Reference 121.639 and 121.647 and assume an aircraft with the following simplified limits:
max zero fuel weight 95,000
max landing weight 100,000
max takeoff weight 130,000
scenario1:
basic operating weight (BOW): 70,000
payload (passengers and cargo): 21,000
zero fuel weight is 91,000
fuel burn reserve holding taxi extra minimum planned fuel
20,000 10,000 0 1000 0 30,000 31,000
takeoff weight 121,000 (after taxi fuel consumed)
landing weight 101,000 * (after fuel burn)
* 1,000 pounds overweight for landing
Can't go like this, captain is correct to ask for 1,000 pounds of payload to be removed.
scenario2:
If (thru different cruise altitude, route or winds) the fuel burn is revised to 22,000,
you would have to revise your fuel planning to at least:
fuel burn reserve holding taxi extra minimum planned fuel
22,000 10,000 0 1000 0 32,000 33,000
You would still end up 1,000 too heavy for landing, you have to reduce payload prior to departure.
It's easy to fall into the trap of busting 121.639 and 121.647 by increasing the fuel burn to make landing weight without adjusting payload.
No big deal in this Eagle case, if their op specs allow fuel planning from the collins fms, or the original release dispatch performance was in error.
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