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Falcon 2000 Easy > Falcon 2000EASy - Limitations > Flashcards

Falcon 2000EASy - Limitations Flashcards

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1
Q

MNPS

What are the min navigation requirements to
Operate in MNPS airspace?

A
  1. 2 FMS are operating and
  2. 2 IRS are in NAV mode or
    2 GPS are in NAV mode or
    1 IRS is in NAV MODE and 1 GPS is in NAV mode
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2
Q

Polar operations

What are the limitations for Polar operations?

A

Polar operations are limited to 85° North or 85° South.

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3
Q

Polar Operations

What must the crew be aware of when passing 73* North, Northbound or 60* South southbound ?

A

Polar Operations

The crew must check that HSI automatically switches to TRUE reference when passing 73° North northbound or 60° South southbound.

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4
Q

B-RNAV & P-RNAV

What equipment is required for B-RNAV operation ?

If GPS is the unique means of B-RNAV navigation
source (GPS stand alone), what must be monitored ?

A
  1. FMS 7.0, and no DGR warning is present on HSI, and
  2. Either of the following navigation modes:
    GPS,
    DME / DME,
    VOR / DME,
    IRS (2 hours time limit after last IRS alignment).

Use of GPS Integrity Monitoring (RAIM) Prediction program is mandatory before B-RNAV operation.

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5
Q

Max PAX

  1. D-BIKA
  2. D-BLUE
A

Max PAX 10

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6
Q

DOM D-BIKA

A

24.800 lbs.

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7
Q

DOM D-BLUE

A

25.130 lbs.

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8
Q

Max Operating altitude ?

A

47.000’

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9
Q

Max Ramp Mass ?

DBIKA
DBLUE

A

DBIKA 42.400 LBS

DBLUE 43.000 LBS

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10
Q

Max Takeoff Mass ?

DBIKA
DBLUE

A

DBIKA 42.200 LBS

DBLUE 42.800 LBS

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11
Q

Max Landing Mass ?

A

39.300 lbs

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12
Q

Max Zero Fuel Mass ?

A

29.700 lbs

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13
Q

Does the position of the Landing Gear have any Influence on CG ?

A

No

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14
Q

Total loading weight into the Baggage compartment?

A

1.600 lbs

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15
Q

Total Payload

A

5.990 lbs

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16
Q

Load distribution in the cabin?

A

200 kg/m*3

For Aisle floor and passenger cabin Floor

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17
Q

Maneuvering Speed VA ?

A

198 kt

CAUTION Full application of rudder or aileron controls, as well
as maneuvers that involve angles-of-attack near the stall must
be confined to speeds below VA. Rapidly alternating large rudder
applications in combination with large sideslip angles may result
in structural failure at any speed.

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18
Q

Maximum Landing gear

Operating speed: VLO / MLO

A

VLO …..190 KIAS
MLO …. MI 0.70

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

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19
Q

Maximum Landing Gear

Extended speed: VLE / MLE

A

VLE .. 245 KIAS
MLE …. MI 0.75

VLE / MLE is the maximum speed at which the airplane can be safety with the landing gear extended,locked and main gears closed.

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20
Q

Flaps extended or operating speed ?

  1. SF 1
  2. SF 2
  3. SF 3

Caution: What is the max altitude with flaps/slats extended or being retracted ?

A
  1. SF 1 = 200 kt
  2. SF 2 = 190 kt
  3. SF 3 = 180 kt

CAUTION
Above 20,000 ft do not establish or maintain a configuration
with the flaps or the slats extended.

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21
Q

Minimum Control speed in the air VMCA?

A

90 kt

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22
Q

Minimum Control speed on the ground VMCG?

A

98 kt

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23
Q

Minimum Control speed during Approach and Landing VMCL?

A

90 kt

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24
Q

Windshield Wiper operating speed VWWO?

A

215 kt

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25
Q

Sliding Window opening speed ?

A

215 kt

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26
Q

Tire maximum operating speed ?

