Fuel System Limitations Flashcards
1
Q
Max en route asymmetry
A
1000 kg
2
Q
If asymmetry exceeds 350 kg - max cross wind
A
20 kt
3
Q
Max Fuel Asymmetry on ground except during refueling
A
500 kg for F100 aircraft weight > 39 000 kg
and
1000 kg for F100 aircraft weight at or < 39 000 kg and all F70
4
Q
Total Useable fuel
A
10 256 kg. ( FK series & UQW, UQN)
Or
10 692 kg. ( F70’s and UQ series except UQW & UQN)
5
Q
Wing tanks quantity
A
7744 kg
(3872 each)
6
Q
Centre tank quantity
A
2512 kg (bladder type)
Or
2980 kg (integral)
