Oral guide questions Flashcards
(213 cards)
1
Q
AIRCRAFT GENERAL - How tall is the tail?
A
17.2ft
2
Q
AIRCRAFT GENERAL - What is the wingspan?
A
55.7ft
3
Q
AIRCRAFT GENERAL -
What is the distance between the main wheels?
A
14.9ft
4
Q
AIRCRAFT GENERAL - What is the curb to curb turning radius?
A
38ft
5
Q
AIRCRAFT GENERAL - What is the wall to wall turning radius?
A
70.6ft
6
Q
AIRCRAFT GENERAL - Which door latching pin actuates the door seal valves?
A
Lower aft
7
Q
AIRCRAFT GENERAL - What is the purpose of the ram air ducts on the dorsal fin?
A
To cool the components in the tail cone
8
Q
ELECTRICAL SYSTEM - EMERGENCY BUS ITEMS - L/H CB PANEL
A
- Cockpit flood lights
- L/R N1 tapes & secondary ignitions
- Gear, flaps, stab & hyd control valve
- gear warning
- stby hsi & p/s heater
9
Q
ELECTRICAL SYSTEM - EMERGENCY BUS ITEMS - R/H CB PANEL
A
- Audio 1&2
- Nav 1
- Comm 1
- RMU 1
- AHRS 2
- stby tuning head
10
Q
ELECTRICAL SYSTEM - If the battery voltage is 23v can you start the APU and then start the engines?
A
No
11
Q
Where are the emergency exits located?
A
Main cabin entrance door
Emergency Exit Door located in aft lav area - right side
12
Q
How would you know if either main or emergency door was unlocked?
A
An annunciator in the cockpit will illuminate if either door is unlocked
13
Q
ELECTRICAL SYSTEM - What is the normal output for each generator?
A
28.5v regulated and 300 amps
14
Q
ELECTRICAL SYSTEM - What is the allowable difference between generator load sharing?
A
10% of total system load (30 amps)
15
Q
ELECTRICAL SYSTEM -
What does the gen. control unit do?
A
Parallels
Protects
Regulates
16
Q
ELECTRICAL SYSTEM - What is the normal output for each generator?
A
28.5v regulated and 300 amps
17
Q
Where are the handheld fire extinguishers located in the aircraft?
A
Under right pilot seat and left rear passenger seat.
18
Q
What equipment is available to the crew for smoke in the cockpit?
A
Crew oxygen masks and smoke goggles
19
Q
What must you do to get oxygen from the oxygen masks into the smoke goggles.
A
A tab on the nose piece of the oxygen mask must be selected down for oxygen to flow into the smoke goggles.
20
Q
Can you use autopilot if electric trim is inop?
A
no
21
Q
ELECTRICAL SYSTEM - How many emer. batts are there and what for
A
4: 2 for avionics, 2 for emer lighting
22
Q
Is there a reversionary mode of operation available if the No. 1 MADC fails?
A
Yes, pressing the ADC reversionary button on the left side will transfer ADC information from the No. 2 MADC to the left PFD
23
Q
What will happen to the vertical mode selected on the FD if the No. 1 MADC fails?
A
The vertical mode will be disengaged and will be re-engaged after selecting ADC revisionary.
24
Q
What happens to the cabin pressurization controller if the No. 1 MADC fails?
A
It switches to ISOBARIC mode of operation
25
Can the left side avionics be tuned with the right side RMU?
Yes, by pressing the 1/2 button on the right RMU, you can tune the appropriate avionics on the left side.
26
ELECTRICAL SYSTEM - with batt switch in EMER, what powers emer bus?
Battery through battery bus
27
What is the max ambient temp for ground ops?
+54C
28
ELECTRICAL SYSTEM - How would you know if a right side current limiter has blown when you turn the batt switch on?
- A steady red master warning on left side
- Only left annunciators illuminated
- Right engine off flags displayed
- AFT J-BOX LMT illuminated
29
ELECTRICAL SYSTEM - How would you know if a current limiter has been blown after both engines started?
