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Kodiak 100 Series User Manual

Kodiak 100 Series
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Pilot’s Operating Handbook
7-53
DO NOT USE FOR FLIGHT OPERATIONS
Section 7
AIRPLANE & SYSTEMS DESCRIPTIONS
100 SERIES
Systems
7-8 WING FLAPS
The electrically controlled, slotted fowler aps enhance the low speed lift
characteristics of the airplane. Each ap is connected to the wing structure at
three ap track assemblies. Each ap track assembly contains two grooves in
which the ap rollers operate. The aps may be positioned at 0°, 10°, 20° and
35° by selecting the desired position on the ap control switch. As the ap
position switch is placed in a given position, sensors in the ap power system
provide input to the ap motor and gearbox; the ap motor and gearbox drives
exible shafts which actuate worm gear assemblies and position the aps
as selected in the cockpit. One asymmetry sensor is installed per each ap
assembly to ensure ap symmetry. If a malfunction occurs within the ap or
between the two aps, the asymmetry sensors will immediately discontinue
ap movement. Flap position indication is provided on the multifunction
display.
7-9 LANDING GEAR SYSTEM
The landing gear is a tricycle type with a steerable nose wheel and two main
wheels. Shock absorption is provided through the tubular spring steel main
landing gear struts with two interconnecting steel cross tubes and the air
and oil-lled nose gear shock strut. The landing gear system is designed
for operations from unimproved runways. To improve the operation from
unimproved runways, the optional oversize tires may be installed. This option
provides greater propeller ground clearance and a wider footprint for better
performance on soft surfaces.
7-10 BAGGAGE/CARGO COMPARTMENT
In the passenger version, the space normally used for carrying baggage is
the raised area aft of the cargo door to the aft cabin bulkhead. Access to
the baggage area is gained through the cargo door or from within the cabin.
Quick-release cargo tie-down straps and a cargo net are provided for securing
baggage and are attached to the compartment oor anchor points. Refer to
“Section 6” of this manual for loading limits and “Section 1” of this manual for
dimensions.
WARNING: Any material that could possibly be hazardous to the airplane
or its occupants should not be placed anywhere in the airplane.
Uncontrolled if printed

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Kodiak 100 Series Specifications

General IconGeneral
ManufacturerDaher
EnginePratt & Whitney Canada PT6A-34
Service Ceiling25, 000 feet
Seating Capacity10
Crew1-2
Range1, 132 nautical miles
TypeUtility aircraft
Length34 feet 2 inches
Wingspan45 feet
Max takeoff weight7, 255 pounds
Power Output750 shp
Cabin Width4 feet 6 inches