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Figure 4-13. Rate of climb - all engines - take-off power - 2850 kg. 4–22
Figure 4-14. Rate of climb - all engines - maximum continuous
power - 2050 kg. 4–23
Figure 4-15. Rate of climb - all engines - maximum continuous
power - 2450 kg. 4–24
Figure 4-16. Rate of climb - all engines - maximum continuous
power - 2850 kg. 4–25
Figure 4-17. Rate of climb - OEI - 2.5 minutes power - 2050 kg. 4–26
Figure 4-18. Rate of climb - OEI - 2.5 minutes power - 2450 kg. 4–27
Figure 4-19. Rate of climb - OEI - 2.5 minutes power - 2850 kg. 4–28
Figure 4-20. Rate of climb - OEI - maximum continuous power -
2050 kg. 4–29
Figure 4-21. Rate of climb - OEI - maximum continuous power -
2450 kg. 4–30
Figure 4-22. Rate of climb - OEI - maximum continuous power -
2850 kg. 4–31
Figure 4-23. Airspeed calibration curve pilot (forward flight) 4–33
Figure 4-24. Airspeed calibration curve copilot (forward flight) 4–34
RFM A109E
List of illustrations (Contd.)
4-ii R.A.I. Approved
Rev. 22
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