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Falcon 2000 EASy > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Ramp Weight

A

42,400 lbs

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2
Q

Max Takeoff Weight

A

42,200 lbs

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3
Q

Max Landing Weight

A

39,300 lbs

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4
Q

Max Zero Fuel Weight

A

29,700 lbs

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5
Q

Max Baggage Compt Weight

A

1,600 lbs

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6
Q

Max Payload

A

5,990 lbs

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7
Q

Maneuvering Speed (VA)

A

198 KIAS

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8
Q

SF1 Max Speed

A

200 KIAS

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9
Q

SF2 Max Speed

A

190 KIAS

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10
Q

SF3 Max Speed

A

180 KIAS

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11
Q

Max Landing Gear Operating Speed (VLO/MLO)

A

190 KIAS/MI 0.7

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12
Q

Max Landing Gear Extended Speed (VLE/MLE)

A

245 KIAS/MI 0.75

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13
Q

Minimum Control Speed in the Air (VMCA)

A

90 KIAS

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14
Q

Minimum Control Speed during Approach and Landing (VMCL)

A

90 KIAS

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15
Q

Minimum Control Speed on the Ground (VMCG)

A

98 KIAS

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16
Q

Windshield Operating Speed (VWWO)

A

215 KIAS

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17
Q

Pilot Sliding Window Speed (V Window)

A

215 KIAS

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18
Q

Tire Max Operating Speed (V Tire)

A

195 KT (Ground Speed)

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19
Q

Max Airport Pressure Altitudes for Takeoff and Landing

A

-1,000 ft/8,000 ft
-1,000 ft/14,000 ft (M2706)

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20
Q

Max Runway Slope for Takeoff and Landing

A

+/- 2%

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21
Q

Runway Type Required for Takeoff and Landing

A

Paved and Hard Surfaced

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22
Q

Max Tailwind for Takeoff and Landing

A

10 KIAS

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23
Q

Max Enroute Operating Altitude

A

47,000 ft

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24
Q

Max Differential Cabin Pressure

A

9.3 PSI

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25
Q

Max Negative Differential Cabin Pressure

A

-0.3 PSI

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26
Q

Can Autopilot be Engaged on the Ground?

A

No

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27
Q

Autopilot Minimum Engagement Speed during climb out

A

V2 + 10 kt

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28
Q

Autopilot Minimum Engagement Speed during Go Around

A

VREF + 10 kt

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29
Q

Autopilot minimum height during climb out

A

400 ft

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30
Q

Autopilot Minimum Height during Level Flight

A

1,000 ft

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31
Q

Autopilot Minimum Height during standard non-precision approach

A

160 ft

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32
Q

Autopilot use height during ILS approach with operational radar altimeter

A

50 ft

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33
Q

Autopilot min height during an ILS approach and inoperative radar altimeter

A

160 ft

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34
Q

Autopilot minimum height during ILS steep approach (between 4.5 and 6.65 degrees in SF3 and AB1 configuration)

A

285 ft

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35
Q

Autopilot minimum use height during circling approach below 200 KIAS in clean configuration

A

500 ft

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36
Q

Autopilot minimum use height during circling approach

A

500 ft

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37
Q

Flight director minimum use height at takeoff

A

400 ft

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38
Q

Can Autothrottle be engaged during takeoff and landing?

A

No

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39
Q

Should Autothrottle be disengaged during go-around?

A

Yes

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40
Q

Autothrottle minimum engagement height during initial climb out

A

400 ft

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41
Q

Autothrottle minimum disengagement height for standard approach path angle

A

50 ft

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42
Q

Autothrottle minimum disengagement height during ILS steep approach (between 4.5 and 6.65 degrees in SF3 and AB1 configuration

A

285 ft

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43
Q

Can the Autothrottle be engaged before aircraft is in clean configuration after takeoff and go around when FMS is selected on guidance panel?

A

No

44
Q

Can the thrust director be displayed before aircraft is in clean configuration after takeoff when FMS speed is selected on guidance panel?

A

No

45
Q

Max DC System Voltage

A

29.5 V

46
Q

Max Engine Generator Output in Flight

A

Stabilized: 400 A
Transient (5 sec): 800 A
Transient (40 sec): 600 A
Transient (160 sec): 500 A

47
Q

Max engine generator output on ground for basic generators

A

300 A

48
Q

WARM BAT CAS Message Temperature

A

48.9 degrees C or above

49
Q

HOT BAT CAS Message temperature

A

71.1 degrees C or above

50
Q

Max Speed with Inoperative Arthur Unit

A

260 KIAS/MI 0.76

51
Q

Can the aircraft maintain a configuration with flaps or slats extended above 20,000 ft?

A

No

52
Q

How is flap extension or retraction executed?

A

One notch at a time

53
Q

Can the airbrake configuration be changed in flight below 300 ft?

A

No

54
Q

Max Usable Fuel Quantity

A

16,674 lbs

55
Q

Minimum inflight fuel tank temperature

A

3 degrees C above freezing point of fuel being used

56
Q

Max fuel dissymmetry

A

2,200 lbs

57
Q

Max fuel feed pressure

A

50 PSI

58
Q

Can the Fuel Quantity Management Computer (FQMC) be inoperative for takeoff?

