Honda HondaJet HA-420 Pilots Operating Manual page 329

HA-420
POM
If an engine failure occurs after V
hand from thrust levers and place it on the yoke. At V
aircraft with a steady, smooth motion to achieve the FD target takeoff
pitch attitude in 3-4 seconds.
NOTE Accomplish initial steps of this procedure from memory.
When time and conditions permit, accomplish the
L(R) ENGINE FLAMEOUT
with the AFM, and confirm those steps completed from
memory.
Retract the landing gear after achieving a positive rate of climb. Adjust
pitch to maintain V
reduce control forces, and engage the autopilot as desired. Further yaw
trim adjustments may be required to maintain coordinated flight.
Pitch target can be adjusted using the control wheel steering (CWS)
button momentarily to set the FD in pitch mode at a pitch attitude that
yields the desired airspeed or by adjusting the pitch wheel. Alternatively,
FLC mode can be selected and speed target set to V
airspeed and climb rate.
When clear of obstacles or at 1,500 ft AGL, accelerate to V
and retract the flaps. Accelerate to and climb at 140 KIAS. Reduce the
thrust levers to MCT, and continue enroute climb. See the figure that
follows.
October 30, 2016
Honda Aircraft Company
during the initial climb. Use yaw and roll trim to
2
HJ1-29000-005-001
FOR TRAINING PURPOSES ONLY
OPERATING PROCEDURES
but before V , at V
1 R
procedure in accordance
AND TECHNIQUES
, remove the
1
, rotate the
R
. Carefully monitor
2
+ 10 KIAS,
2
3-43