Errors:

Invalid Aircraft Selected

Invalid Weight selected
Start Elevation Beyond Performance Envelope!!
End Elevation Beyond Performance Envelope!!
Minimum Cruise Altitude Beyond Performance Envelope!!

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Invalid

Requested Analysis Report:                                                                    Fuel Cost: 5.25 $

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Trip Distance (nm) 100 nm Takeoff Elevation 0 ft Landing Elevation 0 ft Minimum Cruise Alt 0 ft Maximum Cruise Alt 0 ft Aircraft Weight 1000000 lbs Usable Fuel(Gallons) 0

Economy Range | nm w/45 min Reserve Performance Range | nm w/45 min Reserve Requested Distance ----| 100 nm Note: This report does not take into account fuel stops that might be necessary to achieve the requested distance. We suggest breaking such trips into smaller segments to determine optimum altitudes on each fuel leg. This Data is only Advisory in nature we recommend All Aircraft Analysis Reports be backed up by personal flight planning with ones own POH/AFM.

Results:

Most Fuel Efficient Cruise Profile Climb Profile Normal Climb Time (min) 0 Density Altitude ft TAS 0 kts % BHP 0 % Total Trip Time(Hour:Min) 0:00 Total Trip Fuel Burn(G) 0 Total Trip Fuel Cost 0 $ Climb Burn(Gallon) 0 Climb Distance 0 nm FT Fuel CPM 0 $ Avg MPG

Highest Performance Cruise Profile Climb Profile Normal Climb Time (min) 0 Density Altitude ft TAS 0 kts % BHP 0 % Total Trip Time(Hours:Min) 0:00 Total Trip Fuel Burn(G) 0 Total Trip Fuel Cost 0 $ Climb Burn(Gallon) 0 Climb Distance 0 nm FT Fuel CPM 0 $ Avg MPG

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Winds Aloft Profile KTS HW Altitude TW

Optimum Economy Cruise Ideal Cruise Altitude (ft) Cruise BHP Cruise TAS (kts) Gnd Speed (kts) Trip Fuel Burn Trip Time

Optimum Performance Cruise Ideal Cruise Altitude (ft) Cruise BHP Cruise TAS (kts) Gnd Speed (kts) Trip Fuel Burn Trip Time