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
G 115E · Length
Single source7.79 m (25 ft 7 in)[source]
Lasta 95N · Length
Single sourceConfiguration
| Specification | Grob G 115 | Utva Lasta |
|---|---|---|
| Type | Basic trainer[source] | Trainer aircraft[source] |
| Manufacturer | Grob Aircraft[source] | Utva Aviation Industry[source] |
| Status | active[source] | In service[source] |
| Primary users | Royal Air Force Egyptian Air Force Finnish Air Force Royal Navy Army Air Corps (UK)[source] | Serbian Air Force Iraqi Air Force[source] |
7.965 m (26 ft 2 in)[source]
Cruise; G 115E · long range cruising speed
Single sourceMaximum; G 115E · Maximum speed
Single source250 km/h (160 mph, 130 kn)[source]
178 km/h (111 mph, 96 kn) (long range cruising speed)[source]
Cruise; Lasta 95N · Cruise speed
Single sourceMaximum; Lasta 95N · Maximum speed
Single sourceG 115E · 1 × Lycoming AEIO-360-B1F/B 4-cylinder air-cooled horizontally-opposed piston engine
Single source1 × Lycoming AEIO-360-B1F/B 4-cylinder air-cooled horizontally-opposed piston engine, 130 kW (180 hp)[source]
Lasta 95N · 1 × Lycoming AEIO-580-B1A 6-cyl. air-cooled horizontally-opposed piston engine
Single source1 × Lycoming AEIO-580-B1A 6-cyl. air-cooled horizontally-opposed piston engine, 232 kW (311 hp)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1985–present[source] | — |
|---|
| Introduction date | 1999[source] | 2010[source] |
|---|
| First flight | November 1985[source] | Lasta 1 prototype: 2 September 1985 Lasta 95: 26 February 2009[source] |
|---|
| Fuel capacity | 143 L (31 imp gal; 38 US gal) usable[source] | — |
|---|
| Aspect ratio | 8.2:1[source] | 6.3[source] |
|---|
| Airfoil | Eppler 696[source] | — |
|---|
| Propellers | 3-bladed Hoffmann HO-V343K-V/183GY Constant-speed propeller , 1.83 m (6 ft 0 in) diameter[source] | 2-bladed HARTZELL HC-C2YR-4CF/FC 8475-8 constant speed propeller, 1.98 m (6 ft 6 in) diameter[source] |
|---|
| Stall speed | 91 km/h (57 mph, 49 kn) (60 degree flap)[source] | 95 km/h (59 mph, 51 kn)[source] |
|---|
| Never exceed speed | 341 km/h (212 mph, 184 kn)[source] | 425 km/h (264 mph, 229 kn)[source] |
|---|
| g limits | + 6.0/ - 3.0[source] | +6 -3 g[source] |
|---|
| Country of origin | Deutschland[source]Country of design · Entwurfsland | Serbia[source] |
|---|
| Designer | — | Military Technical Institute[source] |
|---|
| Number built | — | 37[source] |
|---|
| Hardpoints | — | 2 with a capacity of 100 kg (220 lb) bombs, 7.62 mm (0.300 in) or 12.7 mm (0.500 in) calibre machine-gun pods or 57 mm (2.244 in) rocket pods (7 rockets each)[source] |
|---|
| Reported operators | — |
|
|---|
Maximum take-off; Lasta 95N · unarmed
Single source