Originally Posted by
ashdaviator
A twin engine aeroplane is certified for a MSTOM and a MSLM of 58 000 kg and
55 000 kg respectfully. What is the limiting take-off mass for the aeroplane?
PLTOM 61 000 kg
PLLM 54 000 kg
MZFM 36 000 kg
Operating mass 55 000 kg
Trip fuel 36 000 kg
Alternative fuel 500 kg
Final reserve 500 kg
Flight duration 3 hours
Fuel consumption 500 kg per hour
The Trip Fuel can't be 36 000 kg if it's 3 hours at 500kg/h!