General dimension and Characteristic of Wide Body Aircraft
with 4 (four) engine.
Item Description Units Aircraft
No. B-747-200 B-747-400 A-340-300 A-340-400
1. ICAO Airport Ref. Code E E E E
2 MTOW (Max. Take-off weight) ton 340.10 394.63 257.00
3 MLW (Max. Design Landing weight) ton 255.80 285.76 186.00
4 Length (A) m 70.40 70.67 63.69
5 Wing span (B) m 59.64 64.94 60.30
6 Wing-tip vertical clearance -min (Y) m 5.36 5.11 7.53
7 Tail height -max. (Z) m 19.58 19.58 17.03
8 Fuselage width (R) m 6.50 6.50 5.64
9 Fuel capacity lt 198,400.00 215,900.00 138,600.00
10 Cargo Volume m3 173.00 173.00 162.80
11 Main gear width (G) m 11.00 11.00 10.70
12 Nose to nose gear (D) m 7.75 7.75 6.67
13 Nose to main forward gear (E) m 33.37 33.37 32.04
14 Nose to door (L1) m 9.50 9.50 5.85
15 Engine (inboard) from acft. cl (L) m 12.12 11.64 9.37
16 Engine (outboard) from acft. cl (M) m 21.29 20.83 19.6
17 Engine clearance above ground
Inboard -min (W) m 1.14 1.14 1.22
Outboard - min (X) m 1.82 1.82 2.34
18 Aircraft Service Point
Pressure refueling from nose (Q) m 32.31 32.31 30
Pressure refueling from CL (Q`) m 14.02 14.02 12.6
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