Page 47 - (KU)01-75GAJ-1.5 - Change 1
P. 47

INTRO


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


                                                  1.2.2 CAUTIONS                                      B
                                                                                                             ACAWS
                                    Alert/Condition                    Crew Action
                              CP HUD FAIL                                                             C     GROUND
                              The copilot HUD computer      The PFD should automatically be
                              has failed or the MC has lost   displayed in the No. 4 position.        D
                              communication with the copilot   If the PFD is not automatically displayed:
                              HUD.                                                                          TAKEOFF
                                                            PFD............................................ Select  E
                                                                Use either the control wheel HDD
                                                                PFD switch or the AMU PFD, HDD        F     FIRE/SMK
  NORM                                                          POS page.
                              CP PITOT HEAT FAIL
                                    NOT FOR FLIGHT
                              CP PITOT switch is ON and a   Icing conditions........................... Avoid  G  PRES/OXY
                              heating element is inoperative.  If icing conditions are encountered:
                                                            CADC 1 data.............................. Select  H  ENG/PROP
                                                                Standby airspeed indicator may be
                                                                inoperative.                          I
                              CP PITOT HEAT OFF                                                                FUEL

                              Any power lever is placed more   CP PITOT switch............................ ON
                              than 5 degrees forward of FLT                                           L
                              IDLE and CP PITOT switch is                                                      AAR
                              OFF.                                                                   M
  SPEC                        DEICE TIMER FAIL                                                                 ELEC
                              Both channels of the propeller   Icing conditions........................... Avoid
                              deicer timer have failed or lost                                        N
                              communication with the MC.                                                       HYD
                              ECBU 1 (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13 or 14) FAIL*            O
                              ECBU has failed or lost       ECBU 1 (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12,
                              communication with the MC. If   13 or 14) FAIL* procedure... Accomplish       FLT CTRL
                              failed, all ECBs lose power and                                         P
                              multiple failures are evident in the
                              ÀLJKW VWDWLRQ  ,I FRPPXQLFDWLRQV                                        R       GEAR
                              have failed, most of the ECBs
                              stay in their last state.
                              EGI 1 (or 2) FAIL                                                       S     DOR/RMP
  PERF                        CNI has lost communication    Select alternate navigation solution on
                              with the respective EGI.
                                                            the NAV SELECT page of the AMU.
                              ELEV BSTR SWITCH OFF                                                    T     JETTISON
                              The ELEVATOR BOOST            If no malfunction or leak exists:
                              hydraulic system CONTROL      CONTROL BOOST, ELEVATOR                   U     LANDING
                              BOOST switch is OFF.          BOOST switch................................ ON
                              ELEV UTIL SWITCH OFF                                                    V
                              The ELEVATOR UTIL hydraulic   If no malfunction or leak exists:               DITCHING
                              system CONTROL BOOST          CONTROL BOOST, ELEVATOR UTIL             W
                              switch is OFF.                switch.............................................. ON
                                                                                                            BAILOUT
                                                                                                      X

  OPER                                                                                                      FAULT LG

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