[{"data":1,"prerenderedAt":-1},["ShallowReactive",2],{"$fA_p8iMurJKsl0tVJLmUYM2a6dtLV7hXl81ToERkXnC0":3},{"answer":4,"createTime":5,"id":6,"options":7,"origin":12,"question":19,"related":20,"source":30,"type":31},[],"2026-04-11 14:16:21",337984462,[8,9,10,11],"干使用重量+商载重量","零燃油重量+储备燃油重量","航程燃油+着陆重量","基本空机重量+机组重量",{"count":13,"courseId":14,"courseImg":15,"courseName":16,"workId":17,"workName":18},9,"53e1d2ef4961cca8eea3e23969ad2cb9","https:\u002F\u002Ftihai-oss-cloud.itihey.com\u002Fimg\u002F03a579384a6dc297c89809b582fcc767.png","默认课程","3d62f12908af44c79e58790f6bee04b1","6.5 重量术语与限制","无油重量或无燃油重量 = ( )",[21,32,38,41,46,55,64,74,81],{"answer":22,"createTime":5,"id":23,"options":24,"question":29,"source":30,"type":31},[],337984460,[25,26,27,28],"飞行机组","发动机滑油","油箱底油","备份燃油","下面的载荷中不属于DOW的是","v1",0,{"answer":33,"createTime":5,"id":34,"options":35,"question":37,"source":30,"type":31},[],337984461,[8,36,10,11],"零燃油重量+燃油重量","飞机在起飞机场的停机坪重量 = ( )",{"answer":39,"createTime":5,"id":6,"options":40,"question":19,"source":30,"type":31},[],[8,9,10,11],{"answer":42,"createTime":5,"id":43,"options":44,"question":45,"source":30,"type":31},[],337984463,[8,36,10,11],"起飞重量 = ( )",{"answer":47,"createTime":5,"id":48,"options":49,"question":54,"source":30,"type":31},[],337984464,[50,51,52,53],"起飞重量、着陆重量、干使用重量","起飞重量、着陆重量、无燃油重量","起飞重量、着陆重量、基本空机重量","干使用重量、着陆重量、无燃油重量","飞机实际运行过程中会受到结构或性能限制的重量有",{"answer":56,"createTime":5,"id":57,"options":58,"question":63,"source":30,"type":31},[],337984465,[59,60,61,62],"OEW","DOW","TOW","ZFW","停机坪重量 - 启动滑行燃油 = ( )",{"answer":65,"createTime":5,"id":66,"options":67,"question":72,"source":30,"type":73},[],337984466,[68,69,70,71],"TOW&le;MZFW+起飞油量","TOW&le;MTOW","TOW&ge;MLW+航程油量","LW&le;MLW","为保证飞行安全,飞机的重量必须满足",1,{"answer":75,"createTime":76,"id":77,"options":78,"question":79,"source":30,"type":80},[],"2026-04-11 19:45:10",338302107,[],"起飞重量的英文简写是 ; 着陆重量的英文简写是 ; 干使用重量的英文简写是 ; 无油重量的英文简写是",2,{"answer":82,"createTime":76,"id":83,"options":84,"question":85,"source":30,"type":80},[],338302108,[],"已知: 结构限制的最大起飞重量为62000kg; 结构限制的最大着陆重量为53700kg; 最大零燃油重量为48000kg; 性能限制的最大起飞重量为75000kg; 性能限制的最大着陆重量为51400kg; 起飞燃油重量为13800kg; 航程燃油重量为5950kg. 则放行最大起飞重量等于 kg"]