Skywest CRJ Oral Study Guide Flashcards
’What are the dimensions’
Nose to tail, 87'10". Wing span, 69'8". Height, 20'8"
1
‘What is the track distance between the main wheels’
2
‘What is the minimum width required for a 180° turn’
3
‘What is the purpose of the winglets’
4
‘What are the APU and radar hazard areas’
5
‘How are the emergency lights powered’
6
‘When does the OXY LO PRESS caution come on’
7
‘How many PBEs are onboard’
8
‘When will WINDSHEAR messages appear’
9
‘How are TCAS RAs presented’
10
‘How long is the emergency escape rope’
11
‘Which overhead lights are illuminated with just the battery master on’
12
‘How can the passenger door be verified closed in addition to the EICAS indication’
13
‘What is the maximum load on the passenger door’
14
‘How many emergency exits are there in the cabin’
15
‘How many oxygen systems does the CRJ have’
16
‘Where is the flight compartment PBE located’
17
‘What is the source of oxygen for the passengers’
18
‘Do the oxygen generators activate when the oxygen masks drop’
19
‘When will the emergency lights illuminate automatically’
20
‘How are the emergency lights charged’
21
‘How long will emergency lights last once activated’
22
‘The AUTO function of the passenger signs will turn the seat beat sign on when’
23
‘Why is there a minimum ops weight.. Minimum flight weight’
24
‘How do you know if the masks have dropped’
25
‘Is Vb / Mb a target or limitation’
26
‘What happens if the EICAS Control Panel (ECP) fails’
27
‘What happens if ED1 fails’
28
‘When will T/O Config warnings occur’
29
‘When are non-critical EICAS messages inhibited’
30
‘How are EICAS caution messages boxed.. Status’
31
‘How are terrain warnings displayed’
32
‘What is the only pressure door not displayed on the Doors synoptic page’
33
‘The APU control system gives priority to what’
34
‘What are VGDs’
35
‘What supplies pressurized fuel to the APU’
36
‘What will cause the APU to shutdown in flight.. Ground’
37
‘The APU LCV interlock is predicated on what.. What does it do’
38
‘How will the 10th stage bleed shutoff valves fail …losed).. 14th.. APU LCV.. 10th and 14th isolation’
39
‘What happens when the APU PWR/FUEL switchlight is pressed in’
40
‘What are the APU intake door indications’
41
‘APU pneumatic output is controlled by modulating what valve’
42
‘What is the start sequence of the APU’
43
‘What ways can the APU be manually shutdown’
44
‘What speed is the APU starter de-energized’
45
‘During an engine start on a single-engine taxi, why do we need N2 < 70%’
46
‘Why start the second engine during a single-engine taxi with the APU’
47
‘What is the rated thrust of the CF34-3B1 engine.. With APR’
48
‘Describe the design of the CF34 engine’
49
‘What PSI is required for a crossbleed start’
50
‘How many igniters does the engine have.. What are their power sources’
51
‘How many valves open when the ENG START switchlight is pressed in’
52
‘Pressing the ENG STOP switchlight does what’
53
‘What items are driven by the N2 accessory drive’
54
‘What does the L or R ENG START message indicate’
55
‘How many horsepower is the Air Turbine Starter (ATS)’
56
‘When does the engine starter cut out’
57
‘How are the ignition systems powered’
58
‘At low power settings, what type of speed control is in effect.. High power settings’
59
‘What happens to the N2 indicator when wing anti-ice is on’
60
‘A failure of the high pressure engine driven fuel pump will result in what’
61
‘What is 7th stage bleed air used for.. 10th.. 14th’
62
‘What is APR, When is it armed When is it activated, What does it do’
63
“What are the N1 bugs’ colors and shape”
64
‘How many fuel nozzles are there for each engine’
65
‘How does N2 vibration indications get displayed’
66
‘What indication will be given if the APR fails’
67
‘What are the “bare essentials” for an engine start’
68
‘What cools the engine oil’
69
‘During climbout, your lunch box falls and turns of…switches. What can you expect, and what do you do’
70
‘If N2 speed control is used for takeoff, is APR thrust available’
71
‘If ignition is left armed during a subsequent engi… failure, will the ignition automatically come on’
72
‘What is necessary for thrust reverse to operate’
73
‘When do we use CONT IGNITION’
74
‘During start on a cold day, what N1 is necessary before fuel is introduced’
75
‘What does an amber REV on the N1 gauge mean, Green’
76
‘What does the EMER STOW switchlight do, What will EICAS display’
77
‘What do you check during the start sequence’
78
‘What are some of the systems that are armed/checked when N1 > 79%’
79
‘How do you do the FFOD fuel feed check valve test and Why are we checking this’
80
“What do you do if you don’t get the R/L FUEL LO PRESS right away”
81
