Advanced Data Results

Errors:

Invalid Aircraft Selected

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

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
.


Winds Aloft Profile

KTS

HWAltitudeTW

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