Page 302 - (KU)01-75GAJ-1.5 - Change 1
P. 302

INTRO


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


                         1.10.5.2 ECBU 2 FAIL*
                                                                                                             ACAWS
                         Condition:

                         The ECBU has failed or lost bus communication with the MC.                         GROUND


                        Q2  ARE MULTIPLE ACAWS DISPLAYED?                                                   TAKEOFF

                          NO      Conventional failure: All ECBs lose power and multiple failures           FIRE/SMK
  NORM                   Lost     DUH HYLGHQW RQ WKH ÀLJKW GHFN  7KH $&$:6 DVVRFLDWHG ZLWK D
                                  conventional failure are:
                         Bus
                         Comm      ‡   CP AMU FAIL (C)                                                      PRES/OXY
                         failure
                                   ‡   CP HUD FAIL (C)
                                                                                                           ENG/PROP
                                   ‡   ADC 2 FAIL (C)
                                   ‡   PUSHER OFF (C)
                                                                                                               FUEL
                                   ‡   CP PITOT HEAT FAIL (C)

                                   ‡   HDD 2 FAIL (A)
                                                                                                               AAR
                                   ‡   HDD 4 FAIL (A)
  SPEC                             ‡  NOT FOR FLIGHT                                                           ELEC
                                       DSDTS FAIL (A)
                                   ‡   BAU I #1 FAIL* (A)
                                   ‡   BAU I #2 FAIL* (A)                                                      HYD

                                   ‡   BAU I #4 FAIL* (A)
                                   ‡   TAWS PWR (A)                                                         FLT CTRL

                                  $   'LVSOD\V                                     5HFRQ¿JXUH  DV UHTXLUHG
                                                                                                              GEAR
                                  B.  Copilot air data source.............................. Select CADC 1
                                       Re-enables autopilot.
                                                                                                            DOR/RMP
  PERF                            C.  Autopilot .....................................Re-engage (as required)

                                  D.  Icing conditions..........................................................Avoid  JETTISON
                                       Copilot upper right pitot,  TAT  probe  and  right AOA
                                       vane heat failed. NESA heat failed.
                                                                                                            LANDING
                                  (   6ORZ ÀLJKW                            $YRLG EHORZ DSSURDFK VSHHGV

                                       Stick pusher inoperative. Stall warning operative but                DITCHING
                                       degraded at high sideslip angles.
                                  F.  Potential Mission Impacts....................................... Review  BAILOUT

                                   ‡   NESA heat failed. Maximum speed below 10,000 feet
  OPER                                 MSL is 187 KIAS.                                                     FAULT LG

                                                         1 -262            Use, copying and/or disclosure is
                                                                           governed by the statement on the
                                                         BACK              title page of this document.      CHARTS
   297   298   299   300   301   302   303   304   305   306   307