Amp imbalance indicated. Side with blow limiter shows less load than good side
30
ELECTRICAL SYSTEM - What is significance of start button illuminating during start?
Start relay has closed
31
ELECTRICAL SYSTEM - If starting engines with a gpu and gen switches in ON, will 2nd start be a GPU start, cross gen start, or batt start?
Generator assisted battery start aka 1/3batt start
32
ELECTRICAL SYSTEM - How long will fully charged battery last?
10min with batt - ON
| 30min with batt - EMER
33
ELECTRICAL SYSTEM - How long will the Meggitt battery power stby attitude indicator?
3.5hrs
34
ELECTRICAL SYSTEM - Will AHRS emer batt pack power the FMS if the batt switch is in emer?
No. The switch must be ON and avionics switch OFF
35
ELECTRICAL SYSTEM - How many emer. batts are there and what for
4: 2 for avionics, 2 for emer lighting
36
ELECTRICAL SYSTEM - Is batt isolation relay (BATT ON) powered open or closed?
Powered closed
37
ELECTRICAL SYSTEM - Can batt charge from gpu if batt switch off
Yes
38
ELECTRICAL SYSTEM - Batt disconnect switch powered open or closed
powered open by removing the ground
39
ELECTRICAL SYSTEM - with batt switch off, what powers emer bus?
Generators through crossfeed bus
40
What are the PRIMUS 1000 limitations?
Ground ops with radome fan failed max 30 min or IC-1 or -2 hot
Dispatch prohibited if IC-1 or -2 hot
Must be preflight tested
41
When must the Meggitt be tested
Before each flight
42
Can passenger masks be deployed if DC power fails?
Yes, but you must manually turn the switch on
43
MASTER WARNING SYS - When will HYD PRESS light begin to flash and illuminate master caution light?
When on > 40 seconds in flight
44
What is the lowest pressure the O2 bottle may have before servicing?
400 PSI, but should be serviced anytime out of the green band (600 PSI)
45
What size oxygen bottle do we have?
76 cu ft
46
Which primary flight controls use cables for operation
Ailerons
Elevator
Rudder
47
Are the ailerons and rudder interconnected?
Yes
48
What are the flap position settings?
0,7,15,35 degrees down
49
Can flaps be set to intermediate positions?
yes
50
When does the stabilizer move?
It moves to down positions anytime flaps selected other than UP.
Moves to UP position when flaps are selected UP
51
What does it mean if the STAB MIS COMP annunciator illuminates?
The stab is not in the same position the flap handle is in.
52
ELECTRICAL SYSTEM - Avionics power relays powered open or closed
Powered open
53
ELECTRICAL SYSTEM - What do the two avionics emergency batt packs power?
Left: Stby attitude indicator (meggitt)
Right: AHRS 2 and FMS
54
MASTER WARNING SYS - What will cause the FUEL BOOST annunciator to flash and activate master caution?
Fuel boost pump was activated due to low fuel pressure sensing
55
ELECTRICAL SYSTEM - How is batt take offline during gpu start?
Batt disconnect relay is auto. powered open
56
ELECTRICAL SYSTEM - Will the battery disconnect switch and relay work with the batt in the OFF position?
No
57
ELECTRICAL SYSTEM - How is batt take offline during apu start?
Batt disconnect relay is auto. powered open
58
ELECTRICAL SYSTEM - What instrument lighting is also powered by the Meggitt's emer battery?
Stby HSI and N1 indicators
59
ELECTRICAL SYSTEM - Will AHRS emer batt pack power the FMS if the batt switch is in emer?
No. The switch must be ON and avionics switch OFF
60
How many trim tabs are there on the flight controls?
4- one on each elevator, one on the rudder, one on the left aileron.
61
If the electric trim fails the pre-flight operation test, can the airplane be hand flown?
no.
62
At what airspeed will stabilizer movement be stopped?
215 knots +/- 10
63
If a major failure were to occur in the stabilizer movement system, what setting will the stabilizer achieve?
