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XLS Initial > Oral guide questions > Flashcards

Oral guide questions Flashcards

1
Q

AIRCRAFT GENERAL - How tall is the tail?

A

17.2ft

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2
Q

AIRCRAFT GENERAL - What is the wingspan?

A

55.7ft

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3
Q

AIRCRAFT GENERAL -

What is the distance between the main wheels?

A

14.9ft

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4
Q

AIRCRAFT GENERAL - What is the curb to curb turning radius?

A

38ft

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5
Q

AIRCRAFT GENERAL - What is the wall to wall turning radius?

A

70.6ft

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6
Q

AIRCRAFT GENERAL - Which door latching pin actuates the door seal valves?

A

Lower aft

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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

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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
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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
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10
Q

ELECTRICAL SYSTEM - If the battery voltage is 23v can you start the APU and then start the engines?

A

No

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11
Q

Where are the emergency exits located?

A

Main cabin entrance door

Emergency Exit Door located in aft lav area - right side

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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

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13
Q

ELECTRICAL SYSTEM - What is the normal output for each generator?

A

28.5v regulated and 300 amps

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14
Q

ELECTRICAL SYSTEM - What is the allowable difference between generator load sharing?

A

10% of total system load (30 amps)

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15
Q

ELECTRICAL SYSTEM -

What does the gen. control unit do?

A

Parallels
Protects
Regulates

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16
Q

ELECTRICAL SYSTEM - What is the normal output for each generator?

A

28.5v regulated and 300 amps

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17
Q

Where are the handheld fire extinguishers located in the aircraft?

A

Under right pilot seat and left rear passenger seat.

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18
Q

What equipment is available to the crew for smoke in the cockpit?

A

Crew oxygen masks and smoke goggles

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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.

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20
Q

Can you use autopilot if electric trim is inop?

A

no

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21
Q

ELECTRICAL SYSTEM - How many emer. batts are there and what for

A

4: 2 for avionics, 2 for emer lighting

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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

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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.

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24
Q

What happens to the cabin pressurization controller if the No. 1 MADC fails?

A

It switches to ISOBARIC mode of operation

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25
Q

Can the left side avionics be tuned with the right side RMU?

A

Yes, by pressing the 1/2 button on the right RMU, you can tune the appropriate avionics on the left side.

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26
Q

ELECTRICAL SYSTEM - with batt switch in EMER, what powers emer bus?

A

Battery through battery bus

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27
Q

What is the max ambient temp for ground ops?

A

+54C

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28
Q

ELECTRICAL SYSTEM - How would you know if a right side current limiter has blown when you turn the batt switch on?

A
  • A steady red master warning on left side
  • Only left annunciators illuminated
  • Right engine off flags displayed
  • AFT J-BOX LMT illuminated
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29
Q

ELECTRICAL SYSTEM - How would you know if a current limiter has been blown after both engines started?

A

Amp imbalance indicated. Side with blow limiter shows less load than good side

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30
Q

ELECTRICAL SYSTEM - What is significance of start button illuminating during start?

A

Start relay has closed

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31
Q

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?

A

Generator assisted battery start aka 1/3batt start

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32
Q

ELECTRICAL SYSTEM - How long will fully charged battery last?

A

10min with batt - ON

30min with batt - EMER

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33
Q

ELECTRICAL SYSTEM - How long will the Meggitt battery power stby attitude indicator?

A

3.5hrs

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34
Q

ELECTRICAL SYSTEM - Will AHRS emer batt pack power the FMS if the batt switch is in emer?

A

No. The switch must be ON and avionics switch OFF

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35
Q

ELECTRICAL SYSTEM - How many emer. batts are there and what for

A

4: 2 for avionics, 2 for emer lighting

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36
Q

ELECTRICAL SYSTEM - Is batt isolation relay (BATT ON) powered open or closed?

A

Powered closed

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37
Q

ELECTRICAL SYSTEM - Can batt charge from gpu if batt switch off

A

Yes

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38
Q

ELECTRICAL SYSTEM - Batt disconnect switch powered open or closed

A

powered open by removing the ground

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39
Q

ELECTRICAL SYSTEM - with batt switch off, what powers emer bus?

A

Generators through crossfeed bus

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40
Q

What are the PRIMUS 1000 limitations?

A

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

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41
Q

When must the Meggitt be tested

A

Before each flight

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42
Q

Can passenger masks be deployed if DC power fails?

A

Yes, but you must manually turn the switch on

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43
Q

MASTER WARNING SYS - When will HYD PRESS light begin to flash and illuminate master caution light?

