PC-12/47E Limitations

Question 1

Engine

Answer 1

Pratt and Whitney PT6A-67P

Question 2

Engine Type

Answer 2

twin shaft turboprop engine with 4 axial and 1 centrifugal compressor stages, annular combustion chamber, 3 stage turbine with one Ng and 2 Np.

Question 3

Thermodynamic HP

Answer 3

1605

Question 4

Shaft HP/takeoff power

Answer 4

1200

Question 5

Max Ng

Answer 5

38967rpm @ 104%

Question 6

Max Np

Answer 6

1700rpm

Question 7

Takeoff torque

Answer 7

44.34psi

Question 8

Takeoff ITT

Answer 8

850C

Question 9

Climb Torque

Answer 9

36.9psi

Question 10

Climb ITT

Answer 10

780C

Question 11

Transient Torque

Answer 11

61.0psi

Question 12

Transient ITT

Answer 12

870C

Question 13

Reverse Torque

Answer 13

34.25psi

Question 14

Reverse ITT

Answer 14

760C

Question 15

Min Battery before start

Answer 15

24V

Question 16

Max ITT before start

Answer 16

150C

Question 17

Starting ITT up to 850C

Answer 17

no time limit

Question 18

Starting ITT 850C to 870C

Answer 18

20 seconds

Question 19

Starting ITT 870C to 1000C

Answer 19

5 seconds

Question 20

Above 1000C on start

Answer 20

HOT START

Question 21

Propeller Manufacture

Answer 21

Hartzell

Question 22

Number of blades

Answer 22

4

Question 23

Propeller diameter

Answer 23

105”

Question 24

Propeller max normal Np

Answer 24

1700rpm

Question 25

Overspeed govener

Answer 25

1802rpm

Question 26

Nf govener

Answer 26

1853rpm

Question 27

Max transient Np

Answer 27

1870rpm

Question 28

Max reverse Np

Answer 28

1650rpm

Question 29

Ground operation not permitted Np

Answer 29

350-950rpm

Question 30

Fuel Types

Answer 30

Jet A, Jet A-1, Jet B, JP-4 all with Prist

Question 31

Total Fuel (gal/lbs)

Answer 31

406.8 US gal / 2736.5lbs

Question 32

Usuable Fuel (gal/lbs)

Answer 32

402 US gal / 2703.6lbs

Question 33

Max fuel Imbalance

Answer 33

26.4 US gal / 178lbs

Question 34

Oil Capacity

Answer 34

3.6 US gal

Question 35

Max Ramp Weight

Answer 35

10495 lbs

Question 36

Max Takeoff Weight

Answer 36

10450 lbs

Question 37

Max Landing Weight

Answer 37

9921 lbs

Question 38

Max Zero Fuel Weight

Answer 38

9039 lbs

Question 39

Max Baggage

Answer 39

400 lbs

Question 40

Cabin Area Max

Answer 40

3300 lbs

Question 41

Vr 15 flaps

Answer 41

82

Question 42

Vr 30 flaps (short field)

Answer 42

76

Question 43

Vx

Answer 43

120

Question 44

Vy 0 flaps

Answer 44

130

Question 45

Vy 15 flaps

Answer 45

95

Question 46

Vy 30 flaps

Answer 46

85

Question 47

10000 climb speed

Answer 47

180

Question 48

20000 climb speed

Answer 48

140

Question 49

30000 climb speed

Answer 49

120

Question 50

Pusher ice climb 0 flaps

Answer 50

140

Question 51

Vmo

Answer 51

240

Question 52

Vfe flaps 15

Answer 52

165

Question 53

Vfe flaps 30/40

Answer 53

130

Question 54

Vlo

Answer 54

180

Question 55

Vle

Answer 55

240

Question 56

emergency gear extension (hydrolic/electric)

Answer 56

110/120

Question 57

Approach Speed flaps 0

Answer 57

120

Question 58

Approach Speed flaps 15

Answer 58

99

Question 59

Approach Speed flaps 30

Answer 59

89

Question 60

Approach Speed flaps 40

Answer 60

85

Question 61

Pusher ice approach speed, 15 flaps

Answer 61

110

Question 62

go around speed 15 flaps

Answer 62

98

Question 63

go around speed 30 flaps

Answer 63

89

Question 64

go around speed 40 flaps

Answer 64

86

Question 65

Max demonstrated Crosswind (contaminated)

Answer 65

30,25,20,15 (50% reduction)

Question 66

Max tailwind landing

Answer 66

10

Question 67

Max tailwind LAHSO

Answer 67

3