# Stinson 108 Voyager _ Station Wagon — timothy_j_briggs_stn108-3 # NOT FOR FLIGHT — source fidelity: unreviewed | operational review: none | completeness: full # Source: Stinson/108 Voyager _ Station Wagon/timothy_j_briggs_stn108-3.txt # Rights: licensed # Checklist hash: faa6f6461d4edb6a70cc07a17359f8385d4fd579eb31cd0cda1739054da5012d # Verify against the aircraft's own approved documentation before use. section_id phase criticality section_title item_index item_id type tickable memory_item indent text response condition detail weight_and_balance normal Weight and Balance Calculator Information 0 note no no 0 White blocks are modifiable; colored blocks contain protected formulas and text. weight_and_balance normal Weight and Balance Calculator Information 1 note no no 0 NOTE: All data and formulas are based on the Airplane Owners Manual for the Stinson 108-3 Aircraft. CAA approved 1947. weight_and_balance normal Weight and Balance Calculator Information 2 subtitle no no 0 SETTING UP THE CALCULATOR FOR YOUR AIRCRAFT weight_and_balance normal Weight and Balance Calculator Information 3 action yes no 0 Enter your aircraft's registration number. ENTER weight_and_balance normal Weight and Balance Calculator Information 4 action yes no 0 Enter your aircraft's max weight and fuel capacity into the appropriate blocks. ENTER weight_and_balance normal Weight and Balance Calculator Information 5 action yes no 0 Enter your aircraft's empty weight and moment into the appropriate blocks. ENTER weight_and_balance normal Weight and Balance Calculator Information 6 action yes no 0 Enter oil weight into the block. Moment will be calculated. ENTER weight_and_balance normal Weight and Balance Calculator Information 7 action yes no 0 "Verify ""ARM"" (station) values are accurate for your aircraft. Change as needed to duplicate W & B data for your aircraft. Default values are based on the Aircraft Flight Manual for the 108-3." VERIFY / CHANGE AS NEEDED weight_and_balance normal Weight and Balance Calculator Information 8 note no no 0 Useful load and full fuel payload values will be calculated. weight_and_balance normal Weight and Balance Calculator Information 9 note no no 0 The calculator is now set up for your Stinson weight_and_balance normal Weight and Balance Calculator Information 10 action yes no 0 "Once you have verified that the correct ""ARM"" values are in the blocks, ""Protect"" those blocks from inadvertent changes." PROTECT weight_and_balance normal Weight and Balance Calculator Information 11 note no no 0 "Click this button to protect ""ARM"" values. You will notice the Arm blocks are now blue, meaning they cannot be modified. If you realize after Protecting the Calculator that you made a mistake, hit this button to ""Unprotect"" and make changes." weight_and_balance normal Using the Calculator 0 subtitle no no 0 USING THE CALCULATOR weight_and_balance normal Using the Calculator 1 action yes no 0 "There is a spot for each seat in the aircraft. Enter the weight of each person into the appropriate white block. If a seat is empty, enter 0 or just hit ""delete""." ENTER weight_and_balance normal Using the Calculator 2 action yes no 0 "Station Wagon models with the rear seats removed for cargo loading should use the ""Cabin Cargo"" block for loads placed there. Otherwise, leave it blank." ENTER weight_and_balance normal Using the Calculator 3 action yes no 0 Enter the weight of baggage compartment items into the corresponding white block. ENTER weight_and_balance normal Using the Calculator 4 action yes no 0 Enter the total fuel load in gallons. ENTER weight_and_balance normal Using the Calculator 5 