The failsafe sets it to cruise positions (+1 degree)
64
If the landing gear is put in motion while the stabilizer is moving, which system gets priority?
The landing gear, the stab will stop moving until the landing gear is finished
65
FUEL - With the boost pump in NORM, when will it activate automatically?
- Engine start
- Crossfeed
- Low fuel pressure at low press. side of fuel pump
- APU running (right side only)
66
How is the power brake system pressurized?
A DC motor drives a hydraulic pump from a separate hydraulic reservoir
67
If the power brakes fail, is there a back-up system?
yes, pneumatically with nitrogen.
68
Is anti-skid protection still available when using the emergency brake system?
no.
69
At what speed will the anti-skid protection activate during taxi and takeoff?
Accelerating through 10-12 knots.
70
If operating with the battery switch in the EMER position, with the power brakes and anti-skid operate normally?
No.
71
Nose tire inflation pressure
135 +/-5 PSI with weight on wheels
100-112 = dismount and inspect
less than 100 = replace
72
Main tire inflation pressure
210 +2/-5 PSI
164-184 = Dismount and inspect
Less than 164 = Replace
73
How is the landing gear controlled and actuated?
Electrically controlled, hydraulically actuated.
74
ELECTRICAL SYSTEM - What 3 relays are controlled by the avionics power switch?
L/H avionics relay
R/H avionics relay
Avionics emergency relay
75
ELECTRICAL SYSTEM - Are the EEC's and digital pressurization control on the emer bus?
No
76
LIGHTING - What does it mean if amber light by EMER LTG switch is on?
Main DC is on and EMER lights are not armed.
77
MASTER WARNING SYS - If a malfunction illuminating the master caution light clears up will master caution light go out automatically?
Yes
78
MASTER WARNING SYS - If a malfunction illuminating the master warning light clears up will master warning light go out automatically?
No
79
MASTER WARNING SYS - What 3 conditions other than a red annunciator activate the master warning light?
- Loss of current limiter and generator on same side.
- Dual gen failure
- Uncommanded TR deploy.
80
MASTER WARNING SYS - When will CAB ALT light illuminate, if pressurization control is in low alt. airport mode?
If cabin alt > 10k ft and a/c alt. is >24.5k ft
81
MASTER WARNING SYS - When will CAB ALT light illuminate, if pressurization control is in high alt. airport mode?
If cabin alt > 14.5k ft and a/c alt. is <24.5k ft
82
How is the landing gear held in the up-locked and down-locked positions?
```
Up = Up-lock hook mechanism are hydraulically actuated to hold the gear.
Down = Internal mechanical lock in the actuator is released by hydraulic pressure.
```
83
How are the landing gear locked in the down position?
by locking mechanisms internal to the gear actuator.
84
Is there a back-up system for landing gear extension?
Yes, the up-locks are released mechanically with cables (also pneumatically with nitrogen)
85
If one of the landing gear does not release from its up-lock when pulling and rotating the emergency gear extension T-handle, is there any other way to release the gear from the up-lock?
Yes, nitrogen from the emergency air bottle will release the up-lock and extend the gear.
86
If the emergency mechanical up-lock release fails to release the gear, how can the gear be extended?
Firing the blow-down bottle will route nitrogen to the hydraulic up-lock actuators to release them before blowing the gear down.
87
If one of the landing gear lights does not illuminate, how do you know if the landing gear is down and locked?
- Red UNLOCK annunciator is not illuminated
- HYD PRESS annunciator is not illuminated
- Rotary test - check bulbs
- Flap selector beyond approach - no gear warning horn.
88
If the backup extension is used, can the landing gear be retracted?
No.
89
Is maintenance required after gear has been blown down?
Yes
90
why does the nose gear have a chine?
deflects water away from the engines
91
Is there any restriction to towing the aircraft with the control lock engaged?
Yes, nose wheel deflection beyond 60 degrees may cause structural damage.
92
With the control lock released, what is the turning limit of the nosewheel?
95 degrees
93
what is the nosewheel turning limit with the use of differential braking?
