Page 357 - (KU)01-75GAJ-1.5 - Change 1
P. 357

INTRO


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


                            B.  ATCS switch.............................................................................. OFF
                                                                                                             ACAWS
                                 ATCS may not properly schedule engine HP.

                            C.  Airspeed........................................ Maintain above approach speed  GROUND

                                 Stick pusher and sideslip warning systems failed. Stall warning
                                 degraded in high side slip angles.
                                                                                                            TAKEOFF
                            Prior to landing:

                            D.  Landing gear position................................................. Visually verify  FIRE/SMK
  NORM
                                 Verify position before landing. Nose gear indication failed.
                                                                                                            PRES/OXY
                                    NOT FOR FLIGHT
                            After engine shutdown:

                            E.  AUX PUMP switch................................................. ON (as required)  ENG/PROP

                            F.  ANTI SKID switch or EMER BRAKE SEL switch............ As required
                                                                                                               FUEL
                                 Select ANTI SKID switch OFF or select EMER BRAKE SEL switch
                                 to EMER prior to setting the parking brake. Setting the parking
                                 brake will not close the parking brake valve.                                 AAR

                            G.  Potential Mission Impacts..................................................... Review
  SPEC                            ‡  Failed Components:                                                        ELEC


                                           ATCS degraded
                                           MC 1 (or 2)                                                         HYD
                                           IFF
                                           TCAS                                                             FLT CTRL
                                           Autopilot
                                           Stall warning/Stick pusher                                         GEAR
                                           UHF DF
                                           P and CP control wheel buttons (ELEV TRIM and INTPH/
                                           RADIO are still functional)                                      DOR/RMP
  PERF

                                  ‡  Failed Indicators:                                                     JETTISON

                                           All electrical indications
                                           Normal and emergency brake indications                           LANDING
                                           APU RPM indication
                                           LOX quantity indication                                          DITCHING
                                           T/R 1-4 loads and MAIN and ESS bus voltage indications
                                           P and CP PITOT HEAT FAIL (C) ACAWS
                                           CREW DOOR OPEN (W) and CREW DOOR OPEN (A)                        BAILOUT
                                           ACAWS
  OPER                                                                                                      FAULT LG

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