JS-MD 3 RES
Flight Manual Supplement
MD11-AFM-00-002
Issue: 02
Rev. 00
Rev. Date: 24-Mar-23
Page 7
–2
Take-Off Performance (dual battery)
Table 7-2 provides performance data for take-off with dual HV battery
operation.
Take-off performance at maximum weight
Max aircraft take-off mass (dual battery)
575 kg (1268 lbs)
Climb rate at MP (40 kW for 1 minute)
Refer to Figure 7-1
Climb rate at MCP (25 kW)
Refer to Figure 7-1
Take off distance - hard surface, 15m obstacle
430 m (1410 ft)
Peak power to clear 15m obstacle
40 kW for 1 min
Energy used to climb 500 m (1640 ft)
2.1 kWh
Max altitude gain
1700 m (5577 ft)
Sustained range after self-launch
120 km (75 mi)
Table 7-2 Take-Off Performance at Maximum Weight
NOTE:
A take-off distance of 430 m was obtained during ideal
conditions (ISA, MSL, no wind and level runway
surface). The take-off distance is affected by factors as
described in Table 7-1.
NOTE:
The maximum altitude gain and sustained range after
self-launch is affected by atmospheric conditions,
aircraft weight, wind, leading edge contamination and
age/condition of batteries.
