Kodiak 100 Series User Manual

Pilot’s Operating Handbook Supplement
9.4-21
DO NOT USE FOR FLIGHT OPERATIONS
Section 9
TKS ICE PROTECTION
TKS Ice Protection
100 SERIES
ENROUTE CLIMB GRADIENT W/ ICE ACCUMULATION
Conditions:
Power
................................................................................. Maximum Climb
Propeller Speed........................................................................... 2200 RPM
Flaps
..........................................................................................................0°
Engine Inlet
....................................................................................BYPASS
Airspeed
........................................................................................ 115 KIAS
Weight
(LB)
Press Alt.
(FT)
CLIMB GRADIENT
(Feet Per Nautical Mile)
-40 °C -20 °C 0 °C
7255
S.L. 678 640 581
5000 576 523 380
10000 421 277 106
15000 142 19 —
20000 — — —
25000 — — —
6000
S.L. 912 866 794
5000 787 722 548
10000 597 422 215
15000 258 110 —
20000 — — —
25000 — — —
5000
S.L. 1174 1116 1029
5000 1020 941 730
10000 789 577 327
15000 378 201 —
20000 45 — —
25000 — — —
Table 9.4-2 – Enroute Climb Gradient
NOTES:
• Climb gradients shown are the gain in altitude for the horizontal
distance traveled and is expressed as Feet Per Nautical Mile.
• Do not exceed the placarded maximum climb torque, ITT (765°C), and
Ng
(101.6%) limits or the charted max climb torque from “Section 5” of
this manual.
• Dashed entries represent a negative climb rate.
• Signicantly improved climb performance may be attained using V
Y
when clear of icing conditions and no longer using the ice protection
system.
Uncontrolled if printed

Kodiak 100 Series Specifications

General

Manufacturer	Daher
Engine	Pratt & Whitney Canada PT6A-34
Service Ceiling	25, 000 feet
Seating Capacity	10
Crew	1-2
Range	1, 132 nautical miles
Type	Utility aircraft
Length	34 feet 2 inches
Wingspan	45 feet
Max takeoff weight	7, 255 pounds
Power Output	750 shp
Cabin Width	4 feet 6 inches