Specifications

SECTION I
MODEL 560 DESCRIPTION AND SPECIFICATIONS
OPERATING LIMITATIONS
WEIGHT
Maximum Design Ramp Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16,830 Pounds
Maximum Design Takeoff Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16,630 Pounds
Maximum Landing Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15,200 Pounds
Maximum Zero Fuel Weight (Standard) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12,600 Pounds
Maximum takeoff and landing weights may be additionally restricted due to altitude, temperature and
field length.
CENTER-OF-GRAVITY
Forward Limit:
At 12,400 pounds - 18.00 percent MAC (296.14 inches aft of datum)
At 16,830 pounds - 21.89 percent MAC (299.29 inches aft of datum)
(Straight line variation between 18.00 and 21.89 percent MAC)
Aft Limit:
At 16,830 pounds or less - 28.0 percent MAC (304.23 inches aft of datum)
AIRSPEED
Maximum Operating Speeds:
M
MO
(Above 28,907 Feet) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.755 Mach (Indicated)
V
MO
(Between 8000 Feet and 28,907 Feet) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 292 KIAS
V
MO (
Below 8000 Feet) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 262 KIAS
The maximum operating limit speeds may not be deliberately exceeded in any phase of flight (climb,
cruise, or descent) unless a higher speed is authorized for flight test or pilot training.
Maximum Maneuvering Speeds (V
A
) . . . . . . . . . . . . . . . Refer to Figure 1-3 and Section II of the basic
FAA Approved Airplane Flight Manual
Full application of rudder and aileron controls as well as maneuvers that involve angles-of-attack near
the stall should be confined to speeds below maximum maneuvering speed.
Maximum Flap Extended Speed (V
FE
):
Partial Flaps 7° (T.O.) and 15° (T.O. & APPR. Position) . . . . . . . . . . . . . . . . . . . . . . . . 200 KIAS
Full Flaps 35° (LAND Position) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 173 KIAS
Maximum Landing Gear Operating Speed, Extend - (V
LO
Extending) . . . . . . . . . . . . . . . . . . . 250 KIAS
Maximum Landing Gear Operating Speed, Retract - (V
LO
Retracting) . . . . . . . . . . . . . . . . . . 200 KIAS
Maximum Landing Gear Extended Speed - (V
LE
) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 250 KIAS
Maximum Speed Brake Operation Speed - (V
SB
) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . No Limit
Minimum Control Speeds (V
MCA
, V
MCL
, V
MCG
) . . . . . . . . . . . . . . . . . . . . . . Refer to Section IV of the
FAA Approved Airplane Flight Manual
Autopilot Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 292 KIAS or 0.755 MACH
Minimum Speed Sustained Flight In Icing Conditions:
(Except Approach and Landing) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 160 KIAS
TAKEOFF AND LANDING
Maximum Altitude Limit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10,000 Feet
Maximum Tailwind Components . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10 Knots
Maximum Ambient Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . ISA +34°C (Refer to Figure 1
> 3)
Minimum Ambient Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . -40°C
Maximum Water/Slush on Runway . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0.5 inches
Autopilot, yaw damper must be OFF for takeoff and landing.
Vertical navigation system must be off below 500 feet above ground level.
Takeoff and landings are limited to paved runway surfaces.
The nosewheel must be in firm contact with the ground prior to extending speed brakes and/or
deploying thrust reversers.
I 56OMB-01 Configuration AA 1-7