‘Would you use the APU to try an engine restart in flight’
82
‘What does NO STRTR CUTOUT mean’
83
‘Without checking the N2 gauges, how could you tell if they were NOT within 2% of each other’
84
‘When the thrust levers are placed in shutoff, specifically how does the engine stop getting fuel’
85
‘Which valves fail open and Closed and Why’
86
‘What are the ratings of the Lead Acid batteries’
87
‘Why is the APU battery bigger’
88
‘What busses power the battery chargers’
89
‘What does the green AC AVAIL light indicate’
90
‘What does the battery master do’
91
‘What happens to the DC system when AC power is established’
92
‘Which busses are powered with external AC connected and the AC SERV Config. switch on’
93
‘What does the DC SERV switch do’
94
‘What is the generator/bus priority’
95
‘What causes the IDG to automatically disconnect’
96
‘What causes an IDG FAULT’
97
‘If AC BUS 1 loses power, how many TRUs lose power’
98
‘When do the AC UTIL busses shed’
99
‘Which bus ties are automatic and Manual’
100
‘When will the APU and MAIN BATT DIR busses power the DC ESS bus through the DC BATT bus’
101
‘When does the AC ESS XFER ALTN light illuminate’
102
‘What does the AUTO XFER FAIL light indicate What is the purpose of the switchlight’
103
‘How do you isolate AC BUS 1’
104
‘When does the DC EMER bus appear on the DC synoptic page’
105
‘What does the DC EMER bus power’
106
‘How is the DC EMER bus powered’
107
‘How is AC converted to DC’
108
‘How many TRUs are on the airplane Rating Location’
109
‘Why are they in the nose compartment’
110
‘A TRU FAIL message will appear when’
111
‘What does the ADG power’
112
‘After ADG deployment, how is normal power returned to the AC ESS bus’
113
‘When will the ADG automatically deploy’
114
‘How many kVA is the ADG’
115
‘If the SERV TRU is powering DC BUS 1 and 2, what precautions must be taken’
116
‘In looking at the electric DC synoptic page, if th…1 fails, what should you do (besides look at QRH)’
117
‘If the ESS TRU 2 fails, what should you do’
118
‘How many circuit breaker panels are there Locations’
119
‘What is a Permanent Magnet Generator (PMG) and what does it do’
120
‘What situation exists where both batteries are connected to each other’
121
‘What RPMs will the constant speed drives provide to the generator’
122
‘With the ADG deployed and not operating, what is powering the DC ESS bus’
123
‘With just the battery master on, will the ALTN light illuminate’
124
‘When will we get a white IDG DISC light’
125
‘Can an IDG be reconnected in flight On the ground’
126
‘If an IDG has been disconnected and deferred, why do we NOT get the light at the gate’
127
‘What is the difference between AUTO XFER FAIL and OFF’
128
‘Where is the AC external receptacle located’
129
‘You show up to the airplane and the battery is dea…an you immediately disconnect the DC external Why’
130
‘What airspeed does the ADG produce maximum power Lose power’
131
‘What does the ADG handle control’
132
‘What happens when you lose AC BUS 1’
133
‘Does DC external charge the batteries’
134
‘When does generator overload occur When is it taken offline’
135
‘If you select AUTO XFER OFF on the left side and G…hat TRUs do you lose and which busses do you lose’
136
‘so all TRUs are still being powered. This is sort … would prevent GEN 2 / APU from powering AC BUS 1’
137
‘Will the PA system work with only DC power’
138
“If during an electrical smoke/fire you’ve exhauste…ate most busses yet keep a decent level of safety”
139
‘How is the DC ESS and DC BATT powered in flight Ground’
140
‘Where, physically on the airplane, are AC BUS 1 and 2, DC BUS 1 and 2 and AC ESS bus located’
141
‘If the AC ESS bus shorts, what have you lost and what can you do about it’
142
‘In the CRJ700-900 you can also pull CB1S2 to disco…ators to power their respective AC busses. CRJ200’
143
‘In automatic mode, what rate does the cabin climb/descend’
144
‘Which display and ARINC cooling fans operate on the ground In flight’
145
‘How do we switch pressure controllers’
146
‘The pressure controller pre-pressurizes the cabin to what value’
147
‘When do you use the manual pressure controller’
148
‘When is pressurization information displayed on PRI, STAT and ECS pages’
149
‘In flight, what supplies cooling air to the pack heat exchangers .. On the ground’
150
‘What happens if a pack experiences an over-pressure condition.. Over-temp’
151
‘How do you tell if the pack valve (PRSOV) is open or closed’
152
‘When may ram air be used for ventilation’
153
‘What happens when the EMER DEPRESS switchlight is pressed in’
154
‘On the ground, what pneumatic sources are available to operate the ECS system’
155
‘What causes a pack to automatically shutdown’
