SECTION 9.2
SUPPLEMENT- SINGLE PLACE CONVERSION
Use the table below to determine the weight and loading
for a single seat aircraft. Note that in the example below,
the rear seat is shown as completely removed. If the
seat is stowed and not removed, remove this from your
calculations. If any changes are made for main gear or
tailwheel, the main gear arm is 62.5 inches and the
tailwheel arm is 261.9 inches.
Aircraft Empty
Fuel
Pilot
Passenger Seat Removal
Rear Stick Removal
Rear Stick Stub Cover
Forward Cargo Compartment (100
lb max)
Cargo Shelf Compartment
(20 lb max)
Table 9-2-3 - Weight & Balance Loading Form
REPORT SC10000AFM
Page Number: 9-2-6
Item
TOTAL
CG Station:
CUB CRAFTERS
Weight
Moment
(lbs)
Arm (in)
83.90
71.40
-6.15
96.08
-0.20
84.08
0.69
84.08
110.40
134.40
Issued: 04/15/09
Date of Revision: 10/31/11
CC11-100
Moment
(in∙lbs)
-590.9
-16.8
58.0