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Kodiak 100 Series User Manual

Kodiak 100 Series
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Pilot’s Operating Handbook
1-13
DO NOT USE FOR FLIGHT OPERATIONS
Section 1
GENERAL
100 SERIES
General
MAC - Mean Aerodynamic Chord of a wing is the chord of an imaginary
airfoil which will have the same force vectors as those of the actual wing,
throughout the ight range.
Maximum Landing Weight The maximum weight approved for the landing
touchdown.
Maximum Ramp WeightThe maximum weight approved for ground
operations. This includes the weight of fuel used for starting, taxi, and
runup.
Maximum Takeoff Weight – The maximum weight approved for the start of
takeoff roll.
Moment The product of the weight of an item multiplied by its arm. (The
actual moment divided by a constant of 1000 is used to simplify balance
calculations by reducing the number of digits.)
MZFW - Maximum Zero Fuel WeightThe maximum allowable weight of
the airplane and all its contents, minus the total weight of the fuel on board.
Ramp Condition – The weight and moment of the aircraft prior to taxi.
Reference Datum An imaginary vertical plane from which all horizontal
distances are measured for weight and balance purposes.
Residual FuelAnother name for undrainable fuel or the fuel remaining
when the airplane is de-fueled. Residual fuel is considered to be a part of
the empty weight of the aircraft.
Standard Empty Weight The weight of a standard airplane including any
residual fuel, full operating uids and full engine oil.
StationA location along the airplane fuselage usually expressed in terms of
distance from the reference datum.
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