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My Falcon > Falcon limitations > Flashcards

Falcon limitations Flashcards

1
Q

Baggage compartment limit

A

2866 Ibs (1300 kgs)

Not to exceed 123 IB/Sq ft (600 kg sq m)

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2
Q

Max T/O Weight

A

46,500 lbs

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3
Q

Max Ramp Weight

A

46,700 lbs

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4
Q

Max Landing Weight

A

42,000 lbs

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5
Q

MZFW

A

30,870 lbs

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6
Q

Average BOW (basic operating weight)

A

26.500 lbs

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7
Q

Minimum Operating Weight (or Min Flight Weight)

A

20,700 lbs

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8
Q

CG Limit

A

14% MAC Forward - 31% MAC Aft.

MAC (Mean Aerodynamic Chord)

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9
Q

Datum

A

25% MAC

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10
Q

Max Approved Operating Altitude

A

51,000 ft

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11
Q

Min/Max Altitude for T/O and Landing

A

-1,000 ft to 14,000 ft

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12
Q

Min/Max Temperature for T/O and Landing

A

-54°C to +50°C

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13
Q

Max Altitude for Operating Flaps or Slats

A

20,000 ft

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14
Q

Vmo

A

350 KIAS below 10,000ft

370 KIAS at or above 10,000 ft

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15
Q

Mmo > 35K

A

ABOVE 35,000 lbs
25,000 ft to 33,000 ft .87 Mach
33,000 ft to 37,000 ft .87 to .84 Mach
above 37,000 ft .84 Mach

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16
Q

Mmo < 35K

A

BELOW 35,000 lbs
25,000 ft to 37,000 ft .87 Mach
37,000 ft to 42,000 ft .87 to .84 Mach
above 42,000 ft .84 Mach

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17
Q

Va

A

228 KIAS

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18
Q

Turbulent Air Penetration Speed

A

280 KIAS / .76 Mach

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19
Q

Vlo (landing gear operation)

A

190 KIAS

VLO/MLO is the maximum speed at which it
is safe to extend or retract the landing gear.

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20
Q

Mlo (landing gear operation)

A

.70 Mach

VLO/MLO is the maximum speed at which it
is safe to extend or retract the landing gear.

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21
Q

Vle (landing gear extended)

A

245 KIAS

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22
Q

Mle (landing gear extended)

A

.75 Mach

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23
Q

Vwwo (windshield wipers operation)

A

215 KIAS

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24
Q

D.V. Window

A

215 KIAS

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25
Q

Cracked or Bubbled Windshield Max Speed

A

7.5 psi max press diff.

230 KIAS

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26
Q

Vabo (air brakes operation)

A

No Limitation

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27
Q

Vabe (air brakes extended)

A

No Limitation

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28
Q

Vfe Slats+Flaps 7° (SF-1)

Operating or Extended Speed

A

200 KIAS

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29
Q

Vfe Slats+Flaps 20° (SF-2)

Operating or Extended Speed

A

190 KIAS

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30
Q

Vfe Slats+Flaps 40° (SF-3)

Operating or Extended Speed

A

180 KIAS

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31
Q

Vmcg (minimum control on ground)

A

No Vmcg

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32
Q

Vmin (minimum selectable)

A

90 KIAS

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33
Q

Vmca (minimum control in air)

A

85.5 Kias

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34
Q

Demonstrated Crosswind

A

30 Knots

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35
Q

Max Tailwind

A

-1,000 to 10,000 ft - 10 Knots
above 10,000 ft - 4 Knots
10 Knots with 195kt (225mph) tires

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36
Q

Max Runway Slope

A

+/- 2.5%

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37
Q

Max Tire Rotation Speed

A

195 KIAS (225 mph tires)

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38
Q

Vp Hydroplanning Speed

A

89 KIAS

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39
Q

Max Speed for Total Hydraulic Loss

A

260 KIAS / .76 Mach

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40
Q

Wing Root Lights On Ground

A

15 min followed by 45 min cool down

41
Q

Load Factor CLEAN

A

+2.53 G to -1G

42
Q

Load Factor FLAPS EXTENDED

A

+2G to 0G

43
Q

Engines Model:

