Specifications

SECTION I
DESCRIPTION AND SPECIFICATIONS
MODEL 560
FUEL LIMITATIONS
Anti-icing must be added to all approved fuels not presently containing additive.
FUEL BOOST Pumps - ON; when low fuel lights illuminate or at 180 ± 20 pounds or less indicated
fuel.
The following fuels are approved for use in accordance with Figure 1-8.
COMMERCIAL KEROSENE JET A, JET A-1, JET B, JP-4,JP-5, and JP-8.
SINGLE POINT REFUELING LIMITATION
Single point refueling operations must be accomplished per the procedures contained on the placard
installed on the single point refueling access door. Refueling pressure range is 10 to 50 PSI,
maximum defueling pressure is -10 PSI.
UNUSABLE FUEL
Fuel remaining in the fuel tanks when the fuel quantity indicator reads zero is not usable in flight.
ALCOHOL
Use TT-I-735 Isopropyl Alcohol for windshield anti-ice.
TIRE PRESSURE
Main Gear Tire Pressure:
1. Main gear tire pressure shall be kept at 152 PSIG, ±5 PSIG (1048 kPa ±34.5 kPa), unloaded, with
an ambient temperature of 21.11° C (70°F).
2. Main gear tire pressure shall be kept at 158 PSIG, ±5 PSIG (1048 kPa ±34.5 kPa), loaded, with an
ambient temperature of 21.11° C (70°F).
(Nose Gear Tire Pressure:
1. Nose gear tire pressure shall be kept at 120 PSIG, ±5 PSIG (827 kPa, ±34.5 kPa), unloaded, with
an ambient temperature of 21.11° C (70°F).
2. Nose gear tire pressure shall be kept at 125 PSIG, ±5 PSIG (862 kPa, ±34.5 kPa), loaded, with an
ambient temperature of 21.11° C (70°F).
Adjust tire pressures for climate change. Climate changes will have an effect on tire pressure when flying
from a hot climate to a cool climate and vice versa. When the temperature change is extreme, such as
changes in excess of 10°C (50°F) for example, a tire inflated in a warm climate will drop in air pressure,
when the airplane on which it is installed is flown to a cold climate. An airplane moved out of a heated
hangar into the cold winter will do the same.
In either circumstance, tires should be overinflated to compensate for the subsequent cooling and loss of
pressure caused by extreme temperature changes. As a general rule, an ambient temperature change of -
15° C (5° F) produces a pressure change of about one percent.
AUTHORIZED OPERATIONS
This airplane is approved for day and night, VFR, IFR flight and flight into known icing conditions. This
airplane is not approved for ditching under FAR 25.801.
NOTE
Icing conditions exist, when operating on the ground or in flight, when visible moisture
is evident and the indicated OAT is between +10°C and -30°C.
I 1-16 Configuration AA 56OMB-01