{"text_format":"3","workbook":"xlsx","n_sheets":7,"sheets":["Introductie","Aquila A210 PH-DHA","Aquila A210 PH-DHB","Cessna C172 PH-DHD","Instructeurs","Envelope Aquila A210","Envelope Cessna C172"],"not_rendered":{"charts":5,"images":7,"defined_names":29,"comments":3},"read":"whole","date_system":"1900"}

{"sheet":"Introductie","index":0,"n_rows":7,"n_cols":2,"rows_kept":7}
[]
[]
[null,"Weight and Balance Spreadsheets"]
[]
[null,"Selecteer het juiste tabblad voor het toestel dat je gaat vliegen en controleer de meest recente weegrapporten bij de toestelpapieren. Vul de gewichten van de piloot, passagiers en bagage in."]
[]
[null,"Versie 6-10-2021"]

{"sheet":"Aquila A210 PH-DHA","index":1,"n_rows":54,"n_cols":9,"rows_kept":54,"merged":[[0,0,28,0],[30,1,30,2],[32,1,32,4],[33,1,33,4],[33,5,33,6],[34,0,34,8],[35,5,35,8],[36,0,36,1],[36,5,36,6],[37,0,37,1],[38,0,38,1],[40,0,40,1],[41,0,41,1],[43,0,43,1],[44,0,44,1],[44,5,44,8],[45,5,45,8],[46,0,46,1],[46,5,46,8],[47,5,47,8],[48,0,48,1],[48,5,48,8],[49,5,49,8],[50,0,50,1],[50,5,50,8],[52,0,52,8],[53,0,53,8]]}
["AQUILA     AT01  PH-DHA"]
{"$rows_empty":29}
["VLIEGTUIG         :","AQUILA  A210",{"$nulls":3},"Date of  FLIGHT :",null,{"$f":"NOW()","v":"2021-10-06T21:36:27.740"}]
[null,"ATO 1-245",{"$nulls":3},"Departure :",null,"EHKD"]
["Registration   : ","PH-DHA",{"$nulls":3},"VIA :"]
[{"$nulls":5},"Destination :"]
[]
[null,null,"Kg","Arm","  M * Kg   ","Address information:"]
["BEW incl. oil and unuseable fuel",null,517,"Mtr",222,"     Naam",null,"Postcode","Huis Nr"]
["LH Seat PIC (length < 1.75 m )",null,null,0.45,{"$f":"C38*D38","v":0}]
["LH Seat PIC (length > 1.75 m )",null,null,0.59,{"$f":"C39*D39","v":0}]
[]
["RH Seat Pas (length < 1.75 m )",null,null,0.45,{"$f":"C41*D41","v":{"v":0,"d":"0.00"}}]
["RH Seat Pas (lenght > 1.75 m )",null,null,0.59,{"$f":"C42*D42","v":0}]
[]
["baggage Area  1  (max  40 kg )",null,null,{"v":1.3,"d":"1.30"},{"$f":"C44*D44","v":0}]
["Zero FUEL Weight",null,{"$f":"SUM(C37:C44)","v":517}," ",{"$f":"SUM(E37:E44)","v":222},"p CHECK in Moment Envelope"]
["Fuel ( LITERS  )",null,{"$f":"B46*0.75","v":0},{"v":0.325,"d":"0.33"},{"$f":"C46*D46","v":0}," Maximum useable  110 ltr * 0.75 = 82,5 kg"]
["Ramp  Weight      (Max. 750 Kg) ",null,{"$f":"SUM(C45:C46)","v":517}," ",{"$f":"SUM(E45:E46)","v":222},"110LL = 0,72 Kg/Ltr - Euro95 = 0,75 kg/Ltr"]
["TAXI  FUEL",{"$f":"7*0.25","v":1.75},{"$f":"B48*0.75","v":1.3125},0.33,{"$f":"C48*D48","v":{"v":0.43312500000000004,"d":"0"}}," Taxi Fuel Consumption 7 ltr per hour (5kg)"]
["Take-Off  Weight  (Max.750 Kg) ",null,{"$f":"(C47-C48)","v":515.6875}," ",{"$f":"(E47-E48)","v":{"v":221.566875,"d":"222"}},"g    CHECK in Moment Envelope"]
["Trip   FUEL",null,{"$f":"B50*0.75","v":0},0.33,{"$f":"C50*D50","v":0}," Trip Fuel Consumption: 17 ltr per Hour"]
["Landing  Weight",null,{"$f":"C49-C50","v":515.6875}," ",{"$f":"E49-E50","v":{"v":221.566875,"d":"222"}},"¨    CHECK in Moment Envelope"]
[]
["Check latest M&B report in Aircraft ships papers for validity before using computed loadsheet."]
["revision 06/10/2021 ACM"]

