Kodiak 100 Series User Manual

Pilot’s Operating Handbook
2-11
DO NOT USE FOR FLIGHT OPERATIONS
Section 2
LIMITATIONS
100 SERIES
Limitations
2-8 CENTER OF GRAVITY LIMITS
CENTER OF GRAVITY RANGE
Forward C.G. Limit at 7,255 lb .............................71.04 inches aft of datum
(Linear variation from 5,000 lb to 7,255 lb)..........................(25.00% MAC)
Forward C.G. Limit at 5,000 lb or less
.................. 63.90 inches aft of datum
(14.00% MAC)
Aft Limit, up to 7,255 lb.........................................80.78 inches aft of datum
(40.00% MAC)
Reference Datum
..................................................... forward face of rewall
MEAN AERODYNAMIC CHORD (MAC)
Leading Edge MAC ..............................................54.81 inches aft of datum
MAC Length
.............................................................................64.92 inches
Figure 2-2 – KODIAK Loading Envelope
NOTE: Any weight above the maximum zero fuel weight of 6490 lb must
be in the form of fuel.
Maximum Zero Fuel Weight (MZFW)
3500
4000
4500
5000
5500
6000
6500
7000
7500
12% 16% 20% 24% 28% 32% 36% 40%
WEIGHT (lb)
C.G. LOCATION (% MAC)
KODIAK LOADING ENVELOPE
MZFW 6490
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