A

When on > 40 seconds in flight

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44
Q

What is the lowest pressure the O2 bottle may have before servicing?

A

400 PSI, but should be serviced anytime out of the green band (600 PSI)

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45
Q

What size oxygen bottle do we have?

A

76 cu ft

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46
Q

Which primary flight controls use cables for operation

A

Ailerons
Elevator
Rudder

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47
Q

Are the ailerons and rudder interconnected?

A

Yes

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48
Q

What are the flap position settings?

A

0,7,15,35 degrees down

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49
Q

Can flaps be set to intermediate positions?

A

yes

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50
Q

When does the stabilizer move?

A

It moves to down positions anytime flaps selected other than UP.
Moves to UP position when flaps are selected UP

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51
Q

What does it mean if the STAB MIS COMP annunciator illuminates?

A

The stab is not in the same position the flap handle is in.

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52
Q

ELECTRICAL SYSTEM - Avionics power relays powered open or closed

A

Powered open

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53
Q

ELECTRICAL SYSTEM - What do the two avionics emergency batt packs power?

A

Left: Stby attitude indicator (meggitt)
Right: AHRS 2 and FMS

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54
Q

MASTER WARNING SYS - What will cause the FUEL BOOST annunciator to flash and activate master caution?

A

Fuel boost pump was activated due to low fuel pressure sensing

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55
Q

ELECTRICAL SYSTEM - How is batt take offline during gpu start?

A

Batt disconnect relay is auto. powered open

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56
Q

ELECTRICAL SYSTEM - Will the battery disconnect switch and relay work with the batt in the OFF position?

A

No

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57
Q

ELECTRICAL SYSTEM - How is batt take offline during apu start?

A

Batt disconnect relay is auto. powered open

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58
Q

ELECTRICAL SYSTEM - What instrument lighting is also powered by the Meggitt’s emer battery?

A

Stby HSI and N1 indicators

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59
Q

ELECTRICAL SYSTEM - Will AHRS emer batt pack power the FMS if the batt switch is in emer?

A

No. The switch must be ON and avionics switch OFF

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60
Q

How many trim tabs are there on the flight controls?

A

4- one on each elevator, one on the rudder, one on the left aileron.

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61
Q

If the electric trim fails the pre-flight operation test, can the airplane be hand flown?

A

no.

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62
Q

At what airspeed will stabilizer movement be stopped?

A

215 knots +/- 10

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63
Q

If a major failure were to occur in the stabilizer movement system, what setting will the stabilizer achieve?

A

The failsafe sets it to cruise positions (+1 degree)

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64
Q

If the landing gear is put in motion while the stabilizer is moving, which system gets priority?

A

The landing gear, the stab will stop moving until the landing gear is finished

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65
Q

FUEL - With the boost pump in NORM, when will it activate automatically?

A
  • Engine start
  • Crossfeed
  • Low fuel pressure at low press. side of fuel pump
  • APU running (right side only)
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66
Q

How is the power brake system pressurized?

A

A DC motor drives a hydraulic pump from a separate hydraulic reservoir

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67
Q

If the power brakes fail, is there a back-up system?

A

yes, pneumatically with nitrogen.

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68
Q

Is anti-skid protection still available when using the emergency brake system?

A

no.

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69
Q

At what speed will the anti-skid protection activate during taxi and takeoff?

A

Accelerating through 10-12 knots.

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70
Q

If operating with the battery switch in the EMER position, with the power brakes and anti-skid operate normally?

A

No.

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71
Q

Nose tire inflation pressure

A

135 +/-5 PSI with weight on wheels
100-112 = dismount and inspect
less than 100 = replace

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72
Q

Main tire inflation pressure

A

210 +2/-5 PSI
164-184 = Dismount and inspect
Less than 164 = Replace

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73
Q

How is the landing gear controlled and actuated?

A

Electrically controlled, hydraulically actuated.

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74
Q

ELECTRICAL SYSTEM - What 3 relays are controlled by the avionics power switch?

A

L/H avionics relay
R/H avionics relay
Avionics emergency relay

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75
Q

ELECTRICAL SYSTEM - Are the EEC’s and digital pressurization control on the emer bus?

A

No

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76
Q

LIGHTING - What does it mean if amber light by EMER LTG switch is on?

A

Main DC is on and EMER lights are not armed.

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77
Q

MASTER WARNING SYS - If a malfunction illuminating the master caution light clears up will master caution light go out automatically?