A

195 kt Ground Speed

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27
Q

Load Factor Limits

  1. Flaps up ?
  2. Flaps down ?
A
  1. Flaps up +2.55 to -1.0 g

2. Flaps down +2.0 to 0 g

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28
Q

Min. and Max. Airport altitude ?

A

-1.000’ - 14.000’

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29
Q

Max. Tailwind component for Take-Off and Landing ?

A

10 kt

Takeoff and Landing with Tailwind not recommended on contaminated runway!

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30
Q

Max Tailwind component for CAT II ?

A

10 kt

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31
Q

Max Crosswind component ?

  1. Normal
  2. CAT II
  3. Icy rwy
A
  1. Normal 35 kt
  2. CAT II 20 kt
  3. Icy rwy 5 kt
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32
Q

Max headwind component for CAT II ?

A

25 kt

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33
Q

Contaminated Runway Operation

Take-off:
Runway contaminated by ice both…

Landing:
Slats / Flap …..
Air brakes ….
At least braking system….

A

Contaminated Runway Operation

Take-off:
Runway contaminated by ice both reversers must be operative.

Landing:
Slats / Flaps must be in position SF3.
Airbrakes must be operative.
At least braking system #1 must be operative.

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34
Q

Contaminated Runway Operation

Take-off: Slats/Flaps position ?

A

Must be in position SF2 for Take-Off.

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35
Q

Contaminated Runway Operation

May FMS TOLD data be used for Contaminated Runways?

A

No !

CAUTION
For operations on contaminated runways, FMS TOLD information must be disregarded and performance must be determined using Contaminated Runway Charts performance

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36
Q

Contaminated Runway Operation

May reverse thrust credit be used for contaminated Runway Operation ?

A

Yes.

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37
Q

Contaminated Runway Operation

Max contaminated depth for standing water.
Take-Off:
Landing:

A

Take-Off: 9,5mm
Landing: 12,7mm

A runway is considered as wet if the surface is reflective and the standing water is equal or less than 3 mm.

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38
Q

Thrust output for PW308C (Sea-level,ISA, etc.)
Take-Off:
Max. Continuous:

A

Take-Off: 6998 lbs
Max Continuous: 6998 lbs

Take-Off thrust is limited to 5 min!

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39
Q

Rotor Speed Limits
Take-Off, max T/O, max continuous,
1. N1 ?
2. N2 ?

Transient for 20sec

1) N1 ?
2) N2 ?

A

Rotor Speed Limits
Take-Off, max T/O, max continuous,
1. N1 ? 102,5
2. N2 ? 102,0

Transient for 20sec

1) N1 ? 103,5
2) N2 ? 103,0

40
Q

ITT limits

Ground Start

A

950°C

41
Q

ITT limits

Airstart

A

950°C

42
Q

ITT limits

Restart max temperature:
Air-start. °C
Ground-start °C

A

Restart max temperature:
Air-start. 500°C
Ground-start 340°C

43
Q

ITT limits

Max Take-Off (APR): °C

A

Max Take-Off (APR) 895°C

5min max.

44
Q

ITT limits

Normal Take-Off °C

A

Normal Take-Off 875°C

Max 5min.

45
Q

ITT limits

Max Continuous °C

A

Max Continuous 860°C

46
Q

Engine start

From start to 5,2% N2: ? sec
From start to light-off: ? sec
From light-off to idle: ? sec

A

Engine start

From start to 5,2% N2: 15sec
From start to light-off: 20 sec
From light-off to idle: 60sec

47
Q

Engine starter Cutout at ? %N2

A

50% N2

48
Q

How long do you have to wait for an engine restart, and why ?

A

Do not attempt an engine restart or motoring (ground only) before the 3 minute lasting Rudder test is over.

49
Q

GPU START
If start is made with GPU (AIR assistance), air flow limitations are

Maximum temperaturen °C
Maximum pressure psi
Maximum flow lb/min

A

GPU START
If start is made with GPU (AIR assistance), air flow limitations are

Maximum temperaturen 480°F / 250°C
Maximum pressure 50 psi
Maximum flow 82 lb/min

50
Q

Autoflight

The use of the Flight director below … is prohibited.

