Credit
MilborneOne · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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At a glance
Measured figures
Cessna 152 · Length
Single source24 ft 1 in (7.34 m)[source]
G 115E · Length
Single sourceConfiguration
| Specification | Cessna 152 | Grob G 115 |
|---|---|---|
| Type | Basic trainer , GA private aircraft[source] | Basic trainer[source] |
| National origin | United States[source] | — |
| Manufacturer | Cessna[source] | Grob Aircraft[source] |
| Primary users | Mexican Navy Bangladesh Army Bolivian Air Force[source] | Royal Air Force Egyptian Air Force Finnish Air Force Royal Navy Army Air Corps (UK)[source] |
7.79 m (25 ft 7 in)[source]
Cessna 152 · Range
Single sourceFerry; Cessna 152 · with long-range tanks
Single source477 mi (768 km, 415 nmi)[source]
795 mi (1,279 km, 691 nmi) with long-range tanks[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]
Cessna 152 · 1 × Lycoming O-235 -L2C flat-4 engine
Single source1 × Lycoming O-235 -L2C flat-4 engine , 110 hp (82 kW)[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]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 7,584[source] | — |
|---|
| Manufactured | 1977–1985[source] | 1985–present[source] |
|---|
| Introduction date | 1977[source] | 1999[source] |
|---|
| Developed from | Cessna 150[source] | — |
|---|
| Capacity | one passenger (plus two children not exceeding 120 lb (54 kg) on optional baggage compartment bench seat)[source] | — |
|---|
| Propellers | 2-bladed fixed pitch, 69 inches (175 cm) McCauley or 72 in (183 cm) Sensenich propeller[source] | 3-bladed Hoffmann HO-V343K-V/183GY Constant-speed propeller , 1.83 m (6 ft 0 in) diameter[source] |
|---|
| Stall speed | 49 mph (79 km/h, 43 kn) (power off, flaps down)[source] | 91 km/h (57 mph, 49 kn) (60 degree flap)[source] |
|---|
| Status | — | active[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] |
|---|
| 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 |
|---|