ࡱ> =< \p Richard Dale Ba===5'8X@"1Arial1Arial1Arial1Arial1Arial1@Arial1Arial1Arial1Arial1Arial1 Arial1Arial1Arial1Arial1Arial1Arial1 Arial1Arial1 Arial1 Arial1$Arial"$"#,##0;\-"$"#,##0"$"#,##0;[Red]\-"$"#,##0"$"#,##0.00;\-"$"#,##0.00#"$"#,##0.00;[Red]\-"$"#,##0.005*0_-"$"* #,##0_-;\-"$"* #,##0_-;_-"$"* "-"_-;_-@_-,)'_-* #,##0_-;\-* #,##0_-;_-* "-"_-;_-@_-=,8_-"$"* #,##0.00_-;\-"$"* #,##0.00_-;_-"$"* "-"??_-;_-@_-4+/_-* #,##0.00_-;\-* #,##0.00_-;_-* "-"??_-;_-@_-"$"#,##0_);\("$"#,##0\)!"$"#,##0_);[Red]\("$"#,##0\)""$"#,##0.00_);\("$"#,##0.00\)'""$"#,##0.00_);[Red]\("$"#,##0.00\)72_("$"* #,##0_);_("$"* \(#,##0\);_("$"* "-"_);_(@_).)_(* #,##0_);_(* \(#,##0\);_(* "-"_);_(@_)?:_("$"* #,##0.00_);_("$"* \(#,##0.00\);_("$"* "-"??_);_(@_)61_(* #,##0.00_);_(* \(#,##0.00\);_(* "-"??_);_(@_)0.0                + ) , *          # +    #  #  # #           #/  #8@  $ #8@    #    # # Q#    # *8@@ *8@ *8 @ " " " "4 "0 "4 "4 "4 "4 "4@ "4 @  "8@  "8@  "8@@ " / "< "< "<  !  ` WeightBalanceM Constants,PLimits=  ;1"bZ  3  @@  F<ItemARMMOMENTFuelTake Off WeightMaximum Takeoff WeightThese are preset from the POHNormal CategoryUtility CategoryPage 2-6aft cog at max weightforward cog limit at max weight"forward cog at this weight or lessaft cog at this weight or less)aft cog at lesser weight to fill in chart-forward cog at lesser weight to fill in chart-same as first entry so line joins up on chart Limit (mm) Weight (kg)!Use these values at your own riskRow 2 Passenger LeftRow 2 Passenger RightRow 1 Pilot LeftRow 1 Passenger RightHalfVery LowFullRange at 100 knots (NM)Endurance (mins)Zero Fuel WeightACTUALTFill in only the areas marked with an ORANGE background. Check the W&B on the chartVThis is not an approved weight, balance and edurance chart. See POH and Flight ManualTabs*These were obtained from the Flight Manual0of the Grumman American AA-5B Tiger 21 July 1975Approved 11 May 1979Reserve (minutes)Endurance less reserveTaxi & Engine Runup AllowanceBasic Empty Weight (incl oil) Weight (lb)Baggage (Max 120 lb)Water in Baggage areaFuel Burn Per Hour (gallons)'Taxi & Engine Runup Allowance (gallons)Fuel Weight Per gallon (pounds)Range at 115 knots (NM)Range at 125 knots (NM)Range at 135 knots (NM)GallonssCreated by Richard Dale, Flight Club, Perth Western Australia. Modified into US units by Gil Alexander - Tucson, AZLimit (inches)ARM at Basic Empty WeightYConstants - You should adjust these to suit the characteristics of your aircraft/airfieldFuel (at startup)v1.1AA5A Load CalculatorD(Note: 10.8 is 75%, 9.6 is 65%) - THIS NEEDS TO BE UDPATED FOR AA-5AB I{&Zcc  7  dMbP?