Tell Flight engineer at 731- to bring 5 black rats and 1 chair

A

TFE731-5BR-1C

44
Q

Engine Computers Limitation

A

Must be operative for Takeoff

45
Q

Takeoff Thrust

A

4750 lbs

46
Q

Max Continuous Thrust

A

4634 lbs

47
Q

N1/N2 Max limits:

ToF:
Transient:

A

Takeoff:
100% - 100.8%

Transient (5 sec max):
103% - 103%

48
Q

ITT TRANSIENT (5 SEC):

A

1006°C

49
Q

ITT START

A

978°C

50
Q

ITT TAKEOFF (5 MIN):

A

978°C

51
Q

ITT MAX CONTINUOUS (30 MIN):

A

968°C

52
Q

ITT RPR OPERATING

A

(5 MINUTES): 996°C

53
Q

Starting Limitations:

N2 10% to lightoff ground or started assisted

Lightoff to idle:

Windmilling air start:

A

N2 10% to lightoff ground or started assisted:
10 seconds

Lightoff to idle (60% N2): 60 seconds

Windmilling air start: 45 seconds max

54
Q

Starter Limitations

A

40 sec on - 3 min off
30 sec on - 3 min off
30 sec on - 30 min off
Double times btw 2 subsequent starts above 30°C

55
Q

Oil Pressure Limitations

IDLE: Min + Max

TOF & MCT: Min + Max

Trasient: Max

A

Idle: 25-46 psi
T/O + MCT : 38-46 psi
Transient: 55 psi (less than 3 minutes)

56
Q

Oil Temperature Limitations:

Sea level to 30,000 ft:
&
> 30K

A

Sea level to 30K 127°C

Above 30K > 140°C

57
Q

Oil Temperature Limitations:

Transient abv 30K :
&
Minimum for exceeding idle:

A

Transient: 149°C (less than 2 minutes)

Minimum for exceeding idle: 30°C

58
Q

Generator Limitations
<43K
>43K

Max Volts:

A 
FL430 and below:
300 amp (350 amp 1 min)

Above FL430:
260 amp

Max system voltage: 32 volts

59
Q

GTCP 36-150 - APU:

Max N1:

Star T5:

Stab T5:

Max Load:

A

N1: 110%

Start (less than 10 sec): 870°-985°C

Stabilized: 679° C

Generator: 300 amp (350 amp for 1 min)

60
Q

Pressurization- Max and Normal Differential?

A

Max press diff: 9.6 psi

Normal press diff: 9.3 psi

61
Q

Fuel

Total Useable:

Left Wing:

Right Wing:

Group 2 :

Min/ Max Refusing press:

A

Total Usable:
2,845 gl - 19,065 lbs

Left wing + G1:
904 gl - 6,058 lbs

Right wing + G3:
904 gl - 6,058 lbs

Front and Rear G2:
1,034 - 6,949 lbs

Min/Max refuelling press:
30-50 psi

62
Q

Fuel Total Usable:

A

Total Usable:

2,845 gl - 19,065 lbs

63
Q

Fuel Left wing + G1:

A

Left wing + G1:

904 gl - 6,058 lbs

64
Q

Fuel Right wing + G3:

A

Right wing + G3:

904 gl - 6,058 lbs

65
Q

Fuel Front and Rear G2:

A

Front and Rear G2:

1,034 - 6,949 lbs

66
Q

Fuel Min/Max refuelling press:

A

Min/Max refuelling press:

30-50 psi

67
Q

Autopilot Limitations

Radio altimeter operative:

Radio altimeter inoperative:

Decision height:

During FMS approach

(no approach) like Dep:

