Credit
Adrian · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
AW169 · Length
Single source14.645 m (48 ft 1 in)[source]
F28F · Length
Single sourceConfiguration
| Specification | AgustaWestland AW169 | Enstrom F-28 |
|---|---|---|
| Crew | 1 or 2[source] | one[source] |
| Type | Helicopter[source] | Light helicopter[source] |
| National origin | Italy[source] | — |
| Manufacturer | Leonardo S.p.A. AgustaWestland[source] | Enstrom Helicopter Corporation[source] |
| Status |
29 ft 3 in (8.92 m)[source]
AW169 · Horizontal stab
Single sourceAW169 · Width
Single source2.530 m (8 ft 4 in) Horizontal stab 3.205 m[source]
AW169 · 2 × Pratt & Whitney PW210A turboshaft with FADEC ( 1,000 shp class each
Single source2 × Pratt & Whitney PW210A turboshaft with FADEC (735 kW, 1,000 shp class each)[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 · Service ceiling
Single source12,000 ft (3,700 m)[source]
F28F · 1,450 ft/min (
Single source1,450 ft/min (7.4 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Active service[source] |
| — |
| Number built | 170+ as of October 2023[source] | — |
|---|
| Manufactured | 2015–present[source] | 1965-present[source] |
|---|
| Introduction date | 2015[source] | 1965[source] |
|---|
| First flight | 10 May 2012[source] | — |
|---|
| Capacity | 8 to 12 passengers, plus 250 kg (551 lbs) baggage and cargo; or 1 stretcher, plus 7 medical attendants; or 2 stretchers, plus 5 medical attendants[source] | two passengers[source] |
|---|
| Never exceed speed | 306 km/h (190 mph, 165 kn) Power on with both engines operative[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 |
|---|