_*+%MMinolta Pi35004C 4dXXA4DINU"4#'-" FXX??U} }  }  } I !}  } }  }  m } } } m } }     @  @hh :  /7$ 9 $3 $)). $ $/ 2 32 3)  3  3&  3  3/  30 41 ## @~ 5I@#6 s@ DZ0 7qq\q@ DZZ<# 78m@ D Z# 7Kh?x@ dD <# 7i/{@ sD <# 7^BO~@ }D <#8^@  D <  ) -  @~ 5I@#6r@ DZ0 788q@ DZZ<# 7pqgl@ D Z 7^Bw@    dL < 7A{ %8{@    sL < 7}@    }L <8@(  L < (,@Z,T@Z [@   LL A~ 9H@#:r@ DZ0 ;qQp@ DZZ<# ;88k@ D Z ;/v@   ;Khy@   ;{ %#|@  <c~@(  %g@*@@ @~ 5F@#6p@ DZ0 788n@ DZZ<# 788h@ D Z 7g/t@   7Kw@   7A{ %y@  8 |@(  %Y@*@@ @~ 5D@#6n@ DZ0 7TUUUUk@ DZZ<# 7TUUUUue@ D Z 7qq@   7qqt@   788Zv@  8#x@(  %f@*_@&@  A!~ 9B@#:k@ DZ0 ;h@ DZZ<# ;_c@ D Z ;TUUUU%p@   ;TUUUUr@   ;.t@  <u@(  %@`@*_@@  @~ 5A@#6@j@ DZ0 7qqg@ DZZ<# 7qqa@ D Z 7m@   7 %@# 6f@ D Z0 798#d@ D ZZ<# 7rq]@  D Z 7 %0h@   7^B{k@   7Lh/@   7K@@  8B@( 0 B~ 9 @#:H@ DZ0 ;qqC@ DZZ<# ; qq D Z >%^$  # >^B{ m' sD < >l/v)  ?+(  0@ Z A0,@A+DD  OVERWEIGHT B OVERWEIGHT &!'C0,-DZ   UNBALANCED B UNBALANCED (~ CD@#Dn@ DZ0 ETUUUUk@ DZZ<# ETUUUUue@ D Z Eqq@  # E78s@ nD <# ETUUUUuu@ xD <#Fpq?w@  D <.gfR]]g]]]x  4>&(  p  6 ,>?(].  MAdobe PDFS odXXLetterPRIV ''''0\KhCDk0EBDAStandard" dXX??3` #%` #%` v ` D ` D` a*` L)` 1PH 0(  ?3dQ!23 33>  ,f  ,@"B  `4 3Q  Normal LimitsQr ; Q ; Q3_  NM   d4E4 3Q  Utility LimitsQr ;Q ;Q3_ " NM  ""d4E4 3Q .Empty Fuel to TakeoffQr): :Q+#): :::Q3_ 3< NM  3< d 4E4D$% MP(3O&Q4$% MP(3O&Q4FA,^ 3OVJl 3*T@@W@??T@N" &! M43*p@@Y@" &! 4%  3Ov&Q 0Centre of Gravity (in)'4% g) Z3Ok&Q "Weight (pounds)'4523 O ,43d" o R hv3Ol L &% M*3O& Q423 M NM4444% 7o(MZ3O@& Q 2Centre of Gravity Chart'4% 5@3O &Q'4% 5@3O &Q'4% @3O& Q'44e@T@@T@ffffffU@33333sT@ W@U@ W@U@ W@U@@T@@T@@T@@T@eЛ@Л@0@@0@@0@Л@0@0@0@0@Л@Л@e ~vB  <D jJ  ']`1>@  7ggh/h    GNO  dMbP?_*+%"??U} m)  6 -~ ? %~ F@ ,~ @ ; .~ @ (~ ,@ G5~ ,T@,n*>@7  #PV W  dMbP?_*+%"??U}  } } %#                " # $  ,   4 ) +@T@Л@   +@0@   + W@0@   + W@0@    + W@0@ +@T@0@ +@T@Л@  ! ! ! ! ! +@T@Л@  !+@@  !+U@@  !+U@Л@  !+U@0@  !+@T@0@  !+@T@Л@  !!:v$$$.$.$2222222" ",,">@7 Oh+'0HPh Richard DaleRichard DaleMicrosoft Excel@8C@T6 @SU,՜.+,0$ PXl t|  daytraderHQG WeightBalance ConstantsLimitsWeightBalance!Print_Area  Worksheets Named Ranges  !"#$%&'()*+-./012356789:;Root Entry FWorkbookKWSummaryInformation(,DocumentSummaryInformation84