[{"data":1,"prerenderedAt":-1},["ShallowReactive",2],{"$fgWuQsbCqPkRI3fpTIo0UE_Em1yP3Zf4e0IVhVNuO2ZM":3},{"answer":4,"createTime":5,"id":6,"options":7,"origin":8,"question":15,"related":16,"source":27,"type":80},[],"2026-04-11 19:45:10",338302107,[],{"count":9,"courseId":10,"courseImg":11,"courseName":12,"workId":13,"workName":14},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","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",[17,29,38,44,49,58,67,77,81],{"answer":18,"createTime":19,"id":20,"options":21,"question":26,"source":27,"type":28},[],"2026-04-11 14:16:21",337984460,[22,23,24,25],"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":30,"createTime":19,"id":31,"options":32,"question":37,"source":27,"type":28},[],337984461,[33,34,35,36],"干使用重量+商载重量","零燃油重量+燃油重量","航程燃油+着陆重量","基本空机重量+机组重量","飞机在起飞机场的停机坪重量 = ( )",{"answer":39,"createTime":19,"id":40,"options":41,"question":43,"source":27,"type":28},[],337984462,[33,42,35,36],"零燃油重量+储备燃油重量","无油重量或无燃油重量 = ( )",{"answer":45,"createTime":19,"id":46,"options":47,"question":48,"source":27,"type":28},[],337984463,[33,34,35,36],"起飞重量 = ( )",{"answer":50,"createTime":19,"id":51,"options":52,"question":57,"source":27,"type":28},[],337984464,[53,54,55,56],"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":59,"createTime":19,"id":60,"options":61,"question":66,"source":27,"type":28},[],337984465,[62,63,64,65],"OEW","DOW","TOW","ZFW","停机坪重量 - 启动滑行燃油 = ( )",{"answer":68,"createTime":19,"id":69,"options":70,"question":75,"source":27,"type":76},[],337984466,[71,72,73,74],"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":78,"createTime":5,"id":6,"options":79,"question":15,"source":27,"type":80},[],[],2,{"answer":82,"createTime":5,"id":83,"options":84,"question":85,"source":27,"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"]