AFM Supplement DA 40 D
Page 5(b)-8
Issue 2
Revision -, Aug. 2015
5.3.8 Climb Performance - Take-off climb
Take-off at 1150 kg, 2535 lb
Notes:
1. For operation in air colder than provided, use coldest data
2. For operation in air warmer than provided, use extreme caution
Table 5(b)-7 Take-off climb performance at 1150 kg, 2535 lb
Weight:
1150 kg / 2535 lb
Flaps: T/O
Airspeed for initial climb:
66 KIAS
Power:
MAX
Pres. Alt.
RATE OF CLIMB (feet per minute)
Temperature (°C/ °F)
(ft) ISA
ISA+10°C
ISA+18°F
ISA+20°C
ISA+36°F
ISA+30°C
ISA+54°F
ISA+35°C
ISA+63°F
SL 769 766 758 705 661
1000 766 764 756 702 659
2000 764 761 753 700 656
3000 762 759 751 697 654
4000 759 757 748 695 651
5000 757 754 746 692 649
6000 754 751 743 689 646
7000 752 749 740 687 643
8000 749 746 738 684 640
9000 728 725 716 664 621
10000 707 704 695 643 601
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