Bombardier_Challenger_Global_00-Engine_Failure_on_Takeoff

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Bombardier_Challenger_Global_00-Engine_Failure_on_Takeoff

 

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ROPAT
Sep 13/2004 Flight Crew Operating Manual Volume 1
REV 1 CSP 100-6 09-14-5
CL300_SOP_004
PF
PNF
“ ” CALL RESPONSE
Initial climb
• V 2 speed
takeoff
flaps
V R rotate
airplane
to command
bar noseup
pitch attitude
V 1 release
thrust levers
“V 1 ”
“POSITIVE RATE”
(when a positive rate of climb is established)
Clear of obstacles
Initial takeoff roll
(standing or rolling
takeoff procedures)
“GEAR UP”
(pitchup to
maintain
V 2 speed)
• Continue climb at
170 KIAS, if necessary
• Reduce thrust to CLB
Clear of obstacles
• Accelerate airplane to
V 2 + 15 kt (min) flaps 10
V 2 + 25 kt flaps 20
Engine Failure (Above V 1 Speed)
Takeoff Continued
Engine
failure
Rudder and ailerons
as required for
directional control
NOTE:
Directional control improves
if nosewheel is kept on the
runway (with forward pressure
on the control wheel) until V R
• “FLAPS 0”
• “ENGINE FAILURE
ABOVE V 1
SPEED
CHECKLIST”
“V 2 + 25”
Keep skid indicator
centered using
rudder or rudder trim
“ROTATE”
(V R )
HDG & FLC
Engine Failure Above V1 Speed
Figure 09-14-02

dul

MANUAL 8 MANUAL 8 MANUAL 8 MANUAL 8 MANUAL 8 MANUAL 8

qiushengsean

好好学习

thank you

bocome

庞巴迪挑战者动力装置