Falcon 2000EASy - Limitations Flashcards
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1
Q
MNPS
What are the min navigation requirements to
Operate in MNPS airspace?
A
- 2 FMS are operating and
- 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
2
Q
Polar operations
What are the limitations for Polar operations?
A
Polar operations are limited to 85° North or 85° South.
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.
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
- FMS 7.0, and no DGR warning is present on HSI, and
- 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.
5
Q
Max PAX
- D-BIKA
- D-BLUE
A
Max PAX 10
6
Q
DOM D-BIKA
A
24.800 lbs.
7
Q
DOM D-BLUE
A
25.130 lbs.
8
Q
Max Operating altitude ?
A
47.000’
9
Q
Max Ramp Mass ?
DBIKA
DBLUE
A
DBIKA 42.400 LBS
DBLUE 43.000 LBS
10
Q
Max Takeoff Mass ?
DBIKA
DBLUE
A
DBIKA 42.200 LBS
DBLUE 42.800 LBS
11
Q
Max Landing Mass ?
A
39.300 lbs
12
Q
Max Zero Fuel Mass ?
A
29.700 lbs
13
Q
Does the position of the Landing Gear have any Influence on CG ?
A
No
14
Q
Total loading weight into the Baggage compartment?
A
1.600 lbs
15
Q
Total Payload
A
5.990 lbs
16
Q
Load distribution in the cabin?
A
200 kg/m*3
For Aisle floor and passenger cabin Floor
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.
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.
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.
20
Q
Flaps extended or operating speed ?
- SF 1
- SF 2
- SF 3
Caution: What is the max altitude with flaps/slats extended or being retracted ?
A
- SF 1 = 200 kt
- SF 2 = 190 kt
- SF 3 = 180 kt
CAUTION
Above 20,000 ft do not establish or maintain a configuration
with the flaps or the slats extended.
21
Q
Minimum Control speed in the air VMCA?
A
90 kt
22
Q
Minimum Control speed on the ground VMCG?
A
98 kt
23
Q
Minimum Control speed during Approach and Landing VMCL?
A
90 kt
24
Q
Windshield Wiper operating speed VWWO?
A
215 kt
25
Sliding Window opening speed ?
215 kt
26
Tire maximum operating speed ?
195 kt Ground Speed
27
Load Factor Limits
1. Flaps up ?
2. Flaps down ?
1. Flaps up +2.55 to -1.0 g
| 2. Flaps down +2.0 to 0 g
28
Min. and Max. Airport altitude ?
-1.000' - 14.000'
29
Max. Tailwind component for Take-Off and Landing ?
10 kt
| Takeoff and Landing with Tailwind not recommended on contaminated runway!
30
Max Tailwind component for CAT II ?
10 kt
31
Max Crosswind component ?
1. Normal
2. CAT II
3. Icy rwy
1. Normal 35 kt
2. CAT II 20 kt
3. Icy rwy 5 kt
32
Max headwind component for CAT II ?
25 kt
33
Contaminated Runway Operation
Take-off:
Runway contaminated by ice both...
Landing:
Slats / Flap .....
Air brakes ....
At least braking system....
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.
34
Contaminated Runway Operation
Take-off: Slats/Flaps position ?
Must be in position SF2 for Take-Off.
35
Contaminated Runway Operation
May FMS TOLD data be used for Contaminated Runways?
No !
CAUTION
For operations on contaminated runways, FMS TOLD information must be disregarded and performance must be determined using Contaminated Runway Charts performance
36
Contaminated Runway Operation
May reverse thrust credit be used for contaminated Runway Operation ?
Yes.
37
Contaminated Runway Operation
Max contaminated depth for standing water.
Take-Off:
Landing:
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.
38
Thrust output for PW308C (Sea-level,ISA, etc.)
Take-Off:
Max. Continuous:
Take-Off: 6998 lbs
Max Continuous: 6998 lbs
Take-Off thrust is limited to 5 min!
39
Rotor Speed Limits
Take-Off, max T/O, max continuous,
1. N1 ?
2. N2 ?
Transient for 20sec
1) N1 ?
2) N2 ?
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
ITT limits
Ground Start
950°C
41
ITT limits
Airstart
950°C
42
ITT limits
Restart max temperature:
Air-start. °C
Ground-start °C
Restart max temperature:
Air-start. 500°C
Ground-start 340°C
43
ITT limits
Max Take-Off (APR): °C
Max Take-Off (APR) 895°C
| 5min max.
44
ITT limits
Normal Take-Off °C
Normal Take-Off 875°C
Max 5min.
45
ITT limits
Max Continuous °C
Max Continuous 860°C
46
Engine start
From start to 5,2% N2: ? sec
From start to light-off: ? sec
From light-off to idle: ? sec
Engine start
From start to 5,2% N2: 15sec
From start to light-off: 20 sec
From light-off to idle: 60sec
47
Engine starter Cutout at ? %N2
50% N2
48
How long do you have to wait for an engine restart, and why ?
Do not attempt an engine restart or motoring (ground only) before the 3 minute lasting Rudder test is over.
49
GPU START
If start is made with GPU (AIR assistance), air flow limitations are
Maximum temperaturen °C
Maximum pressure psi
Maximum flow lb/min
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
Autoflight
The use of the Flight director below ... is prohibited.
The use of the Flight director below 400ft is prohibited.