A

Yes

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78
Q

MASTER WARNING SYS - If a malfunction illuminating the master warning light clears up will master warning light go out automatically?

A

No

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79
Q

MASTER WARNING SYS - What 3 conditions other than a red annunciator activate the master warning light?

A
  • Loss of current limiter and generator on same side.
  • Dual gen failure
  • Uncommanded TR deploy.
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80
Q

MASTER WARNING SYS - When will CAB ALT light illuminate, if pressurization control is in low alt. airport mode?

A

If cabin alt > 10k ft and a/c alt. is >24.5k ft

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81
Q

MASTER WARNING SYS - When will CAB ALT light illuminate, if pressurization control is in high alt. airport mode?

A

If cabin alt > 14.5k ft and a/c alt. is <24.5k ft

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82
Q

How is the landing gear held in the up-locked and down-locked positions?

A 
Up = Up-lock hook mechanism are hydraulically actuated to hold the gear.
Down = Internal mechanical lock in the actuator is released by hydraulic pressure.
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83
Q

How are the landing gear locked in the down position?

A

by locking mechanisms internal to the gear actuator.

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84
Q

Is there a back-up system for landing gear extension?

A

Yes, the up-locks are released mechanically with cables (also pneumatically with nitrogen)

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85
Q

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?

A

Yes, nitrogen from the emergency air bottle will release the up-lock and extend the gear.

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86
Q

If the emergency mechanical up-lock release fails to release the gear, how can the gear be extended?

A

Firing the blow-down bottle will route nitrogen to the hydraulic up-lock actuators to release them before blowing the gear down.

87
Q

If one of the landing gear lights does not illuminate, how do you know if the landing gear is down and locked?

A
  • 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
Q

If the backup extension is used, can the landing gear be retracted?

A

No.

89
Q

Is maintenance required after gear has been blown down?

A

Yes

90
Q

why does the nose gear have a chine?

A

deflects water away from the engines

91
Q

Is there any restriction to towing the aircraft with the control lock engaged?

A

Yes, nose wheel deflection beyond 60 degrees may cause structural damage.

92
Q

With the control lock released, what is the turning limit of the nosewheel?

A

95 degrees

93
Q

what is the nosewheel turning limit with the use of differential braking?

A

20 degrees

94
Q

MASTER WARNING SYS - If STAB MISCOMP light illuminates on ground what else illuminates?

A

NO TAKEOFF

95
Q

MASTER WARNING SYS - What 4 items will illuminate the NO TAKEOFF light on ground?

A
  • Flaps <7 or >15
  • Speed brakes extended
  • Horiz stab out of position
  • Trim not set for takeoff
96
Q

MASTER WARNING SYS - What will ccause the NO TAKEOFF light to flash and activate master caution?

A

Advancing power beyond climb setting

97
Q

MASTER WARNING SYS - What will illuminate EMER PRESS?

A
  • ACM overheat

- Cabin alt >14.5k ft

98
Q

MASTER WARNING SYS - When can you expect to see AHRS 1/2 light?

A

A/C power on with avionics master OFF and stby power switch ON

99
Q

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?

A

Nacelle lip is not up to temp or stator valve didnt open

100
Q

MASTER WARNING SYS - What does it mean if the ENG ANTI-ICE light flashes after turning engine anti-ice off?

A

Stator valve didnt close

101
Q

MASTER WARNING SYS - What subsystems inop if EEC MANUAL light illuminates?

A

Throttle detents and engine sync

102
Q

MASTER WARNING SYS - What 3 failures can illuminate TAIL DEICE FAIL light?

A
  • Tail deice valve loss of power
  • Tail deice system loss of pressure
  • Fault in the tail deice timer
103
Q

MASTER WARNING SYS - What causes the FUEL XFEED to flash and activate master caution?

A

Crossfeed was turned off but the crossfeed valve did not close

104
Q

MASTER WARNING SYS - What will cause the FUEL BOOST annunciator to flash and activate master caution?

A

Fuel boost pump was activated due to low fuel pressure sensing

105
Q

Could the gear ever be inadvertently retracted on the ground

A

Yes, if the gear handle is moved out of position

106
Q

What happens to the down-locking solenoid in the gear handle if DC power is lost while the handle is down?

A

it stays locked because it must be energized to open.

107
Q

What three conditions will sound the gear warning horn?

A

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
Q

After landing using emergency brakes, can you taxi to parking?

A

No.

109
Q

What systems operate from the main aircraft hydraulic pumps?

