▁ 1 ▁cabin ▁crew ▁| cap acity = 9 ▁| length ▁ft = 7 6 ▁| length ▁in = 1 0 ▁| length ▁note = ▁| span ▁ft = 1 0 2 ▁| span ▁in = ▁| span ▁note = ▁| height ▁ft = 1 7 ▁| height ▁in = 1 0 ▁| height ▁note = ▁| wing ▁area ▁sq ft = 1 2 9 7 ▁| wing ▁area ▁note = ▁| as pect ▁ratio = 8 . 0 2 ▁| air fo il = root : ▁N AC A ▁ 2 3 0 1 8 ; ▁tip : ▁N AC A ▁ 2 3 0 1 2 ▁| empty ▁weight ▁lb = 3 7 1 9 0 ▁| empty ▁weight ▁note = equ ipped ▁| g ross ▁weight ▁lb = 6 5 0 0 0 ▁| g ross ▁weight ▁note = ▁Max imum ▁landing ▁weight : ▁ ▁| max ▁take off ▁weight ▁lb = ▁| max ▁take off ▁weight ▁note = ▁| f uel ▁capacity = ▁in ▁wing ▁t anks , ▁with ▁ ▁in ▁bomb - bay ▁t anks ▁| more ▁general = ▁ ▁| eng 1 ▁number = 4 ▁| eng 1 ▁name = R oll s - Ro y ce ▁Mer lin ▁ 2 4 / 2 ▁| eng 1 ▁type = V - 1 2 ▁liquid - co o led ▁p ist on ▁engines ▁| eng 1 ▁h p = 1 6 2 0 ▁| eng 1 ▁note = ▁ ▁| prop ▁bla de ▁number = 3 ▁| prop