Page 309 - (KU)01-75GAJ-1.5 - Change 1
P. 309

INTRO


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

                            Lost
                            Bus      C.  ELEV TAB power selector switch................. Select EMER
                            Comm           Normal elevator trim failed.                                      ACAWS
                            failure
                                     D.  Autopilot pitch............................ Select OFF (as required)
                                           Autopilot pitch unusable.                                        GROUND

                                     E.  Pilot RAD ALT source............................ Select RAD ALT 2
                                                                                                            TAKEOFF
                                           Restores TCAS and GCAS.

                                     F.  Copilot air data source................................. Select ADC 1  FIRE/SMK
  NORM                                     Selecting  ADC 1 will minimize airspeed and altitude
                                           variances when sideslipping the aircraft.
                                                                                                            PRES/OXY
                                     G.  Icing conditions...................................... Avoid, if practical
                                           Standby airspeed indicator and altimeter (in slide slips)
                                           may indicate erroneously if the copilot lower left pitot        ENG/PROP
                                           tube freezes (pitot heat failed). P and CP PITOT HEAT
                                           FAIL (C) ACAWS inoperative.
                                                                                                               FUEL
                                     H.  Potential Mission Impacts...................................... Review

                                       ‡   Reduced electrical redundancy. Generator No. 3 control              AAR
                                           relay has lost power and is no longer powering its
                                           respective bus(es).
  SPEC                              NOT FOR FLIGHT                                                             ELEC
                                       ‡
                                           Loss of brake pressure indication and alerting. NORM
                                           BRAKES FAIL (C) and EMER BRAKES FAIL (C) ACAWS
                                           are due to sensor failures.
                                                                                                               HYD
                                       ‡   Degraded mission capability due to loss of displays (P
                                           HUD, DIG MAP, P CNI-MU).
                                       ‡   Degraded radar.                                                  FLT CTRL
                                       ‡   Failure of VOR/ILS MB No. 1.

                                       ‡   Chute release (bomb rack) inoperative.                             GEAR
                                       ‡   Airspeed or altitude difference will not indicate on a
                                           single ADC source. Copilot lower left pitot heat failed.         DOR/RMP
                                           Standby airspeed indicator and altimeter (in sideslips)
  PERF                                     may indicate erroneously if the copilot No. 4 lower left

                                           pitot tube freezes.  The PILOT/CP PITOT HEAT FAIL                JETTISON
                                           ACAWS is inoperative.

                                       ‡   Right AR pod emergency trail/response test function is lost.
                                                                                                            LANDING
                                       ‡   Right AR hose will rewind if trailed.
                                     I.  Fault Log.................................................................. Review
                                           MC 1 AC, BIU #1 AC, CNI-SP 1, RAD ALT 1                          DITCHING
                                           P HUD, VOR/ILS 1, P CNI-MU
                                           GBE RELAY 3A/4A, GEN 3                                           BAILOUT
                                           ELEV TAB CNTL-NORM, PITOT HEAT MON

  OPER                                     BRAKE SEL VLV-EMER, NORM/EMER BRAKE                              FAULT LG

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