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Measured figures
G 115E · Length
Single source7.79 m (25 ft 7 in)[source]
G 115E · Wingspan
Single source10.00 m (32 ft 10 in)[source]
G 115E · Height
Single source2.82 m (9 ft 3 in)[source]
G 115E · 45% power at FL 80, 45 min reserves
Single source1,150 km (710 mi, 620 nmi) (45% power at FL 80, 45 min reserves)[source]
G 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]
G 115E · Wing area
Single source12.21 m 2 (131.4 sq ft)[source]
G 115E · Service ceiling
Single source6,095 m (20,000 ft)[source]
G 115E · 1,050 ft/min
Single source5.3 m/s (1,050 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Grob G 115 | L-15Z |
|---|---|---|
| Type | Basic trainer[source] | — |
| Manufacturer | Grob Aircraft[source] | — |
| Status | active[source] | — |
| Primary users | Royal Air Force Egyptian Air Force Finnish Air Force Royal Navy Army Air Corps (UK)[source] | — |
| Manufactured | 1985–present[source] | — |
| Introduction date | 1999[source] | — |
| First flight | November 1985[source] | — |
| Fuel capacity | 143 L (31 imp gal; 38 US gal) usable[source] | — |
| Aspect ratio | 8.2:1[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] | — |
| Stall speed | 91 km/h (57 mph, 49 kn) (60 degree flap)[source] | — |
| Never exceed speed | 341 km/h (212 mph, 184 kn)[source] | — |
| g limits | + 6.0/ - 3.0[source] | — |
| Country of origin | Deutschland[source]Country of design · Entwurfsland | — |
| Variant description | — | L-15Z : Designation of L-15 advanced fighter trainer in Zambian Air Force service.[source]Only the source-declared variant L-15Z |