Kodiak 100 Series User Manual

Pilot’s Operating Handbook Supplement
9.6-9
DO NOT USE FOR FLIGHT OPERATIONS
Section 9
EXTERNAL CARGO COMPARTMENT
ECC
100 SERIES
9.6-5 PERFORMANCE
MAXIMUM TAKEOFF WEIGHTS WITH ECC
(Refer to the table below)
Conditions:
• Maximum Takeoff Power
• Flaps 20°
Altitude
Climb Speed – V
y
(KIAS)
S.L. 87
2000 87
4000 86
6000 85
8000 83
10000 82
12000 81
NOTES:
• These weights assure the availability of a steady gradient of climb of at
least 243 FT/NM with the aps at 20°.
• Dashed entries correspond to outside air temperatures beyond the aircraft
operating limits.
• Yellow shaded areas correspond to weight limits below the maximum
takeoff weight.
NOTE: For temperatures below 3°C and altitudes below 5000 ft, the
takeoff weight limit is 7,255 lb.
NOTE: Blue numbers indicate performance with Air Conditioning
ON, black numbers indicate performance with Air Conditioning OFF.
OAT
(°C)
OAT
(°F)
PRESSURE ALTITUDE (FEET)
5000 6000 7000 8000 9000 10000 11000 12000
3 37 7255 7255 7255 7255 7255 7255 7255
7255
7205
5 41 7255 7255 7255 7255 7255 7255 7255
7255
7099
7 45 7255 7255 7255 7255 7255 7255 7255
7255
6990
9 48 7255 7255 7255 7255 7255 7255
7255 7204
7235 6880
11 52 7255 7255 7255 7255 7255 7255
7255 7093
7119 6765
Table 9.6-1 – Maximum Takeoff Weight with External Cargo Compartment
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