Kodiak 100 Series User Manual

Pilot’s Operating Handbook
2-35
DO NOT USE FOR FLIGHT OPERATIONS
Section 2
LIMITATIONS
100 SERIES
Limitations
52. Located on the wings, adjacent to each inboard fuel tank ller cap:
53. Located on the wings, adjacent to each outboard fuel tank ller cap:
54. Located on top of the wings, near each grounding clip:
55. Located on the lower portion of each wing just outboard of the pitot tube:
MAGNETOMETER –
USE NON-MAGNETIC
TOOLS AND SCREWS.
100-910-0061
FUEL NOZZLE
ELECTRIC GROUNDING
CLIP
TOTAL INBOARD CAPACITY:
96.5 US GALLONS (365.3 L)
ANTI-ICE ADDITIVE IS REQUIRED. REFER TO THE AFM/POH
FOR EXCEPTIONS, AND FOR OTHER APPROVED FUELS,
QUANTITIES, AND ADDITIVES.
GROUND FUELING EQUIPMENT TO AIRFRAME, AND
FUEL NOZZLE TO FUEL NOZZLE GROUNDING CLIP.
CAUTION!
DO NOT OPEN WHEN WING FUEL QUANTITY EXCEEDS
96.5 US GALLONS (365.3 LITERS) OR 640 LB
100-910-0113
JET FUEL
ONLY
TOTAL OUTBOARD CAPACITY:
160 US GALLONS
(
605.6 LITERS)
ANTI-ICE ADDITIVE IS REQUIRED. REFER TO THE
AFM/POH FOR EXCEPTIONS, AND FOR OTHER
APPROVED FUELS, QUANTITIES, AND ADDITIVES.
GROUND FUELING EQUIPMENT TO AIRFRAME, AND
FUEL NOZZLE TO FUEL NOZZLE GROUNDING CLIP.
100-910-0112
JET FUEL
ONLY
NOTE: For airplanes equipped with alternate placard part numbers
100-910-0063 and 100-910-0087, anti-ice additive is ALWAYS required,
with NO exceptions.
NOTE: For airplanes equipped with alternate placard part numbers
100-910-0062 and 100-910-0086, anti-ice additive is ALWAYS required,
with NO exceptions.
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