Page 354 - (KU)01-75GAJ-1.5 - Change 1
P. 354

INTRO


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


                         E.  Aircraft hydraulic system....................................................... Monitor
                                                                                                             ACAWS
                             Periodically scan aircraft and booster hydraulic reservoir for signs
                             RI ÀXLG ORVV RU OHDNDJH  0RQLWRU ERRVWHU UXGGHU ERRVW SUHVVXUH IRU
                             indication of booster system pressure (rudder pressure will be in              GROUND
                             ORZ ERRVW ZLWK ÀDSV UHWUDFWHG   %RRVWHU V\VWHP SUHVVXUH LQGLFDWLRQ
                             and HYD PMP 3 and 4 PRESS LO (C) ACAWS failed.
                                                                                                            TAKEOFF
                         F.  AIR COND panel, UNDERFLOOR switch.........................................
                          ......................................................................FAN (below 15,000’ MSL)
                                                                                                            FIRE/SMK
                             8QGHUÀRRU GXFW RYHUKHDW GHWHFWLRQ LV IDLOHG  %OHHG DLU OHDN GHWHFWLRQ
  NORM                       operative.
                                                                                                            PRES/OXY
                         G.  OIL COOLER FLAPS (No. 3 and No. 4).................... Select Manual
                                    NOT FOR FLIGHT
                             2LO FRROHU ÀDSV 1R    DQG   ZLOO IXOO\ H[WHQG
                                                                                                           ENG/PROP
                         H.  OIL COOLER FLAP (No. 2)....................................... Manual/OPEN

                             2LO FRROHU ÀDS 1R    QRW IDLO VDIH WR RSHQ OLNH 1R    DQG 1R                      FUEL
                             2LO  FRROHU  ÀDS  1R      FDQQRW  EH  FORVHG   0RQLWRU  UHPDLQLQJ  RLO
                             temperatures.
                                                                                                               AAR
                         Prior to landing:
  SPEC                   I.  Landing gear................................................................ Visually verify  ELEC


                             Visually verify landing gear position before landing or before
                             exceeding limiting speeds after gear retraction. Right main gear                  HYD
                             indication failed.

                         J.  Performance data................................................................. Review  FLT CTRL

                             If gear was up or ANTI SKID switch OFF at time of failure, then
                             anti-skid will be failed (ANTI-SKID FAIL (C) ACAWS is inhibited                  GEAR
                             when gear is up). In this case, use brakes cautiously since anti-
                             skid is not available. Determine takeoff/landing distance for anti-
                             skid inoperative.                                                              DOR/RMP
  PERF                   Prior to engine shutdown:

                                                                                                            JETTISON
                         K.  Aircraft..................................................................................... Chock

                             Ensure aircraft is chocked and use emergency brake pressure for
                             parking, normal brake pressure may bleed off when setting the                  LANDING
                             parking brake (parking brake valve will remain as-is).

                         L.  Potential Mission Impacts.................................................... Review  DITCHING

                               ‡  Failed Components:
                                                                                                            BAILOUT
                                       Engine No. 3 start valve
                                       Aux Feather pumps 2 and 3
  OPER                                                                                                      FAULT LG

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