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Falcon 2000 > Limitations > Flashcards

Limitations Flashcards

1
Q

Authorized Limitations

A
  1. Day and Night VFR
  2. IFR and auto. approaches to CAT I and II wx mins.
  3. Extended overwater and uninhabited terrain
  4. Icing Conditions
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2
Q

Maximum Passengers

A

19 Passengers

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3
Q

Minimum Flight Crew

A

Two Pilots (One Pilot, One Copilot)

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4
Q

Maximum Permissable Altitude

A

47,000 ft

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5
Q

Weight Limitations (with Mod M57)

A

Max Ramp: 36,700 lbs
Max Takeoff: 36,500 lbs
Max Landing: 33,000 lbs
Max ZFW: 28,660 lbs

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6
Q

Weight Limitations (without Mod M57)

A

Max Ramp: 36,000 lbs
Max Takeoff: 35,800 lbs
Max Landing: 33,000 lbs
Max ZFW: 28,660 lbs

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7
Q

Max Landing Weight w/ SBF2000-186 installed

A

34,500 lbs

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8
Q

Baggage Compartment Loading Limits

A

1,600 lbs (not to exceed 61.4 lb/sqft)

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9
Q

Coat Compartment Loading Limits

A

81.9 lb.sqft

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10
Q

Max Payload

A

5,990 lbs

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11
Q

Maximum Weight Main Cabin Door

A

1,500 lbs
(440 lbs/step)

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12
Q

Max Weight Baggage Cpmt Door

A

320 lbs

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13
Q

Maximum Runway Slope

A

+/- 2.0%

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14
Q

Min Airport Press Alt for TO/Ldg

A

-1,000 ft

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15
Q

Max Airport Press Alt for TO/Ldg

A

+10,000 ft

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16
Q

Type of Runway Required

A

Paved and Hard-Surface

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17
Q

Flaps Up Load Factor

A

+2.64g to -1.0g

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18
Q

Flaps Down Load Factor

A

+2.0g to 0g

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19
Q

Max Tailwind Component

A

10 kts (TO/Ldg)

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20
Q

Max Demonstrated Crosswind

A

35 kts

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21
Q

Landing Light Limitation

A

15 minutes ON/45 minutes OFF

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22
Q

Max Operating Speed

A

Vmo/Mmo (Red Line)

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23
Q

Max Maneuvering Speed (Va)

A

198 KIAS

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24
Q

Min Control Speed in the AIR (Vmca)

A

90 KIAS

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25
Q

Min Control Speed during Landing App (Vmcl)

A

90 KIAS

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26
Q

Min Control Speed on the ground (Vmcg)

A

98 KIAS

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27
Q

Windshield Wiper Operating Speed

A

215 KIAS

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28
Q

Direct Vision (DV) Window Opening Speed

A

215 KIAS

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29
Q

Max Tire Operating Speed

A

195 KIAS (Ground Speed)

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30
Q

Stall Speed

A

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

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31
Q

Vmo/Mmo Limits

A

Sea Level: 350 kt
10,000 - 25,000 ft: 370 kt
25,000 - 38,000 ft: 0.862 M
38,000 - 42,000 ft: 0.862/0.85 M
42,000 - 47,000 ft: 0.85 M

32
Q

Max Landing Gear Operating Speed (Vlo/Mlo)

A

190 KIAS/0.70 M

33
Q

Max Landing Gear Extended Speed (Vle/Mle)

A

245 KIAS/0.75 M

34
Q

Flaps Speed Limits

A

Slats + Flaps 10: 200 KIAS
Slats + Flaps 20: 160 KIAS
Slats + Flaps 40: 160 KIAS

35
Q

Flaps Altitude Limit

A

20,000 ft

36
Q

Airbrakes Limitation

A

Do not extend below 300 ft AGL

37
Q

Autopilot Altitude Restrictions

A

Coupled ILS w/ RA Operative: 70 ft
Coupled ILS w/o RA Operative: 160 ft
Non-Precision Approach: 250 ft
Cruise: 1,000 ft

