Specifications

SECTION I
MODEL 560 DESCRIPTION AND SPECIFICATIONS
LOAD FACTOR
In Flight:
Flaps - UP Position (0°) . . . . . . . . . . . . . . . . . . . . . . . . . .
$ 1.44 to +3.6G at 16,630 Pounds
Flaps - T.O., T.O. & APPR and LAND Position (7° to 35°) . . 0.0 to +2.0G at 16,630 Pounds
NOTE
These accelerations limit the angle-of-bank in turns and limit the severity of
pull-up/push-over maneuvers.
Landing :
Flaps LAND Position (35°) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . +3.46G at 15,200 Pounds
NOTE
This acceleration limits the airplane to a maximum landing sink rate of 600
feet-per-minute.
CABIN PRESSURIZATION LIMITATIONS
Normal Cabin Pressurization Limits . . . . . . . . . . . . . . . . 0.0 to 8.9 PSI +0.1 or
> 0.1 PSI Differential
Airplane must be depressurized for takeoff and landing.
PASSENGER COMPARTMENT
For all takeoff and landings, seats must be fully upright and outboard. The seat just aft of the
emergency exit must be to the most aft position (toward rear of airplane) and passenger seat belts and
shoulder harnesses must be fastened. The maximum number of passenger seats is 11.
ENROUTE OPERATIONAL LIMITS
Maximum Operating Altitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 45,000 Feet
Maximum Ambient Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (Refer to Figure 1-3)
Minimum Ambient Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (Refer to Figure 1-3)
Generator Load (Above High Idle) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 300 Amperes in Flight
Generator Load (High Idle) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 225 Amperes in Flight
I 56OMB-01 Configuration AA 1-17