{"sheet":"Aquila A210 PH-DHB","index":2,"n_rows":54,"n_cols":9,"rows_kept":54,"merged":[[0,0,28,0],[30,1,30,2],[32,1,32,4],[33,1,33,4],[33,5,33,6],[34,0,34,8],[35,5,35,8],[36,0,36,1],[36,5,36,6],[37,0,37,1],[38,0,38,1],[40,0,40,1],[41,0,41,1],[43,0,43,1],[44,0,44,1],[44,5,44,8],[45,5,45,8],[46,0,46,1],[46,5,46,8],[47,5,47,8],[48,0,48,1],[48,5,48,8],[49,5,49,8],[50,0,50,1],[50,5,50,8],[52,0,52,8],[53,0,53,8]]}
["AQUILA     AT01  PH-DHB"]
{"$rows_empty":29}
["VLIEGTUIG         :","AQUILA  A210",{"$nulls":3},"Date of  FLIGHT :",null,{"$f":"NOW()","v":"2021-10-06T21:36:27.740"}]
[null,"ATO 1-203",{"$nulls":3},"Departure :",null,"EHKD"]
["Registration   : ","PH-DHB",{"$nulls":3},"VIA :"]
[{"$nulls":5},"Destination :"]
[]
[null,null,"Kg","Arm","  M * Kg   ","Address information:"]
["BEW incl. oil and unuseable fuel",null,529.5,"Mtr",233.5,"     Naam",null,"Postcode","Huis Nr"]
["LH Seat PIC (length < 1.75 m )",null,null,0.45,{"$f":"C38*D38","v":0}]
["LH Seat PIC (length > 1.75 m )",null,null,0.59,{"$f":"C39*D39","v":0}]
[]
["RH Seat Pas (length < 1.75 m )",null,null,0.45,{"$f":"C41*D41","v":{"v":0,"d":"0.00"}}]
["RH Seat Pas (lenght > 1.75 m )",null,null,0.59,{"$f":"C42*D42","v":0}]
[]
["baggage Area  1  (max  40 kg )",null,5,{"v":1.3,"d":"1.30"},{"$f":"C44*D44","v":{"v":6.5,"d":"7"}}]
["Zero FUEL Weight",null,{"$f":"SUM(C37:C44)","v":534.5}," ",{"$f":"SUM(E37:E44)","v":240},"p CHECK in Moment Envelope"]
["Fuel ( LITERS  )",null,{"$f":"B46*0.75","v":0},{"v":0.325,"d":"0.33"},{"$f":"C46*D46","v":0}," Maximum useable  110 ltr * 0.75 = 82,5 kg"]
["Ramp  Weight      (Max. 750 Kg) ",null,{"$f":"SUM(C45:C46)","v":534.5}," ",{"$f":"SUM(E45:E46)","v":240},"110LL = 0,72 Kg/Ltr - Euro95 = 0,75 kg/Ltr"]
["TAXI  FUEL",{"$f":"7*0.25","v":1.75},{"$f":"B48*0.75","v":1.3125},0.33,{"$f":"C48*D48","v":{"v":0.43312500000000004,"d":"0"}}," Taxi Fuel Consumption 7 ltr per hour (5kg)"]
["Take-Off  Weight  (Max.750 Kg) ",null,{"$f":"(C47-C48)","v":533.1875}," ",{"$f":"(E47-E48)","v":{"v":239.566875,"d":"240"}},"g    CHECK in Moment Envelope"]
["Trip   FUEL",null,{"$f":"B50*0.75","v":0},0.33,{"$f":"C50*D50","v":0}," Trip Fuel Consumption: 17 ltr per Hour"]
["Landing  Weight",null,{"$f":"C49-C50","v":533.1875}," ",{"$f":"E49-E50","v":{"v":239.566875,"d":"240"}},"¨    CHECK in Moment Envelope"]
[]
["Check latest M&B report in Aircraft ships papers for validity before using computed loadsheet."]
["revision 06/10/2021 ACM"]

