Specifications
Table Of Contents
- 560 ENCORE OPERATING MANUAL

SECTION IV
OPERATING INFORMATION
MODEL 560
EXTERIOR INSPECTION
During inspection, make a general check for security, condition and cleanliness of the airplane and
components. Check particularly for damage; fuel, oil and hydraulic fluid leakage; security of access
panels; and removal of keys from locks.
NOTE
f
Expedite all checks with electrical power on and ensure that the air conditioner
switch is OFF, if external power is not used.
f
Landing and nav lights may be omitted if night flight is not anticipated.
1. Hot Items/Lights - ON and CHECK.
a. Left, Right and Standby Static Ports - CLEAR and WARM.
b. Left, Right and Standby Pitot Tubes - CLEAR and HOT.
c. Landing Lights - ALL ON (if not observed from cockpit).
d. Recognition Lights - ALL ON (if not observed from cockpit).
e. Angle-of-attack Vane - FREE and HOT.
f. Beacon Light - ON and FLASHING (if not observed from cockpit).
g. Right Wing Inspection, Navigation, and Anti-collision - ON (if not observed from cockpit).
h. Tail Navigation Light - ON.
i. Left Wing Inspection, Navigation, and Anti-collision Lights - ON (if not observed from
cockpit).
j. Hot Items/Lights and Battery Switches - OFF.
2. Left Nose - CHECK.
a. Brake Fluid Reservoir Sight Gauges - FLUID VISIBLE.
b. Power Brake Accumulator Charge - MINIMUM. Grey band (675 psi) with brake
accumulator not charged. System Charged - IN GREEN ARC.
NOTE
If airplane has been cold soaked in ambient temperature below -10°C (+14°F), the
accumulator charge may indicate below the grey band (675 psi), but the needle must
be visibly above the lower stop.
c. Nose Baggage Door - SECURE and LOCKED.
d. Nose Gear, Doors, Wheel and Tire - CONDITION.
3. Right Nose and Fuselage Right Side - CHECK.
a. Windshield Alcohol Reservoir Sight Gauge - FLUID VISIBLE.
b. Brake and Gear Pneumatic Pressure Gauge - IN GREEN ARC.
c. Nose Baggage Door - SECURE and LOCKED.
d. Ram Air Temperature Probe - CLEAR.
e. Overboard Vent Lines - CLEAR.
f. Top and Bottom Antennas - CONDITION and SECURE.
g. Dorsal Fin Air Inlet - CLEAR.
4. Right Wing - CHECK.
a. Pylon Air Inlet - CLEAR.
b. Engine Temperature
Sensors (2) - CONDITION.
c. Engine Fan Duct and Fan - CONDITION.
d. Wing Inspection Light - CONDITION.
(Continued Next Page)
I
4-4 Configuration AA 56OMB-01










