SECTION 4 - PERFORMANCE DATA
GENERAL
The maximum power available with the Bleed-Air Heater system operating is
less than that available with the helicopter in basic configuration.
This power loss is caused by the compressor bleed-air used for the heater
system.
Performance charts with the bleed-air heater switched ON are provided for all
engine operative.
During single engine operation the bleed-air heater system must be switched
OFF.
Performance with the bleed-air heater system switched OFF is the same as that
shown in the basic Rotorcraft Flight Manual.
List of Performance Data Charts:
— Figure 4-1. Hovering ceiling - IGE - take-off power.
— Figure 4-2. Hovering ceiling - IGE - maximum continuous power.
— Figure 4-3. Hovering ceiling - OGE - take-off power.
— Figure 4-4. Hovering ceiling - OGE - maximum continuous power.
— Figure 4-5. Rate of climb - all engines - take-off power - 2050 kg.
— Figure 4-6. Rate of climb - all engines - take-off power - 2450 kg.
— Figure 4-7. Rate of climb - all engines - take-off power - 2850 kg.
— Figure 4-8. Rate of climb - all engines - maximum continuous power -
2050 kg.
— Figure 4-9. Rate of climb - all engines - maximum continuous power -
2450 kg.
— Figure 4-10. Rate of climb - all engines - maximum continuous power -
2850 kg.
RFM A109E
APPENDIX 6
Page 8 of 18 R.A.I. Approved
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