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Falcon 900 EX > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Ramp Weight

A

48,500

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2
Q

Max Takeoff Weight

A

48,300

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3
Q

Max Landing Weight

A

42,000

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4
Q

Max Zero Fuel Weight

A

30,864

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5
Q

Min Flight Weight

A

20,700

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6
Q

Datum

A

25% MAC or station 420.43

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7
Q

Baggage total weight

A

2,866

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8
Q

Payload

A

5,990

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9
Q

VMO / MMO

A

VMO 370 kts

MMO .87

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10
Q

Maneuvering Speed

A

Va 228kts

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11
Q

Slats out Flaps 7•

A

200 kias

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12
Q

Slats out flaps 20•

A

190 kias

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13
Q

Slats out flaps 40•

A

180 kias

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14
Q

VLO

Safety speed for extending & retracting

A

190 kias or .70 Mach

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15
Q

VLE

A

245 kias or .75 Mach

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16
Q

VMCA

A

85.2 KCAS

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17
Q

All Engines Operative

VMCL

A

85 KCAS

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18
Q

One engine inoperative Vmcl

A

83 KCAS

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19
Q

Vmcg

A

88.9 KCAS

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20
Q

V wwo

A

215 KCAS

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21
Q

V window

A

215 KCAS

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22
Q

Max Tire Speed

A

195 kts

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23
Q

Runway Slop limitations

A

+/- 2.5%

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24
Q

Airport Pressure Altitude

A

-1,000 ft / +14,000 ft

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25
Q

Max Tailwind Takeoff & Landing

A

10 kts

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26
Q

Runway

A

Paved and Hard Surface

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27
Q

Max Operating Altitude

A

51,000

28
Q

Cabin Pressure Differential

A

9.6 psi

29
Q

Max Negative Pressure Differential

A

-0.29

30
Q

Cabin Pressure Dump

A

14,500 ft + / - 500 ft

31
Q

Autopilot min height to engage after t/off

A

400 ft

32
Q

Autopilot min height for operation except during approach and climb

A

1,000 ft

33
Q

Autopilot coupled approach

ILS with radio altimeter

A

80 ft

34
Q

Coupled ILS no radio altimeter

A

150 ft

35
Q

Autopilot coupled non-precision approach

A

250 ft

36
Q

Auto throttle min height to engage in climb

A

400 ft

37
Q

Auto throttle min to disengage during descent

A

80 ft

38
Q

DC Voltage limits

A

32V

39
Q

Engine Gen Max
Transient
Up to 43,000 ft
Above 43,000 ft

A

350A
300A
260A

40
Q

Battery Limits

A

Amber 120•F

Red 160•F

41
Q

Max Speed with Arthur inop

A

260 kias or .76 Mach

42
Q

Max altitude for slats and flaps

A

20,000

43
Q

Fuel:
Engine 1
Engine 2
Engine 3

A

Engine 1: 1,050. (7,036 lbs)
Engine 2: 1,027. (6,885 lbs)
Engine 3: 1,056.5. (7,079 lbs)

Total: 3,133.5 (21,000 lbs)

44
Q

Hydraulic Fluid

A

5606

45
Q

Engine Anti-Ice

A

During climb and cruise it must be used below +10•C TAT

and above -40•C SAT and in visible moisture

46
Q

Wing Anti-Ice

A

Do not use with a TAT above 10•C / 50•F

Do not use on the ground

47
Q

Landing Lights

A

Ground operation limited to 15 min with 45 min cooling between use

48
Q

Max N1 speed

A

110%

49
Q

Passenger Door
Max weight on door
One step
On baggage door

A

1200 lbs
440 lbs
220 lbs

50
Q

Max thrust takeoff

A

5,000 lbs (N1)

51
Q

Max Continuous Thrust

A

4,525 lb (N1)

52
Q

Max Engine Rotor Speed Takeoff

N1

A

100% takeoff max continuous

100.5% transient one second max

53
Q

N2 Max Continuous

A

Takeoff 100%

Transient 101.5% 1 second max

54
Q

Max ITT

A

Ground Start 994•C
Air Start 994•C
T/Off 5 min max 1,022•C
Max Continuous 991•C

55
Q

Starting Time

Ground & Starter assist air start

A

10 seconds max

56
Q

Starting time
Windmilling air start
60% N2

A

45 seconds max

57
Q

Starter
Ground start
Light off to idle

A

60 seconds max

58
Q

Oil Pressure

Max Continuous

A

Min pressure 65 psi

Max pressure 80 psi

59
Q

Oil Pressure

Idle

A

Min 60 psi

Max 80 psi

60
Q

Oil Pressure

Transient

A

100 psi less than 3 min

61
Q

Red Oil Pressure Lights come up on panel when?

A

Below 50 psi

All Engines

62
Q

Oil Temp

SL - 30,000 ft

A

127•C max

63
Q

Oil Temp

Above 30,000 ft

A

140•C max

64
Q

Oil Temp

Transient all altitudes

A

149•C

Less than 2 minutes

65
Q

Oil temp

Min for exceeding idle power

A

30•C

66
Q

Max Standing Water

A

.5”

Falcon 900 EX (9 decks)

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