Aircraft Speeds & Limitations

Question 1

Vlo

Answer 1

180

Question 2

Flaps >15 Extension Speed Vfe:

Answer 2

130

Question 3

Flap Cycle Limitations for -55 to 25 Celsius:

Answer 3

10 cycles per hour

Question 4

Vmo

Answer 4

240

Question 5

AFCS is approved for coupled missed approaches if:

Answer 5

initiated at DA or MDA.

Question 6

Maximum Takeoff Weight:

Answer 6

10,450 lbs

Question 7

Maximum Demonstrated Crosswind (dry runway):

Answer 7

Flaps 0 - 30 kts
Flaps 15 - 25 kts
Flaps 30 - 20 kts
Flaps 40 - 15 kts

Question 8

Landing Flaps 30 Speed:

Answer 8

89

Question 9

Amber Caution CAS Message PSI:

Answer 9

6.0 PSI

Question 10

Flaps 30 Go Around Speed:

Answer 10

89

Question 11

Maximum ITT (Turbine Temperature)

Answer 11

150 Celsius

Question 12

Maximum Ramp Weight:

Answer 12

10,495 lbs

Question 13

Maximum Operating Altitude:

Answer 13

30,000 feet

Question 14

Flap Cycle Limitations for 25 to 50 Celsius:

Answer 14

8 cycles per hour

Question 15

Minimum Boot Operating Temperature:

Answer 15

-40 Celsius

Question 16

Maximum Demonstrated Crosswind when Braking Action is reported less than Good:

Answer 16

Flaps 0 - 15 kts
Flaps 15 - 12.5 kts
Flaps 30 - 10 kts
Flaps 40 - 7.5 kts

Question 17

Landing Flaps 15 Speed:

Answer 17

99

Question 18

Engine Reverse Limitations:

Answer 18

Maximum Reverse HP: 900 HP
Torque: 34.25 PSI
ITT: 760 Celsius
Np (Propeller Speed): 1650 RPM

Question 19

Red Warning CAS Message PSI:

Answer 19

6.35 PSI

Question 20

Maximum Aircraft Operating Temperature:

Answer 20

50 Celsius

Question 21

Flaps 30 Short Field Takeoff Rotation Speed Vr:

Answer 21

76

Question 22

Brakes require a 45 minute cool down period if:

Answer 22

• Takeoff is rejected at +20 kts of Vr and heavy braking is used.
• Flaps 0 full stop with heavy braking.

Question 23

Total Fuel Capacity:

Answer 23

406.8 Gallons

Question 24

Flaps 15 Normal T/O Rotation Speed Vr:

Answer 24

82

Question 25

Total Unusable Fuel:

Answer 25

4.8 Gallons

Question 26

Engine Cruise Limitations:

Answer 26

Maximum Continuous Cruise HP: 1000 HP
Torque: 36.9 PSI
ITT: 820 Celsius 
Ng (Gas Generator Speed): 104%
Np (Propeller Speed): 1700 RPM

Question 27

Flaps 40 Go Around Speed:

Answer 27

85

Question 28

Mmo

Answer 28

0.48

Question 29

Oil Type:

Answer 29

2380 Turbo

Question 30

Up to 850 Celsius:

Answer 30

No Limit

Question 31

Pusher Ice Approach/Landing/Failure/Go Around Speed:

Answer 31

110

Question 32

Voltage at which no Battery or GPU start:

Answer 32

Less than 20 Volts

Question 33

Flaps 15 Extension Speed Vfe:

Answer 33

165

Question 34

Maximum Landing Weight:

Answer 34

9921 lbs

Question 35

Engine Model Number:

Answer 35

PT6A-67P

Question 36

Landing Flaps 0 Speed:

Answer 36

120

Question 37

Landing Flaps 40 Speed:

Answer 37

85

Question 38

Over 1000 Celsius:

Answer 38

Hot Start

Question 39

Boot Failure Approach/Landing/Go Around Speed:

Answer 39

137

Question 40

Flaps 15 Go Around Speed:

Answer 40

98

Question 41

Propeller Governors:

Answer 41

Constant Speed Unit - 1700 RPM
Overspeed Governor - 1802 RPM
Nf Governor - 1853 RPM

Question 42

Maximum Boot Operating Temperature:

Answer 42

40 Celsius

Question 43

Time Limit 850 to 870 Celsius:

Answer 43

20 Seconds

Question 44

Oxygen flows to PAX masks:

Answer 44

13,500 feet

Question 45

Maximum Baggage Weight:

Answer 45

400 lbs

Question 46

Fuel Auto Balancing System;

Maximum Fuel Imbalance at:

Answer 46

3 LCD Segments (26.4 Gallons)

Question 47

Red Warning CAS Message Altitude:

Answer 47

10,500 feet

Question 48

Maximum Zero Fuel Weight:

Answer 48

9039 lbs

Question 49

Engine Transient Limitations:

Answer 49

Torque: 61.0 PSI
ITT: 870 Celsius
Np (Propeller Speed): 1870 RPM

Transient is defined as 20 Seconds

Question 50

Vle

Answer 50

240

Question 51

Minimum Voltage to Start on Battery:

Answer 51

24 Volts

Question 52

Vx

Answer 52

120

Question 53

Pressure Relief Valve opens at PSI:

Answer 53

6.0 - 6.35 PSI

Question 54

Do not move PCL aft of the idle detent unless:

Answer 54

engine is running and the airplane is on the ground.

Question 55

Minimum Voltage in which a GPU may be used:

Answer 55

20 Volts

Question 56

Minimum Aircraft Operating Temperature:

Answer 56

-55 Celsius

Question 57

Holding Pattern in Icing Flaps 0:

Answer 57

145-175

Question 58

Fuel Types Allowed:

Answer 58

Jet A, Jet A-1, Jet B, JP-4

Question 59

Emergency Gear Extension Speed:

Answer 59

110/120

Question 60

Total Usable Fuel:

Answer 60

402 Gallons

Question 61

Time Limit 870 to 1000 Celsius:

Answer 61

5 Seconds

Question 62

Fuel Auto Balancing System;

System Stops Balancing at:

Answer 62

6 LCD Segments (40 Gallons)

Question 63

Best Glide:

Answer 63

116

Question 64

Engine Takeoff Limitations:

Answer 64

Shaft HP: 1200 HP
Torque: 44.34 PSI
ITT: 850 Celsius (first 5 minutes)
Ng (Gas Generator Speed): 104%
Np (Propeller Speed): 1730 RPM

Question 65

Flight into freezing precipitation (FZFG, FZRA, FZBR) is:

Answer 65

Prohibited

Question 66

Fuel Auto Balancing System;

System Activates at:

Answer 66

2 LCD Segments (10.5 Gallons)

Question 67

Engine Climb Limitations:

Answer 67

Max Continuous Climb HP: 1200
Torque: 44.34 PSI
-Plane Sense torque limitations during climb is: 36.9
ITT: 820 Celsius
-Plane Sense ITT limitations during climb is:780 Celsius
Ng (Gas Generator Speed): 104%
Np (Propeller Speed): 1700 RPM

Question 68

Maneuvering Speed Vo:

Answer 68

123-166

Question 69

Vy

Answer 69

130

Question 70

Engine Manufacturer:

Answer 70

Pratt & Whitney

Question 71

Max Cabin Differential PSI:

Answer 71

5.75 PSI