Page 311 - (KU)01-75GAJ-1.5 - Change 1
P. 311

INTRO


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


                                 FLT STN CB LTS
                                 DIGITAL MAP                                                                 ACAWS
                                 CHUTE RELEASE, SPTU 1, CP PITOT HEAT 4
                                 EXT MASS MEM UNIT                                                          GROUND
                                 R POD E-TRAIL/R-TEST
                                 R POD TRAIL
                                                                                                            TAKEOFF
                            (End of Procedure)

                            1.10.5.6 ECBU 6 FAIL*                                                           FIRE/SMK
  NORM                      Condition:


                            The ECBU has failed or lost bus communication with the MC.                      PRES/OXY


                           Q1  ARE MULTIPLE ACAWS DISPLAYED?                                               ENG/PROP


                              NO     Conventional failure: All ECBs lose power and multiple failures           FUEL
                                     DUH HYLGHQW RQ WKH ÀLJKW GHFN  7KH $&$:6 DVVRFLDWHG ZLWK D
                             Lost    conventional failure are:
                             Bus                                                                               AAR
                             Comm      ‡   RADAR FAIL (C)
                                       ‡
                                           INU 1 FAIL (C)
  SPEC                       failure NOT FOR FLIGHT                                                            ELEC
                                       ‡   CP AP FAIL (C)
                                       ‡   CP HUD FAIL (C)
                                                                                                               HYD
                                       ‡   GCAS FAIL (C)
                                       ‡   GEN 4 FAIL (C)
                                                                                                            FLT CTRL
                                       ‡   CAB ALT HIGH (C)

                                                           NOTE
                                                                                                              GEAR
                                           ACAWS is not valid, system is functional.

                                       ‡   TCAS FAULT (A)                                                   DOR/RMP
  PERF                                 ‡   RADALT 2 FAIL (A)

                                       ‡   HF 2 FAIL (A)                                                    JETTISON
                                       ‡   CNI SP 2 FAIL (A)
                                       ‡   VOR/ILS 2 FAIL (A)
                                                                                                            LANDING
                                     A.  Pilot attitude source........................ Select ATT REF INU 2
                                           Recovers pilot autopilot and GCAS.
                                                                                                            DITCHING
                                     B.  CNI-MU NAV CTRL.......................................................Set
                                           Select INS No. 2 for INAV 1 sensor on CNI-                       BAILOUT
                                           MU INAV CTRL SENSORS page 2 of 3. Then
                                           reselect desired solution for INAV 1 on page 1
  OPER                                     of 3.                                                            FAULT LG

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