Credit
Dmitry Mottl · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
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BMilitary transport & logistics
Measured figures
BA609 · Length
Single source13.4 m (44 ft 0 in)[source]
Configuration
| Specification | Leonardo AW609 | Suzuki DR-Z400 |
|---|---|---|
| Type | VTOL corporate transport[source] | — |
| National origin | United States / Italy[source] | — |
| Manufacturer | Bell/Agusta Aerospace AgustaWestland Leonardo S.p.A.[source] | Suzuki[source] |
| Status | Final Certification Testing[source] | — |
| Introduction date | Late 2020s (expected)[source] | — |
BA609 · rotors turning
Single source18.3 m (60 ft 0 in) rotors turning[source]
BA609 · distance between rotor centres
Single source10 m (32 ft 10 in) (distance between rotor centres)[source]
BA609 · 2 ×
Single source2 × 7.9 m (25 ft 11 in)[source]
BA609 · to top of fin
Single source4.6 m (15 ft 1 in) to top of fin[source]
Empty; BA609 · Empty weight
Single sourceMaximum take-off; BA609 · Cabin height: 4 ft 8 in (1.42 m) Cabin width: 4 ft 10 in (1.47 m) Cabin length: 13 ft 5 in (4.09 m)
Single source4,765 kg (10,505 lb)[source]
7,620 kg (16,799 lb) Cabin height: 4 ft 8 in (1.42 m) Cabin width: 4 ft 10 in (1.47 m) Cabin length: 13 ft 5 in (4.09 m)[source]
(S version) ( wet )
Single source144 kg (317 lb) (S version) ( wet )[source]
BA609 · with normal fuel
Single source3 hours with normal fuel[source]
BA609 · * Hover Ceiling out of Ground Effect (HOGE)
Single sourceBA609 · Service ceiling
Single source7,620 m (25,000 ft) * Hover Ceiling out of Ground Effect (HOGE) : 1,525 m (5,003 ft)[source]
BA609 · (1,499.2 ft/min) at sea level
Single source7.616 m/s (1,499.2 ft/min) at sea level[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| First flight | 7 March 2003[source] | — |
|---|
| Capacity | 6 to 9 passengers or 5,500 lb (2,500 kg) payload[source] | — |
|---|
| Cabin height | 4 ft 8 in (1.42 m)[source] | — |
|---|
| Cabin width | 4 ft 10 in (1.47 m)[source] | — |
|---|
| Cabin length | 13 ft 5 in (4.09 m)[source] | — |
|---|
| Main rotor area | 49 m 2 (530 sq ft) each[source] | — |
|---|
| g limits | +3.1 −1[source] | — |
|---|
| Disk loading | 77.4 kg/m 2 (15.9 lb/sq ft) max[source] | — |
|---|
| Predecessor | — | DR350[source] |
|---|
| Successor | — | DR-Z4S[source] |
|---|
| Class | — | Dual-sport[source] |
|---|
| Engine | — | 398 cc (24.3 cu in) 4-stroke single[source] |
|---|
| Bore / stroke | — | 90.0 mm × 62.6 mm (3.54 in × 2.46 in)[source] |
|---|
| Compression ratio | — | 11.3:1[source] |
|---|
| Top speed | — | 94 mph (151 km/h)[source] |
|---|
| Torque | — | 39.2 N⋅m (28.9 lb⋅ft) @ 6,600 rpm[source] |
|---|
| Transmission | — | 5-speed manual , constant-mesh, chain-drive[source] |
|---|
| Frame type | — | Diamond Block[source] |
|---|
| Brakes | — | Disc[source] |
|---|
| Seat height | — | E/S: 935 mm (36.8 in) SM: 890 mm (35.0 in)[source] |
|---|
| Fuel capacity | — | 10 L (2.2 imp gal; 2.6 US gal)[source] |
|---|
| Fuel consumption | — | 44.4 mpg ‑US (5.30 L/100 km; 53.3 mpg ‑imp )[source] |
|---|
| Related | — | Suzuki DR-Z125[source] |
|---|
| Country of origin | — | Japan[source]Inventory Origin column; table 4, row 15, cell 2; revision 1374923116; retrieved 2026-09-30 |
|---|