{"sheet":"Cessna C172 PH-DHD","index":3,"n_rows":55,"n_cols":9,"rows_kept":55,"merged":[[0,0,28,0],[30,1,30,4],[32,1,32,4],[33,1,33,4],[33,5,33,6],[34,0,34,8],[35,5,35,8],[36,0,36,1],[36,5,36,6],[37,0,37,1],[38,0,38,1],[40,0,40,1],[41,0,41,1],[43,0,43,1],[43,5,43,8],[44,0,44,1],[45,0,45,1],[45,5,45,8],[46,5,46,8],[47,0,47,1],[47,5,47,8],[48,5,48,8],[49,0,49,1],[49,5,49,8],[50,5,50,8],[51,0,51,1],[51,5,51,8],[53,0,53,8],[54,0,54,8]]}
["Cessna 172N Skyhawk  PH-DHD"]
{"$rows_empty":29}
["VLIEGTUIG         :","Cessna C172N Skyhawk",{"$nulls":3},"Date of  FLIGHT :",null,{"$f":"NOW()","v":"2021-10-06T21:36:27.740"}]
[null,"172-69065",{"$nulls":3},"Departure :",null,"EHKD"]
["Registration   : ","PH-DHD",{"$nulls":3},"VIA :"]
[{"$nulls":5},"Destination :"]
[]
[null,null,"Kg","Arm","  M * Kg   ","Address information:"]
["BEW incl. oil and unuseable fuel",null,695.8,"Mtr",767.64,"     Naam",null,"Postcode","Huis Nr"]
["LH Seat PIC (37\")",null,null,0.94,{"$f":"C38*D38","v":0}]
["RH Seat Pas (37\")",null,null,0.94,{"$f":"C39*D39","v":0}]
[]
["LHR Seat Pas (73\")",null,null,1.85,{"$f":"C41*D41","v":{"v":0,"d":"0.00"}}]
["RHR Seat Pas (73\")",null,null,1.85,{"$f":"C42*D42","v":0}]
[]
["baggage Area  1  (max  54 kg )",null,null,2.41,{"$f":"C44*D44","v":0},"Maximum combined baggage Area = 54 kg"]
["baggage Area  2  (max  22 kg )",null,null,3.12,{"$f":"C45*D45","v":0}]
["Zero FUEL Weight",null,{"$f":"SUM(C37:C45)","v":695.8}," ",{"$f":"SUM(E37:E44)","v":{"v":767.64,"d":"768"}},"p CHECK in Moment Envelope"]
["Fuel ( LITERS  )",null,{"$f":"B47*0.72","v":0},{"v":0.325,"d":"0.33"},{"$f":"C47*D47","v":0}," Maximum useable  164 ltr * 0.72 = 118 kg"]
["Ramp  Weight      (Max. 1043Kg) ",null,{"$f":"SUM(C46:C47)","v":695.8}," ",{"$f":"SUM(E46:E47)","v":{"v":767.64,"d":"768"}},"110LL = 0,72 Kg/Ltr"]
["TAXI  FUEL",null,{"$f":"B49*0.72","v":0},0.33,{"$f":"C49*D49","v":0}," Taxi Fuel Consumption 5L  (3,6 kg)"]
["Take-Off  Weight  (Max.1043Kg) ",null,{"$f":"(C48-C49)","v":695.8}," ",{"$f":"(E48-E49)","v":{"v":767.64,"d":"768"}},"g    CHECK in Moment Envelope"]
["Trip   FUEL",null,{"$f":"B51*0.72","v":0},0.33,{"$f":"C51*D51","v":0}," Trip Fuel Consumption: 40 ltr per hour"]
["Landing  Weight",null,{"$f":"C50-C51","v":695.8}," ",{"$f":"E50-E51","v":{"v":767.64,"d":"768"}},"¨    CHECK in Moment Envelope"]
[]
["Check latest M&B report in Aircraft ships papers for validity before using computed loadsheet."]
["revision 06/10/2021 ACM"]

{"sheet":"Instructeurs","index":4,"n_rows":7,"n_cols":3,"rows_kept":7}
["Naam","Gewicht","Lengte"]
["R. den Hartog",85,1.8]
["C. Petrus"]
["P. de Hondt",95,1.9]
["C. Cocheret"]
["B. Sindram",65,1.76]
["J. Mooijman",64,1.75]

{"sheet":"Envelope Aquila A210","index":5,"n_rows":6,"n_cols":4,"rows_kept":6,"hidden":true}
["Normal Category",null,"Utility Category"]
["weight","moment","weight","moment"]
[540,235]
[750,320]
[750,390]
[540,290]

{"sheet":"Envelope Cessna C172","index":6,"n_rows":9,"n_cols":6,"rows_kept":9,"hidden":true}
["Normal Category",null,null,"Utility Category"]
["weight","Arm","moment","weight","Arm","moment"]
[600,0.89,{"$f":"A3*B3","v":534},600,0.89,{"$f":"D3*E3","v":534}]
[885,0.89,{"$f":"A4*B4","v":787.65},885,0.89,{"$f":"D4*E4","v":787.65}]
[1089,1,1089,953,0.93,886.2900000000001]
[1089,1.2,1306.8,953,1.03,981.59]
[885,1.2,1062,996,1.03,1025.88]
[600,1.2,720,600,1.03,618]
[600,0.89,534,600,0.89,534]