-
60
-40
-20
0
20
40
60
20
25
30
35
40
45
E
N
G
IN
E
T
O
R
Q
U
E
~
P
S
I
EXAMP LE:
PRESS URE ALTITUDE 8000 FT
OUTS IDE AIR TEMPERATURE 26 C
STATIC TAKEOFF TORQUE 38.7 P S I
1
4000
1
2000
S TATIC TAKEOFF TORQUE
ACS INHIBIT
I
S
A
~
C
OUTS IDE AIR TEMP ERATURE (ENGINE T1) ~ C
0
4
000
0
+
20
+
30
P ROP ELLER S PEED: 1700 RPM
ICE PROTECTION:
P ROBES ON / WINDS HIELD ON
INERTIAL SEPERATOR OPERATION:
HAS NO EFFECT ON TORQUE
DE-ICE / ANTI-ICE S YS TEMS:
CAN REDUCE TORQUE BY 0.5 P S I
P
R
E
S
S
U
R
E
A
LT
IT
U
D
E
~
F
T
6
000
8
000
M
A
X
O
A
T
L
IM
IT
M
IN
O
A
T
L
IM
IT
1
0000
2
000
+
40
+
10
ICN-12-C-A150503-A-S4080-00248-A-001-01
Figure 5-3-2-2: Performance - Static Takeoff Torque - ACS OFF
Section 5 - Performance (EASA Approved)
Performance Data - Takeoff Performance
Pilot's Operating Handbook
Report No: 02406
Issue date: Mar 06, 2020
Page 5-3-2-2
12-C-A15-60-0503-02A-030A-A
FOR
GENERAL
AND
FAMILIARIZATION
PURPOSES
ONLY
