Page 157 - (KU)01-75GAJ-1.5 - Change 1
P. 157

INTRO


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


                                                 1.2.3 ADVISORIES                                     B
                                                                                                             ACAWS
                                    Alert/Condition                    Crew Action                    C
                              NAC 1 (2, 3 or 4) ISOLATED                                                    GROUND

                              Electrical power has been     Bleed air system...................... Monitor  D
                              removed from the nacelle          Monitor the bleed air system for
                              shutoff valve or the valve has    automatic isolation.                        TAKEOFF
                              been commanded closed for                                               E
                              QDFHOOH ¿UH RYHUKHDW  ZLQJ    If an auto-close condition has cleared:
                              overheat, FIRE handle pulled,   Control logic................................ Reset
                              excessive pneumatic pressure/     Reset the control logic by setting    F     FIRE/SMK
  NORM                        temperature or low actuating      the respective switch to CLOSE
                              pressure.                         and then back to AUTO.                      PRES/OXY
                                    NOT FOR FLIGHT
                              NAC 1 (2, 3 or 4) LEAK DET FAIL                                        G
                              F/ODS loop A is open, shorted   On the ground:
                              or has a sensor monitor                                                 H    ENG/PROP
                              failure and loop B is either   0DLQWHQDQFH UHTXLUHG EHIRUH ÀLJKW
                              open, shorted or has a sensor   ,Q ÀLJKW                                I
                              monitor failure. Nacelle bleed                                                   FUEL
                              air leak detection is inoperative;   0RQLWRU IRU LQGLFDWLRQV RI VPRNH RU ¿UH
                              KRZHYHU  HQJLQH ¿UH GHWHFWLRQ                                           L
                              is available.                                                                    AAR
                              NAC 1 (2, 3 or 4) SOV NOT CLOSED                                       M

  SPEC                        The respective nacelle        Nacelle shutoff valve................... Cycle     ELEC
                              shutoff valve fails to go
                                                            Cycle from AUTO or OPEN to CLOSE
                              to the commanded closed                                                 N
                              position either in the manual    Immediately after boot up:
                              or automatic mode.            Bleed air manifold............. Pressurize         HYD
                                                            BAECS CHAN 1 and BAECS CHAN 2            O
                                                            MCBs................................... Pull, reset
                                                                                                            FLT CTRL
                                                                           NOTE                       P
                                                                If the BA/ECS CHAN  A FAIL                    GEAR
                                                                (A) or BA/ECS CHAN B FAIL             R
                                                                (A) ACAWS do not clear after
                                                                resetting the MCB, then an
                                                                airplane reboot will be required.     S     DOR/RMP
  PERF                                                      L ICE DETECT ECB (208)....................

                                                            ...................................... PULL, RESET  T  JETTISON
                                                            R ICE DETECT ECB (706)...................
                                                            ...................................... PULL, RESET  U
                                                            If the message is displayed after               LANDING
                                                            engine shutdown:
                                                            No crew action required. May be           V
                                                            considered a nuisance fault.                    DITCHING
                                                                                                     W
                                                                                                            BAILOUT
                                                                                                      X

  OPER                                                                                                      FAULT LG

                            Use, copying and/or disclosure is   1 -129
                            governed by the statement on the
                            title page of this document.  BACK                                               CHARTS
   152   153   154   155   156   157   158   159   160   161   162