Kodiak 100 Series User Manual

Pilot’s Operating Handbook
5-60
DO NOT USE FOR FLIGHT OPERATIONS
Section 5
PERFORMANCE
100 SERIES
Performance
5-20 RANGE AND ENDURANCE PROFILES
Conditions:
Weight
..................................................................................... 7255 pounds
Propeller
...................................................................................... 2000 RPM
Temperature
............................................................................................ISA
Winds
....................................................................................................Zero
Total Fuel
........................................................................................ 320 GAL
Air Conditioning
....................................................................................... Off
Engine Inlet
.......................................................................................Normal
External Cargo Compartment................................................... Not Installed
Example:
Power
................................................................................ Maximum Cruise
Takeoff Press Alt
............................................................................ 2000 feet
Cruise Press Alt
........................................................................... 10000 feet
Fuel to Climb: 49 pounds
Cruise Fuel Flow: 336 LB/HR
Endurance: 5.5 hours
Range: 946 NM
True Airspeed: 172 KTAS
NOTES:
• Fuel Remaining for Cruise is equal to 2110 pounds usable, less fuel
required for climb from sea level at maximum climb power, less 153
pounds for 45 minutes IFR reserve fuel at Maximum Range Power
(ISA @10,000 ft PA), less fuel for descent to sea level, less 50 pounds
for fuel used prior to takeoff.
• Range and endurance values include descent to nal destination
at approximately 140 KIAS above 16,000 feet and 160 KIAS below
16,000 feet.
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