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CAE Phenom 300 FLASHCARDS > FC Phenom 300 > Flashcards

FC Phenom 300 Flashcards

Aviation

1
Q

Max Ramp Weight

A

18,078 lbs

8,200 kg

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2
Q

Max Takeoff Weight (MTOW)

A

17,968 lbs

8,150 kg

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3
Q

Max Landing Weight (MLW)

A

16,865 lbs

7,650 kg

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4
Q

Max Zero-fuel Weight (MZFW)

A

13,999lbs

6,350 kg

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5
Q

Maximum Speed at which the landing gear can be safely extended & retracted (Vlo)

A

250 KIAS

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6
Q

Maximum Speed at which the airplane can be flown with the landing gear extended and locked (Vle)?

A

250 KIAS

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7
Q

Minimum Control Speed ( Vmc) for takeoff (takeoff flaps):

A

97 KIAS

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8
Q

Minimum Control Speed ( Vmc) for landing (landing flaps) in ‘ No Icing Conditions’:

A

91 KIAS

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9
Q

Minimum Control Speed ( Vmc ) for landing (landing flaps) in ‘Icing Conditions’:

A

95 KIAS

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10
Q

Operating Maneuvering Speed ( Vo ):

A

205 KIAS

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11
Q

Maximum Flap Extended Speed (Vfe)

Flap 1:
Flap 2:
Flap 3:
Flap Full:

A

Flap 1 : 180 KIAS
Flap 2 : 170 KIAS
Flap 3 : 170 KIAS
Flap Full : 160 KIAS

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12
Q

Maximum Altitude with extended Flaps:

A

18,000 ft

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13
Q

Maximum Tire Ground Speed:

A

182 Kts

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14
Q

Runway slope

A

-2% to +2%

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15
Q

Type of runway surface

A

Paved

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16
Q

Load Factor Limit ( G loads) with Flaps UP

A

3.00 g

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17
Q

Load Factor Limit ( G loads) with Flaps DOWN (1,2,3 & FULL)

A

2.00 g

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18
Q

Maximum loading:

LH Forward Cabinet

A

44lb (20 kg)

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19
Q

Maximum loading:

Lavatory Cabinet

A

33 lb (15 kg)

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20
Q

Maximum loading:

Aft Baggage Compartment

A

463 lb (210 kg)

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21
Q

Maximum loading:

Forward Baggage Compartment

A

110 lb (50kg)

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22
Q

Maximum loading:

Refreshment Center

A

71 lb ( 32 kg)

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23
Q

Maximum loading:

Side-Facing Divan Stowage Compartments

A

36lb (16.5kg)

24
Q

Max Takeoff and landing tailwind component

25
Q

Max crosswind component allowed to apply static takeoff power

26
Q

Hydraulic System Accumulator pre-charge check interval

A

15 consecutive calendar days or before the next flight, whichever occurs last

27
Q

Stall Warning and Protection System must be tested

A

Prior to each flight

28
Q

What are the prohibition associated with the use of the SVS?

A

Use of the SVS as primary information to base decisions and/or plan maneuvers, to navigate, or to avoid terrain, obstacles, or traffic is prohibited.

29
Q

Minimum battery voltage required for engine start

30
Q

Minimum GPU voltage required for battery charging

31
Q

Maximum generator load on Ground

A

330 Amps each

32
Q

Maximum generator load in flight

A

390 Amps each

33
Q

Maximum usable fuel quantity per tank

A

ANAC/EASA - 1,512 L (1,214 kg)

34
Q

Unusable fuel quantity per tank

A

ANAC/EASA - 14L (11 kg)

35
Q

Maximum Fuel capacity

A

ANAC/EASA - 3,052L (2,450kg)

36
Q

Maximum permitted imbalance between tanks

A

ANAC/EASA - 125L (100 KG)

37
Q

Minimum Fuel tank temperature

38
Q

Maximum fuel tank temperature ( on Ground)

A

52°C

Note: Maximum Fuel temp can be exceeded up to 80°C in flight

39
Q

Position of ‘XFEED’ Knob during Takeoff & Landing

40
Q 
Max Thrust (operating limits):
Time Limit
Maximum ITT(°C)
N2(%)
N1(%)
Oil Pressure (PSID)
Oil Temperature (°C)
A 
10 minutes
725
101
100
45 to 160
10 to 132.2
41
Q 
Takeoff Thrust (operating limits):
Time Limit
Maximum ITT(°C)
N2(%)
N1(%)
Oil Pressure (PSID)
Oil Temperature (°C)
A 
5 minutes
700
101
100
45 to 160
10 to 132.2
42
Q 
Max continuous (operating limits):
Time Limit
Maximum ITT(°C)
N2(%)
N1(%)
Oil Pressure (PSID)
Oil Temperature (°C)
A 
N/A
680
101
100
45 to 160
10 to 132.2
43
Q 
Max climb (operating limits):
Time Limit
Maximum ITT(°C)
N2(%)
N1(%)
Oil Pressure (PSID)
Oil Temperature (°C)
A 
N/A
680
101
100
45 to 160
10 to 132.2
44
Q 
Ground idle (operating limits):
Time Limit
Maximum ITT(°C)
N2(%)
N1(%)
Oil Pressure (PSID)
Oil Temperature (°C)
A 
N/A
N/A
min 55.1(OEI) / min 51.2 (AEO)
-
25 to 160
-40 to 132.2
45
Q 
Flight idle (operating limits):
Time Limit
Maximum ITT(°C)
N2(%)
N1(%)
Oil Pressure (PSID)
Oil Temperature (°C)
A 
N/A
N/A
55.1
-
25 to 160
-
46
Q 
Starting (operating limits):
Time Limit
Maximum ITT(°C)
N2(%)
N1(%)
Oil Pressure (PSID)
Oil Temperature (°C)
A 
5 seconds
765
-
-
-
-40 minimum
47
Q 
Transient (operating limits):
Time Limit
Maximum ITT(°C)
N2(%)
N1(%)
Oil Pressure (PSID)
Oil Temperature (°C)
A 
20 seconds
765 
103
102
0-20
-

______________________________

200 seconds
-
-
-
-
140.5 Maximum

_____________________________

400 seconds
-
-
-
20-270
-
48
Q 
Starter Limit
Motoring Attempt
1
2
3
4
A

60 seconds
60 seconds
15 minutes
30 minutes

NOTE: after four sequencial motorings, cycle may be repeated following a 30 minute cool-down period.

49
Q

For air conditioning system operation on ground

A

The gpu must be used or one engine generator must be turned ON

50
Q

Pressurization

Maximum differential pressure

51
Q

pressurization

Maximum differential overpressure

52
Q

pressurization

Maximum differential negative pressure

53
Q

pressurization

Maximum differential pressure for takeoff and landing

54
Q

Ice and Rain Protection

When must the crew activate the ice protection system

A

Crew must activate the ice protection system when icing conditions exist or are anticipated, as per Section 3, Normal Procedures.

55
Q

Ice and Protection

Define: “when icing conditions exist or are anticipated”?

A

Icing Conditions may exist whenever;

1) The Static Air Temperature ( SAT) on the ground or for takeoff, or Total Air Temperature (TAT) in flight, is 10°C or bellow and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet or ice crystals).
2) SAT on the ground is 10°C or below and ramps, taxiways, or runways are contaminated with surface snow, ice, standing water, or slush.

CAE Phenom 300 FLASHCARDS (1 decks)

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