Piper PA-28-235 Cherokee — Eric_Duensing_pa28_235_wb NOT FOR FLIGHT — source fidelity: unreviewed | operational review: none | completeness: full Source: Piper/PA-28-235 Cherokee/Eric_Duensing_pa28_235_wb.txt Rights: licensed Checklist hash: cbd96a36ddb4178466ecd707449bcae23d809111c7119fb137a0e54c8e14c47c Verify against the aircraft's own approved documentation before use. ======================================================================== WEIGHT & BALANCE ---------------- ** NOTE: INSTRUCTIONS: FILL OUT ALL NUMBERS IN BLUE. BLACK NUMBERS GIVE YOU THE ANSWER. ** NOTE: WEIGHT AND BALANCE — DO NOT DELETE THE DATA IN RED ITEM / WEIGHT / ARM / MOMENT [ ] Basic Empty Weight ............. 1530.76 lb, Arm 83.11, Moment 127220 [ ] Pilot ................................ 200 lb, Arm 88.9, Moment 17780 [ ] Co-Pilot ................................... 0 lb, Arm 88.9, Moment 0 [ ] Rear Seats ................................ 0 lb, Arm 118.5, Moment 0 [ ] Baggage (200 lb max) ........................ 0 lb, Arm 142, Moment 0 [ ] Fuel (in gallons) .............. 84 gal, 504 lb, Arm 95, Moment 47880 [ ] TAKEOFF ... Weight 2234.76 lb, C.G. 86.30904437165512 in, Moment 192880 [ ] LANDING ... Weight 1808.7600000000002 lb, C.G. 84.26214644286692 in, Moment 152410 [ ] MAX GROSS WEIGHT ............................................ 2900 lb C.G. VS WEIGHT LIMITS [ ] Takeoff C.G.: 86.30904437165512 in at 2234.76 lb [ ] Landing C.G.: 84.26214644286692 in at 1808.7600000000002 lb [ ] Normal: 83 in / 1400 lb, 83 in / 2100 lb, 91.55 in / 2900 lb, 93 in / 2900 lb [ ] Utility: 83 in / 1400 lb, 83 in / 1950 lb, 83.7 in / 2020 lb, 93 in / 2020 lb, 93 in / 1400 lb [ ] Fuel (Taxi, Climb) ............................................ 1 gal [ ] Fuel Burn ................................................. 14 gal/hr [ ] Planned Flight Time ........................................... 5 hrs [ ] Estimated Fuel Used .......................................... 71 gal [ ] Estimated Fuel Remaining ..................................... 13 gal [ ] Estimated Time Remaining ..................... 0.9285714285714286 hrs COMPUTATIONS ------------ TEMPERATURE [ ] Enter oC: ........................................................ 29 [ ] Get oF: ........................................................ 84.2 DENSITY ALTITUDE [ ] Field Elevation — Departure ..................................... 295 [ ] Field Elevation — Arrival ....................................... 295 [ ] Altimeter Setting — Departure ................................. 29.95 [ ] Altimeter Setting — Arrival ................................... 30.21 [ ] Temp, deg F — Departure .......................................... 86 [ ] Temp, deg F — Arrival ............................................ 86 [ ] Std Temp at Field — Departure .................................... 56 [ ] Std Temp at Field — Arrival .................................. 40.268 [ ] Pressure Altitude — Departure ..................... 324.9999999999976 [ ] Pressure Altitude — Arrival ....................... 584.9999999999991 [ ] Density Altitude — Departure ..................... 2324.9999999999977 [ ] Density Altitude — Arrival ....................... 3633.7999999999993 WEIGHT-ADJUSTED V-SPEEDS (KIAS) [ ] Vso — MGW ........................................................ 60 [ ] Vso — Your weight .................................. 52.6705309218182 [ ] 1.2 x Vso — MGW .................................................. 72 [ ] 1.2 x Vso — Your weight .......................... 63.204637106181835 [ ] 1.3 x Vso — MGW .................................................. 78 [ ] 1.3 x Vso — Your weight ........................... 68.47169019836366 [ ] Vx — MGW ......................................................... 90 [ ] Vx — Your weight ................................... 79.0057963827273 [ ] Best glide — MGW ................................................. 80 [ ] Best glide — Your weight .......................... 70.22737456242426 [ ] Vy — MGW ........................................................ 100 [ ] Vy — Your weight .................................. 87.78421820303033 [ ] Vfe — MGW ....................................................... 115 [ ] Vfe — Your weight ................................ 100.95185093348488 [ ] Va — MGW ........................................................ 111 [ ] Va — Your weight .................................. 97.44048220536367 [ ] Vno — MGW ....................................................... 126 [ ] Vno — Your weight ................................ 110.60811493581821 [ ] Vne — MGW ....................................................... 166 [ ] Vne — Your weight ................................ 145.72180221703036 OLD W&B ------- [ ] Basic Empty Weight .... Weight 1530.76, Arm 83.11, Moment 127221.4636 [ ] Pilot ............................................................. 0 [ ] Front Seat Passenger .............................................. 0 [ ] Rear Seat Passenger(s) ............................................ 0 [ ] Baggage (200lb Max) ............................................... 0 [ ] Fuel (gals x 6lbs.) .............................................. 84 [ ] Total ....................................................... 1614.76 [ ] Total Moment / Total Weight = Center of Gravity in Inches [ ] Result ............ 135350.1436 / 1614.76 = 83.82059476330849 (83-93)