Grob G 140TP
(Redirected from Grob G 140)
| Grob G 140TP | |
|---|---|
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| |
| Role | Trainer |
| National origin | Germany |
| Manufacturer | Grob Aircraft |
| First flight | 12 December 2002 |
| Status | Active in production |
| Produced | 2003-present |
The Grob G140TP is a four-seat light aircraft built by Grob Aircraft.
Development
[edit]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]
Specifications (G 140TP)
[edit]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
References
[edit]- ^ Coarse test flow G 140TP. In: European Business Air News . May 3, 2003- Retrieved on November 20, 2011 (English): "Following its successful first flight on December 12, 2002, flight tests of the four-seat turboprop G 140TP have begun at Grob Aerospace."
- ^ "Grob G 140 TP performance and specifications". Retrieved 16 February 2017.
Further reading
[edit]
Wikimedia Commons has media related to Grob G 140.
- Grob G 115,120 and 140 Information brochure and Technical Datasheet (Grob Aerospace Sales Department, 2004)