Pilot’s Operating Handbook Section 5
EXTRA 500 Performance
TAKEOFF CLIMB PERFORMANCE
Conditions: Landing gear down and flaps 15
2030 RPM - BLEED 2
CLIMBSPEED 87 KIAS
111 % Torque or 810 Deg.CTOT
RATE OF CLIMB (FT/MIN)
RATE OF CLIMB (FT/MIN)
Pressure 3900 LB (1769 KG)
Pressure 4696 LB (2130 KG)
Altitude
Altitude
(Feet) ISA ISA ISA ISA ISA
(Feet) ISA ISA ISA ISA ISA
-20 C +10 C +20 C +30 C
-20 C +10 C +20 C +30 C
SL 1650 1575 1545 1490 1265
SL 12
45 1175 1135 1100 890
1000 1635 1565 1530 1435 1190
1000 1230 1165 1125 1050 830
2000 1625 1550 1515 1355 1120
2000 1220 1150 1110 980 770
3000 1610 1540 1500 1275 1045
3000 1205 1140 1100 910 705
4000 1595 1530 1425 1200 975 4000 1190 1130 1035 845 645
5000 1585 1520 1340 1120 900 5000 1180 1115 960 775 585
6000 1570 1485 1255 1040 830 6000 1165 1085 885 705 520
7000 1555 1390 1170 960 755
7000 1150 1005 810 640 460
8000 1540 1295 1085 885 685
8000 1140 920 740 570 *
9000 1530 1195 995 805 610
9000 1125 840 665 500 *
10000 1500 1100 910 725 540 10000 1100 755 590 435 *
RATE OF CLIMB (FT/MIN)
*Denotes conditions where the
Pressure 4200 LB (1905 KG) takeoff climb gradient can not
Altitude
be maintained
(F
eet) ISA ISA ISA ISA ISA
-20 C +10 C +20 C +30 C
SL 1485 1410 1375 1335 1110
1000 1470 1400 1360 1280 1045
2000 1455 1385 1350 1205 975
3000 1445 1375 1335 1130 910
4000 1430 1360 1265 1055 840
5000 1415 1350 1185 985 770
6000 1400 1320 1105 910 705
7000 1390 1235 1025 835 635
8000 1375 1145 945 760 570
9000 1360 1060 865 685 500
10000 1335 975 785 610 435
Example refer to 5.4.a
Fig 5-5
Takeoff (Sheet 4 of 4)
26. January 2011
5-19