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operational and related restrictions. It must not exceed maximum landing weight.
Operational Takeoff Weight - This is the weight at the start at the takeoff run. It is subject to airport,
operational and related restrictions. It must not exceed maximum takeoff weight.
Payload - Zero fuel weight minus basic empty weight. This is the weight available for crew,
passengers, baggage and cargo.
(Continued Next Page)
510WB-00 6-7
SECTION VI - WEIGHT AND BALANCE DATA MODEL 510
CONTROL - GENERAL
FAA APPROVED
U.S.
Definitions - General (Continued)
Ramp Weight - Operational takeoff weight plus fuel necessary for start, taxi and run-up. It must not
exceed maximum ramp weight.
Standard Empty Weight - Weight of standard airplane including standard items.
Standard Items - Equipment and fluids not an integral part of a particular airplane and not a variation
for the same type of airplane. These items may include, but are not limited to the following:
• Unusable Fuel
• Trapped Fuel
• Engine Oil
• All Hydraulic Fluid
• Serviced Fire Extinguisher
Trapped Fuel - Fuel remaining when airplane is de-fueled by normal means using the procedures
and attitudes specified for draining the tanks.
Unusable Fuel - Fuel remaining after a fuel run-out test has been completed in accordance with
governmental regulations.
Usable Fuel - Fuel available for flight planning.
Useful Load - Difference between takeoff weight, or ramp weight if applicable and basic empty
weight. It includes payload, usable fuel and other usable fluids not included as standard items.
Zero Fuel Weight - Basic empty weight plus payload. It must not exceed maximum zero fuel weight.
Definitions - Weight Limitations
Maximum Landing Weight - Maximum weight approved for the landing touchdown.
Maximum Ramp Weight - Maximum weight for ground maneuvers as limited by airplane strength
and airworthiness requirements. It includes weight of start, taxi and run-up fuel.
Maximum Takeoff Weight - Maximum weight for takeoff as limited by airplane strength and
airworthiness requirements. This is the maximum weight approved for the start of the takeoff run.
Maximum Zero Fuel Weight - Maximum weight allowed exclusive of usable fuel.
6-8 510WB-00
MODEL 510 SECTION VI - WEIGHT AND BALANCE DATA
CONTROL - GENERAL
FAA APPROVED
U.S.
Maximum Weight Limits
Maximum Ramp Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8730 Pounds (3960 Kilograms)
Maximum Takeoff Weight * . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8645 Pounds (3921 Kilograms)
Maximum Landing Weight * . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8000 Pounds (3629 Kilograms)
Maximum Zero Fuel Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6750 Pounds (3062 Kilograms)
Maximum Nose Baggage Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 320 Pounds (145 Kilograms)
Maximum Tailcone Baggage Weight. . . . . . . . . . . . . . . . . . . . . . . . . . . . 300 Pounds (136 Kilograms)
*Refer to the FAA Approved Airplane Flight Manual for additional restrictions which may apply due to
runway, pressure, altitude and temperature.
Maximum Design Center-of-Gravity Limits (U.S. Units)
Forward Limit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 285.59 inches aft of the datum (19.00% MAC)
at 5550 pounds to 6927 pounds.
and/or . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 287.04 inches aft of the datum (21.32% MAC)
at 8730 pounds with straight line variation
between these points.
Aft Limit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 292.46 inches aft of the datum (30.00% MAC)
at 5314 pounds to 8730 pounds.
Maximum Design Center-of-Gravity Limits (Metric Units)
Forward Limit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7254 millimeters aft of the datum (19.00% MAC)
at 2517 kilograms to 3142 kilograms.
and/or . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7291 millimeters aft of the datum (21.32% MAC)
at 3960 kilograms with straight line variation
between these points.
Aft Limit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7428 millimeters aft of the datum (30.00% MAC)
at 2410 kilograms to 3960 kilograms.
Takeoff Trim Settings
Refer to the FAA Approved Airplane Flight Manual for takeoff trim settings in relation to airplane
center-of-gravity.
510WB-00 6-9
SECTION VI - WEIGHT AND BALANCE DATA MODEL 510
CONTROL - GENERAL
FAA APPROVED
U.S.
Principle Dimensions
Figure 1 presents principle dimensions with gear in the static positions.
　
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