DA 62 AFM
Normal Operating
Procedures
4A.6.7 TAKE-OFF
a) Standard Procedure (Take-off with Flaps T/O)
1. Transponder . . . . . . . . . . . . . . . . . . . . . . . . . as required
2. POWER lever . . . . . . . . . . . . . . . . . . . . . . . . MAX
NOTE
The proper and symmetric performance of the engines at
MAX should be checked early during the take-off run, so that
the take-off can be aborted if necessary.
3. Elevator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . neutral
4. Rudder. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . maintain direction
NOTE
In strong crosswinds steering can be augmented by use of
the toe brakes. It should be noted, however, that this method
increases the take-off roll, and should not generally be used.
5. Nose wheel lift-off: . . . . . . . . . . . . . . . . . . . . . up to 1999 kg (4407 lb):
v
R
min. 76 KIAS
above 1999 kg (4407 lb):
v
R
min. 78 KIAS
6. Airspeed for initial climb: . . . . . . . . . . . . . . . . up to 1999 kg (4407 lb):
min. 83 KIAS
above 1999 kg (4407 lb):
min. 86 KIAS
CONTINUED
Doc. No. 11.01.05-E Rev. 0 11-Jan-2019 Page 4A - 35