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Wing
Span - Overall . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 43.17 Feet (13.16 Meters)
Area - Total Less Tips . . . . . . . . . . . . . . . . . . . . . . . . . . . .210.00 Square Feet (19.51 Square Meters)
Root Chord (WS 100.00) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6.856 Feet (2.090 Meters)
Tip Chord (Construction) (WS 353.844) . . . . . . . . . . . . . . . . . . . . . . . . . . . 3.085 Feet (0.940 Meters)
Dihedral . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3 Degrees
Sweepback (25 Percent Chord) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.500 Degrees
MAC (WS 110.875). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.209 Feet (1.588 Meters)
Aspect Ratio . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8.500
Flaps
Type . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Extensible Single Slotted Panel
Horizontal Tail
Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .56.542 Square Feet (5.253 Square Meters)
Dihedral . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.00 Degrees
Vertical Tail
Area (Exposed). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .37.473 Square Feet (3.481 Square Meters)
Fuselage
Maximum Height. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.00 Feet (1.52 Meters)
Maximum Width . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.00 Feet (1.52 Meters)
Interior (Standup) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.50 Feet (1.37 Meters)
Interior Width . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.58 Feet (1.40 Meters)
Length - Nose to Tail. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40.56 Feet (12.36 Meters)
6-10 510WB-00
MODEL 510 SECTION VI - WEIGHT AND BALANCE DATA
CONTROL - GENERAL
FAA APPROVED
U.S.
PRINCIPLE DIMENSIONS - EXTERIOR
NOTE
Tail height varies depending on oleo compression, cargo loading and airplane
configuration.
Figure 1
510WB-00 6-11/6-12
MODEL 510 SECTION VI - WEIGHT AND BALANCE DATA
CONTROL - FUEL
FAA APPROVED
U.S.
FUEL
Fuel Limits, Restrictions and Loading Management
CAUTION
• MAXIMUM ASYMMETRIC FUEL LOADING SHALL NOT EXCEED 200
POUNDS (90.7 KILOGRAMS) FOR TAKEOFF.
• MINIMUM FUEL LOADING PER WING TANK FOR TAKEOFF IS 200
POUNDS (90.7 KILOGRAMS).
• THE FUEL BOOST PUMP ON THE NON-FEED TANK MUST BE OFF
DURING CROSS-FEED.
NOTE
There is no restriction for asymmetric fuel loading during normal refueling operations.
Refer to the FAA Approved Airplane Flight Manual - Operating Limitations.
Fuel Tank Location
Figure 2 presents the fuel tank location in the airplane.
Fuel Loading Table
Figure 3 presents the weight and moment in 100 pound increments of the usable fuel which may be
carried in the airplane.
Figure 4 presents the weight and moment in 50 kilogram increments of the usable fuel which may be
carried in the airplane.
Unusable Fuel Table
Figure 5 presents the Unusable Fuel in the airplane.
510WB-00 6-13
SECTION VI - WEIGHT AND BALANCE DATA MODEL 510
CONTROL - FUEL
FAA APPROVED
U.S.
FUEL TANK LOCATION
Figure 2
6-14 510WB-00
MODEL 510 SECTION VI - WEIGHT AND BALANCE DATA
CONTROL - FUEL
FAA APPROVED
U.S.
FUEL LOADING TABLE - U.S. UNITS
Figure 3*
510WB-01 6-15
SECTION VI - WEIGHT AND BALANCE DATA MODEL 510
CONTROL - FUEL
FAA APPROVED
U.S.
FUEL LOADING TABLE - METRIC UNITS
Figure 4*
6-16 510WB-01
MODEL 510 SECTION VI - WEIGHT AND BALANCE DATA
CONTROL - FUEL
FAA APPROVED
U.S.
UNUSABLE FUEL TABLE
NOTE
Fuel weight is 6.70 pounds per gallon.
NOTE
Fuel weight is 0.803 kilograms per liter.
Figure 5*
TRAPPED AND UNUSABLE FUEL - U.S. UNITS
INCREMENTS VOLUME
(GALLONS)
WEIGHT
(POUNDS)
ARM = FS
(INCHES)
MOMENT/100
(INCH-POUNDS)
TRAPPED
UNUSABLE 0.36 2.40 292.33 7.02
DRAINABLE
UNUSABLE 4.33 29.00 291.06 84.41
TOTAL
UNUSABLE 4.69 31.40 291.16 91.42
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本文链接地址：Citation Mustang airplane flight manual 3(21)
