Kodiak 100 Series User Manual

Pilot’s Operating Handbook
5-31
DO NOT USE FOR FLIGHT OPERATIONS
Section 5
PERFORMANCE
100 SERIES
Performance
5-16 TIME, FUEL AND DISTANCE TO CLIMB
Conditions:
Weight
..................................................................................... 7255 pounds
Flaps
..........................................................................................................0°
Power
...................................................................... Maximum Climb Power
Inertial Separator
...............................................................................Normal
Airspeed
.............................................................................................V
climb
Air Conditioning ....................................................................................... Off
Winds
....................................................................................................Zero
Press
Alt
(FT)
ISA
OAT
(°C)
Climb
Speed
(KIAS)
Rate of
Climb
(FPM)
Time, Fuel & Distance – from Sea Level
Time
(MIN)
Fuel
(LB)
Distance
(NM)
SL 15 101 1371 0 0 0
5000 5 101 1141 4.0 26.4 7.0
10000 -5 101 874 9.9 59.6 18.8
15000 -15 101 563 20.9 111.0 42.7
20000 -25 101 238 49.9 229.7 110.9
25000 -35 101 -102 367.6 1470.6 889.1
Table 5-12 – Time, Fuel, and Distance to Climb
NOTES:
• Taxi Fuel: Add 50 pounds of fuel for start, taxi and takeoff.
• Temperature: Add 10% to calculated values for each 10°C above
standard.
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