51
Autoflight
When may you use the Autopilot after Take-Off?
1) Altitude
2) Speed
1) Altitude: above 400'
| 2) Speed: V2 +10
52
Autoflight
During a go around, what speed restriction do I have, if I want to activate the Autopilot?
Vref + 10
53
Autoflight
During an ILS coupled approach, until what min. height may I use the Autopilot RA operative ?
50'
54
Autoflight
During an ILS coupled approach, until what min. height may I use the Autopilot RA inoperative ?
160'
55
Autoflight
During cruise, what is my min. height using the Autopilot ?
1.000'
56
Autoflight
During a non precision approach, until what min. height may I use the Autopilot ?
160'
57
Autoflight
During a circling approach, until what min. height may I use the Autopilot ?
500'
58
Autoflight
What is the minimum height to engage the autothrottle?
400'
59
Autoflight
What is the minimum height to disengage the autothrottle at landing?
50 ft
60
Auto-throttle
If FMS SPEED is selected on Guidance Panel:
The autothrottle must not be engaged before the airplane is in.......?
Clean configuration at take-off and go-around.
61
The fire category for the Falcon 2000EASy is?
4
62
Jeppesen Terminal Charts
The use of the Jeppesen Electronic Terminal charts requires:
In flight 4 DU's operative.
63
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.
Info only
64
When shall you arm the approach?
Arm APP when the track of the aircraft is less than 90° from the final approach course.
65
TERR INHIB MKB pushbutton shall be used when?
1)
2)
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
AUXILIARY POWER UNIT (APU)
1) Maximum operating altitude ?
2) Maximum starting altitude?
3) Maximum N1 speed?
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
AUXILIARY POWER UNIT (APU)
Exhaust Gas Temperature Limits (EGT)
1) Starting?
2) Stabilized?
AUXILIARY POWER UNIT (APU)
Exhaust Gas Temperature Limits (EGT)
1) Starting? 988 °C less than 10 sec.
2) Stabilized? 746 °C
68
APU
Maximum generator output:
Stabilized:
0 to 10,000 ft
10,000 to 25,000 ft
25,000 to 35,000 ft
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
OIL PRESSURE
At how much psi will ENG...: OIL PRESS msg appear?
Below....psi
OIL PRESSURE
At how much psi will ENG...: OIL PRESS msg appear?
Below 20psi
70
OIL PRESSURE
What is the maximum Oil pressure for a cold start?
OIL PRESSURE
The maximum Oil pressure during cold starting is 240 psi.
71
Oil Temperature limits
1) Maximum:
2) Minimum for take-off:
3) Minimum in flight:
4) Cold start:
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
Fuel
The total usable fuel quantity
1) In Liters ?
2) In pounds ?
1) 9,450 ltr.
| 2) 16,730 lbs.
73
What is the nose gear tire pressure?
btn 184 and 190 psi
74
What is the main gear tire pressure?
btn 219 and 228 psi
75
Fuel
Maximum fuel dissymmetry?
Fuel
Maximum fuel dissymmetry? 2.200lb
76
Fuel
Maximum feed pressure for fueling?
Fuel
Maximum feed pressure for fueling? 50psi
77
Fuel
In flight tank fuel temperature must be maintained at least at ...°C above the freezing point of fuel being used.
Fuel
In flight tank fuel temperature must be maintained at least at 3°C above the freezing point of fuel being used.
78
Fuel
Does the Fuel Quantity Management Computer (FQMC) need to be operative for T/O?
Fuel
Yes
79
Electrical Power
Maximum voltage of DC System: ?
Electrical Power
29,5 V
80
Electrical Power
Battery temperature limitation
Warm ? ...°C
Hot ? ...°C
Electrical Power
Battery temperature limitation
Warm ? 49°C/120°F
Hot ? 71°C/160°F
81
Air Conditining System
Maximum differential pressure?
Air Conditining System
9.3psi
82
Hydraulic
Hydraulic quantity
Reservoir 1....?
Reservoir 2....?
Hydraulic
Hydraulic quantity
Reservoir 1...7.4 ltr
Reservoir 2...6 ltr.
83
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.
Info only
84
Radio Management
Note:
It is recommended to wait 5 seconds between swapping of HF frequency and pushing the HF Push-to-talk button
Info only
85
Flight Controls
Maximum speed with ARTHUR UNIT inoperative.....?
Flight Controls
260 KIAS/M 0.76
86
Ice and Rain Protection
When does icing conditions exist ?
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
Ice and Rain Protection
When shall Engine Anti-Ice be used?
Between 10°C TAT and -40°C SAT in visible Moisture.
| and also in PICs decision flying through Cumuliform clouds.
88
Ice and Rain Protection
When shall Wing Anti-Ice be used?
Not above 10°C and not on the ground!
| Functionality test on the ground is allowed.
89
Oxygen
Passenger oxygen mask drop at .....ft
Above 14,500ft +/- 500ft
90
Passenger door max weight is....lb
1200lb(560kg)
91
Passenger door max weight on one step is....lb.
440lb(200kg)
92
EFB
When must the EFB be stored in the book rack behind the pilots seat?
1000ft AGL
93
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.
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
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?
In the left gear box for the main gear and in the nose gear box for the nose gear.
95
Lights
What are the limits using the landing lights on ground?
15 minutes cycle with a 45min. cooling period.