A

No

59
Q

Approved Hydraulic Fluid Types

A

Fluid Conforming to:
AIR 3520
MIL-H-5606

60
Q

Hydraulic Reservoir 1 max capacity

A

1.95 gallons

61
Q

Hydraulic Reservoir 2 max capacity

A

1.58 gallons

62
Q

Normal hydraulic operating pressure (green range)

A

3,000 +/- 200 PSI

63
Q

Normal Standby Pump Auto mode pressure

A

1,650 - 2,300 +/- 100 PSI

64
Q

When do Icing Conditions Exist?

A

TAT + 10 degrees C and visible moisture
OAT + 10 degrees C on ground when moisture may be ingested or freeze

65
Q

Is the Ice Detection System a Primary Detection System?

A

No - it is a secondary or backup detection system

66
Q

Is prolonged flight in icing conditions with slats/flaps extended authorized?

A

No

67
Q

When should engine anti-ice be deactivated?

A

TAT exceeds 10 degrees C

68
Q

When should wing anti-ice be deactivated?

A

TAT exceeds 10 degrees C

69
Q

When can wing anti-ice be used during ground operations?

A

Only for limited checks conducted in accordance with AFM

70
Q

What type of tires must be installed on Nose Wheel?

A

Chinned Tires

71
Q

Max Brake Energy

A

16,875 kJ per brake

72
Q

Reference to minimum turn around table is not required prior to taxi if each brake temperature is below what?

A

160 degrees C and decreasing

73
Q

Is brake cooling time affected by park brake application?

A

No

74
Q

Ground operating limitations of landing lights

A

15 min On
45 min cooling time

75
Q

Passenger Oxygen System automatically drops masks at what cabin altitude?

A

14,500 ft +/- 500 ft

76
Q

What APU is installed on the aircraft?

A

Honeywell GTCP 36-150 (F2M)

77
Q

Max Operating Altitude (APU)

A

35,000 ft

78
Q

APU max starting altitude

A

35,000 ft

79
Q

Can APU be operated with PAX in the cabin without crew monitoring?

A

No

80
Q

APU max N1 speed

A

110%

81
Q

APU average fuel flow

A

100 lb/hr

82
Q

APU EGT limit during start

A

988 degrees C for less than 10 sec

83
Q

APU stabilized EGT limit

A

746 degrees C

84
Q

APU Max Generator Output - Stabilized

A

0-10,000 ft: 300 A
10,000-25,000 ft: 250 A
25,000-35,000 ft: 200 A

85
Q

APU Max Generator Output - Transient

A

40 sec: 450 A
180 sec: 375 A

86
Q

Max weight authorized of PAX door

A

1,500 lbs

87
Q

Max Weight authorized on one step of PAX door

A

440 lbs

88
Q

When is the in cabin baggage compartment door required to be closed and latched?

A

When access to baggage compartment is not required

89
Q

What type of engine is installed on the aircraft?

A

Pratt & Whitney 308C

90
Q

Engine Takeoff Thrust Rating

A

6,998 lbs

91
Q

Max Continuous Thrust Rating

A

6,998 lbs

92
Q

Engine Takeoff Thrust time limit

A

5 minutes

93
Q

What is used as thrust setting parameter?

A

N1

94
Q

Engine Rotor Speed Limits
(N1/N2)

A

Normal Takeoff (5 min max): 102.5%/102%
Max Takeoff (5 min max): 102.5%/102%
Max Continuous: 102.5%/102%
Transient (20 sec): 103.5%/103%

95
Q

Max Rotor Speed Limit at 100% N1

A

10,400 rpm

96
Q

Max Rotor Speed Limit at 100% N2

A

26,780 rpm

97
Q

Overall Engine Vibration Limit

A

0.96 in/sec average

98
Q

Engine ITT Limits (Starts)

A

Ground Start: 950 degrees C
Airstart: 950 degrees C
Airstart - Max restart: 500 degrees C
Ground Start - Max Restart: 340 degrees C

99
Q

Engine ITT Limits

A

Max TO (APR) transient: 905 C (2 min max)
Max TO (APR): 895 C (5 min max)
Normal TO: 875 C (5 min max)
Max Continuous: 860 C
Flight Transient: 890 C (20 sec max)
875 C (5 min max)

100
Q

Engine Start Times (Ground)

A

From Start to 5.2% N2: 15 sec max
From start to light off: 20 sec max
From light off to idle: 60 sec max

101
Q

Airstart Time Limits (From Lightoff to Idle)

A

Assisted: 90 sec
Windmilling: 180 sec

102
Q

Max N2 starter re-engagement limit

A

Starter Cutout N2 (50%)

103
Q

Engine GPU start Limitations

A

Max Temp: 250 C
Max Pressure: 50 PSI
Max Flow: 82 lb/min

104
Q

Are the Thrust Reversers Authorized in flight?

A

No

105
Q

Engine Oil Pressure Limits

A

Start: 0-240 PSI
Ground & Idle: 20-100 PSI
Above Idle: 36-100 PSI

106
Q

Engine Max Transient Oil Pressure Limits

A

0-10 PSI: 20 sec
10&20 psi Engine Idle: 90 sec
10&36 psi Engine above Idle: 90 sec
100 & 220 psi: 90 sec

107
Q

Engine Oil Temperature Limits

A

Maximum: 135 C
Minimum for Takeoff: 27 C
Minimum: 16 C
Transient for 90 sec: 143 C
Cold Start: -40 C

Falcon 2000 EASy (3 decks)

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