AFM Supplement DA 40 D
Page 5(a)-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(a)-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
SL 646 630 614 598
1000 645 629 613 597
2000 643 627 612 596
3000 642 626 610 594
4000 641 625 609 593
5000 640 624 608 592
6000 638 622 606 590
7000 637 621 605 589
8000 636 619 603 587
9000 614 598 582 567
10000 587 572 557 541
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