Page 212 - (KU)01-75GAJ-1.5 - Change 1
P. 212

INTRO


   EP'S                  (KU)01-75GAJ-1.5                                                                   FIGURES


                                                        NOTE
                                                                                                             ACAWS
                                The target pitch attitude and the takeoff trim setting were
                                chosen so that if the critical engine fails between refusal
                                speed and rotate speed, the aircraft will be approximately                  GROUND
                                in longitudinal trim at obstacle clearance speed passing
                                50 foot height.
                                                                                                            TAKEOFF
                         D.  Bank angle...................2-5 degrees into the operating engines (PF)

                             Establish 2-5 degrees angle of bank away from the shutdown
                             engines and then adjust angle of bank and rudder pedal force for               FIRE/SMK
  NORM                       zero side slip and apply rudder trim to reduce pedal force.


                                                     WARNING                                                PRES/OXY


                                Apply rudder trim, as required, after takeoff to reduce                    ENG/PROP
                                rudder forces and to increase margin above V      MCA .
                                Operating with rudder out of trim may cause V   MCA  to
                                increase above en route climb speed and cause possible                         FUEL
                                loss of control resulting in loss of aircraft. With rudder
                                trim set, best climb speed, one engine inoperative, is
                                above V MCA2   HYHQ LQ ORZ ERRVW ZLWK ÀDSV XS  :LWK UXGGHU                     AAR
                                trim set, en route climb speed, one engine inoperative,
                                is above V MCA2   HYHQ LQ ORZ ERRVW ZLWK ÀDSV XS
  SPEC                              NOT FOR FLIGHT                                                             ELEC
                         E.  Airspeed...............................................................Capture V
                                                                                     OBS   (PF)
                         When safely airborne with a positive rate of climb:
                                                                                                               HYD
                         F.  GEAR....................................................................................UP (PM)

                                                     WARNING                                                FLT CTRL


                                5HWUDFWLQJ JHDU DQG ÀDSV VLPXOWDQHRXVO\ LQFUHDVHV 9 MCA                       GEAR
                                because of the reduction in available hydraulic pressure
                                to the rudder booster assembly.
                                                                                                            DOR/RMP
  PERF                                                  NOTE

                                Prior to reaching V OBS , the capability of the aircraft to climb           JETTISON
                                is seriously reduced while the landing gear is retracting
                                (18 seconds) and the propeller is being feathered.
                                                                                                            LANDING
                         Once the gear is up and clear of obstacles (400 feet AGL minimum):

                         G.  Airspeed...................................................................Accelerate (PF)
                                                                                                            DITCHING
                            ,I SUHGLFWHG   HQJLQH FOLPERXW ÀLJKW SDWK LV UHTXLUHG  REVHUYH WKH
                            climb dive marker angle when stable at V   OBS . When the gear is
                            up, lower the climb dive marker halfway to the horizon. This will               BAILOUT
                            DSSUR[LPDWH  WKH  FOLPERXW  ÀLJKW  SDWK  RQ  WKH  SHUIRUPDQFH  FKDUW
                            during acceleration to best climb speed.
  OPER                                                                                                      FAULT LG

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