JS-MD 3 RES
Flight Manual Supplement
MD11-AFM-00-002
Issue: 02
Rev. 00
Rev. Date: 24-Mar-23
Page 7
–4
WARNING:
The data presented are for sea-level standard
atmospheric conditions. With reduced air-density (higher
temperature or higher altitude) the propeller RPM will
increase with the risk of exceeding the maximum
propeller RPM. Ensure the RPM remains within the
operating limits at all times.
Take-Off Performance (single battery)
Take-off with a single battery is not allowed due to the high electrical
current requirement on the battery that will reduce battery life.
Sustained Performance (dual battery)
Table 7-3 provides performance data for sustained flight with dual HV
battery operation when fully charged.
Sustained performance with dual batteries
Reference Mass
480 kg (1058 lbs)
Max Continuous Power (MCP)
25 kW (33.5 hp)
Rate of Climb at MCP
2.4 m/s (472 ft/min)
Max altitude gain (approx.)
2000 m (6562 ft)
Max sustained range in 18m (approx.)
157 km (98 mi)
Table 7-3 Sustained Performance (dual battery)
Figure 7-3 illustrates the flight profile including RES HV battery
temperature variation.