20 degrees
94
MASTER WARNING SYS - If STAB MISCOMP light illuminates on ground what else illuminates?
NO TAKEOFF
95
MASTER WARNING SYS - What 4 items will illuminate the NO TAKEOFF light on ground?
- Flaps <7 or >15
- Speed brakes extended
- Horiz stab out of position
- Trim not set for takeoff
96
MASTER WARNING SYS - What will ccause the NO TAKEOFF light to flash and activate master caution?
Advancing power beyond climb setting
97
MASTER WARNING SYS - What will illuminate EMER PRESS?
- ACM overheat
| - Cabin alt >14.5k ft
98
MASTER WARNING SYS - When can you expect to see AHRS 1/2 light?
A/C power on with avionics master OFF and stby power switch ON
99
MASTER WARNING SYS - What does it mean if the ENG ANTI-ICE light begins to flash 4 MINUTES AND 45 SECONDS after it was turned on?
Nacelle lip is not up to temp or stator valve didnt open
100
MASTER WARNING SYS - What does it mean if the ENG ANTI-ICE light flashes after turning engine anti-ice off?
Stator valve didnt close
101
MASTER WARNING SYS - What subsystems inop if EEC MANUAL light illuminates?
Throttle detents and engine sync
102
MASTER WARNING SYS - What 3 failures can illuminate TAIL DEICE FAIL light?
- Tail deice valve loss of power
- Tail deice system loss of pressure
- Fault in the tail deice timer
103
MASTER WARNING SYS - What causes the FUEL XFEED to flash and activate master caution?
Crossfeed was turned off but the crossfeed valve did not close
104
MASTER WARNING SYS - What will cause the FUEL BOOST annunciator to flash and activate master caution?
Fuel boost pump was activated due to low fuel pressure sensing
105
Could the gear ever be inadvertently retracted on the ground
Yes, if the gear handle is moved out of position
106
What happens to the down-locking solenoid in the gear handle if DC power is lost while the handle is down?
it stays locked because it must be energized to open.
107
What three conditions will sound the gear warning horn?
Gear up, both throttles below 70% N2 and:
- Flaps greater than 15
OR
-Radio Altimeter below 500 ft AGL
OR
an inop Radio Altimeter and speed below 150 Kts.
108
After landing using emergency brakes, can you taxi to parking?
No.
109
What systems operate from the main aircraft hydraulic pumps?
- Landing Gear
- Flaps
- Speed brakes
- Thrust reversers
- Horizontal stabilizer
110
What indication would you expect to see if the right engine hydraulic pump failed?
the LO HYD FLO/R annunciator will illuminate flashing and the Master Caution will illuminate
111
What is indicated by a HYD FLOW LOW light?
Probable pump failure
112
MASTER WARNING SYS - Will LAV DOOR light illuminate any time the lavatory door is not latched open?
No, only if the flaps are not up.
113
MASTER WARNING SYS - What subsystem is directly affected if the BLD AIR O'HEAT illuminates?
The wing anti-ice system on that side shuts down
114
MASTER WARNING SYS - What is indicated by a CHECK PFD light?
A display unit wrap-around failure between the indicated IAC and PFD
115
FUEL - Total usable fuel
6790lbs 1006USG
116
FUEL - How many drains and where?
5 in each tank: 4 along center wing skid and 1 outboard of wheel well
117
FUEL - What powers primary ejector pump
Motive flow from respective engine driven pump
118
FUEL - What is the purpose of primary ejector pump?
Provides positive pressure to engine driven fuel pump
119
FUEL - What indication would you expect to see if the right primary ejector pump failed?
Right engine would flame out
120
FUEL - What indication would you expect to see if the right primary ejector pump failed?
- Momentary illumination of LO FUEL PRESS / R annunciator
| - Automatic operation of the right electric fuel boost pump and illumination of its annunciator
121
FUEL - With boost pump switch in OFF position, when will it operate?
It will not.
122
FUEL - With the boost pump in NORM, when will it activate automatically?
