Specifications

SECTION I
MODEL 560 DESCRIPTION AND SPECIFICATIONS
NOTES
1. Maximum Asymmetrical Fuel Differential for normal operations is 200 pounds.
2. Flight characteristics requirements were not demonstrated with unbalanced fuel above 200
pounds. A lateral fuel imbalance of 600 pounds has been demonstrated for emergency
return.
Figure 1-7. Fuel Limitations
Figure 1-8. Jet B / JP-4 Fuel Operating Limitations
FUEL
GRADE
FUEL
SPECIFICATION
MINIMUM FUEL
TEMPERATURE
(TAKEOFF)
MAXIMUM FUEL
TEMPERATURE
(TAKEOFF)
MAXIMUM
ALTITUDE
JET A ASTM-D1655 -40°C +55°C 45,000 FEET
JET A-1 ASTM-D1655 -40°C +55°C 45,000 FEET
JET B ASTM-D1655 -45°C
REFER TO
FIGURE 1-8
REFER TO
FIGURE 1-8
JP-4 MIL-DTL-5624 -52°C
REFER TO
FIGURE 1-8
REFER TO
FIGURE 1-8
JP-5 MIL-DTL-5624 -40°C +55°C 45,000 FEET
JP-8 MIL-T-83133 -40°C +55°C 45,000 FEET
I 56OMB-01 Configuration AA 1-15