01PA-28-161
Aircraft
Set the baseline
Operating category
Utility selection clears rear seats and baggage.
Piper · PA-28-161 · Warrior II
Flight Balance
Digital load sheet · POH Report VB-1180 profile
Know where the airplane sits
before it leaves the ramp.
POH Report VB-1180 profile · 2440 lb maximum
02
Payload
Build the cabin load
Front seatsStation 80.5 in
Rear seatsStation 118.1 in
Baggage compartmentStation 142.8 in · 200 lb max
03Station 95.0 in
Fuel plan
Track ramp to landing
Calculation detail
Moment ledger
Moment = weight × arm. CG = total moment ÷ total weight. Values are shown in imperial units.
| Load item | Weight (lb) | Arm (in) | Moment / 1000 (lb·in) |
|---|---|---|---|
| Basic empty aircraft | 1500.0 | 85.9 | 128.85 |
| Pilot | 180.0 | 80.5 | 14.49 |
| Front passenger | 0.0 | 80.5 | 0.00 |
| Rear left | 140.0 | 118.1 | 16.53 |
| Rear right | 0.0 | 118.1 | 0.00 |
| Fuel at ramp | 216.0 | 95.0 | 20.52 |
| Baggage compartment | 20.0 | 142.8 | 2.86 |
| Ramp total | 2056.0 | 89.13 | 183.25 |
| Less taxi fuel | −7.2 | 95.0 | −0.68 |
| Takeoff total | 2048.8 | 89.11 | 182.57 |
| Less planned trip fuel | −108.0 | 95.0 | −10.26 |
| Landing total | 1940.8 | 88.78 | 172.31 |