
95
Where is fuel temp measured
Right tank
96
Will wing anti ice operate on ground
No
97
What slats does wing anti ice reach
The first 3 of 5
98
Window Heat Inop Light
Switch off
Overheat
Fault
99
Auto seatbelt sign on when
Gear not up
Flaps not up
Below 10000
Oxygen masks out
100
Outflow valve automatically closes above
11000
| Returns to norm at 9500
101
Pressurization Auto Inop Light
Both controllers failed
| Man mode selected
102
Pressure Auto rate selector index mark
500' climb 300' descent
103
Pressure Auto rate selector min
50' climb 30' descent
104
Pressure Auto rate selector max
2000' climb 1200' descent
105
Max cabin differential
8.6 +or- 0.5
106
Max PSID for Takeoff or Landing
0.125
107
Equipment smoke light
FLT deck supply fan turns off
Recirc fan turns off
Overboard exhaust valve opens
Packs to high flow
108
CAB ALT Light
Exceeds 10000. Light off at 8500
109
CAB ALT Light with high alt landing
Cabin exceeds 14650. Light out at 11,800
110
Pack off Light
Pack is off
Loss of air
Pack overheat
111
Pack Inop Light
Excessive outlet temp- pack will go full cold
| Fault- pack valve will freeze
112
Pack Control Selector in Stby at N regulates
75 degrees
113
Caution system inhibited on takeoff
From 80 knots until first of 400' or 20 sec
| On abort TO, inhibit removed at 75 knots
114
Warning system inhibited on takeoff
From rotation until 20 sec or 400' , whichever is first
115
When will I get ATT disagree
3 degree pitch or roll difference
116
When will pitch limit indicator show up
Flaps extended
117
When does HSI compass change to true
Above 73 N and 60 S
118
Failed SG will blank
EFIS displays
119
Failed IRU will blank
HDG, ATT, ALT
120
Captain RDMI gets input from
R side
121
How many ADC
2
122
How many IRU
3
123
How many SG
3
124
How many ILS
3
125
How many FCC
3
126
How many FMC
2
127
What does EFI Alt control
Symbol Gen
ILS
Radio Alt
128
Autopilot controls
Aileron
Elevator
Rudder- only in multi AP approach
129
How can approach mode be cancelled after glide slope intercept
GA button OR
| Disengage AP and turn both FD switches off
130
Can ASA change below 200'
Yes. Only to indicate No Autoland
131
The aircraft will capture LNAV regardless of heading if
Within 2.5 NM
132
Max angle to capture localizer
120 degrees
133
ASA comes on below
1500'
134
When is GA mode armed
When flaps extended or GS captured
135
When does GA mode stop being armed
2 sec past RA 5'
136
What does GA mode command
Vref+5 and 2000 fpm
137
What powers norm brakes
Right hydraulic system.
138
What powers alternate brakes
Left system. No auto brakes.
139
What powers reserve brakes
Right system standpipe. Anti skid and auto brakes are functional.
140
BRAKE SOURCE light
Both norm and alt brake pressures low. With reserve selected, accumulator is only power for brakes
141
FIRE light
Engine, APU, wheel well or cargo fire
142
CONFIG light for takeoff
Flaps
Park brake
Spoilers
Stab trim
143
CONFIG for landing
Gear not down AND-
Flaps 25 or 30
Thrust idle less than 800'
144
SPEED BRAKES light
Speed brakes out AND-
RA 800 to 15
Landing flaps selected
145
ALT ALERT light
200 to 500 off MCP altitude
146
How to disarm auto brakes
MASS
Man brakes
Spoiler up
Switch disarm or off
Advance power
147
When is RTO armed
85 knots
148
When do auto brakes engage
Idle
Wheel spin up
1 degree pitch
149
DTO 1 and DTO 2 reductions
91% and 81%
150
Derated CLB 1 and 2
92% and 85%
151
What is needed for a bleed air valve to open
Switch on
Bleed supply
Bleed demand
152
HI STAGE light
Too much pressure, valve closes, cannot be reset
153
BLEED light
Temperature excessive. Valve closed. Can be reset
154
Isolation valve powered by
Standby AC and DC
155
How many fans in FWD E and E cooling
3- supply, alt supply, aux
156
How many fans in aft E and E cooling
2
157
What happens if recirc fan fails
Pack switches to high flow
158
How many cooling zones are there
4. Lowest determines output of pack. Rest use trim air
159
When does pressurization enter cruise mode
Level for 1 min. Stays until alt changes by 500'
160
How many HF radios
3
161
How many HF antennae
1
162
RTU FAIL
Radio failure
163
RTU PANEL
RTU fail
164
No HF transmissions within
200' of fuel
165
HF tuning takes
Max 15 sec
166
Altimeter reminder light
900 to 300'
167
Where does input for Capt RDMI come from
R side
168
What powers standby ADI
Stby DC bus
169
What bus detects fire
Battery
170
What bus fights fire
Hot battery
171
What does pulling a fire handle do
```
FAGSHB
Fuel- eng and spar valves
Arms bottles
Generator
Silence bell
Hydraulic pump
Bleed air valve
```
172
How many fire loops in engine
2 in engine. 1 overheat loop in strut
173
Crew action for wheel well fire
Put gear down
174
What does RAT power
C hydraulics for aileron, elevator, rudder
175
4 ways to trim
Electric
Alternate
Autopilot
Mach speed
176
Can I trim ailerons with autopilot
No. Yoke doesn't move
177
STAB TRIM light
Trim running half rate
178
UNSCHED STAB TRIM
Uncommanded movement. Use Cutout switches or move yoke