note no no 0 That's it!! The calculator will compute weights, moments, CG point and MAC percentages. It will also plot the CG point on the envelope graph. (you can hit the button to center up the graph on your monitor) weight_and_balance normal Using the Calculator 6 note no no 0 If a CG, weight or MAC limit is exceeded it will alert you with RED TEXT adjacent the exceeded value. weight_and_balance normal Using the Calculator 7 note no no 0 If you have questions or comments, E-mail me at mplstim@bellsouth.net weight_and_balance normal Using the Calculator 8 note no no 0 Good luck and happy landings - Tim Briggs weight_and_balance normal Using the Calculator 9 note no no 0 P.S. I also have similar spreadsheets programmed for: Piper Cherokee, Cessna 172 and Grumman Tiger aircraft. Drop me an E-mail if you'd like one or if you would like one designed for another aircraft. weight_and_balance normal Stinson 108-3 Weight and Balance 0 action yes no 0 AIRCRAFT N6968M weight_and_balance normal Stinson 108-3 Weight and Balance 1 action yes no 0 MAX T/O WEIGHT 2400 weight_and_balance normal Stinson 108-3 Weight and Balance 2 action yes no 0 TOTAL FUEL CAPACITY 46 weight_and_balance normal Stinson 108-3 Weight and Balance 3 action yes no 0 MAX USEFUL LOAD 986 weight_and_balance normal Stinson 108-3 Weight and Balance 4 action yes no 0 FULL FUEL PAYLOAD 710 weight_and_balance normal Stinson 108-3 Weight and Balance 5 note no no 0 All data is based on POH for Aircraft 991PK weight_and_balance normal Stinson 108-3 Weight and Balance 6 action yes no 0 EMPTY WEIGHT 1397 / 11.4 / 15947.5 weight_and_balance normal Stinson 108-3 Weight and Balance 7 action yes no 0 OIL 17 / -49 / -833 weight_and_balance normal Stinson 108-3 Weight and Balance 8 action yes no 0 Front Seats 230 / 230 / 16 / 3680 weight_and_balance normal Stinson 108-3 Weight and Balance 9 action yes no 0 Back Seats 0 / 48 / 0 weight_and_balance normal Stinson 108-3 Weight and Balance 10 action yes no 0 Cabin Cargo (Station Wagons) 42 / 0 weight_and_balance normal Stinson 108-3 Weight and Balance 11 action yes no 0 Rear Baggage 75.5 / 0 weight_and_balance normal Stinson 108-3 Weight and Balance 12 action yes no 0 Fuel (Enter Gals) 46 / 276 / 22 / 6072 weight_and_balance normal Stinson 108-3 Weight and Balance 13 action yes no 0 TOTALS 1920 / 24866.5 weight_and_balance normal Stinson 108-3 Weight and Balance 14 action yes no 0 CG 12.951302083333333 weight_and_balance normal Stinson 108-3 Weight and Balance 15 action yes no 0 %MAC (LIMITS = 18.2-37.5) 22.39874249249249 weight_and_balance normal Stinson 108-3 Weight and Balance 16 subtitle no no 0 UTILITY CAT CG RANGE FIGURES weight_and_balance normal Stinson 108-3 Weight and Balance 17 action yes no 0 Utility Cat CG Range 1300 18.2 / 1750 18.2 / 2000 22.3 / 2000 30 / 1300 30 / 1300 18.2 weight_and_balance normal Stinson 108-3 Weight and Balance 18 subtitle no no 0 NORMAL CAT CG RANGE FIGURES weight_and_balance normal Stinson 108-3 Weight and Balance 19 action yes no 0 Normal Cat CG Range 1300 18.2 / 1750 18.2 / 2400 28.8 / 2400 38.5 / 1300 38.5 / 1300 18.2 Crosswind Calculator normal Crosswind Calculator 0 action yes no 0 RUNWAY HEADING 280 Crosswind Calculator normal Crosswind Calculator 1 action yes no 0 WIND DIRECTION 200 Crosswind Calculator normal Crosswind Calculator 2 action yes no 0 WIND VELOCITY 15 Crosswind Calculator normal Crosswind Calculator 3 action yes no 0 CROSSWIND COMPONENT 12.395277334996043 Crosswind Calculator normal Crosswind Calculator 4 action yes no 0 HEADWIND COMPONENT 2.604722665003956 Crosswind Calculator normal Crosswind Calculator 5 action yes no 0 TAILWIND COMPONENT 0