Weight & Balance
| Item | Gal | Weight | Arm | Moment |
|---|---|---|---|---|
| Aircraft BEW | ||||
| Pilot/Co-pilot | ||||
| Back Seat | ||||
| Baggage 1 | ||||
| Baggage 2 | ||||
| TOTAL - ZERO FUEL | ||||
| Fuel | ||||
| Subtract Taxi/Runup | ||||
| TAKEOFF WEIGHT | ||||
| Subtract Fuel Used | ||||
| LANDING WEIGHT |
Takeoff/Landing Distances
| 'Drome | RWY | LEN | HWC | XWC | PALT | TEMP | 50' Takeoff | 50' Land |
|---|---|---|---|---|---|---|---|---|
Weight in pounds, Arm in inches. Aircraft
BEW and Arm from recorded weight and
balance. POH/AFM for other stations. Fuel weight
is Gal(lons) × 6.
TOTAL = Sum Weight, Moment.
CG = (Moment
× 1000) ÷ Weight.
Check envelope with POH/AFM loading charts.
Calculate Taxi/Runup for all takeoffs en route.
2016-06-01 (2016-10-28) / jrlf / Derived from Island Air Flight Schoool VFR Navigation Log form.
Fuel
| TAXI/RUNUP | ||
|---|---|---|
| ENROUTE | ||
| RESERVE | D / N | |
| FUDGE | % | |
| Required | Gallons | |
| Pounds | ||
| Start | Gallons | |
| Pounds | ||
| Used | Gallons | |
| Pounds | ||
| Remaining | Gallons | |
| Pounds | ||