Where it fits well
- 136 kt cruise supports efficient local and regional flying.
- 267 nm published range creates a practical planning radius of about 179 nm with 4 occupants.
- 434 kg realistic payload proxy and 5 seats define the usable cabin mission.
4-occupant turbine helicopter · Private helicopters · in production 1982-today · See its reach on the 3D globe
Photo: Adrian Pingstone (Arpingstone) · Public domainIndicative planning data, compiled 2026-07. Verify against the AFM and records.
| Seats | 5 |
| Realistic payload with mission fuel | 434 kg |
| Published planning range | 267 nm |
| Practical planning radius (4 people) | 179 nm |
| Cruise speed | 136 kt |
| Runway need | Vertical |
| Pressurised | No |
| Fuel | Jet A-1 |
| Fixed annual base | €131k |
| Direct cost per flight hour | €720 |
The MD 500E combines 4-seat helicopter capability with about 170 NM reported range and about 135 kt reported cruise, while payload, runway and operating-cost figures remain indicative and should be verified for the specific aircraft before making a decision.
Older examples add calendar-driven maintenance: a 2011-built airframe is estimated at €201k per year at 80 hours. Condition, engine time remaining and avionics matter more than the year itself, so price the aircraft in front of you, not the model.