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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.
CITATION MUSTANG OPERATING MANUAL
510OM-00 19-3
CITATION MUSTANG OPERATING MANUAL
Payload—Zero fuel weight minus basic empty
weight. This is the weight of crew, passengers,
baggage, and cargo.
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 defueled 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.
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.
19-4 510OM-00
CITATION MUSTANG OPERATING MANUAL
MAXIMUM WEIGHT LIMITS
Maximum ramp weight ................................................................. 8,730 pounds (3,960 kilograms)
Maximum takeoff weight* ........................................................... 8,645 pounds (3,921 kilograms)
Maximum landing weight*........................................................... 8,000 pounds (3,629 kilograms)
Maximum zero fuel weight........................................................... 6,750 pounds (3,062 kilograms)
Maximum nose baggage weight ......................................................... 320 pounds (145 kilograms)
Maximum tail cone baggage weight .................................................. 300 pounds (136 kilograms)
*Refer to the FAA-approved Aircraft Flight Manual for additional restrictions that 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 5,550 pounds to 6,927 pounds
and/or................................................................ 287.04 inches aft of the datum (21.32% MAC)
at 8,730 pounds with straight line variation
between these points
Aft limit .................................................................. 292.46 inches aft of the datum (30.00% MAC)
at 5,314 pounds to 8,730 pounds
MAXIMUM DESIGN CENTER-OF-GRAVITY LIMITS (METRIC UNITS)
Forward limit .................................................. 7,254 millimeters aft of the datum (19.00% MAC)
at 2,517 kilograms to 3,142 kilograms
and/or ......................................................... 7,291 millimeters aft of the datum (21.32% MAC)
at 3,960 kilograms with straight line variation
between these points
Aft limit ........................................................... 7,428 millimeters aft of the datum (30.00% MAC)
at 2,410 kilograms to 3,960 kilograms
BALANCE LIMITS FOR
NORMAL GROUND
OPERATIONS
Removal of any large components forward of the
wing may require temporary ballast in the nose.
There are no balance limits for fuel loading operations.
For example, one wing fuel tank can
be completely filled prior to adding fuel to the
opposite wing fuel tank.
As with any aircraft, use caution when loading.
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