PC-12/47E Limitations Flashcards
1
Q
Engine
A
Pratt and Whitney PT6A-67P
2
Q
Engine Type
A
twin shaft turboprop engine with 4 axial and 1 centrifugal compressor stages, annular combustion chamber, 3 stage turbine with one Ng and 2 Np.
3
Q
Thermodynamic HP
A
1605
4
Q
Shaft HP/takeoff power
A
1200
5
Q
Max Ng
A
38967rpm @ 104%
6
Q
Max Np
A
1700rpm
7
Q
Takeoff torque
A
44.34psi
8
Q
Takeoff ITT
A
850C
9
Q
Climb Torque
A
36.9psi
10
Q
Climb ITT
A
780C
11
Q
Transient Torque
A
61.0psi
12
Q
Transient ITT
A
870C
13
Q
Reverse Torque
A
34.25psi
14
Q
Reverse ITT
A
760C
15
Q
Min Battery before start
A
24V
16
Q
Max ITT before start
A
150C
17
Q
Starting ITT up to 850C
A
no time limit
18
Q
Starting ITT 850C to 870C
A
20 seconds
19
Q
Starting ITT 870C to 1000C
A
5 seconds
20
Q
Above 1000C on start
A
HOT START
21
Q
Propeller Manufacture
A
Hartzell
22
Q
Number of blades
A
4
23
Q
Propeller diameter
A
105”
24
Q
Propeller max normal Np
A
1700rpm
25
Q
Overspeed govener
A
1802rpm
26
Q
Nf govener
A
1853rpm
