Page 340 - (KU)01-75GAJ-1.5 - Change 1
P. 340

INTRO


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


                                                        NOTE
                                                                                                             ACAWS
                                LANDING GEAR and TOO LOW GEAR Special Alerts
                                will annunciate during approach.
                                                                                                            GROUND
                         C.  Autopilot PITCH......................................................................... OFF

                             Autopilot pitch axis will not engage.
                                                                                                            TAKEOFF
                         D.  Icing conditions...................................................... Avoid, if practical

                             A failure of the primary vertical tail boot de-icing timer may not be          FIRE/SMK
  NORM                       reported.


                         E.  Landing gear............................................................... Visually verify  PRES/OXY
                                    NOT FOR FLIGHT
                             Right main landing gear indication failed. Visually verify landing
                             gear position before landing or before exceeding limiting speeds              ENG/PROP
                             after gear retraction.

                         F.  Aircraft hydraulic systems..................................................... Monitor  FUEL

                             Booster system pressure indication and HYD PMP 3 and 4 PRESS
                             LO (C)  ACAWS failed. Periodically scan aircraft and booster                      AAR
                             K\GUDXOLF  UHVHUYRLU  IRU  VLJQV  RI  ÀXLG  ORVV  RU  OHDNDJH   0RQLWRU
                             booster rudder boost pressure for indication of booster system
  SPEC                       SUHVVXUH  UXGGHU SUHVVXUH ZLOO EH LQ ORZ ERRVW ZLWK ÀDSV UHWUDFWHG                ELEC

                         G.  UNDERFLOOR switch.......................... OFF (below 15,000 ft MSL)

                             8QGHUÀRRU GXFW RYHUKHDW GHWHFWLRQ IDLOHG  %OHHG DLU OHDN GHWHFWLRQ                HYD
                             operative.
                         H.  Potential Mission Impacts..................................................... Review  FLT CTRL


                               ‡  Hydraulic pumps No. 3 and No. 4 fail-safe on. Hydraulic pumps
                                No. 3 and No. 4 cannot be isolated using the HYDRAULIC                        GEAR
                                ENGINE PUMPS, BOOST (No. 3 and No. 4) switches in the
                                event of a hydraulic leak. Engine shutdown may be required.
                                                                                                            DOR/RMP

  PERF                                                  NOTE

                                                                                                            JETTISON
                                These values may remain in their last state if BAU lost
                                1553 bus communications but is still powered.
                                                                                                            LANDING
                               ‡  Right landing light inoperative.

                                                        NOTE                                                DITCHING

                                This item may remain in its last state if BAU lost 1553
                                bus communications but is still powered.                                    BAILOUT

                               ‡  IFF 1 degraded: ZEROIZE not functional. ZEROIZE the IFF via
  OPER                          pushbutton switch on front of IFF RT.                                       FAULT LG

                                                         1 -300            Use, copying and/or disclosure is
                                                                           governed by the statement on the
                                                         BACK              title page of this document.      CHARTS
   335   336   337   338   339   340   341   342   343   344   345