A
  • Landing Gear
  • Flaps
  • Speed brakes
  • Thrust reversers
  • Horizontal stabilizer
110
Q

What indication would you expect to see if the right engine hydraulic pump failed?

A

the LO HYD FLO/R annunciator will illuminate flashing and the Master Caution will illuminate

111
Q

What is indicated by a HYD FLOW LOW light?

A

Probable pump failure

112
Q

MASTER WARNING SYS - Will LAV DOOR light illuminate any time the lavatory door is not latched open?

A

No, only if the flaps are not up.

113
Q

MASTER WARNING SYS - What subsystem is directly affected if the BLD AIR O’HEAT illuminates?

A

The wing anti-ice system on that side shuts down

114
Q

MASTER WARNING SYS - What is indicated by a CHECK PFD light?

A

A display unit wrap-around failure between the indicated IAC and PFD

115
Q

FUEL - Total usable fuel

A

6790lbs 1006USG

116
Q

FUEL - How many drains and where?

A

5 in each tank: 4 along center wing skid and 1 outboard of wheel well

117
Q

FUEL - What powers primary ejector pump

A

Motive flow from respective engine driven pump

118
Q

FUEL - What is the purpose of primary ejector pump?

A

Provides positive pressure to engine driven fuel pump

119
Q

FUEL - What indication would you expect to see if the right primary ejector pump failed?

A

Right engine would flame out

120
Q

FUEL - What indication would you expect to see if the right primary ejector pump failed?

A
  • Momentary illumination of LO FUEL PRESS / R annunciator

- Automatic operation of the right electric fuel boost pump and illumination of its annunciator

121
Q

FUEL - With boost pump switch in OFF position, when will it operate?

A

It will not.

122
Q

FUEL - With the boost pump in NORM, when will it activate automatically?

A
  • Engine start
  • Crossfeed
  • Low fuel pressure at low press. side of fuel pump
  • APU running (right side only)
123
Q

If both engine driven hydraulic pumps fail, can you extend the landing gear?

A

Yes, blow it down

124
Q

What does an illuminated HYD PRESS annunciator indicate?

A

Hydraulic system is pressurized

125
Q

How are the speed brakes held extended?

A

Trapped hydraulic pressure.

126
Q

If a total hydraulic system failure occurs, with the speed brakes extended, can the speed brakes be stowed?

A

Yes, moving the speed brake switch to the retract position will allow the speed brakes to float in trail

127
Q

If a total electrical system failure occurs with speed brakes extended, will the speed brakes retract manually or automatically?

A

automatically

128
Q

How are the flaps held extended?

A

trapped hydraulic pressure

129
Q

How are the Thrust reversers held in the extended position?

A

Constant hydraulic pressure

130
Q

How are the thrust reversers held in the EMER position?

A

Constant hydraulic pressure.

131
Q

FUEL - When does LO FUEL LEVEL annunciator illuminate

A

Remaining fuel is 360+-20lbs

132
Q

FUEL - What does an illuminated FUEL FILTER BP annunciator mean?

A

Actual or impending fuel filter bypass

133
Q

FUEL - What indications when you select fuel crossfeed?

A

FUEL XFEED and FUEL BOOST L/R illuminate

134
Q

FUEL - How would you know fuel crossfeed is taking place?

A

Monitor quantity guages

135
Q

FUEL - Crossfeed rate

A

700-900lb/hr depending on demand

136
Q

FUEL - What happens when you pull down the defuel selector lever for left tank?

A

Left tank will NOT be defueled

137
Q

FUEL - If a fuel gauge annunciator illuminates, what must you do after landing?

A

Leave DC power on until mx can read faults

138
Q

What main aircraft hydraulic systems will work normally when operating with the battery switch in the EMER position?

A

Flaps
Stabilizer
Landing gear

139
Q

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?

A

The landing gear, flaps, and stabilizer will still operate with the battery in EMER because their control valves are on the EMER bus.

140
Q

How do you know if any of the three hydraulic filters are bypassing?

A

you don’t

141
Q

How is hydraulic system overpressure protection provided?

A

by a 1500 PSI protection valve.

142
Q

Where do you find the hydraulic reservoir quantity indicator?

A

In the tailcone

143
Q

PRESSURIZATION: on the pressurization controller there are two lights, one yellow and one red. If the yellow light illuminates, what does it mean?

A

The pressurization controller has switched from the auto schedule to the isobaric mode

144
Q

PRESSURIZATION: How would you control cabin pressurization in isobaric mode?

