{"text_format":"3","workbook":"xls","n_sheets":3,"sheets":["W & B","CG Envelope","CG Limits"],"not_rendered":{"charts":2,"external_links":1},"read":"whole","date_system":"1900","formulas":"cached_only"}

{"sheet":"W & B","index":0,"n_rows":52,"n_cols":6,"rows_kept":52,"flags":["formulas_cached_only"]}
[]
[null,"Weight and Balance Calculator"]
[]
[]
[]
[null,"N5429R",null,"Weight(lbs)","Arm (inches)","Moment (in-lb)"]
[null,"Last weight & balance 8/24/12"]
[null,1493.55]
[]
[1,"Basic Empty Weight",null,1493.55,{"v":38.3,"d":"38.30"},{"v":57.202965,"d":"57.2"}]
[null,"(includes unusable fuel and oil)"]
[]
[2,"Usable Fuel (@ 6 lbs per gal)",null,336,{"v":48,"d":"48.00"},{"v":16.128,"d":"16.1"}]
[null,"Standard Tanks (56 gal max)"]
[]
[]
[3,"Pilot & Front Passenger",null,400,{"v":37,"d":"37.00"},14.8]
[null,"(Sta 34 to 46)"]
[]
[4,"Second Row Passengers",null,400,{"v":73,"d":"73.00"},29.2]
[]
[5,"Baggage Area \"1\"",null,0,{"v":95,"d":"95.00"},{"v":0,"d":"0.0"}]
[null,"(Sta 82 to 108) 120 lb max"]
[]
[6,"Baggage Aft (Area \"2\")",null,0,{"v":123,"d":"123.00"},{"v":0,"d":"0.0"}]
[null,"(Sta 108 to 142) 50 lbs max"]
[]
[7,"Ramp Weight and Moment",null,2629.55,null,{"v":117.33096499999999,"d":"117.3"}]
[]
[8,"Fuel Allowance (2 gal)",null,-8,null,-0.4]
[null,"engine start, taxi, runup"]
[]
[9,"Takeoff Weight and Moment",null,2621.55,{"v":44.60375159733744,"d":"44.6"},{"v":116.93096499999999,"d":"116.9"}]
[null,"(subtract step 8 from step 7)"]
[]
[10,"Locate weight and moment on the "]
[null,"\"Center of Gravity Moment\" "]
[null,"envelope to see if it falls within"]
[null,"acceptable range."]
[]
[null,"MAX T/O WEIGHT -  2550 LB"]
[null,"MAX LNG WEIGHT – 2550 LB"]
[null,"NEW CENTER OF GRAVITY",{"v":44.60375159733744,"d":"44.6"}]
[]
[null,"LANDING INFORMATION",null,"LNDG WGT","NEW CG","LNDG MOMENT"]
[]
[11,"FUEL BURN (gph) TO DESTINATION",12,2405.55,{"v":44.29879445449066,"d":"44.3"},{"v":106.562965,"d":"106.6"}]
[12,"TIME ENROUTE (MIN)",180,120]
[{"$nulls":3},{"v":5.76,"d":"5.8"}]
[null,"FUEL REMAINING (GAL)",20,{"v":106.562965,"d":"106.6"}]
[]
[13,"Calculate"]

{"sheet":"CG Envelope","index":1,"n_rows":13,"n_cols":11,"rows_kept":13,"flags":["formulas_cached_only"]}
[]
[]
[{"$nulls":3},"N5429R"]
[{"$nulls":3},"Last weight & balance 8/24/12",{"$nulls":3},60,1800,85,1800]
[{"$nulls":3},{"v":1493.55,"d":"1493.6"},{"$nulls":3},74,2260,145,3100]
[{"$nulls":7},85,2480]
[{"$nulls":7},95,2700]
[{"$nulls":7},127,3100,127,3100]
[]
[]
[{"$nulls":3},"TAKEOFF WEIGHT",{"v":2621.55,"d":"2621.6"}]
[]
[{"$nulls":3},"MOMENT",{"v":116.93096499999999,"d":"116.9"}]

{"sheet":"CG Limits","index":2,"n_rows":16,"n_cols":5,"rows_kept":16,"flags":["formulas_cached_only"]}
[]
[]
[{"$nulls":3},"N5429R"]
[{"$nulls":3},"Last weight & balance 8/24/12"]
[{"$nulls":3},1493.55]
[]
[]
[]
[]
[{"$nulls":3},"AIRCRAFT WEIGHT - TAKEOFF",{"v":2621.55,"d":"2621.6"}]
[]
[{"$nulls":3},"CENTER OF GRAVITY - TAKEFOFF",{"v":44.60375159733744,"d":"44.6"}]
[]
[{"$nulls":3},"CENTER OF GRAVITY - LANDING",{"v":44.29879445449066,"d":"44.3"}]
[]
[{"$nulls":3},"AIRCRAFT WEIGHT - LANDING",{"v":2405.55,"d":"2405.6"}]