Credit
e2a2j · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
T-34C · Length
Single source28 ft 8 + 1 ⁄ 2 in (8.750 m)[source]Only the source-declared variant T-34C Turbo-Mentor
Length
Single sourceConfiguration
| Specification | T-34C Turbo-Mentor | Grob G 120TP |
|---|---|---|
| Variant description | T-34C Turbo-Mentor[source]Only the source-declared variant T-34C Turbo-Mentor Two-seat primary trainer, fitted with a turboprop engine.[source]Only the source-declared variant T-34C Turbo-Mentor | — |
| Fuel capacity | 130 US gal (110 imp gal; 490 L)[source]Only the source-declared variant T-34C Turbo-Mentor | 360 litres (79 imp gal; 95 US gal)[source] |
| Propellers | 3-bladed Hartzell constant-speed[source]Only the source-declared variant T-34C Turbo-Mentor | 5-bladed MT Propeller , 2.1 m (6 ft 11 in) diameter[source] |
8.4 m (27 ft 7 in)[source]
Empty; T-34C · Empty weight
Single sourceMaximum take-off; T-34C · Max takeoff weight
Single source2,960 lb (1,343 kg)[source]Only the source-declared variant T-34C Turbo-Mentor
4,300 lb (1,950 kg) (T-34C-1 weapons trainer 5,500 lb (2,500 kg))[source]Only the source-declared variant T-34C Turbo-Mentor
Empty; Empty weight
Single sourceMaximum take-off; Max takeoff weight
Single sourceCruise; T-34C · at 17,000 ft (5,200 m) (max cruise)
Single source214 kn (246 mph, 396 km/h) at 17,000 ft (5,200 m) (max cruise)[source]Only the source-declared variant T-34C Turbo-Mentor
T-34C · at 180 kn (210 mph; 330 km/h) and 20,000 ft (6,100 m)
Single source708 nmi (815 mi, 1,311 km) at 180 kn (210 mph; 330 km/h) and 20,000 ft (6,100 m)[source]Only the source-declared variant T-34C Turbo-Mentor
T-34C · 1 × Pratt & Whitney Canada PT6 A-25 turboprop , 550 shp (
Single source1 × Pratt & Whitney Canada PT6 A-25 turboprop , 550 shp (410 kW)[source]Only the source-declared variant T-34C Turbo-Mentor
1 × Rolls-Royce M250-B17F Turboprop aircraft engine
Single source1 × Rolls-Royce M250-B17F Turboprop aircraft engine , 340 kW (456 hp)[source]
at 10,000 ft and maximum endurance power setting
Single source6 hours at 10,000 ft and maximum endurance power setting[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Stall speed | 53 kn (61 mph, 98 km/h) (flaps down, power off)[source]Only the source-declared variant T-34C Turbo-Mentor | 107 km/h (67 mph, 58 kn) (MSL, landing configuration)[source] |
|---|
| Never exceed speed | 280 kn (320 mph, 520 km/h)[source]Only the source-declared variant T-34C Turbo-Mentor | — |
|---|
| g limits | +6, -3[source]Only the source-declared variant T-34C Turbo-Mentor | +6/-4G[source] |
|---|
| Hardpoints | 4 with a capacity of 600 lb (272 kg) inner, 300 lb (136 kg) outer, 1,200 lb (544 kg) total[source]Only the source-declared variant T-34C Turbo-Mentor | — |
|---|
| Manufacturer | Beechcraft[source]Manufacturer of the explicitly named T-34C Turbo-Mentor only. Beechcraft[source]T-34C Turbo-Mentor | Grob Aircraft[source] |
|---|
| Country of origin | USA[source]T-34C Turbo-Mentor | — |
|---|
| Type | — | Trainer[source] |
|---|
| National origin | — | Germany[source] |
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| Status | — | In production[source] |
|---|
| Primary users | — | Indonesian Air Force Mexican Air Force Bangladesh Air Force UK Military Flying Training System Swedish Air Force[source] |
|---|
| Manufactured | — | 2010-present[source] |
|---|
| Introduction date | — | 2013[source] |
|---|
| First flight | — | 2010[source] |
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| Developed from | — | Grob G 120[source] |
|---|