A
  • 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
Q

PRESSURIZATION: with the battery switch in the EMER position, how would you control cabin pressurization?

A
  • Pressurization system, select - MANUAL

- Control cabin pressurization with the manual toggle switch

146
Q

Will the manual dump switch work with the battery switch in the EMER position?

A

No

147
Q

PRESSURIZATION: What is the normal cabin differential?

A

9.3 PSI

148
Q

PRESSURIZATION: If the oxygen bottle reads 1800 PSI, does that mean oxygen is available to crew and passengers?

A

no

149
Q

PRESSURIZATION: How would you confirm oxygen is available to the crew and passengers?

A

By manually checking that a continuous supply of oxygen is available at the crew masks. (hold 2 buttons at the same time)

150
Q

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?

A

no

151
Q

PRESSURIZATION: To what altitude will sea level pressure be maintained?

A

25,230 ft

152
Q

PRESSURIZATION: What should the cabin altitude be at 45,000’?

A

6800 Ft.

153
Q

PRESSURIZATION: The outflow valves are not spring loaded, what provides pressure opposing the control pressure to move the outflow valves?

A

Differential pressure from tailcone air.

154
Q

PRESSURIZATION: at what altitude does the max altitude limiter close the outflow valves?

A

14,500 +/- 500’

155
Q

PRESSURIZATION: What are the climb and dive rates in AUTO schedule mode?

A

Climb: +600 fpm
Dive: -500 fpm

156
Q

PRESSURIZATION: What should you see when pressing the EXER button on the ground?

A

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
Q

PRESSURIZATION: What happens if you do the EXER test in flight?

A

Only a lap test is performed

158
Q

PRESSURIZATION: When will the control go into the High altitude airport mode?

A

When the aircraft is landing or departing from field elevations between 8000’ - 14,500’

159
Q

PRESSURIZATION: What happens to the pressurization control if the signal from the No. 1 ADC is subsequently restored?

A

It resets to automatic mode

160
Q

PRESSURIZATION: What indicates a pressurization controller failure?

A

A red light illuminates and the altitude and rate windows go blank.

161
Q

PRESSURIZATION: How is pressurization controlled if the controller fails?

A

By using the manual toggle switch

162
Q

PRESSURIZATION: What does moving the manual toggle switch to the UP position do?

A

It opens the outflow valve, climbing the cabin.

163
Q

PRESSURIZATION: At what throttle setting does the cabin begin to pre-pressurize?

A

85% N2 on both throttles.

164
Q

AIR CONDITIONING: What are the three air distribution networks?

A

Overhead cold air
Lower cabin air
Cockpit air

165
Q

AIR CONDITIONING: Which networks get cold/warm air mixture?

A

Lower cabin and cockpit air

166
Q

AIR CONDITIONING: If an ACM O’HEAT condition occurs, what comes on automatically?

A

Emergency pressurization

167
Q

AIR CONDITIONING: Will the system reset automatically once the ACM cools down?

A

Yes

168
Q

AIR CONDITIONING: Will one engine maintain the cabin at max differential at idle power.

A

Yes

169
Q

AIR CONDITIONING: Will EMER pressurization work on the ground

A

No, the annunciator will illuminate, but the valves will remain closed.

170
Q

AIR CONDITIONING: If the EMER PRESS annunciator is illuminated, which engine is supplying pressurization to the cabin?

A

The left engine

171
Q

AIR CONDITIONING: What would cause the emergency pressurization to activate automatically?

A

ACM overheat and shutdown. OR cabin altitude above 14,500 ft.

172
Q

ICE AND RAIN PROTECTION: when should anti-ice protection be turned on?

A

When operating in visible moisture between +10C and -30C

173
Q

ICE AND RAIN PROTECTION: Which engine components are ice protected and how?

A 
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
Q

ICE AND RAIN PROTECTION: What turns on the heat to the T0 probe?

A

The engine anti-ice switch

175
Q

ICE AND RAIN PROTECTION: What does the T0 probe do?

A

The T0 probe provides temperature information to the EECS and the RAT

176
Q

ICE AND RAIN PROTECTION: What does the TT0 probe do?

A

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
Q

ICE AND RAIN PROTECTION: If the STBY P/S HTR annunciator illuminates, what two systems may be be be affected?

A

The Meggitt airspeed and altitude may not be reliable.

The horizontal stabilizer may not operate normally

178
Q

ICE AND RAIN PROTECTION: If the AOA HTR FAIL annunciator illuminates, what two systems may not be reliable?

