2 MAIN DIMENSIONS
2.1 LANDPLANE
Span .......................................................................................................... 422.5 in.
Length (level flight attitude) .......................................................................... 271 in.
Length (three point attitude) ......................................................................... 275 in.
Height ........................................................................................................ 119.0 in.
Height (tail wheel on ground, propeller blade vertical at top)* ................... 95.75 in.
Propeller Ground Clearance* ........................................................................ 10 in.
Design Gross Weight ................................................................................ 2300 lbs
*With Sensenich Metal propeller model 76EM8 propeller and 8.50x6 wheels
2.2
WIPAIRE 2100A AMPHIBIOUS FLOATS
Length (ground attitude) ............................................................................... 287 in.
Height ........................................................................................................ 126.5 in.
Design Gross Weight ................................................................................ 2300 lbs
2.3 WIPAIRE 2100S SEAPLANE FLOATS
Design Gross Weight ................................................................................ 2300 lbs
3 WINGS
Type ......................................................................... Externally Braced, High Wing
Airfoil Section .......................................................... USA 35B Mod at Root and Tip
Chord at Root ................................................................................................. 63 in.
Dihedral (measured on underside of front spar) ....................................... 0º 45 min
Area ....................................................................................................... 178.5 sq ft
Aspect Ratio ................................................................................................... 6.944
4 AILERONS
Area (Both ailerons) ............................................................................... 18.80 sq ft
5 FLAPS
Area (Both flaps) ................................................................................... 11.50 sq ft.
6 STABILIZER
Span ............................................................................................................. 105 in.
Maximum Chord ............................................................................................. 27 in.
Incidence (in neutral position).......................................................................... -2.5
Dihedral ................................................................................................................ 0º
Area (including elevators) ...................................................................... 15.90 sq ft.
06-00
Page: 6
CUB CRAFTERS, INC.
CC18-180 MAINTENANCE MANUAL
Manual number TC10000AMM
Date: 11/20/12