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CAE Phenom 300 Limitations > CAE Phenom 300 Limitations REV 10 > Flashcards

CAE Phenom 300 Limitations REV 10 Flashcards

Memorize CAE's flash cards for the P300 limitations

1
Q

Max Ramp Weight (MRW)

A

18,078 Lbs.

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2
Q

Max Takeoff Weight (MTOW)

A

17,968 Lbs.

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3
Q

Max Landing Weight (MLW)

A

16,865 Lbs.

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4
Q

Max Zero Fuel Weight (MZFW)

A

13,999 Lbs.

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5
Q

Max speed at which the Landing Gear can be safely extended and retracted (VLO)

A

250 KTS.

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6
Q

Max speed at which the airplane can be flown with the Landing Gear can be safely extended and locked (VLE)

A

250 KTS.

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7
Q

Minimum Control Speed (VMC) for takeoff

takeoff flaps

A

97 KTS

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8
Q

Minimum Control Speed (VMC) for landing

(landing flaps) in “No Icing Conditions’

A

91 KTS

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9
Q

Minimum Control Speed (VMC) for landing

(landing flaps) in “Icing Conditions’

A

95 KTS

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10
Q

Operating Maneuvering Speed (VO)

A

205 KTS

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11
Q 
Maximum Flap Extended Speed (VFE)
Flap 1
Flap 2
Flap 3
Flap Full
A

180 KTS
170 KTS
170 KTS
160 KTS

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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%

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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 and FULL)

A

2.00 g

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18
Q

Maximum Loading LH Forward Cabinet

A

44 LBS

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19
Q

Maximum Loading Lavatory Cabinet

A

33 LBS

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20
Q

Max Loading of Aft Baggage Compartment

A

463 LBS

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21
Q

Max Loading of Forward Baggage Compartment

A

110 LBS

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22
Q

Max loading of Refreshment Center

A

71 LBS

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23
Q

Max loading of Side-Facing Divan Stowage Compartments

A

36 LBS

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 prohibitions associated with the use of the SVS?

A

May not be used as primary source of information to base decisions and or plan maneuvers, to navigate or to avoid terrain, obstacles or traffic

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 the Ground:

A

330 Amps each

32
Q

Maximum Generator Load in Flight:

A

390 Amps each

33
Q

Maximum useable fuel quantity per tank:

A

2676 LBS

34
Q

Unusable fuel quantity per tank:

A

25.13 LBS

35
Q

Maximum Fuel Capacity

A

5401 LBS

36
Q

Maximum permitted imbalance between the tanks:

A

220 LBS

37
Q

Minimum Fuel Tank Temperature

A

-37c

38
Q

Maximum Fuel Tank Temperature (On Ground)

A

52 C

NOTE: Max fuel temp can be exceeded up to 80c in flight

39
Q

Position of ‘XFEED’ knob during Takeoff and Landing

A

OFF

40
Q

Engine Operational Limits:
Max Thrust:
Takeoff Thrust:

A

Time Limit | Max ITT | N2 | N1 | Oil pressure | Oil Temp
10 minutes | 725 ITT | 101 | 100 45-160 10 - 132.2
5 Minutes | 700 ITT 101 100 45-160 10-132.2

41
Q

Engine Operational Limits:
Max Continuous:
Max Climb:

A

Time Limit | Max ITT | N2 | N1 | Oil pressure | Oil Temp
N/A | 680 ITT | 101 | 100 45-160 10 - 132.2
N/A | 680 ITT 101 100 45-160 10-132.2

42
Q 
Starter Limits:
1st
2nd
3rd
4th
A 
Cool Down Time:
1 Minute
1 Minute
15  Minutes
30 Minutes
43
Q

For use of the air conditioning system operation on the ground:

A

The GPU must be used or one engine generator must be turned on

44
Q

Maximum Differential Pressure:

A

9.4 PSI

45
Q

Maximum Differential Overpressure:

A

9.6 PSI

46
Q

Maximum Differential Negative Pressure:

A

-0.3 PSI

47
Q

Pressurization: Takeoff and Landing:

A

0.2 PSI

48
Q

When must the crew activate the Ice Protection System?

A

When icing conditions exist or are anticipated per Section 3 Normal Procedures

49
Q

Maximum Takeoff and Landing altitude in ICE

A

10,000 FT

50
Q

OPERATION IN ICING CONDITIONS:
Minimum Airspeed (Flap and gear up)
Wing and Stabilizer Anti-ice system Inhibited:
Wing and Stabilizer Anti-ice system Armed:
Wing and Stabilizer Anti-ice system Uninhibited:

A

165 KTS
165 KTS
150 KTS

51
Q

When must the wing inspection light be operative?

A

Prior to flight into known or forecast icing conditions, at night

52
Q

Autopilot / Yaw Damper:

Minimum engagement height (dual engine)

A

600 ft AGL

53
Q

Autopilot / Yaw Damper:

Minimum engagement height (single engine)

A

1000 ft AGL

54
Q

Autopilot / Yaw Damper:

Minimum use height (dual engine)

A

195 ft AGL

55
Q

Autopilot / Yaw Damper:

Minimum use height (single engine)

A

220 ft AGL

56
Q 
Autopilot / Yaw Damper
Altitude Loss (maneuvering / cruise)
A

160 ft AGL

57
Q

Yaw Damper OFF airspeed is limited to ___ if in icing conditions:

A

180 KTS

CAE Phenom 300 Limitations (1 decks)

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