Kodiak 100 Series User Manual

Pilot’s Operating Handbook
4-12
DO NOT USE FOR FLIGHT OPERATIONS
Section 4
NORMAL PROCEDURES
100 SERIES
Procedures
TAKEOFF
Normal Takeoff
1. Wing Flaps ............................................................................................ 0°-20°
2. Elevator Trim...........................................................RECHECK set for takeoff
3. Power ........... SET FOR TAKEOFF (observe takeoff torque, ITT, and
Ng
limits)
4. Annunciators .......................................................................................CHECK
5. Engine Instruments
.............................................................................CHECK
6. Rotate
...........................................................................................60-65 KIAS
7. Climb Speed
.................................................................................85-95 KIAS
8. Wing Flaps
.......................................................... RETRACT at a safe altitude
(Retract to 10° after reaching 85 KIAS and 0° after reaching 95 KIAS.)
Short Field Takeoff
1. Wing Flaps .................................................................................................20°
2. Elevator Trim.............................................................................Set for takeoff
3. Power ........... SET FOR TAKEOFF (observe takeoff torque, ITT, and
Ng
limits)
4. Annunciations .....................................................................................CHECK
5. Engine Instruments
.............................................................................CHECK
6. Brakes.............................................................................................RELEASE
7. Rotate
................................................................................................60 KIAS
8. Climb Speed
................................................. 73 KIAS until clear of obstacles
9. Wing Flaps
.......................................................... RETRACT at a safe altitude
(Retract to 10° after reaching 85 KIAS and 0° after reaching 95 KIAS.)
CAUTION: The Flap/Trim Compensation Unit is disabled on the ground
through an airspeed switch. The airspeed switch activates the Flap/
Trim Compensation Unit above approximately 35 knots. If the airplane is
positioned into winds in excess of approximately 35 knots while the aps
are being set for takeoff, the trim will move from its previously set position
and could result in an out-of-trim condition on takeoff.
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