Given the following information, calculate the estimated estimated Landing Mass at the destination for a helicopter Commercial Air Transport flight. Assume the Basic Fuel Scheme WITHOUT variations applies.
DOM: 9900 lb
Traffic Load: 3160 lb
Remaining useable fuel: 2100 lb
Remaining Trip Fuel to Destination: 800 lb
Destination Alternate Fuel: 485 lb
Final Reserve Fuel: 420 lb
Extra fuel: 0 lb
Discretionary Fuel: 0 lb
The Revised Estimated Landing Mass at the Destination aerodrome is: Zero Fuel Mass + Fuel at Destination.
The Zero Fuel Mass (ZFM) is: Dry Operating Mass (DOM) + Traffic Load = 9900 lb + 3160 lb = 13 060 lb.
The Fuel at Destination is: Remaining useable fuel - Remaining Trip Fuel to Destination = 2100 lb - 800 lb = 1300 lb.
Thus, the Revised Estimated Landing Mass at the Destination aerodrome will be: 13 060 lb + 1300 lb = 14 360 lb.
NOTE:
The Remaining useable fuel includes the Alternate and the Final Reserve Fuel.
Your Notes (not visible to others)
This question has appeared on the real examination, you can find the related countries below.
Use Keyboard Shortcuts
