CAE Phenom 300 Limitations REV 10

Question 1

Max Ramp Weight (MRW)

Answer 1

18,078 Lbs.

Question 2

Max Takeoff Weight (MTOW)

Answer 2

17,968 Lbs.

Question 3

Max Landing Weight (MLW)

Answer 3

16,865 Lbs.

Question 4

Max Zero Fuel Weight (MZFW)

Answer 4

13,999 Lbs.

Question 5

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

Answer 5

250 KTS.

Question 6

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

Answer 6

250 KTS.

Question 7

Minimum Control Speed (VMC) for takeoff

takeoff flaps

Answer 7

97 KTS

Question 8

Minimum Control Speed (VMC) for landing

(landing flaps) in “No Icing Conditions’

Answer 8

91 KTS

Question 9

Minimum Control Speed (VMC) for landing

(landing flaps) in “Icing Conditions’

Answer 9

95 KTS

Question 10

Operating Maneuvering Speed (VO)

Answer 10

205 KTS

Question 11

Maximum Flap Extended Speed (VFE)
Flap 1
Flap 2
Flap 3
Flap Full

Answer 11

180 KTS
170 KTS
170 KTS
160 KTS

Question 12

Maximum altitude with extended Flaps:

Answer 12

18,000 ft.

Question 13

Maximum Tire Ground Speed:

Answer 13

182 KTS

Question 14

Runway Slope:

Answer 14

+/- 2%

Question 15

Type of Runway Surface:

Answer 15

Paved

Question 16

Load Factor Limit (G Loads) with Flaps UP:

Answer 16

3.00 g

Question 17

Load Factor Limit (G Loads) with Flaps DOWN (1,2,3 and FULL)

Answer 17

2.00 g

Question 18

Maximum Loading LH Forward Cabinet

Answer 18

44 LBS

Question 19

Maximum Loading Lavatory Cabinet

Answer 19

33 LBS

Question 20

Max Loading of Aft Baggage Compartment

Answer 20

463 LBS

Question 21

Max Loading of Forward Baggage Compartment

Answer 21

110 LBS

Question 22

Max loading of Refreshment Center

Answer 22

71 LBS

Question 23

Max loading of Side-Facing Divan Stowage Compartments

Answer 23

36 LBS

Question 24

Max takeoff and landing tailwind component

Answer 24

10 KTS

Question 25

Max crosswind component allowed to apply static takeoff power

Answer 25

18 KTS

Question 26

Hydraulic System Accumulator pre-charge check interval:

Answer 26

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

Question 27

Stall warning and protection system must be tested:

Answer 27

Prior to each flight

Question 28

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

Answer 28

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

Question 29

Minimum battery voltage required for engine start:

Answer 29

24 V

Question 30

Minimum GPU voltage required for battery charging:

Answer 30

27 V

Question 31

Maximum generator load on the Ground:

Answer 31

330 Amps each

Question 32

Maximum Generator Load in Flight:

Answer 32

390 Amps each

Question 33

Maximum useable fuel quantity per tank:

Answer 33

2676 LBS

Question 34

Unusable fuel quantity per tank:

Answer 34

25.13 LBS

Question 35

Maximum Fuel Capacity

Answer 35

5401 LBS

Question 36

Maximum permitted imbalance between the tanks:

Answer 36

220 LBS

Question 37

Minimum Fuel Tank Temperature

Answer 37

-37c

Question 38

Maximum Fuel Tank Temperature (On Ground)

Answer 38

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

Question 39

Position of 'XFEED' knob during Takeoff and Landing

Answer 39

OFF

Question 40

Engine Operational Limits: Max Thrust: Takeoff Thrust:

Answer 40

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

Question 41

Engine Operational Limits: Max Continuous: Max Climb:

Answer 41

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

Question 42

``` Starter Limits: 1st 2nd 3rd 4th ```

Answer 42

``` Cool Down Time: 1 Minute 1 Minute 15 Minutes 30 Minutes ```

Question 43

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

Answer 43

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

Question 44

Maximum Differential Pressure:

Answer 44

9.4 PSI

Question 45

Maximum Differential Overpressure:

Answer 45

9.6 PSI

Question 46

Maximum Differential Negative Pressure:

Answer 46

-0.3 PSI

Question 47

Pressurization: Takeoff and Landing:

Answer 47

0.2 PSI

Question 48

When must the crew activate the Ice Protection System?

Answer 48

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

Question 49

Maximum Takeoff and Landing altitude in ICE

Answer 49

10,000 FT

Question 50

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:

Answer 50

165 KTS 165 KTS 150 KTS

Question 51

When must the wing inspection light be operative?

Answer 51

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

Question 52

Autopilot / Yaw Damper: | Minimum engagement height (dual engine)

Answer 52

600 ft AGL

Question 53

Autopilot / Yaw Damper: | Minimum engagement height (single engine)

Answer 53

1000 ft AGL

Question 54

Autopilot / Yaw Damper: | Minimum use height (dual engine)

Answer 54

195 ft AGL

Question 55

Autopilot / Yaw Damper: | Minimum use height (single engine)

Answer 55

220 ft AGL

Question 56

``` Autopilot / Yaw Damper Altitude Loss (maneuvering / cruise) ```

Answer 56

160 ft AGL

Question 57

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

Answer 57

180 KTS