Kodiak 100 Series User Manual

Pilot’s Operating Handbook
6-13
DO NOT USE FOR FLIGHT OPERATIONS
Section 6
WEIGHT AND BALANCE
100 SERIES
Weight & Bal.
STANDARD SEATING POSITIONING (CONFIGURATION A)
Registration No.: Date:
Serial No.: Initials:
Description
WEIGHT (LB) ARM (IN) MOMENT / 1000
1.
BASIC EMPTY WEIGHT:
Includes full oil and unusable fuel. Use data pertaining to
your airplane as it is presently equipped.
–
2.
FUEL LOADING: (FS 83.4)
315 Gallons Usable @ 6.7lb/gal (Max Capacity)
83.4
3
TKS FLUID
16.3 Gallons Capacity @ 9.2 lb/gal
48.4
3. Seats, Occupants, and Cargo Loading
ROW 1 AND ZONE 1 (CREW):
WEIGHT (LB) ARM (IN) MOMENT / 1000
Installed Crew Seats, (see seat weights) (FS 41.0)
41.0
Occupants Actual Weight (FS 35.0)
35.0
Zone 1 Cargo, Baggage, or Equipment (FS 40.0)
40.0
External Cargo Compartment Bay 1 (FS 26.0)
26.0
ROW 2 AND ZONE 2 (PASSENGER):
WEIGHT (LB) ARM (IN) MOMENT / 1000
Installed Passenger Seats, (see seat weights) (FS 79.3)
79.3
Occupants Actual Weight (FS 73.2)
73.2
Zone 2 Cargo, Baggage, or Equipment (FS 71.0)
71.0
External Cargo Compartment Bay 2 (FS 75.3)
75.3
ROW 3 AND ZONE 3 (PASSENGER):
WEIGHT (LB) ARM (IN) MOMENT / 1000
Installed Passenger Seats, (see seat weights) (FS 110.3)
110.3
Occupants Actual Weight (FS 104.2)
104.2
Zone 3 Cargo, Baggage, or Equipment (FS 102.0)
102.0
External Cargo Compartment Bay 3 (FS 110.8)
110.8
ROW 4 AND ZONE 4 (PASSENGER):
WEIGHT (LB) ARM (IN) MOMENT / 1000
Installed Passenger Seats, (see seat weights)(FS 141.3)
141.3
Occupants Actual Weight (FS 135.2)
135.2
Zone 4 Cargo, Baggage, or Equipment (FS 133.0)
133.0
ROW 5 AND ZONE 5 (PASSENGER):
WEIGHT (LB) ARM (IN) MOMENT / 1000
Installed Passenger Seats, (see seat weights) (FS 172.3)
172.3
Occupants Actual Weight (FS 166.2)
166.2
Zone 5 Cargo, Baggage, or Equipment (FS 164.0)
164.0
ZONE 6 (CARGO): MAXIMUM 200 LB
Zone 6 Cargo, Baggage, or Equipment (FS 195.0)
195.0
4.
TOTAL RAMP WEIGHT AND MOMENT:
Add items 1 through 3
–
5.
STARTING, TAXI, AND RUN-UP FUEL:
Normally 50 LB (moment of 4170)
83.4
6.
TAKEOFF WEIGHT AND MOMENT:
Subtract item 5 from item 4
–
Table 6-5 – Weight and Balance Loading Form (Conguration A)
NOTE: The basic weight of the aircraft is as dened by the “Installed
Equipment List” (AM905.0). If a seat is removed from the aircraft that was
installed in the basic conguration, subtract the weight of the seat using the
form below.
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