- Engine start
- Crossfeed
- Low fuel pressure at low press. side of fuel pump
- APU running (right side only)
123
If both engine driven hydraulic pumps fail, can you extend the landing gear?
Yes, blow it down
124
What does an illuminated HYD PRESS annunciator indicate?
Hydraulic system is pressurized
125
How are the speed brakes held extended?
Trapped hydraulic pressure.
126
If a total hydraulic system failure occurs, with the speed brakes extended, can the speed brakes be stowed?
Yes, moving the speed brake switch to the retract position will allow the speed brakes to float in trail
127
If a total electrical system failure occurs with speed brakes extended, will the speed brakes retract manually or automatically?
automatically
128
How are the flaps held extended?
trapped hydraulic pressure
129
How are the Thrust reversers held in the extended position?
Constant hydraulic pressure
130
How are the thrust reversers held in the EMER position?
Constant hydraulic pressure.
131
FUEL - When does LO FUEL LEVEL annunciator illuminate
Remaining fuel is 360+-20lbs
132
FUEL - What does an illuminated FUEL FILTER BP annunciator mean?
Actual or impending fuel filter bypass
133
FUEL - What indications when you select fuel crossfeed?
FUEL XFEED and FUEL BOOST L/R illuminate
134
FUEL - How would you know fuel crossfeed is taking place?
Monitor quantity guages
135
FUEL - Crossfeed rate
700-900lb/hr depending on demand
136
FUEL - What happens when you pull down the defuel selector lever for left tank?
Left tank will NOT be defueled
137
FUEL - If a fuel gauge annunciator illuminates, what must you do after landing?
Leave DC power on until mx can read faults
138
What main aircraft hydraulic systems will work normally when operating with the battery switch in the EMER position?
Flaps
Stabilizer
Landing gear
139
What is the effect on the hydraulic system and subsystems driven by it, if main DC power is lost and only the EMER bus is powered?
The landing gear, flaps, and stabilizer will still operate with the battery in EMER because their control valves are on the EMER bus.
140
How do you know if any of the three hydraulic filters are bypassing?
you don't
141
How is hydraulic system overpressure protection provided?
by a 1500 PSI protection valve.
142
Where do you find the hydraulic reservoir quantity indicator?
In the tailcone
143
PRESSURIZATION: on the pressurization controller there are two lights, one yellow and one red. If the yellow light illuminates, what does it mean?
The pressurization controller has switched from the auto schedule to the isobaric mode
144
PRESSURIZATION: How would you control cabin pressurization in isobaric mode?
- Manually set desired level off in the SET ALT window
- during descent for landing, press the FL button on the controller
- CA will replace FL in the SET ALT window
- Set the landing field elevation in the SET ALT window.
145
PRESSURIZATION: with the battery switch in the EMER position, how would you control cabin pressurization?
- Pressurization system, select - MANUAL
| - Control cabin pressurization with the manual toggle switch
146
Will the manual dump switch work with the battery switch in the EMER position?
No
147
PRESSURIZATION: What is the normal cabin differential?
9.3 PSI
148
PRESSURIZATION: If the oxygen bottle reads 1800 PSI, does that mean oxygen is available to crew and passengers?
no
149
PRESSURIZATION: How would you confirm oxygen is available to the crew and passengers?
By manually checking that a continuous supply of oxygen is available at the crew masks. (hold 2 buttons at the same time)
150
PRESSURIZATION: If the passenger oxygen selector is in the OFF position, will the passenger oxygen masks drop automatically drop when the cabin altitude exceeds 14,500 ft?
no
151
PRESSURIZATION: To what altitude will sea level pressure be maintained?
25,230 ft
152
PRESSURIZATION: What should the cabin altitude be at 45,000'?
6800 Ft.
153
PRESSURIZATION: The outflow valves are not spring loaded, what provides pressure opposing the control pressure to move the outflow valves?
Differential pressure from tailcone air.
154
PRESSURIZATION: at what altitude does the max altitude limiter close the outflow valves?
14,500 +/- 500'
155
PRESSURIZATION: What are the climb and dive rates in AUTO schedule mode?