A

The use of the Flight director below 400ft is prohibited.

51
Q

Autoflight

When may you use the Autopilot after Take-Off?

1) Altitude
2) Speed

A

1) Altitude: above 400’

2) Speed: V2 +10

52
Q

Autoflight

During a go around, what speed restriction do I have, if I want to activate the Autopilot?

A

Vref + 10

53
Q

Autoflight

During an ILS coupled approach, until what min. height may I use the Autopilot RA operative ?

A

50’

54
Q

Autoflight

During an ILS coupled approach, until what min. height may I use the Autopilot RA inoperative ?

A

160’

55
Q

Autoflight

During cruise, what is my min. height using the Autopilot ?

A

1.000’

56
Q

Autoflight

During a non precision approach, until what min. height may I use the Autopilot ?

A

160’

57
Q

Autoflight

During a circling approach, until what min. height may I use the Autopilot ?

A

500’

58
Q

Autoflight

What is the minimum height to engage the autothrottle?

A

400’

59
Q

Autoflight

What is the minimum height to disengage the autothrottle at landing?

A

50 ft

60
Q

Auto-throttle

If FMS SPEED is selected on Guidance Panel:

The autothrottle must not be engaged before the airplane is in…….?

A

Clean configuration at take-off and go-around.

61
Q

The fire category for the Falcon 2000EASy is?

A

4

62
Q

Jeppesen Terminal Charts

The use of the Jeppesen Electronic Terminal charts requires:

A

In flight 4 DU’s operative.

63
Q

Note:

Take-off and Landing (TOLD) Performances

TOLD Data for take-off and for landing are for advisory purpose only. TOLD must not be used for failure cases implying landing penalties. In such cases crew must select Manual Vspeeds in Landing data tab and enter each speed value.

A

Info only

64
Q

When shall you arm the approach?

A

Arm APP when the track of the aircraft is less than 90° from the final approach course.

65
Q

TERR INHIB MKB pushbutton shall be used when?
1)
2)

A

TERR INHIB MKB pushbutton shall be used when:

1) When within 15 NM of take-off, approach or landing at an airport that is not included in the airport database.
2) For operation with QFE reference if both GPS’s are not in NAVIGATION mode as in SENSORS window navigation tab when setting QFE.

66
Q

AUXILIARY POWER UNIT (APU)

1) Maximum operating altitude ?
2) Maximum starting altitude?
3) Maximum N1 speed?

A

AUXILIARY POWER UNIT (APU) HONEYWELL GTCP 36-150 (F2M)

1) Maximum operating altitude 35,000 ft
2) Maximum starting altitude 35,000 ft
3) Maximum N1 speed 110 %

67
Q

AUXILIARY POWER UNIT (APU)

Exhaust Gas Temperature Limits (EGT)

1) Starting?
2) Stabilized?

A

AUXILIARY POWER UNIT (APU)

Exhaust Gas Temperature Limits (EGT)

1) Starting? 988 °C less than 10 sec.
2) Stabilized? 746 °C

68
Q

APU

Maximum generator output:

Stabilized:
0 to 10,000 ft
10,000 to 25,000 ft
25,000 to 35,000 ft

A

APU

Maximum generator output:

Stabilized:
0 to 10,000 ft. 300 A
10,000 to 25,000 ft. 250 A
25,000 to 35,000 ft. 200 A

69
Q

OIL PRESSURE

At how much psi will ENG…: OIL PRESS msg appear?

Below….psi

A

OIL PRESSURE

At how much psi will ENG…: OIL PRESS msg appear?

Below 20psi

70
Q

OIL PRESSURE

What is the maximum Oil pressure for a cold start?

A

OIL PRESSURE

The maximum Oil pressure during cold starting is 240 psi.

71
Q

Oil Temperature limits

1) Maximum:
2) Minimum for take-off:
3) Minimum in flight:
4) Cold start:

A

Oil Temperature limits

1) Maximum: 135°C
2) Minimum for take-off: 27°C
3) Minimum in flight: 16°C
4) Cold start: -40°C

72
Q

Fuel

The total usable fuel quantity

1) In Liters ?
2) In pounds ?

