P I L O T ’ S O P E R A T I N G H A
N D B O O K
V I P E R J E T M K I I
Revision 1
6-3
June 1, 2008
Scale Position
Scale
Reading
Tare
Symbol
Net Weight
Left Wheel
L
Right Wheel
R
Nose Wheel
N
Sum of Net Weights (As Weighed)
W
X = CG ARM = (A)
–
(N) x (B);
X = ( )
–
( ) x ( ) = ( ) IN.
W
( )
ITEM
Weight (Lbs.) X CG Arm (In.) =
Moment/1000
(Lbs.-In.)
Aircraft Weight (From Item 5 Page 6-2)
Equipment Changes
Aircraft Basic Empty Weight
Figure 6-2. Sample Aircraft Weighing
WEIGHT AND BALANCE
The following information will enable you to operate your ViperJet Mk II within the
prescribed weight and center of gravity limitations. To figure weight and balance, use the
Sample Loading Problem and Center of Gravity Moment Envelope Table as follows:
CG Range:
15% to 25% MAC (Mean Aerodynamic Chord), or Fuselage
Station (as measured aft of the Datum) 158.0 inches to
162.5 inches.
Maximum Gross Weight:
5500 Lbs.
Pilot Station:
82.0 In.
Co-Pilot Station:
129.5 In.
Baggage Station:
142.0 In.
Center Fuel Tank:
160.0 In.
Wing Fuel Tank:
164.5 In.
Summary of Contents for ViperJet MkII
Page 1: ...MK II PILOT S OPERATING HANDBOOK...
Page 3: ...THIS PAGE INTENTIONALLY LEFT BLANK...
Page 5: ......
