Takeoff and Initial Climb
777/787 Flight Crew Training Manual
Initial Climb - One Engine Inoperative
The initial climb attitude should be adjusted to maintain a minimum of V2 and a positive climb. After liftoff the flight director provides proper pitch guidance. Cross check indicated airspeed, vertical speed and other flight instruments. The flight director commands a minimum of V2, or the existing speed up to a maximum of V2 + 15. If the flight director is not used, indicated airspeed and attitude become the primary pitch references. Retract the landing gear after a positive rate of climb is indicated on the altimeter. The initial climb attitude should be adjusted to maintain a minimum of V2. If an engine fails at an airspeed between V2 and V2 + 15, climb at the airspeed at which the failure occurred. If engine failure occurs above V2 + 15, increase pitch to reduce airspeed to V2 + 15 and maintain until flap retraction altitude. The flight director roll mode commands ground track after liftoff until LNAV engagement or another roll mode is selected. If ground track is not consistent with desired flight path, use HDG SEL/TRK SEL/LNAV to achieve the desired track. Indications of an engine fire, impending engine breakup or approaching or exceeding engine limits, should be dealt with as soon as possible. Accomplish the appropriate recall checklist items as soon as the airplane is under control, the gear has been retracted and a safe altitude (typically 400 feet AGL or above) has been attained. Accomplish the reference checklist items after the flaps have been retracted and conditions permit. If an engine failure has occurred during initial climb, accomplish the appropriate checklist after the flaps have been retracted and conditions permit.
Immediate Turn after Takeoff - One Engine Inoperative
Obstacle clearance or departure procedures may require a special engine out departure procedure. If an immediate turn is required, initiate the turn at the appropriate altitude (normally at least 400 feet AGL). Maintain V2 to V2 + 15 with takeoff flaps while maneuvering. Note: The AFDS limits the bank angle to 15° until V2 + 10 knots to maintain at least adequate maneuver margin. The bank angle limit increases to 25° by V2 + 20 knots if LNAV is engaged, or when HDG SEL or TRK SEL is engaged with the bank limit in AUTO. After completing the turn, and at or above flap retraction altitude, accelerate and retract flaps.
Copyright © The Boeing Company. See title page for details.
3.36
FCT 777/787 Preliminary (TM)
October 31, 2006
飞行翻译公司 www.aviation.cn
本文链接地址：787机组训练手册Flight Crew Training Manual 787_split_2.pdf
777/787 Flight Crew Training Manual
Initial Climb - One Engine Inoperative
The initial climb attitude should be adjusted to maintain a minimum of V2 and a positive climb. After liftoff the flight director provides proper pitch guidance. Cross check indicated airspeed, vertical speed and other flight instruments. The flight director commands a minimum of V2, or the existing speed up to a maximum of V2 + 15. If the flight director is not used, indicated airspeed and attitude become the primary pitch references. Retract the landing gear after a positive rate of climb is indicated on the altimeter. The initial climb attitude should be adjusted to maintain a minimum of V2. If an engine fails at an airspeed between V2 and V2 + 15, climb at the airspeed at which the failure occurred. If engine failure occurs above V2 + 15, increase pitch to reduce airspeed to V2 + 15 and maintain until flap retraction altitude. The flight director roll mode commands ground track after liftoff until LNAV engagement or another roll mode is selected. If ground track is not consistent with desired flight path, use HDG SEL/TRK SEL/LNAV to achieve the desired track. Indications of an engine fire, impending engine breakup or approaching or exceeding engine limits, should be dealt with as soon as possible. Accomplish the appropriate recall checklist items as soon as the airplane is under control, the gear has been retracted and a safe altitude (typically 400 feet AGL or above) has been attained. Accomplish the reference checklist items after the flaps have been retracted and conditions permit. If an engine failure has occurred during initial climb, accomplish the appropriate checklist after the flaps have been retracted and conditions permit.
Immediate Turn after Takeoff - One Engine Inoperative
Obstacle clearance or departure procedures may require a special engine out departure procedure. If an immediate turn is required, initiate the turn at the appropriate altitude (normally at least 400 feet AGL). Maintain V2 to V2 + 15 with takeoff flaps while maneuvering. Note: The AFDS limits the bank angle to 15° until V2 + 10 knots to maintain at least adequate maneuver margin. The bank angle limit increases to 25° by V2 + 20 knots if LNAV is engaged, or when HDG SEL or TRK SEL is engaged with the bank limit in AUTO. After completing the turn, and at or above flap retraction altitude, accelerate and retract flaps.
Copyright © The Boeing Company. See title page for details.
3.36
FCT 777/787 Preliminary (TM)
October 31, 2006
飞行翻译公司 www.aviation.cn
本文链接地址：787机组训练手册Flight Crew Training Manual 787_split_2.pdf
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