Climb: +600 fpm
Dive: -500 fpm
156
PRESSURIZATION: What should you see when pressing the EXER button on the ground?
The aircraft will pressurize to -200 ft and a rate of 100 fpm, when releasing the button, a display test will be performed and the cabin will come back up to an unpressurized state.
157
PRESSURIZATION: What happens if you do the EXER test in flight?
Only a lap test is performed
158
PRESSURIZATION: When will the control go into the High altitude airport mode?
When the aircraft is landing or departing from field elevations between 8000' - 14,500'
159
PRESSURIZATION: What happens to the pressurization control if the signal from the No. 1 ADC is subsequently restored?
It resets to automatic mode
160
PRESSURIZATION: What indicates a pressurization controller failure?
A red light illuminates and the altitude and rate windows go blank.
161
PRESSURIZATION: How is pressurization controlled if the controller fails?
By using the manual toggle switch
162
PRESSURIZATION: What does moving the manual toggle switch to the UP position do?
It opens the outflow valve, climbing the cabin.
163
PRESSURIZATION: At what throttle setting does the cabin begin to pre-pressurize?
85% N2 on both throttles.
164
AIR CONDITIONING: What are the three air distribution networks?
Overhead cold air
Lower cabin air
Cockpit air
165
AIR CONDITIONING: Which networks get cold/warm air mixture?
Lower cabin and cockpit air
166
AIR CONDITIONING: If an ACM O'HEAT condition occurs, what comes on automatically?
Emergency pressurization
167
AIR CONDITIONING: Will the system reset automatically once the ACM cools down?
Yes
168
AIR CONDITIONING: Will one engine maintain the cabin at max differential at idle power.
Yes
169
AIR CONDITIONING: Will EMER pressurization work on the ground
No, the annunciator will illuminate, but the valves will remain closed.
170
AIR CONDITIONING: If the EMER PRESS annunciator is illuminated, which engine is supplying pressurization to the cabin?
The left engine
171
AIR CONDITIONING: What would cause the emergency pressurization to activate automatically?
ACM overheat and shutdown. OR cabin altitude above 14,500 ft.
172
ICE AND RAIN PROTECTION: when should anti-ice protection be turned on?
When operating in visible moisture between +10C and -30C
173
ICE AND RAIN PROTECTION: Which engine components are ice protected and how?
```
Nacelle inlet - bleed air
Nose cone - bleed air
T1 probe - bleed air
first and second stage stator vanes - bleed air
T0 probe - electric
TT0 probe - bleed air
```
174
ICE AND RAIN PROTECTION: What turns on the heat to the T0 probe?
The engine anti-ice switch
175
ICE AND RAIN PROTECTION: What does the T0 probe do?
The T0 probe provides temperature information to the EECS and the RAT
176
ICE AND RAIN PROTECTION: What does the TT0 probe do?
The TT0 probe provides temperature information to the FCU when the EECS fail or during engine operation with the EECS switch in the manual position.
177
ICE AND RAIN PROTECTION: If the STBY P/S HTR annunciator illuminates, what two systems may be be be affected?
The Meggitt airspeed and altitude may not be reliable.
| The horizontal stabilizer may not operate normally
178
ICE AND RAIN PROTECTION: If the AOA HTR FAIL annunciator illuminates, what two systems may not be reliable?
The AOA indicator and tape
| The stick shaker
179
ICE AND RAIN PROTECTION: What indication do you have that the wing and engine anti-ice systems are operating correctly?
- ITT rise and ignition lights when selecting Engine Anti-ice - ON
- The WING ANTI-ICE and ENG ANI-ICE annunciators remain extinguished
180
ICE AND RAIN PROTECTION: What indication do you have that the tail de-ice is operating correctly in AUTO?
TAIL DE-ICE PRESS white annunciator illuminates 6 seconds on, 6 seconds off, 6 seconds on, approximately 3 minutes off.
181
ICE AND RAIN PROTECTION: What is the minimum temperature for tail de-ice boot operation and why?