A

Min height Radio altimeter operative:
50 ft

Min height Radio altimeter inoperative:
150 ft

Min decision height:
200 ft

Min height during FMS approach:
300 ft

Minimum height (no approach):
1,000ft
68
Q

Fuel Burn Rule

constant cruise .78 Mach

A

First hour:
3,200 lbs

2nd hour:
2,200 lbs

Third hour and beyond:
2,000 lbs

69
Q

Wingspan

A

63ft 5in

70
Q

Height

A

24ft 9in without satcom

25ft 2in

71
Q

Length

A

66ft 4in

72
Q

Autopilot Limitations - Min height wt FMS approach:

A

300 ft

73
Q

Autopilot Limitations- Min height RA operative:

A

50 ft

74
Q

Autopilot Limitations- Min height RA inop :

A

150 ft

75
Q

Autopilot Limitations - Min decision height:

A

Min decision height:

200 ft

76
Q

Autopilot Limitations - Minimum height (no approach):

A 
Minimum height (no approach):
1,000ft
77
Q

MINIMUM TURNING RADIUS

WITH NOSEWHEEL STEERING

A

47 FT. 9 IN.

78
Q

Total usable fuel capacity is

A

19,065 lbs

an additional 119 LBS unusable

79
Q

Air Brakes Steady and flashing

A

Steady: AB not stowed

Flashing: Auto Stowed

80
Q

Configuration Panel Black Arrow (Red)

A

Disagreement btwn slat/Flap VS Slats Postion

81
Q

Main gear Red Lights

A

Main gear doors not closed

82
Q

Oil Amber light

A

Low oil Pressure (<25 PSI)

Chip detected (metal)

83
Q

2 P BK Steady, Flashing

A

Steady: Num2 Brk Pressure > 230 PSI

Flashing:

The brake accumulator need to charge
< 1500 PSI PB Accumulator

84
Q

Pitch Feel:

A

Dis aggrement : Elevator Arthur Position VS Hor Stab

85
Q

TRANS Fire panel

A

Disagreement:

Btw Eng Fuel Shutoff Valve
VS
Fuel Shutoff Switch

86
Q

Max Spd total hydraulic Loss

A

260 kts / 0.76 M

87
Q

MZFW

A

30,870 LB

88
Q

Bleed APU

A

Disagreement: Btwn APU Bleed Valve OPen Vs Apu bleed Switch

Or
PWL > 54 Degree and APU
Bleed Valve Not Closed

89
Q

What causes T/O Config: “FATS’

A

Any PWR LVL >82D and:

Flaps <7D or 22D
AB not Stowed
Trim not in green
SLATS (Inboard not ext)

90
Q

CABIN - Audio Warning and with Audio

A

With Audio : Cabin Altitude > 10K

Without “CABIN” Audio warning:

The main entry door is not locked or
Forward lav service panel not closed

91
Q

Eng 2 Fail

A

GRD: PWL > 84D
ENG 2 N1< 85%

Grd or Flight: S Duct not closed

92
Q

Windshield Cracked or Bubbles

A

230 kts

Max 7.5 PSI

93
Q

BAG ISOL

A

The baggage compartment isolation valve is closed

94
Q

BAG Access

A

Cabin baggage access door not closed

95
Q

REV UNLOCK

A

DISagreement btw Thrus REV LVL Stowed Vs Thr Rev Claw locks not locked

96
Q

Fueling

A 
Refueling control panel door
refuel connnector door
Vent valve lever not stowed
Vent Valves 2 not closed
Gravity fueling switch on
Defueling switch on
REF/DEF valve open
B2 bus not powered
97
Q

Ail Feel

A

Dis AileronArthur Q Position VS Airspeed (ADC1 or ADC2)

98
Q

MACH TRIM

A

Mach trim sys not engaged

AP oon 0.80M max

99
Q

AIL ZERO

A

Emergency aileron actuator not in the neutral position

My Falcon (2 decks)

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