Page 325 - (KU)01-75GAJ-1.5 - Change 1
P. 325

INTRO


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

                            Lost
                            Bus            procedures. Use caution when dumping to avoid large
                            Com            fuel imbalances.                                                  ACAWS
                            failure    ‡   UTIL and BSTR RUD PRESS HI/LO (C) ACAWS and
                                           system status page pressure indications inoperative.
                                           Flap position indicator inoperative. Visually verify             GROUND
                                           ÀDS  SRVLWLRQ  ZKHQ  H[WHQGLQJ  DQG  UHWUDFWLQJ   5XGGHU
                                           HI/LO boost control should function normally.  The
                                           pressure gauge on the rudder booster panel assembly              TAKEOFF
                                           at approximately FUS STA 1023 can be used to verify
                                           booster pressure.
                                                                                                            FIRE/SMK
  NORM                                 ‡   Auxiliary hydraulic pump and pressure indications
                                           failed. Emergency brakes will fail after accumulator is
                                           discharged. Recharge accumulator using manual hand               PRES/OXY
                                           pump and direct reading pressure sight gauge.

                                       ‡   Utility hydraulic system aileron/elevator/rudder control        ENG/PROP
                                           boost shutoff valves failed open.

                                       ‡   GPS 2 unavailable because of antenna electronics
                                           power failure. No GPS functionality with EGI 2.                     FUEL
                                       ‡   Electronic control of chute release inoperative.

                                       ‡   $LU  GHÀHFWRUV  IDLO  LQ  FXUUHQW  SRVLWLRQ   FDQQRW  H[WHQG        AAR
                                           retract. Monitor airspeed if extended.

                                       ‡
                                           Exterior lighting degraded: Upper strobe, covert
  SPEC                              NOT FOR FLIGHT                                                             ELEC
                                           anticollision light, loading lights, pod/hose illumination
                                           lights and main landing gear wheel-well inspection lights
                                           failed.
                                                                                                               HYD
                                       ‡   UHF DF unusable.
                                       ‡   HF 2 inoperative.
                                                                                                            FLT CTRL
                                     F.  BAU II #3 FAIL*....................................................... Review

                                     G.  Fault Log................................................................ Review  GEAR

                                           ADS CNTL, AIL/ELEV/RUD SOV-UTIL
                                           AIR DEFLECT-EXT/RETR                                             DOR/RMP
  PERF                                     AUX HYD PMP RELAY, BAU II #3

                                           CGO RAMP/DOOR-OPEN/CLOSE, FLT DATA RECORDER                      JETTISON
                                           FUEL MGMT CNTL A, HF 2 DC PWR
                                           L AUX XFER PMP, L EXT TK FWD PMP, LOADING LTS
                                           MAIN GEAR WELL LTS                                               LANDING
                                           RUD BSTR/UTIL HYD PRESS SENS, STICK PUSHER
                                           TK 2 BOOST PMP, TK 4 XFER PUMP, TOP STROBE                       DITCHING
                                           UHF/DF ANT SEL SW, WING FLAP POSN SENS
                                     (End of Procedure)                                                     BAILOUT

                            Lost Bus Comm failure: If communications have failed, most ECBs stay
  OPER                      in their last state.                                                            FAULT LG

                            Use, copying and/or disclosure is   1 -285
                            governed by the statement on the
                            title page of this document.  BACK                                               CHARTS
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