Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

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

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Max Takeoff Weight (MTOW)

A

17,968 lbs

8,150 kg

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Max Landing Weight (MLW)

A

16,865 lbs

7,650 kg

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Max Zero-fuel Weight (MZFW)

A

13,999lbs

6,350 kg

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

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

A

250 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

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

A

250 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

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

A

97 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

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

A

91 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

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

A

95 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Operating Maneuvering Speed ( Vo ):

A

205 KIAS

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
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

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Maximum Altitude with extended Flaps:

A

18,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Maximum Tire Ground Speed:

A

182 Kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Runway slope

A

-2% to +2%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Type of runway surface

A

Paved

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Load Factor Limit ( G loads) with Flaps UP

A

3.00 g

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

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

A

2.00 g

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Maximum loading:

LH Forward Cabinet

A

44lb (20 kg)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Maximum loading:

Lavatory Cabinet

A

33 lb (15 kg)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

Maximum loading:

Aft Baggage Compartment

A

463 lb (210 kg)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

Maximum loading:

Forward Baggage Compartment

A

110 lb (50kg)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

Maximum loading:

Refreshment Center

A

71 lb ( 32 kg)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

Maximum loading:

Side-Facing Divan Stowage Compartments

A

36lb (16.5kg)

24
Q

Max Takeoff and landing tailwind component

A

10 KTS

25
Q

Max crosswind component allowed to apply static takeoff power

A

18 KTS

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

A

24 V

30
Q

Minimum GPU voltage required for battery charging

A

27 V

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

A

-37°C

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

A

‘OFF’

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

A

9.4 psi

51
Q

pressurization

Maximum differential overpressure

A

9.6 PSI

52
Q

pressurization

Maximum differential negative pressure

A

-0.3 PSI

53
Q

pressurization

Maximum differential pressure for takeoff and landing

A

0.2 PSI

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)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions