Credit
Alan Wilson · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Length
Single source8.4 m (27 ft 7 in)[source]
PC-9M · Only the source-declared variant PC-9M · PC-9M
Single sourceConfiguration
| Specification | Grob G 120TP | PC-9M |
|---|---|---|
| Crew | two[source] | one or two pilots[source]Only the source-declared variant PC-9M |
| Type | Trainer[source] | — |
| National origin | Germany[source] | — |
| Manufacturer | Grob Aircraft[source] | Pilatus Aircraft[source]Manufacturer of the source-named PC-9M only; no base PC-9 geometry or variant feature inherited. |
| Status | In production |
10.14 m (33 ft 3 in)[source]Only the source-declared variant PC-9M
Empty; Empty weight
Single sourceMaximum take-off; Max takeoff weight
Single source1,095 kg (2,414 lb)[source]
1,590 kg (3,505 lb)[source]
Empty; PC-9M · Only the source-declared variant PC-9M · PC-9M
Single sourceGross; PC-9M · Only the source-declared variant PC-9M · PC-9M
Single source1,725 kg (3,803 lb)
Cruise; at MCP, 10,000 ft
Single sourceMaximum; Maximum speed
Single source454 km/h (282 mph, 245 kn)[source]
435 km/h (270 mph, 235 kn) (at MCP, 10,000 ft)[source]
Cruise; PC-9M · Only the source-declared variant PC-9M · PC-9M · at 7,620 m (25,000 ft)
Single sourceMaximum; PC-9M · Only the source-declared variant PC-9M · PC-9M
Single sourceat 5,000 ft and 75% power
Single sourceFerry; at 10,000 ft and 45% power
Single source1,070 km (670 mi, 580 nmi) at 5,000 ft and 75% power[source]
1,361 km (846 mi, 735 nmi) at 10,000 ft and 45% power[source]
PC-9M · Only the source-declared variant PC-9M · PC-9M
Single source1,537 km (955 mi, 830 nmi)[source]Only the source-declared variant PC-9M
1 × Rolls-Royce M250-B17F Turboprop aircraft engine
Single source1 × Rolls-Royce M250-B17F Turboprop aircraft engine , 340 kW (456 hp)[source]
PC-9M · Only the source-declared variant PC-9M · PC-9M · 1 × Pratt & Whitney Canada PT6A -62 turboprop
Single sourcePC-9M · Only the source-declared variant PC-9M · PC-9M · flat-rated at 950 shp
Single source1 × Pratt & Whitney Canada PT6A -62 turboprop, 857 kW (1,149 hp) flat-rated at 708 kW (950 shp)[source]Only the source-declared variant PC-9M
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| 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] | — |
|---|
| Developed from | Grob G 120[source] | — |
|---|
| Fuel capacity | 360 litres (79 imp gal; 95 US gal)[source] | — |
|---|
| Propellers | 5-bladed MT Propeller , 2.1 m (6 ft 11 in) diameter[source] | — |
|---|
| Stall speed | 107 km/h (67 mph, 58 kn) (MSL, landing configuration)[source] | 143 km/h (89 mph, 77 kn) EAS flaps and gear up, 128 km/h (80 mph; 69 kn) flaps and gear down[source]Only the source-declared variant PC-9M |
|---|
| g limits | +6/-4G[source] | + 7.0 g to −3.5 g[source]Only the source-declared variant PC-9M |
|---|
| Variant description | — | PC-9M[source]Only the source-declared variant PC-9M This version was introduced in 1997 as the new standard model. It has an enlarged dorsal fin in order to improve longitudinal stability, modified wingroot fairings, stall strips on the leading edges as well as new engine and propeller controls.[source]Only the source-declared variant PC-9M |
|---|
| Take-off distance over 50 ft (15 m) obstacle at sea level | — | 1,280 ft (391 m)[source]Only the source-declared variant PC-9M |
|---|
| Landing distance over 50 ft (15 m) obstacle at sea level | — | 2,295 ft (700 m)[source]Only the source-declared variant PC-9M |
|---|
| Hardpoints | — | seven hardpoints, 3 under each wing, inner two rated at 250 kg (550 lb), outer rated at 110 kg (240 lb)[source]Only the source-declared variant PC-9M Hardpoints: seven hardpoints, 3 under each wing, inner two rated at 250 kg (550 lb), outer rated at 110 kg (240 lb)[source]Only the source-declared variant PC-9M |
|---|
| Country of origin | — | Switzerland[source]Inventory Origin column; table 1, row 21, cell 2; revision 1376580369 Switzerland[source]Inventory Origin column; table 1, row 14, cell 2; revision 1372375479 Switzerland[source]Inventory Origin column; table 2, row 19, cell 2; revision 1365898407 |
|---|
2,350 kg (5,181 lb)[source]Only the source-declared variant PC-9M
3,200 kg (7,055 lb) A view of the interior of the cockpit of a Pilatus PC-9 aircraft.[source]Only the source-declared variant PC-9M