Page 40 - (KU)01-75GAJ-1.5 - Change 1
P. 40

INTRO


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


                                              1.2.2 CAUTIONS                                          B
                                                                                                             ACAWS
                                Alert/Condition                     Crew Action
                          ATCS FAIL                                                                   C     GROUND
                          This alert can only occur on the   0DLQWHQDQFH UHTXLUHG EHIRUH ÀLJKW
                          ground and is generated by the   If maintenance cannot be performed         D
                          same condition that creates    and takeoff is necessary:
                          the AC CONFIG INVALID                                                             TAKEOFF
                          (C) ACAWS. MC is unable        Refer to AC CONFIG INVALID (C)               E
                          to determine which aircraft    ACAWS for additional aircraft system
                          (serial number) it is installed in;   information.                          F     FIRE/SMK
  NORM                    therefore, ATCS is inoperative.
                          ATCS OFF
                                    NOT FOR FLIGHT
                          The automatic thrust control   ATCS switch..................................... ON  G  PRES/OXY
                          system has been turned off.
                          AUX HYD PMP PRESS LO                                                        H    ENG/PROP
                          The auxiliary pump output      Check the direct reading gauge at the
                          pressure is less than 1,000 psi   ramp control panel.
                          and the AUX PUMP switch is     If pressure is normal:                       I        FUEL
                          ON.
                                                         Continue operation.
                                                         If pressure is less than 1,000 psi:          L
                          This may be an indication of                                                         AAR
                          pump cavitation during high    AUX PUMP switch........................ OFF
                          altitude operation of the cargo   If pressure is below 1,000 psi during    M
  SPEC                    door and ramp.                 operation of cargo door and ramp                      ELEC
                                                         in a high altitude operation:
                                                         Operate ramp and door independently.         N
                                                         If cavitation persists:                               HYD
                                                         Altitude..................................... Reduce  O
                                                            Reduce altitude until normal
                                                            operating pressure is restored.           P     FLT CTRL
                                                         AUX PUMP switch................................
                                                         ..................... OFF, as soon as possible       GEAR
                          AV BAT DISCHARGE                                                            R
                          The avionics battery is        Disregard this ACAWS if all generators
                          powering the Avionics dc bus.  have been lost.                              S     DOR/RMP
  PERF                                                   If landing within 30 minutes:
                                                         No crew action required. Battery should      T
                                                         last approximately 30 minutes.                     JETTISON
                                                         If unable to land within 30 minutes:
                                                         AVIONIC BAT CONT MCB.............. Pull      U     LANDING
                                                            (P FWD R2 #7)
                                                            This will conserve battery power.         V
                                                         ECB status page........................ Review     DITCHING
                                                            Refer to ECB AV DC BUS list No.          W
                                                            100.
                                                         Fault Log.................................... Review  X  BAILOUT
                                                            Refer to AV DC BUS OFF Fault Log.
  OPER                                                                                                      FAULT LG

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