1
Section 5 – PERFORMANCE
TAKE-OFF RATE OF CLIMB
P-Mentor – Aircraft Flight Manual Page 5 - 11
10. Take-Off Rate of Climb
Throttle Lever: Full FWD, Propeller Lever: Full Forward
Flaps Take-off
Weight
[kg/lbs]
Pressure
Altitude
720 /
1587
0 822 762 678 599 525 433 599
8000 386 331 252 178 110 24
670 /
1477
0 928
865 776 693 615 518
693
10000 354 296 214 138 67 -22
12000 240 183 103 28 -42 -129
620 /
1367
0 1048 981 886 798 715 611 798
13000 256 196 112 33 -41 -133