Kodiak 100 Series User Manual

Pilot’s Operating Handbook Supplement
9.8-24
DO NOT USE FOR FLIGHT OPERATIONS
Section 9
OVERSIZED TIRES
100 SERIES
Oversized Tires
9.108 -7 AIRPLANE & SYSTEMS DESCRIPTION
FUEL (LB) ENTRY SECTION
Estimated Landing Weight (Calculation Field) - When the aircraft is in the
air and a destination way point has been entered, the fuel calculations
can be completed. Landing weight is automatically calculated based on
the following information: [ Estimated landing weight = zero fuel weight
+ estimated landing fuel]. If the estimated landing weight is greater than
6,690 pounds, the estimated landing weight will be displayed in amber.
Landing weights up to 7,255 pounds are acceptable if accomplished in
accordance with the limitations of this supplement.
9.108 - 8 HANDLING, SERVICE & MAINTENANCE
No change.
NOTE: If the aircraft is on the ground or a destination way point has not
been entered, the estimated landing weight eld displays invalid values
consisting of six dashes.
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