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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
Min Control Speed during Landing App (Vmcl)
90 KIAS
26
Min Control Speed on the ground (Vmcg)
98 KIAS
27
Windshield Wiper Operating Speed
215 KIAS
28
Direct Vision (DV) Window Opening Speed
215 KIAS
29
Max Tire Operating Speed
195 KIAS (Ground Speed)
30
Stall Speed
Do not intentionally fly the airplane slower than the initial stall warning onset
31
Vmo/Mmo Limits
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
Max Landing Gear Operating Speed (Vlo/Mlo)
190 KIAS/0.70 M
33
Max Landing Gear Extended Speed (Vle/Mle)
245 KIAS/0.75 M
34
Flaps Speed Limits
Slats + Flaps 10: 200 KIAS Slats + Flaps 20: 160 KIAS Slats + Flaps 40: 160 KIAS
35
Flaps Altitude Limit
20,000 ft
36
Airbrakes Limitation
Do not extend below 300 ft AGL
37
Autopilot Altitude Restrictions
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
Approved Hydraulic Fluids
MIL-H-5606 or AIR 3520
39
Hydraulic Reservoir Quantities
Reservoir 1: 1.95 USG Reservoir 2: 1.59 USG
40
Hydraulic Green Range Pressure
2,850 - 3,100 PSI
41
Max Voltage of the DC System
29.5 VDC
42
Max Engine Gen. Output in-flight
Stabilized: 400A Transient (5 Sec): 800A Transient (40 Sec): 600A Transient: (160 Sec): 500A
43
Max Engine Gen. Output on the ground
300A
44
Battery Temps
Amber Light (WARM): 120 degrees F Red Light (HOT): 160 degrees F
45
Fuel Capacity - without modification
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
Fuel Capacity - with modification - M3072
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
Maximum Fuel Imbalance
2,200 lbs
48
Minimum Fuel Temp
3 degrees above fuel freezing temp being used
49
Maximum Refuel Press
50 PSI
50
Can the Fuel Quantity Management Computer (FQMC) be inoperative for Takeoff?
No, the FQMC must be operative for Takeoff
51
Max differential press
9.3 PSI
52
Normal Differential Press
9.0 PSI
53
Max Negative differential Press
-0.3 PSI
54
Max Operating Altitude for the APU
35,000 ft
55
Maximum Starting Altitude for APU
35,000 ft
56
Can passengers be allowed unmonitored in cabin while APU is operating?
No, passengers must be monitored while in the cabin with APU running
57
Max APU N1 Speed
110%
58
APU EGT Starting Limit
974 degrees C
59
APU EGT Stabilized Limit
746 degrees C
60
APU Max Generator Output
0 - 10,000 ft: 300A 10,000 - 25,000 ft: 250A 25,000 - 35,000 ft: 200A
61
Power Plant Takeoff Thrust Rating
5,888 lbs
62
Power Plant Max Continuous Thrust Rating
5,613 lbs
63
Max Takeoff N1/N2 Speeds
N1: 96.7% N2: 106%
64
How long can Max Takeoff Thrust be used for?
5 min max
65
Max Continuous N1/N2 Speeds
N1: 96.7% N2: 104.9%
66
Engine Vibration Limits N1/N2
N1: 1.0 in/sec N2: 1.5 in/sec
67
Engine ITT Limits
Ground Start: 815 degrees C Airstart: 890 degrees C Max Continuous: 861 degrees C
68
Engine Ground Start Time Limits
From Start to Light-off: 10 sec max From Light-off to Idle: 60 sec max
69
Engine Airstart Start Time Limits
Assisted: 90 Sec Windmilling: 180 sec
70
Engine Oil Press Limits
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
Oil Temp Limits
Max: 138 degrees C Min: 30 degrees C Transient for 3 min: 138 - 155 degrees C Cold Start: -40 degrees C
72
Thrust Reverser Limitations
Ground Use Only All 3 Wheels on ground Not to be used in-flight
73
Thrust Reversers Min Speed for Max Reverse
20 KIAS
74
Definition of Icing Conditions
OAT is +10 degrees C or below and visible moisture is present
75
Max Temp for Engine Anti Ice
+10 degrees C
76
Max Temp for Wing Anti Ice
+10 degrees C

Falcon 2000 (3 decks)

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