Page 382 - (KU)01-75GAJ-1.5 - Change 1
P. 382

INTRO


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


                         E.  CNI-SP 1 ECB (419)............................................................. RESET
                                                                                                             ACAWS

                        Q4  DID SP 1 RECOVER?
                                                                                                            GROUND

                          NO
                                  If at least one valid navigation solution is obtained, no further
                                  action is necessary.                                                      TAKEOFF
                           F
                                  (End of Procedure)

                                                                                                            FIRE/SMK
                         F.  Land.................................................................. As soon as possible
  NORM
                            If navigation function is not recovered, recovery is not possible. After
                            landing, power down the aircraft and perform CNI Master Avionics                PRES/OXY
                                    NOT FOR FLIGHT
                            power up.

                         (End of Procedure)                                                                ENG/PROP


                         1.10.11 CNI-MS RECOVERY ON THE GROUND (DUAL                                           FUEL
                         MODE FAILURE)

                         Upon initial boot-up, if the CNI-SPs fail to attain dual-mode operation               AAR
                         or if CNI-MS-controlled equipment fails to establish communications,
  SPEC                   perform this procedure.                                                               ELEC
                                                        NOTE

                                Certain boot-up anomalies may induce a processor                               HYD
                                FRQÀLFW  RU  D  FRPPXQLFDWLRQV  IDLOXUH  ZLWK  &200 1$9
                                radios. When such anomalies occur, the CNI-MUs may
                                revert uncommanded to the TIME OUT page or INDEX                            FLT CTRL
                                page, and fail to attain dualmode operation.

                         A.  CNI-SP 1 ECB (419).................................................. PULL, RESET  GEAR

                         B.  CNI-SP 2 ECB (119).................................................. PULL, RESET
                                                                                                            DOR/RMP

  PERF                  Q1  DID ALL CNI-MS FUNCTIONS RECOVER?
                                                                                                            JETTISON
                           NO
                                  If CNI SP 1 annunciates SP 2 FAIL and INDEPENDENT                         LANDING
                           C      OPERATIONS, evaluate the operation of the CNI to determine
                                  further action.
                                                                                                            DITCHING
                                  If the single remaining navigation solution recovers, no further
                                  action is necessary.

                                  (End of Procedure)                                                        BAILOUT

                         C.  LRU............................................... Attempt to isolate the failed LRU
  OPER                                                                                                      FAULT LG

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