Kodiak 100 Series User Manual

Pilot’s Operating Handbook
6-10
DO NOT USE FOR FLIGHT OPERATIONS
Section 6
WEIGHT AND BALANCE
100 SERIES
Weight & Bal.
PASSENGER AND CREW SEAT WEIGHT AND BALANCE
The KODIAK is equipped with removable passenger and crew seats. A
maintenance log book entry is not required when the seats are removed or
installed, but the aircraft weight and balance must be calculated to reect the
seat conguration for each ight.
Refer to the KODIAK 100 Installed Equipment List (AM905.0) for the current
aircraft conguration weight and balance record. For weight and balance
calculations regarding the removal or installation of seats, refer to the
following congurations.
Standard Seating Positioning - (Conguration A)
Seat
Row
Ref. Point (FS), IN.
Empty Seat CG
(IN.)
Occupant CG
(IN.)
1
40.0
(Crew Seat Rear Stop located at FS 50.0)
41.0 35.0
2 84.0 79.3 73.2
3 115.0 110.3 104.2
4 146.0 141.3 135.2
5 177.0 172.3 166.2
Table 6-3 – Weight and Balance Calculations (Conguration A)
Standard Seating Positioning - (Conguration B)
Seat
Row
Ref. Point (FS), IN.
Empty Seat CG
(IN.)
Occupant CG
(IN.)
1
40.0
(Crew Seat Rear Stop located at FS 44.0)
41.0 35.0
2 78.0 73.3 67.2
3 109.0 104.3 98.2
4 140.0 135.3 129.2
5 171.0 166.3 160.2
Table 6-4 – Weight and Balance Calculations (Conguration B)
NOTE: Seats may only be installed within the limitations given in this
section. Crew seat rear stops must be installed in the location dened
by the congurations below. Failure to install the seat stop in the dened
location could result in seat positioning that does not meet the minimum
seat pitch requirements.
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