The Grob G140TP is a four-seat light aircraft built by Grob Aircraft.

The aircraft was presented at the Paris Air Show in 2001 and completed its maiden flight on December 12, 2002. Powered by a Rolls-Royce 250-B17F turboprop engine, the Grob G 140TP is fully aerobatic capable. So far, Grob Aircraft has not decided to resume construction of the G 140. The coarse G 140TP could have been certified in the utility and aerobatic classes, with the utility version being used as a reconnaissance aircraft.^[1]

Data from ^[2]

General characteristics

• Crew: 2
• Capacity: 4
• Length: 8.9 m (29 ft 2 in)
• Wingspan: 10.6 m (34 ft 9 in)
• Height: 2.8 m (9 ft 2 in)
• Wing area: 13.3 m² (143 sq ft)
• Empty weight: 800 kg (1,764 lb)
• Max takeoff weight: 1,500 kg (3,307 lb)
• Fuel capacity: 256 litres (56 imp gal; 68 US gal)
• Powerplant: 1 × Rolls-Royce 250-B17F turboprop engine, 340 kW (460 hp)
• Propellers: 3-bladed

Performance

• Maximum speed: 425 km/h (264 mph, 229 kn)with full flaps
• Range: 1,850 km (1,150 mi, 1,000 nmi)
• g limits: +6/-4G