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Jack Point Locations. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-38
Lateral Moment of Wing Fuel Tanks - U.S. Units . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-39
Lateral Moment of Wing Fuel Tanks - Metric Units . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-40
Airplane Weighing Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-41
Example Airplane Weighing Form - U.S. Units . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-44
Example Airplane Weighing Form - Metric Units . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-45
Oleo Strut Measurement Nose Landing Gear - U.S. Units . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-46
Oleo Strut Measurement Nose Landing Gear - Metric Units. . . . . . . . . . . . . . . . . . . . . . . . . . 6-47
Oleo Strut Measurement Main Landing Gear - U.S. Units . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-48
Oleo Strut Measurement Main Landing Gear - Metric Units . . . . . . . . . . . . . . . . . . . . . . . . . . 6-49
Examples . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-51
General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-51
Sample Loading Problem . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-51
Example Weight and Balance Computation Form - U.S. Units. . . . . . . . . . . . . . . . . . . . . . . . 6-54
Example Weight and Balance Computation Form - Metric Units . . . . . . . . . . . . . . . . . . . . . . 6-55
Example Center-of-Gravity Limits Envelope Graph - U.S. Units. . . . . . . . . . . . . . . . . . . . . . . 6-56
Example Center-of-Gravity Limits Envelope Graph - Metric Units . . . . . . . . . . . . . . . . . . . . . 6-57
6-6 510WB-00
MODEL 510 SECTION VI - WEIGHT AND BALANCE DATA
CONTROL - GENERAL
FAA APPROVED
U.S.
GENERAL
Manual Applicability
This manual is applicable to the Model 510 (Citation Mustang) airplane.
CAUTION
THIS MANUAL PRESENTS DATA IN BOTH U.S. AND METRIC UNITS.
MAKE SURE THAT YOU USE THE APPROPRIATE DATA IN THE WEIGHT
AND BALANCE COMPUTATIONS FOR YOUR AIRPLANE.
Zero Reference Datum Line
The zero reference datum line of the Model 510 is located 143.70 inches (3650 millimeters) in front
of the jig point (nose jack pad location). Horizontal distance from zero datum line to the leading edge
of the Mean Aerodynamic Chord (MAC) is 273.71 inches (6952 millimeters). The addition of any
weight in any location therefore, results in a positive moment change.
Reference Lines Control Drawings
Cabin Lines Control Drawing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7011510
Tailcone Lines Control Drawing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7012510
Nose Lines Control Drawing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7013510
Wing Lines Control Drawing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7020510
Vertical Fin and Rudder Lines Control Drawing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7031510
Horizontal Stabilizer and Elevator Lines Control Drawing. . . . . . . . . . . . . . . . . . . . . . . . . . . . 7032510
Main Landing Gear Points Control Drawing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7041510
Nose Landing Gear Points Control Drawing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7042510
Wing - Fuselage Fairing Master Geometric Drawing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . x7010000
Engine Pylon Master Geometric Drawing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . x7012100
Nacelle Master Geometric Drawing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . x7050000
Definitions - General
Basic Empty Weight - Standard Empty Weight plus installed optional equipment. This is the weight
reflected on the Weight and Balance Data Form supplied with the airplane.
MAC - Mean Aerodynamic Chord, MAC, is an engineering term which represents an airfoil’s chord in
aircraft design. As such, it is a constant length which is also used in the calculation of center-ofgravity
location in terms of percent MAC.
Operational Landing Weight - This is the weight at the start of touchdown. It is subject to airport,
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Citation Mustang airplane flight manual 3(19)
