Specifications

SECTION IV
MODEL 560 OPERATING INFORMATION
NORMAL PROCEDURES
PREFLIGHT INSPECTION
1. Battery - CONNECTED.
2. Engine Covers (2) - REMOVED.
3. Pitot Covers (3) - REMOVED.
NOTE
Refer to Normal Procedures, Cold Weather Operations, if the airplane has been
exposed to ambient temperatures below -10°C (+14°F) for a prolonged period.
PRELIMINARY COCKPIT INSPECTION
1. Documents - CHECK ABOARD.
a. To be displayed in airplane at all times:
(1) Airworthiness and Registration Certificates.
(2) Radio Station License(s) (if required).
b. To be carried in the airplane at all times:
(1) FAA Approved Airplane Flight Manual.
(2) Honeywell Primus 1000 Pilot’s Manual.
(3) Applicable FMS Pilot’s Manual (if required).
2. Flashlight - ABOARD.
3. Portable Fire Extinguisher - SERVICED and SECURE (under copilot's seat).
4. Microphones, Headsets, Oxygen Masks and Smoke Goggles - ABOARD and PROPERLY
STOWED.
5. Oxygen Quantity - CHECK in Green arc.
6. CONTROL LOCK - UNLOCKED.
7. Gear Handle - DOWN.
8. Rudder, Aileron and Elevator Trim - POSITION Elevator trim tab indicator just below top of
takeoff trim range and aileron and rudder trim tabs in neutral.
9. Flap Handle - AGREES with Flaps position.
10. Circuit Breakers - IN.
11. Generator Switches - L GEN and R GEN (OFF, if external power is to be used for start).
12. All other switches - OFF, NORM or AUTO.
13. Throttles - OFF.
14. Battery Switch - BATT (24 volts minimum).
15. Fuel Quantity and Balance - CHECK.
NOTE
Maximum lateral fuel imbalance is 200 pounds. If imbalance exceeds 200 pounds,
correct prior to flight.
16. Battery Switch - EMER. Check Engine Display LH Reversionary Channel, RMU 1, Standby HSI
and Landing Gear Indicator receiving power.
NOTE
Standby Flight Display will be blank.
17. Battery Switch - BATT.
I 56OMB-01 Configuration AC 4-3.1