Page 414 - (KU)01-75GAJ-1.5 - Change 1
P. 414

INTRO


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


                         1.12.5.3 Horizontal Tail (One or Both Zones) Ice
                         Accumulation                                                                        ACAWS


                         $   $SSURDFK ÀDS VHWWLQJ
                                                                                                            GROUND
                             )O\ DSSURDFK DQG ODQGLQJV ZLWK    SHUFHQW ÀDSV  'R QRW VHOHFW
                             SHUFHQW ÀDSV
                                                                                                            TAKEOFF

                                                     WARNING
                                                                                                            FIRE/SMK

  NORM                          6HOHFWLQJ     SHUFHQW ÀDSV ZLWK LFH DFFXPXODWHG RQ WKH
                                horizontal tail may lead to pitch instability and loss of
                                control.                                                                    PRES/OXY
                                    NOT FOR FLIGHT
                         (End of Procedure)
                                                                                                           ENG/PROP


                         1.12.5.4 Vertical Tail Ice Accumulation                                               FUEL



                                                     WARNING                                                   AAR


  SPEC                          Relatively low rudder force inputs by the pilot can result                     ELEC
                                in exceeding safe side slip limits. Carefully monitor
                                HUD side slip display during low speed maneuvering
                                especially at high power settings.
                                                                                                               HYD

                                                        NOTE
                                                                                                            FLT CTRL
                                Empennage bleed air isolation or vertical tail ice
                                protection system failures while the wing/empennage
                                ice protection system is operating with ice detected,                         GEAR
                                results in activation of a X-WIND LIMITED (C) ACAWS.
                                This cannot be reset until the aircraft has slowed below
                                60 knots on the ground.                                                     DOR/RMP
  PERF

                        Q1  IS THE CROSSWIND COMPONENT GREATER                                              JETTISON
                           THAN 15 KNOTS?

                           NO                                                                               LANDING
                                  A.  Divert............................................................... As required
                           EoP
                                       Consider diversion to an alternate airport with
                                       suitable crosswinds.                                                 DITCHING

                                  (End of Procedure)
                                                                                                            BAILOUT
                         No further action is required.

  OPER                   (End of Procedure)                                                                 FAULT LG

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