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Falcon 2000 > Limits > Flashcards

Limits Flashcards

1
Q

Max Altitude

A

47,000 ft.

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2
Q

Max. Ramp Weight

A

36,700 Lbs.

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3
Q

Max Takeoff Weight

A

36,500 Lbs.

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4
Q

Max. Landing Weight

A

34,500 Lbs.

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5
Q

Max Zero Fuel Weight

A

28,660 Lbs.

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6
Q

Baggage Compartment

A

1600 Lbs. 61.4 lb/sqft

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7
Q

Payload

A

5,990 Lbs.

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8
Q

Max Weight Main Cabin Door

A

1,500 Lbs.

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9
Q

Max Weight One Step Main door

A

440 Lbs.

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10
Q

Max Weight Baggage Door

A

320 Lbs.

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11
Q

Runway Slope

A

+/- 2.0%

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12
Q

Airport Pressure Altitude

A

-1000 ft. / 10,000ft

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13
Q

Runway

A

Hard and Paved

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14
Q

Maneuvering Load Factor Flaps Up

A

+2.64g to -1.0g

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15
Q

Maneuvering Load Factor Flaps down

A

+2.0g to 0g

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16
Q

Max Tail Wind

A

10 kts.

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17
Q

Max Demonstrated Cross Wind

A

35 kts.

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18
Q

Landing Lights (on ground)

A

15 minutes on / 45 minutes off

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19
Q

Taxi Light

A

No Limit

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20
Q

Max Operating Limit Speed

A

Vmo/Mmo (red line)

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21
Q

Max Maneuvering speed

A

198 KIAS

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22
Q

Min Control speed in the Air - Vmca

A

90 KIAS

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23
Q

Min Control speed on the Ground - Vmcg

A

98 KIAS

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24
Q

Min control speed during landing approach - Vmcl

A

90

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25
Q

Windshield wiper operating speed

A

215 KIAS

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26
Q

Direct vision window opening speed

A

215 KIAS

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27
Q

Tire Max operating speed

A

195 kts

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28
Q

Vmo/Mmo Limits

A

SL ……………………………………… 350 kt
10,000 ft to 25,000 ft …………. 370 kt
25,000 ft to 38,000 ft ………….. 0.862 Mmo
38,000 ft to 42,000 ft ………….. 0.862/0.85 Mmo
42,000 ft to 47,000 ft ………….. 0.85 Mmo

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29
Q

Max Landing Gear operating speed: Vlo/Mlo

A

190 KIAS Vlo
0.70 Mmo

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30
Q

Max Landing Gear extedded speed Vle/Mle

A

245 KIAS Vle
0.75 Mmo

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31
Q

Slats extended + Flaps 10

A

200 KIAS

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32
Q

Slats extended + Flaps 20

A

160 KIAS

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33
Q

Slats Extended + Flaps 40

A

160 KIAS

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34
Q

Flaps altitude limit

A

20,000 ft

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35
Q

Airbrakes

A

do not extend at or below 300 ft AGL

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36
Q

Auto-pilot Coupled ILS approach

A

RA operative …………………….70 ft
RA inoperative ………………… 160 ft

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37
Q

Auto Pilot Cruise

A

1000 ft

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38
Q

Auto Pilot Non-Precision Approach

39
Q

Hydraulic System Fluids

A

MIL-H-5606

40
Q

Hydraulic Quantity

A

Reservoir 1 ……………. 1.95 USG
Reservoir 2 ……………. 1.59 USG

41
Q

Hydraulic Pressure Green Range

A

2,850 - 3,100 PSI

42
Q

Maximum Voltage

43
Q

Max. engine generator output in flight

A

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

44
Q

Max engine generator output on the ground

45
Q

Battery Temp

A

Amber Light (Warm) 120 F
Red Light (Hot) 160 F

46
Q

Max Operating Speed

A

370 Knts .862 Mach

47
Q

What is the Maximum Speed Brake Extension Speed?

48
Q

Maximum Flap Extension Speeds

A

Flaps 10 - 200
Flaps 20 - 160
Flaps 40 - 160

49
Q

Minimum and Maximum Take Off And Landing Altitude

A

-1000 - 10,000 Ft

50
Q

Maximum Temperature for Takeoff and Landing

A

50 degrees C at Sea level

51
Q

Is the Anti Skid required for Takeoff?

A

Anti Skid MUST be operational for Takeoff.

52
Q

Maximum Crosswind - demonstrated

53
Q

Maximum Tailwind

54
Q

Maximum pressurization differential

55
Q

Maximum Negative Pressure Differential

56
Q

Total Usable Fuel Quantity

A

Left Wing 6,070
Right Wing 6,085
Total 12,155

57
Q

Minimum in tank fuel temperature

A

> = 3 Deg C above the freezing point of the fuel used. (-40C Jet A)

58
Q

Maximum Fuel Imbalance

A

2,200 Lbs.

59
Q

Maximum Fuel Pressure

60
Q

Anti Ice must be operated

A

Visible Moisture
> 10 degrees C

61
Q

Continuous use of supplemental oxygen system is prohibited above

A

Carrying passengers 25,000
Crew 40,000

62
Q

Thrust Rating sea level takeoff

63
Q

Thrust Rating sea level Continuous

64
Q

Which engine parameter is used for setting thrust?

65
Q

Maximum N1 & N2

A

N1 N2
Max Continuous 96.7 104.9
Normal TO. 96.7 106

66
Q

Engine Vibration limit

A

N1: 1 inch/sec
N2: 1.5 inch/sec

67
Q

ITT LIMITS
Ground Start

68
Q

ITT LIMITS
Airstart

69
Q

ITT LIMITS
Restart max temp

70
Q

ITT LIMITS
Max Takeoff (5 min)

71
Q

ITT LIMITS
Normal Takeoff

72
Q

ITT LIMITS
Maximum Continuous

73
Q

Start time limits- ground

A

Start to light off 10 seconds after reaching 22% N2
Light off to idle 60 seconds

74
Q

Start time limits- Airstart

A

Assisted: 90 seconds
Windmilling: 180 seconds

75
Q

APU Maximum starting operating altitude

A

35,000 feet

76
Q

APU Maximum Generator output

A

0-10,000 ft. 300 amps
10,000-25,000ft. 250 amps
25,00-35,000ft. 200 amps

77
Q

Maximum Passengers

78
Q

Coat Compartment Weight

A

81.9 lbs/sqft

79
Q

Stall Speed

A

Do not intentionally fly the airplane slower than stall warning onset.

80
Q

APU Starting temp limit

81
Q

APU Stabilized EGT

82
Q

Maximum APU Generator

A

0 - 10,000 ft ……………….. 300A
10,000-25,000 ……………. 250A
25,000-35000 …………….. 200A

83
Q

Wind-milling Max. Temperature

A

970°c (10 seconds)
1000°c (2 seconds)

84
Q

Oil pressure limits
Operating range

85
Q

Oil pressure limits
Transient (3 min)

A

85-100 PSI

86
Q

Oil pressure limits
Minimum (at idle)

87
Q

Oil pressure limits
Cold Start

88
Q

Oil Temperature Limits
Maximum

89
Q

Oil Temperature Limits
Minimum

90
Q

Oil Temperature Limits
Transient for 3 min

A

138-155°C

91
Q

Oil Temperature Limits
Cold Start

92
Q

Thrust Reverser

A

Ground use only
All 3 wheels on the ground
Not to be used in flight
Max Rev Down to 20 KIAS

93
Q

Maximum temperature for Wing and Engine anti-ice

94
Q

Starter engagement limits
Max N2

Falcon 2000 (3 decks)

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