Kodiak 100 Series User Manual

Pilot’s Operating Handbook
5-67
DO NOT USE FOR FLIGHT OPERATIONS
Section 5
PERFORMANCE
100 SERIES
Performance
5-23 OBSTACLE LANDING DISTANCE
(Max Weight 6690 LB Short Field)
(Refer to the tables on the following pages)
Conditions:
Winds
....................................................................................................Zero
Runway
............................................................................Dry, Level, Paved
Flaps
........................................................................................... 35° (FULL)
• Power for 3° descent to 50 foot obstacle, then gradual reduction to
IDLE at touchdown. BETA range (lever against spring) after touchdown.
Example:
Outside Air Temp
.................................................................................. 20°C
Weight
..................................................................................... 6690 pounds
Pressure Altitude
........................................................................... 2000 feet
Headwind
..............................................................................................Zero
Obstacle Speed (V
ref
): 74 KIAS
Landing Ground Roll: 760 FT
Total Distance Over 50' Obstacle: 1551
NOTES:
• Short eld technique utilized as outlined in “Section 4” of this manual.
• Decrease distances 10% for each 14 knots headwind.
• For operation in tailwinds up to 10 knots, increase distances 10% for
each 2 knots.
• For operation on a hard, dry, grass runway, increase distances by
20% of the ground roll calculation.
• To land with the aps up, increase approach speed by 22 KIAS and
allow for approximately 55% longer distances.
• Use of maximum reverse thrust after touchdown will reduce ground
roll by approximately 5%.
• For sloped runways (up to 3% slope), increase the distances by 27%
of the ground roll distance for each 1% of downslope. Decrease
distances by 9% of the ground roll distance for each 1% of upslope.
• For operation in air colder than this table provides, use the coldest
data for landing distances.
• Dashed entries indicate atmospheric temperatures beyond the aircraft
operating limits.
NOTE: Red shaded areas represent data at temperatures greater than
the maximum approved operating OAT, but may be used for the purpose of
interpolating.
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