38
Q

Approved Hydraulic Fluids

A

MIL-H-5606 or AIR 3520

39
Q

Hydraulic Reservoir Quantities

A

Reservoir 1: 1.95 USG
Reservoir 2: 1.59 USG

40
Q

Hydraulic Green Range Pressure

A

2,850 - 3,100 PSI

41
Q

Max Voltage of the DC System

A

29.5 VDC

42
Q

Max Engine Gen. Output in-flight

A

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

43
Q

Max Engine Gen. Output on the ground

A

300A

44
Q

Battery Temps

A

Amber Light (WARM): 120 degrees F
Red Light (HOT): 160 degrees F

45
Q

Fuel Capacity - without modification

A

LH Wing + half center wing box: 906 gal/6,070 lbs
RH Wing + half center wing box: 908 gal/6,085 lbs
Total: 1,814 gal/12,155 lbs

46
Q

Fuel Capacity - with modification - M3072

A

LH Wing + half center wing box: 902 gal/6,042 lbs
RH Wing + half center wing box: 904 gal/6,057 lbs
Total: 1,806 gal/12,099 lbs

47
Q

Maximum Fuel Imbalance

A

2,200 lbs

48
Q

Minimum Fuel Temp

A

3 degrees above fuel freezing temp being used

49
Q

Maximum Refuel Press

A

50 PSI

50
Q

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

A

No, the FQMC must be operative for Takeoff

51
Q

Max differential press

A

9.3 PSI

52
Q

Normal Differential Press

A

9.0 PSI

53
Q

Max Negative differential Press

A

-0.3 PSI

54
Q

Max Operating Altitude for the APU

A

35,000 ft

55
Q

Maximum Starting Altitude for APU

A

35,000 ft

56
Q

Can passengers be allowed unmonitored in cabin while APU is operating?

A

No, passengers must be monitored while in the cabin with APU running

57
Q

Max APU N1 Speed

A

110%

58
Q

APU EGT Starting Limit

A

974 degrees C

59
Q

APU EGT Stabilized Limit

A

746 degrees C

60
Q

APU Max Generator Output

A

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

61
Q

Power Plant Takeoff Thrust Rating

A

5,888 lbs

62
Q

Power Plant Max Continuous Thrust Rating

A

5,613 lbs

63
Q

Max Takeoff N1/N2 Speeds

A

N1: 96.7%
N2: 106%

64
Q

How long can Max Takeoff Thrust be used for?

A

5 min max

65
Q

Max Continuous N1/N2 Speeds

A

N1: 96.7%
N2: 104.9%

66
Q

Engine Vibration Limits N1/N2

A

N1: 1.0 in/sec
N2: 1.5 in/sec

67
Q

Engine ITT Limits

A

Ground Start: 815 degrees C
Airstart: 890 degrees C
Max Continuous: 861 degrees C

68
Q

Engine Ground Start Time Limits

A

From Start to Light-off: 10 sec max
From Light-off to Idle: 60 sec max

69
Q

Engine Airstart Start Time Limits

A

Assisted: 90 Sec
Windmilling: 180 sec

70
Q

Engine Oil Press Limits

A

Operating Range: 60 - 85 PSI
Transient (3 min): 85 - 100 PSI
Minimum (At idle): 30 PSI
Cold Start (2.5 min max below 0 degrees C): 135 PSI

71
Q

Oil Temp Limits

A

Max: 138 degrees C
Min: 30 degrees C
Transient for 3 min: 138 - 155 degrees C
Cold Start: -40 degrees C

72
Q

Thrust Reverser Limitations

A

Ground Use Only
All 3 Wheels on ground
Not to be used in-flight

73
Q

Thrust Reversers Min Speed for Max Reverse

A

20 KIAS

74
Q

Definition of Icing Conditions

A

OAT is +10 degrees C or below and visible moisture is present

75
Q

Max Temp for Engine Anti Ice

A

+10 degrees C

76
Q

Max Temp for Wing Anti Ice

A

+10 degrees C

Falcon 2000 (3 decks)

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