ENROUTE RATE OF CLIMB WITH ICE ACCUMULATION
Conditions:
Power
................................................................................. Maximum Climb
Propeller Speed........................................................................... 2200 RPM
Flaps
..........................................................................................................0°
Engine Inlet
....................................................................................BYPASS
Airspeed
........................................................................................ 115 KIAS
Weight
(LB)
Press Alt.
(FT)
Enroute Rate of Climb
(Feet Per Minute)
-40°C -20°C 0°C
7255
S.L. 1162 1143 1080
5000 1084 1025 766
10000 872 599 238
15000 325 46 —
20000 — — —
25000 — — —
6000
S.L. 1556 1540 1469
5000 1476 1412 1117
10000 1235 913 483
15000 591 263 —
20000 — — —
25000 — — —
5000
S.L. 1987 1972 1892
5000 1902 1830 1482
10000 1626 1245 735
15000 867 479 —
20000 116 — —
25000 — — —
Table 9.4-3 – Enroute Rate of Climb
NOTES:
• Rate of climb shown is the gain in altitude in feet per unit time and is
expressed as Feet Per Minute.
• Do not exceed the placarded maximum climb torque, ITT (765°C), and
N
(101.6%) limits or the charted max climb torque from “Section 5” of
this manual.
• Dashed entries represent a negative climb rate.
• Signicantly improved climb performance may be attained using V
Y
when clear of icing conditions and no longer using the ice protection
system.