A

1) 9,450 ltr.

2) 16,730 lbs.

73
Q

What is the nose gear tire pressure?

A

btn 184 and 190 psi

74
Q

What is the main gear tire pressure?

A

btn 219 and 228 psi

75
Q

Fuel

Maximum fuel dissymmetry?

A

Fuel

Maximum fuel dissymmetry? 2.200lb

76
Q

Fuel

Maximum feed pressure for fueling?

A

Fuel

Maximum feed pressure for fueling? 50psi

77
Q

Fuel

In flight tank fuel temperature must be maintained at least at …°C above the freezing point of fuel being used.

A

Fuel

In flight tank fuel temperature must be maintained at least at 3°C above the freezing point of fuel being used.

78
Q

Fuel

Does the Fuel Quantity Management Computer (FQMC) need to be operative for T/O?

A

Fuel

Yes

79
Q

Electrical Power

Maximum voltage of DC System: ?

A

Electrical Power

29,5 V

80
Q

Electrical Power

Battery temperature limitation
Warm ? …°C
Hot ? …°C

A

Electrical Power

Battery temperature limitation
Warm ? 49°C/120°F
Hot ? 71°C/160°F

81
Q

Air Conditining System

Maximum differential pressure?

A

Air Conditining System

9.3psi

82
Q

Hydraulic

Hydraulic quantity
Reservoir 1….?
Reservoir 2….?

A

Hydraulic

Hydraulic quantity
Reservoir 1…7.4 ltr
Reservoir 2…6 ltr.

83
Q

Radio Management

Note:
When transmitting in power set on High, HF tone may be activated in the frequency band btn 4 and 5.5MHz or btn 9.9 and 11 MHz. In that case, set power on ´MED´ or on `LOW´in order to recover HF use.

A

Info only

84
Q

Radio Management

Note:
It is recommended to wait 5 seconds between swapping of HF frequency and pushing the HF Push-to-talk button

A

Info only

85
Q

Flight Controls

Maximum speed with ARTHUR UNIT inoperative…..?

A

Flight Controls

260 KIAS/M 0.76

86
Q

Ice and Rain Protection

When does icing conditions exist ?

A

OAT on the ground and for T/O, or TAT in flight is 10°C or below, and visible moisture in any form is present.

87
Q

Ice and Rain Protection

When shall Engine Anti-Ice be used?

A

Between 10°C TAT and -40°C SAT in visible Moisture.

and also in PICs decision flying through Cumuliform clouds.

88
Q

Ice and Rain Protection

When shall Wing Anti-Ice be used?

A

Not above 10°C and not on the ground!

Functionality test on the ground is allowed.

89
Q

Oxygen

Passenger oxygen mask drop at …..ft

A

Above 14,500ft +/- 500ft

90
Q

Passenger door max weight is….lb

A

1200lb(560kg)

91
Q

Passenger door max weight on one step is….lb.

A

440lb(200kg)

92
Q

EFB

When must the EFB be stored in the book rack behind the pilots seat?

A

1000ft AGL

93
Q

Landing Gear and Brakes

Before taxiing the brake temperature shall be ….°C or lower and decreasing. During taxi the temperature can be higher than …°C if the following has not occured:
….full stops at 20kt or
….full stops at 10kt.

A

Landing Gear and Brakes

Before taxiing the brake temperature shall be 160°C or lower and decreasing. During taxi the temperature can be higher than 160°C if the following has not occured:
5 full stops at 20kt or
20 full stops at 10kt.

94
Q

Landing Gear and Brakes

On the acft, where can you find a placard informing you the shock absorber height for a weight of 40,900lb?

A

In the left gear box for the main gear and in the nose gear box for the nose gear.

95
Q

Lights

What are the limits using the landing lights on ground?

A

15 minutes cycle with a 45min. cooling period.

Falcon 2000 Easy (3 decks)

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