FC Phenom 300

Question 1

Max Ramp Weight

Answer 1

18,078 lbs

8,200 kg

Question 2

Max Takeoff Weight (MTOW)

Answer 2

17,968 lbs

8,150 kg

Question 3

Max Landing Weight (MLW)

Answer 3

16,865 lbs

7,650 kg

Question 4

Max Zero-fuel Weight (MZFW)

Answer 4

13,999lbs

6,350 kg

Question 5

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

Answer 5

250 KIAS

Question 6

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

Answer 6

250 KIAS

Question 7

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

Answer 7

97 KIAS

Question 8

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

Answer 8

91 KIAS

Question 9

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

Answer 9

95 KIAS

Question 10

Operating Maneuvering Speed ( Vo ):

Answer 10

205 KIAS

Question 11

Maximum Flap Extended Speed (Vfe)

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

Answer 11

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

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% to +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 & FULL)

Answer 17

2.00 g

Question 18

Maximum loading:

LH Forward Cabinet

Answer 18

44lb (20 kg)

Question 19

Maximum loading:

Lavatory Cabinet

Answer 19

33 lb (15 kg)

Question 20

Maximum loading:

Aft Baggage Compartment

Answer 20

463 lb (210 kg)

Question 21

Maximum loading:

Forward Baggage Compartment

Answer 21

110 lb (50kg)

Question 22

Maximum loading:

Refreshment Center

Answer 22

71 lb ( 32 kg)

Question 23

Maximum loading:

Side-Facing Divan Stowage Compartments

Answer 23

36lb (16.5kg)

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 prohibition associated with the use of the SVS?

Answer 28

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.

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 Ground

Answer 31

330 Amps each

Question 32

Maximum generator load in flight

Answer 32

390 Amps each

Question 33

Maximum usable fuel quantity per tank

Answer 33

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

Question 34

Unusable fuel quantity per tank

Answer 34

ANAC/EASA - 14L (11 kg)

Question 35

Maximum Fuel capacity

Answer 35

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

Question 36

Maximum permitted imbalance between tanks

Answer 36

ANAC/EASA - 125L (100 KG)

Question 37

Minimum Fuel tank temperature

Answer 37

-37°C

Question 38

Maximum fuel tank temperature ( on Ground)

Answer 38

52°C Note: Maximum Fuel temp can be exceeded up to 80°C in flight

Question 39

Position of 'XFEED' Knob during Takeoff & Landing

Answer 39

'OFF'

Question 40

``` Max Thrust (operating limits): Time Limit Maximum ITT(°C) N2(%) N1(%) Oil Pressure (PSID) Oil Temperature (°C) ```

Answer 40

``` 10 minutes 725 101 100 45 to 160 10 to 132.2 ```

Question 41

``` Takeoff Thrust (operating limits): Time Limit Maximum ITT(°C) N2(%) N1(%) Oil Pressure (PSID) Oil Temperature (°C) ```

Answer 41

``` 5 minutes 700 101 100 45 to 160 10 to 132.2 ```

Question 42

``` Max continuous (operating limits): Time Limit Maximum ITT(°C) N2(%) N1(%) Oil Pressure (PSID) Oil Temperature (°C) ```

Answer 42

``` N/A 680 101 100 45 to 160 10 to 132.2 ```

Question 43

``` Max climb (operating limits): Time Limit Maximum ITT(°C) N2(%) N1(%) Oil Pressure (PSID) Oil Temperature (°C) ```

Answer 43

``` N/A 680 101 100 45 to 160 10 to 132.2 ```

Question 44

``` Ground idle (operating limits): Time Limit Maximum ITT(°C) N2(%) N1(%) Oil Pressure (PSID) Oil Temperature (°C) ```

Answer 44

``` N/A N/A min 55.1(OEI) / min 51.2 (AEO) - 25 to 160 -40 to 132.2 ```

Question 45

``` Flight idle (operating limits): Time Limit Maximum ITT(°C) N2(%) N1(%) Oil Pressure (PSID) Oil Temperature (°C) ```

Answer 45

``` N/A N/A 55.1 - 25 to 160 - ```

Question 46

``` Starting (operating limits): Time Limit Maximum ITT(°C) N2(%) N1(%) Oil Pressure (PSID) Oil Temperature (°C) ```

Answer 46

``` 5 seconds 765 - - - -40 minimum ```

Question 47

``` Transient (operating limits): Time Limit Maximum ITT(°C) N2(%) N1(%) Oil Pressure (PSID) Oil Temperature (°C) ```

Answer 47

``` 20 seconds 765 103 102 0-20 - ``` ______________________________ ``` 200 seconds - - - - 140.5 Maximum ``` _____________________________ ``` 400 seconds - - - 20-270 - ```

Question 48

``` Starter Limit Motoring Attempt 1 2 3 4 ```

Answer 48

60 seconds 60 seconds 15 minutes 30 minutes NOTE: after four sequencial motorings, cycle may be repeated following a 30 minute cool-down period.

Question 49

For air conditioning system operation on ground

Answer 49

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

Question 50

*Pressurization* | Maximum differential pressure

Answer 50

9.4 psi

Question 51

*pressurization* | Maximum differential overpressure

Answer 51

9.6 PSI

Question 52

*pressurization* | Maximum differential negative pressure

Answer 52

-0.3 PSI

Question 53

*pressurization* | Maximum differential pressure for takeoff and landing

Answer 53

0.2 PSI

Question 54

*Ice and Rain Protection* When must the crew activate the ice protection system

Answer 54

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

Question 55

*Ice and Protection* Define: "when icing conditions exist or are anticipated"?

Answer 55

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.