Credit
Tim Felce · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
SA 341G · including rotor
Single source11.97 m (39 ft 3 in) including rotor[source]
F28F · Length
Configuration
| Specification | Aérospatiale Gazelle | Enstrom F-28 |
|---|---|---|
| Crew | 1 or 2[source] | one[source] |
| Type | Utility helicopter / Armed helicopter[source] | Light helicopter[source] |
| National origin | France[source] | — |
| Manufacturer | Sud Aviation , later Aérospatiale[source] | Enstrom Helicopter Corporation[source] |
29 ft 3 in (8.92 m)[source]
Cruise; SA 341G · max cruise at sea level
Single sourceMaximum; SA 341G · at sea level
Single source310 km/h (190 mph, 170 kn) at sea level[source]
264 km/h (164 mph, 143 kn) max cruise at sea level[source]
Cruise; F28F · econ cruise
Single sourceMaximum; F28F · Maximum speed
Single sourceSA 341G · 1 × Turbomeca Astazou IIIA turboshaft
Single source1 × Turbomeca Astazou IIIA turboshaft , 440 kW (590 hp)[source]
F28F · 1 × Lycoming HIO-360-F1AD four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engine
Single source1 × Lycoming HIO-360-F1AD four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engine, 225 hp (168 kW)[source]
F28F · Endurance
Single source3 hr 30 min[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Built by |
|---|
ABHCO SOKO Westland Aircraft[source] |
| — |
| Status | In service[source] | — |
|---|
| Primary users | French Army British Army (retired) Egyptian Air Force Lebanese Air Force[source] | — |
|---|
| Number built | 1,700[source] | — |
|---|
| Manufactured | 1967–1996[source] | 1965-present[source] |
|---|
| Introduction date | 1973[source] | 1965[source] |
|---|
| First flight | 7 April 1967 (SA.340)[source] | — |
|---|
| Developed from | Aérospatiale Alouette III[source] | — |
|---|
| Capacity | up to 3 or 4 passengers[source] | two passengers[source] |
|---|
| Fuel capacity | 735 L (194 US gal; 162 imp gal)[source] | — |
|---|
| Guns | Two forward-firing 7.62 mm (0.300 in) machine-guns (optional)[source] | — |
|---|
| Oil | 13 L (3.4 US gal; 2.9 imp gal) for engine, 3.5 L (0.92 US gal; 0.77 imp gal) for gearbox[source] | — |
|---|
| Main rotor area | 86.5 m 2 (931 sq ft) NACA 0012 section[source] | 804 sq ft (74.7 m 2 ) NACA 0013.5[source] |
|---|
| economical cruise speed | 233 km/h (145 mph; 126 kn)[source] | — |
|---|
| Range with pilot and 500 kg (1,100 lb) | 233 km (145 mi; 126 nmi)[source] | — |
|---|
| Hover ceiling IGE | 2,850 m (9,350 ft)[source] | — |
|---|
| Hover ceiling OGE | 2,000 m (6,600 ft)[source] | — |
|---|
| Disk loading | 19.5 kg/m 2 (4.0 lb/sq ft)[source] | — |
|---|
| Rockets | Matra or Brandt 70 mm (2.75 in) or 68 mm (2.68 in) rocket pods (optional)[source] | — |
|---|
| Missiles | Four AS.11 or two AS.12 wire-guided missiles; four or six Euromissile HOT (optional)[source] | — |
|---|
| Variants | — | Enstrom TH180 Spitfire Mark I[source] |
|---|
| Developed into | — | Enstrom 480[source] |
|---|
| Country of origin | — | Vereinigte Staaten[source]Country of design · Entwurfsland |
|---|
| Reported operators |
| — |
|---|