-40C, the boots will crack
182
ICE AND RAIN PROTECTION: When are the windshield ice detection lights on?
Anytime the instrument panel lights are on
183
ICE AND RAIN PROTECTION: What turns the heat to the rosemount probe on?
avionics power switch and squat switch
184
ICE AND RAIN PROTECTION: What is the function of the OVERRIDE position on the windshield heat switch?
It heats up faster
185
ICE AND RAIN PROTECTION: What is indicated if the W/S O'HEAT and the same side W/S FAULT lights cycle on and off? and can the system still be used?
A controller failure, yes if necessary but should be turned off if not needed.
186
ICE AND RAIN PROTECTION: What does it mean if the engine anti-ice annunciators do not go out, but start flashing 4 minutes and 45 seconds after the engine anti-ice was turned on?
The nacelle inlet did not get up to operating temperature, or the stator vane valve did not open.
187
ICE AND RAIN PROTECTION: What does it mean if after turning engine anti-ice off, the annunciator starts to flash?
The stator vane valve did not close
188
ICE AND RAIN PROTECTION: What does it mean if the wing anti-ice annunciators do not go out, but start flashing 4 minutes and 45 seconds after wing anti-ice was turned on?
The wing did not get up to operating temperature
189
ICE AND RAIN PROTECTION: If a wing overheat condition occurs, will it reset automatically?
Yes, if the wing temperature drops below 160F
190
ICE AND RAIN PROTECTION: What may happen differently than normal if you perform an engine anti-ice test when the ambient temperature is above 15C, and how do you know it's working?
The anti-ice lights may not come on, in this case an ITT rise is the only indication the system is working.
191
PNEUMATICS: What systems utilize service air?
Tail de-ice boots
Door seals
Outflow valves
Throttle detents
192
PNEUMATICS: How is bleed air pre-cooled on the ground and in the air?
Ground: Engine bypass air
Flight: Ram air
193
PNEUMATICS: How is bleed air outlet temperature controlled?
An electrically actuated door on the ram air inlet scoop
194
PNEUMATICS: What happens to the anti-ice system if a BLD AIR O'HEAT light illuminates?
The wing anti-ice on that side shuts down
195
THRUST REVERSERS: At what speed must thrust reversers be reduced to idle?
60 kts
196
THRUST REVERSERS: What is maximum reverse thrust?
75% of takeoff thrust
197
THRUST REVERSERS: What is max deployed time?
3 minutes in any 10 minute period
198
OIL SYSTEM: When is the best time to check the oil quantity?
10 minutes after engine shutdown
199
OIL SYSTEM: How do you check the oil level?
Visually check the oil level on the sight indicator
200
OIL SYSTEM: What is the rate of oil consumption per quart?
1 quart per 8 hours
201
OIL SYSTEM: What is the oil sump quantity?
2.44 quarts
202
POWERPLANT - What engines?
PW 545B twin spool, high bypass(80%), turbofan. 4095lbs thrust @ sea level
203
POWERPLANT - Primary indication to set power
N1
204
POWERPLANT - Purpose of compressor bleed-off valve?
To prevent engine surges and compressor stalls.
205
POWERPLANT - Pressing fire button does what 5 things
Cutoff: fuel, hydro, oil
Arms bottles
Opens Gen field relay
Lockout TR on that side
206
POWERPLANT - Ignition in NORM when does it activate
- Start
| - Anti-ice on
207
POWERPLANT - Does green light mean igniters are working?>
No. Only that the exciter box is being powered
208
POWERPLANT - Engine instrumentation available with batt in EMER
N1 tapes and digital readout
209
POWERPLANT - When ignition is in SEC what does it mean
Secondary power to igniters from EMER bus
210
POWERPLANT - Normal ground idle N2
about 50%
211
POWERPLANT - Normal flight idle N2
about 60%
212
POWERPLANT - Where is the fuel heater located?
Inside FCU between low pressure and high pressure stages of the engine driven fuel pump
213
POWERPLANT - Will engine sync work with throttles in TO detent?
No
