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11,063 mm
Min Flight Weight
14,000 lb (6350 kg)
7.0% MAC
F.S. 419.87 in.
10,665 mm
Max Landing Weight
19,200 lb (8709 kg)
1.0% MAC
F.S. 414.64 in.
10,532 mm
28.0% MAC
F.S. 438.19 in.
11,130 mm
CENTER-OF GRAVITY — % MAC
100 22
Max Ramp Weight
21,750 lb (9865 kg)
19.5% MAC
F.S. 430.77 in.
10,942 mm
18.7% MAC
F.S. 430.08 in.
10,924 mm
Max Takeoff Weight
21,500 lb (9752 kg)
25.3% MAC
F.S. 435.84 in.
11,070 mm
26.2% MAC
F.S. 436.62 in.
11,090 mm
Max Zero Fuel Weight
16,000 lb (7258 kg)
Limitations
1-4.3 FM-126
FAA Approved 5-19-2004
AIRSPEED/MACH LIMITS
PRIMARY PITOT-STATIC SYSTEM
Figure 1-2.3
EFFECTIVITY
Aircraft 45-002 & Subsequent
modified by SB 45-11-4
MMO with Mach Trim Inoperative &
Autopilot Disengaged
MMO Limit
VA 21,500 Lb/9752 kg
VA 19,200 Lb/8709 kg
VA 17,000 Lb/7711 kg
VA 14,000 Lb/6350 kg
Mach Trim Inoperative
& Autopilot Disengaged
VMO Limit
45-600
Limitations
FM-126 1-5
FAA Approved 5-19-2004
Change 1
AIRSPEED/MACH LIMITS
MAXIMUM OPERATING SPEED VMO/MMO
VMO/MMO shall not be deliberately exceeded in any regime of flight
(climb, cruise, or descent) unless a higher speed is authorized for flight
test.
Primary Display
VMO .............................................................................................. 330 KIAS
MMO
- with Mach trim operative......................................................0.81 MI
- with Mach trim inoperative and Autopilot engaged .......0.81 MI
- with Mach trim inoperative and Autopilot disengaged
- 23,400 to 42,000 feet ..................................................... 0.76-0.78 MI
- Above 42,000 feet..................................................................0.78 MI
Standby Instruments
VMO .............................................................................................. 325 KIAS
MMO ...................................................................................................0.75 MI
MANEUVERING SPEED VA
Avoid rapid and large alternating control inputs,
especially in combinations with large changes in
pitch, roll or yaw as they may cause structural failure
at any speed, including below VA.
Refer to applicable figure entitled AIRSPEED/MACH LIMITS, this section,
for VA. Maneuvers involving full application of rudder and aileron
controls, as well as maneuvers that involve angles of attack near
stall should be confined to speeds below VA.
MAXIMUM LANDING GEAR OPERATING SPEED VLO.............200 KIAS
MAXIMUM LANDING GEAR EXTENDED SPEED VLE ................260 KIAS
MAXIMUM FLAP EXTENDED SPEED VFE
- Flaps 8° ............................................................................... 250 KIAS
- Flaps 20° ............................................................................. 200 KIAS
- Flaps 40° ............................................................................. 150 KIAS
CAUTION
Limitations
1-6 FM-126
FAA Approved 5-19-2004
AIRSPEED/MACH LIMITS (Cont)
MINIMUM CONTROL SPEED AIR VMCA
VMCA is a function of altitude and temperature. During flight tests, the
aircraft was controllable down to stall speed. The speed shown is the
minimum demonstrated speed corrected for maximum thrust effect
with rudder boost on or off.
VMCA
- Flaps 8° ............................................................................... 103 KIAS
- Flaps 20° ............................................................................. 101 KIAS
MINIMUM CONTROL SPEED GROUND VMCG
VMCG is a function of altitude and temperature. The speed shown is a
maximum, which occurs at maximum thrust conditions.
VMCG
- Rudder Boost On, APR On .............................................. 102 KIAS
- Rudder Boost On, APR Off .............................................. 100 KIAS
- Rudder Boost OFF, APR On............................................. 125 KIAS
- Rudder Boost OFF, APR Off ............................................ 123 KIAS
MINIMUM CONTROL SPEED LANDING VMCL
VMCL is a function of altitude and temperature. The speed shown is a
maximum, which occurs at maximum thrust conditions.
VMCL
- Flaps 8° ............................................................................... 105 KIAS
- Flaps 40° ............................................................................... 98 KIAS
TAKEOFF DECISION SPEED V1
Refer to applicable figure entitled TAKEOFF SPEEDS, Section V.
　
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