Minuteman
I HAVE STRONG OPINIONS ABOUT AUTOMOTIVE LIGHTING!
I got to wondering about the Maximum Zero Fuel Weight (MZFW) Limit most manufacturers have for their aircraft. Its usually defined as something like, "the maximum weight allowed before usable fuel is included."
So lets say I have an aircraft with a big center fuel tank. Did the manufacturer set the MZFW limit to be as low as possible by subtracting a full center tank fuel weight from the design max. structural load?
For example, lets say there is an aircraft with a 14,000lb center tank, but it's making a short hop to its destination and needs only the fuel in the wings. The plane is already already at MZFW with more payload sitting on the ramp. Is the operator stuck flying around with an additional 14,000lb of unused capacity? I.e., is that how MZFW works?
So lets say I have an aircraft with a big center fuel tank. Did the manufacturer set the MZFW limit to be as low as possible by subtracting a full center tank fuel weight from the design max. structural load?
For example, lets say there is an aircraft with a 14,000lb center tank, but it's making a short hop to its destination and needs only the fuel in the wings. The plane is already already at MZFW with more payload sitting on the ramp. Is the operator stuck flying around with an additional 14,000lb of unused capacity? I.e., is that how MZFW works?