Credit
Dave1185 · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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At a glance
Measured figures
ULB/MD530F · Length
Single source32 ft 7 in (9.94 m)[source]
F28F · Length
Single sourceConfiguration
| Specification | Boeing AH-6 | Enstrom F-28 |
|---|---|---|
| Type | Light attack / reconnaissance helicopter[source] | Light helicopter[source] |
| National origin | United States[source] | — |
| Manufacturer | Boeing Rotorcraft Systems[source] | Enstrom Helicopter Corporation[source] |
| Status | Under development[source] | — |
| First flight | ULB: September 8, 2004 MELB: September 20, 2006[source] |
29 ft 3 in (8.92 m)[source]
ULB/MD530F · Wingspan
Single source27 ft 4 in (8.33 m)[source]
F28F · Main rotor diameter
Single source32 ft 0 in (9.75 m)[source]
ULB/MD530F · 1 × One Allison 250-C30 turboshaft , 425 shp ( ) takeoff power (derated
Single source1 × One Allison 250-C30 turboshaft , 425 shp (317 kW) takeoff power (derated)[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]
ULB/MD530F · Wing area
Single source587.5 sq ft (54.6 m 2 )[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.
| — |
| Developed from | MD Helicopters MD 500 MD Helicopters MH-6 Little Bird[source] | — |
|---|
| Capacity | 5 total[source] | two passengers[source] |
|---|
| Guns | 2× 12.7 mm (.50 cal) GAU-19 ; or 2× 7.62 mm (.30 cal) M134 Minigun[source] | — |
|---|
| Rockets | 2× LAU-68D/A seven-tube rocket pods firing 2.75 in (70 mm) Hydra 70 or APKWS rocket projectiles[source] | — |
|---|
| Missiles | Anti-tank guided missile: 2 or 4× AGM-114 Hellfire Anti-air missile: 2 or 4× FIM-92 Stinger ATAS for self-defense[source] | — |
|---|
| Manufactured | — | 1965-present[source] |
|---|
| Introduction date | — | 1965[source] |
|---|
| Variants | — | Enstrom TH180 Spitfire Mark I[source] |
|---|
| Developed into | — | Enstrom 480[source] |
|---|
| Main rotor area | — | 804 sq ft (74.7 m 2 ) NACA 0013.5[source] |
|---|
| Country of origin | — | Vereinigte Staaten[source]Country of design · Entwurfsland |
|---|