Aero AT AT-3 R100

The Aero AT-3 R100 is a model in the AT-3 Series family. It is described here as a Two-seat all-metal low-wing piston single. EASA type-certificate reference: EASA.A.021.

The AT-3 R100 is a two-seat, all-metal low-wing trainer and touring aircraft certified under EASA.A.021. Published operating data identify the Rotax 912 S2 at 100 hp, a 582 kg maximum takeoff mass and a 70 L fuel capacity. The design uses side-by-side seating and fixed tricycle landing gear. Because individual aircraft may have different propellers, avionics and optional equipment, the model page should treat these figures as the certified/base configuration and direct operational loading back to the aircraft-specific AFM and weight-and-balance record.

Standard total fuel: 18.5 U.S. gallons. Published AT-3 R100 operating/specification data identify a 70 L fuel capacity.

Apply the data to an AT-3 R100 only after confirming serial number and approved equipment. Optional propellers, avionics and equipment affect empty mass and balance even when the type-level maximum mass is unchanged.

Maximum takeoff weight: 1,283 lb. Use the approved AT-3 R100 loading schedule for baggage and station limits. Maximum takeoff mass represented here is 582 kg (1,283 lb). Fuel capacity is 70 L (18.5 U.S. gal). Use the actual empty weight and CG for every operational calculation. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific Aero AT-3 R100 calculator.