SECTION 9.1
CUB CRAFTERS
SUPPLEMENT-FLOATS CC11-100
REPORT SC10000AFM
Issued: 04/15/09
Page Number: 9-1-20
Date of Revision: 04/09/13
9.1.6.4.21
Stopping Engine
Flaps ................................................................. Retract
Electrical Equipment ................................................. Off
Avionics Master Switch ............................................. Off
Throttle .................................................................... Idle
Mixture ......................................................... Idle cut off
Magnetos/Ignition ..................................................... Off
Master Switch ........................................................... Off
9.1.7 WEIGHT AND BALANCE
9.1.7.1 INTRODUCTION
This section provides the position of the center of gravity
relative to the datum. It also describes how to calculate
the empty weight of the aircraft based on data for the
landplane. Should it be necessary to weigh the aircraft on
floats, please consult the maintenance manual.
9.1.7.2 PERTINENT INFORMATION FOR WEIGHT
AND BALANCE OF THE CC11-100 AIRCRAFT
EQUIPPED WITH FLOATS
Position of Datum ...................................... 60 inches ahead
of wing leading edge
Maximum Gross Weight ......................................... 1430 lb.
Center of Gravity Limits at 1430 lb.
Forward ................................................73.0 in. aft of datum
Aft ........................................................78.5 in. aft of datum
Center of Gravity Limits at 1100 lb. or less
Forward ................................................70.5 in. aft of datum
Aft ....................................................... 78.5 in. aft of datum
