Sean Parsons

Tecnam P2006T — Weight & Balance

Imperial units (lb · ft · ft·lb). Fuel at 6 lb/USG.

Aircraft Settings

MTOW Take-off / landing limit

Variant

MTOW (lb)

Most Tecnam P2006T aircraft are certified to 2601 lb (1180 kg). Some upgraded MkII airframes are certified to 2712 lb (1230 kg). Check your aircraft’s POH/registration. Max landing weight is assumed equal to MTOW.

Stations

Basic Empty Weight From your aircraft’s current W&B sheet

Weight (lb)

Arm (ft)

Moment (ft·lb)

Pilot + Co-Pilot Arm = −2.973 ft

Weight (lb)

Arm (ft)

Moment (ft·lb)

Rear Passengers Arm = 0.345 ft

Weight (lb)

Arm (ft)

Moment (ft·lb)

Cockpit Baggage Max 176 lb · Arm = 3.895 ft

Weight (lb)

Arm (ft)

Moment (ft·lb)

Fuel (Main Tanks) Max 308 lb (51.33 USG) · 6 lb/USG · Arm = 2.450 ft

Fuel (USG)

Weight (lb)

Moment (ft·lb)

Totals

Zero Fuel Max 2524 lb

Weight (lb)

CG (ft)

Moment (ft·lb)

Take-Off Max 2601 lb (1180 kg)

Weight (lb)

CG (ft)

Moment (ft·lb)

Zero Fuel Wt

— lb

Takeoff Wt

— lb

Takeoff CG

— ft

Status

—

Limits Check

Enter weights above to begin.

W&B Diagram

Your loading 16.5% MAC (fwd) 23% MAC 31% MAC (aft)

Styled after the W&B diagram in the Sharper Edge P2006T supplement. Diagonal MAC lines and MTOW (1180 kg / 2601 lb) shown. Always verify against the W&B section of your aircraft’s current POH before flight.

Fuel Converter

Liters (L)

US Gallons (USG)

1 USG = 3.78541 L

P2006T main tanks hold 51.33 USG (194.4 L) usable. Fuel weight assumed 6 lb/USG.

Personal flight-planning aid. Not a substitute for the POH. Verify all results against your aircraft’s current weight and balance documentation.