SECTION 9.2
CUB CRAFTERS
SUPPLEMENT- SINGLE PLACE CONVERSION
CC11-100
REPORT SC10000AFM
Issued: 04/15/09
Page Number: 9-2-6
Date of Revision: 10/31/11
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.
Item
Weight
(lbs)
Moment
Arm (in)
Moment
(
in∙lbs)
Aircraft Empty
Fuel
83.90
Pilot
71.40
Passenger Seat Removal
-6.15
96.08
-590.9
Rear Stick Removal
-0.20
84.08
-16.8
Rear Stick Stub Cover
0.69
84.08
58.0
Forward Cargo Compartment (100
lb max)
110.40
Cargo Shelf Compartment
(20 lb max)
134.40
TOTAL
CG Station:
Table 9-2-3 - Weight & Balance Loading Form