179
How many spoilers
12
180
Which spoilers are ground only
4 and 9
181
What Hyd system powers R aileron
C and L
182
What spoilers do C hydraulics power
1 and 12
183
What spoilers do R hydraulics power
2,4,6,7,9,11
184
RUDDER RATIO light
```
Failure
L hydraulics fail
L ADC fail
**avoid large inputs above 160kts
**if L Hyd normal, max cross 15kts
```
185
Auto speed brakes require arming AND
Ground
Idle
Hydraulic pressure to gear truck tilt
186
AUTO SPEEDBRAKE light
Do not arm handle
187
Thrust reverser deploy also deploys
SPEEDBRAKE
188
What powers flap power drive units
L Hyd or PTU or electric motors
189
How many positions do slats have
3. TO land and up
190
Max derated TO
75%
191
What does L Hyd system power
Gear flaps steering HDG yaw damper
192
When does PTU come on
When L pump press low. Powered by R system
193
HYD RSVR light
Low bleed pressure or quantity less than 50%
194
HYD SYS PRESS
Low pressure in system
195
HYD PRESS Light
Pump output press low
196
HYD OVHT light
Pump temp high
197
Hydraulic EICAS message RF at
75% quantity
198
L standpipe fluid for
PTU
199
C standpipe fluid for
RAT
200
R standpipe fluid for
Reserve brakes
201
PTU powers
Slat/flap, gear, steering, HDG
202
RAT powers
C flight controls
203
RAT deploys when
Armed when above 80 kts
Both engines under 50% N2
Switch- hot batt bus
204
Speed for RAT power
Above 130 kts. Will get green press light
205
Gear retraction time
25 sec
206
Gear truck tilt
9.6 degrees
207
Alt Gear ext uses L Hyd fluid and
DC pump from hot batt bus. Doors stay down
208
Auto brakes require
One IRS
209
ANTI SKID light
Failure or power loss
210
LEADING EDGE light
Slat asymmetry or disagree
211
TRAILING EDGE light
Flap asymmetry or disagree.
| Load relief system not operating
212
Max alt flaps
20
213
With alt flaps at 20, slats will be
In landing position
214
BRAKE TEMP light
Temp is 5 or above
215
Terrain dotted green
2000 below to 500 below
216
Terrain dotted amber
500 below to 2000 above
217
Terrain dotted red
More than 2000 above
218
Terrain caution
40-60 sec from impact
219
Terrain warning
20-30 sec from impact
220
PARK BRAKE light
Park brake valve not open
221
LEADING EDGE light
Slat asymmetry or disagree
222
TRAILING EDGE light
Flap asymmetry or disagree.
| Load relief system not operating
223
Max alt flaps
20
224
With alt flaps at 20, slats will be
In landing position
225
BRAKE TEMP light
Temp is 5 or above
226
Terrain dotted green
2000 below to 500 below
227
Terrain dotted amber
500 below to 2000 above
228
Terrain dotted red
More than 2000 above
229
Terrain caution
40-60 sec from impact
230
Terrain warning
20-30 sec from impact
231
PARK BRAKE light
Park brake valve not open
232
How should engine stack look after engine start
1,2,3,6,10
233
4 times to abort an engine start
Oil press fails to rise prior to RUN
EGT fails to rise 20 sec after RUN
N1 fails to rise with EGT
N2 fails to stabilize at idle 120 sec after RUN
234
Reject after 80 knots for
Fire
Eng failure
Predicted windshear
Aircraft not going to fly
235
When will ignition operate in AUTO
Slats extended
| Eng anti ice on
236
What does CONT ignition do
Continuos power to one igniter. Required for severe turbulence
237
What does FLT ignition do
Powers both igniters. Dual engine failure.
238
EPR corrections for wing anti ice use
Valve position
239
EPR corrections for engine anti ice use
Switch position
240
Max PSIG decrease when checking oxygen
100
241
Set heading reference true if N or S of
82 degrees
242
PWS is enabled
Thrust levers set for takeoff OR
| Below 2300'
243
Alerts listed in priority
Wind shear immed alert warning
GPWS immed alert warning
GPWS look ahead warning
Wind shear predictive warning
244
GS can be inhibited below
1000 AGL
245
AUTO BRAKES light
System disarmed or Inop
246
When are RAs inhibited on TCAS
500'
247
Windshear recovery procedure
Disengage auto throttle and autopilot. GA switch. Max power. 15 degrees pitch. Speed brakes in.
248
Reactive windshear is active below
1500'
249
Predictive windshear issues alerts below
1200'
250
Predictive windshear cautions are inhibited from
80 kts to 400'
251
Predictive windshear warnings are inhibited from
100 kts to 50'
252
What systems does ASA monitor
```
FAIRI
FCC
Autopilot
IRS
Radar Alt
ILS
```
253
Equipment SMOKE light
Smoke in fwd equipment cooling ducts
254
ALTN equipment cooling switch
1. Selects Alt supply fan
2. Activates aux fan if both supply fans fail
3. Opens overboard exhaust valve if L recirc fan not operating
255
OVHT equipment cooling light
```
ILBSSS
Insufficient airflow
L recirc fan not operating and overboard exhaust valve closed
Both aft cooling fans Inop
Selected supply fan not operating
Smoke in DV stateroom
Smoke detected and ALTN not selected
```
256
Max N1 to pull out of parking
35%
257
RA- aircraft will enter collision airspace within
20-30 sec
258
TA- aircraft will enter collision airspace within
35-40 sec
259
RAs are inhibited below
1000 AGL
