Page 376 - (KU)01-75GAJ-1.5 - Change 1
P. 376

INTRO


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



                                                      CAUTION                                                ACAWS


                                Oil cooler augmentation, oil temperature display and                        GROUND
                                OIL 1 (2, 3 or 4) HOT (C) ACAWS are not available. The
                                possibility of engine damage from high oil temperature
                                after landing increases with the ambient temperature,
                                tailwind, power lever angle and length of engine                            TAKEOFF
                                operation after landing. Consider engine shutdown as
                                soon as practicable after landing.
                                                                                                            FIRE/SMK

  NORM                                                  NOTE
                                                                                                            PRES/OXY
                                    NOT FOR FLIGHT
                                ATCS is inoperative. If executing a go-around in BIU
                                Backup mode, consider limiting power on the outboard
                                engines until reaching V  .                                                ENG/PROP
                                                       MPR
                         D.  Before Landing checklist......................................“Complete” (PM)
                                                                                                               FUEL



                                                                                                               AAR
                         AFTER LANDING CHECKLIST

  SPEC                     A.  WING/EMP switch...........................................................OFF (CP)  ELEC




                                                      CAUTION                                                  HYD


                                The vertical tail leading edge components can be                            FLT CTRL
                                damaged if the wing/empennage ice protection system
                                is allowed to operate on the ground. The system is not
                                locked out below 60 knots.                                                    GEAR

                         B.  DEICE TIMER A and B ECBs (441, 890)...........Verify OPEN (CP)
                                                                                                            DOR/RMP
  PERF
                                                      CAUTION
                                                                                                            JETTISON

                                If the WOW sensing fails, the propeller ice protection will
                                remain on after landing. To prevent possible propeller                      LANDING
                                spinner dome heat damage, verify the DITU ECBs are open.

                         C.  PITOT HEAT ECBs (705, 247, 204, 207)......................PULL (CP)            DITCHING
                         D.  SAFETY VLV OPEN ECB (639).......................Verify RESET (CP)
                         E.  Exterior lights..................................................................“Set” (CP)  BAILOUT
                         F.  FLAPS.....................................................“____” (as required) (CP)
                         * ௘  7   DEFENSIVE SYSTEMS MASTER switch.................“STBY” (CP)
  OPER                                                                                                      FAULT LG

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