Kodiak 100 Series User Manual

Pilot’s Operating Handbook
5-18
DO NOT USE FOR FLIGHT OPERATIONS
Section 5
PERFORMANCE
100 SERIES
Performance
5-10 MAXIMUM TAKEOFF WEIGHTS
(Refer to the table on the following page)
Conditions:
• Maximum Takeoff Power
• Flaps 20°
Altitude
Climb Speed – Vy
(KIAS)
S.L. 88
2000 88
4000 87
6000 86
8000 84
10000 83
12000 82
NOTES:
• These weights assure the availability of a steady gradient of climb of at
least 243 FT/NM with the aps at 20°.
• Dashed entries correspond to outside air temperatures beyond the aircraft
operating limits.
• Yellow shaded areas correspond to weight limits below the maximum
takeoff weight.
NOTE: For temperatures below 9°C and altitudes below 6000 ft, the
takeoff weight limit is 7,255 lb.
NOTE: Blue numbers indicate performance with Air Conditioning
ON, black numbers indicate performance with Air Conditioning OFF.
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