A

The AOA indicator and tape

The stick shaker

179
Q

ICE AND RAIN PROTECTION: What indication do you have that the wing and engine anti-ice systems are operating correctly?

A
  • ITT rise and ignition lights when selecting Engine Anti-ice - ON
  • The WING ANTI-ICE and ENG ANI-ICE annunciators remain extinguished
180
Q

ICE AND RAIN PROTECTION: What indication do you have that the tail de-ice is operating correctly in AUTO?

A

TAIL DE-ICE PRESS white annunciator illuminates 6 seconds on, 6 seconds off, 6 seconds on, approximately 3 minutes off.

181
Q

ICE AND RAIN PROTECTION: What is the minimum temperature for tail de-ice boot operation and why?

A

-40C, the boots will crack

182
Q

ICE AND RAIN PROTECTION: When are the windshield ice detection lights on?

A

Anytime the instrument panel lights are on

183
Q

ICE AND RAIN PROTECTION: What turns the heat to the rosemount probe on?

A

avionics power switch and squat switch

184
Q

ICE AND RAIN PROTECTION: What is the function of the OVERRIDE position on the windshield heat switch?

A

It heats up faster

185
Q

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

A controller failure, yes if necessary but should be turned off if not needed.

186
Q

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?

A

The nacelle inlet did not get up to operating temperature, or the stator vane valve did not open.

187
Q

ICE AND RAIN PROTECTION: What does it mean if after turning engine anti-ice off, the annunciator starts to flash?

A

The stator vane valve did not close

188
Q

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?

A

The wing did not get up to operating temperature

189
Q

ICE AND RAIN PROTECTION: If a wing overheat condition occurs, will it reset automatically?

A

Yes, if the wing temperature drops below 160F

190
Q

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?

A

The anti-ice lights may not come on, in this case an ITT rise is the only indication the system is working.

191
Q

PNEUMATICS: What systems utilize service air?

A

Tail de-ice boots
Door seals
Outflow valves
Throttle detents

192
Q

PNEUMATICS: How is bleed air pre-cooled on the ground and in the air?

A

Ground: Engine bypass air
Flight: Ram air

193
Q

PNEUMATICS: How is bleed air outlet temperature controlled?

A

An electrically actuated door on the ram air inlet scoop

194
Q

PNEUMATICS: What happens to the anti-ice system if a BLD AIR O’HEAT light illuminates?

A

The wing anti-ice on that side shuts down

195
Q

THRUST REVERSERS: At what speed must thrust reversers be reduced to idle?

A

60 kts

196
Q

THRUST REVERSERS: What is maximum reverse thrust?

A

75% of takeoff thrust

197
Q

THRUST REVERSERS: What is max deployed time?

A

3 minutes in any 10 minute period

198
Q

OIL SYSTEM: When is the best time to check the oil quantity?

A

10 minutes after engine shutdown

199
Q

OIL SYSTEM: How do you check the oil level?

A

Visually check the oil level on the sight indicator

200
Q

OIL SYSTEM: What is the rate of oil consumption per quart?

A

1 quart per 8 hours

201
Q

OIL SYSTEM: What is the oil sump quantity?

A

2.44 quarts

202
Q

POWERPLANT - What engines?

A

PW 545B twin spool, high bypass(80%), turbofan. 4095lbs thrust @ sea level

203
Q

POWERPLANT - Primary indication to set power

A

N1

204
Q

POWERPLANT - Purpose of compressor bleed-off valve?

A

To prevent engine surges and compressor stalls.

205
Q

POWERPLANT - Pressing fire button does what 5 things

A

Cutoff: fuel, hydro, oil
Arms bottles
Opens Gen field relay
Lockout TR on that side

206
Q

POWERPLANT - Ignition in NORM when does it activate

A
  • Start

- Anti-ice on

207
Q

POWERPLANT - Does green light mean igniters are working?>

A

No. Only that the exciter box is being powered

208
Q

POWERPLANT - Engine instrumentation available with batt in EMER

A

N1 tapes and digital readout

209
Q

POWERPLANT - When ignition is in SEC what does it mean

A

Secondary power to igniters from EMER bus

210
Q

POWERPLANT - Normal ground idle N2

A

about 50%

211
Q

POWERPLANT - Normal flight idle N2

A

about 60%

212
Q

POWERPLANT - Where is the fuel heater located?

A

Inside FCU between low pressure and high pressure stages of the engine driven fuel pump

213
Q

POWERPLANT - Will engine sync work with throttles in TO detent?

A

No

XLS Initial (8 decks)

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