Page 413 - (KU)01-75GAJ-1.5 - Change 1
P. 413

INTRO


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


                            1.12.5.1 Landing with Ice Accumulation
                                                                                                             ACAWS
                            A.  Leading edge surfaces........................................................... Check

                                 Check leading edge surfaces for ice accumulation.                          GROUND


                                                           NOTE
                                                                                                            TAKEOFF
                                   The wing zones and the outboard 1/3 of the horizontal
                                   tail ice protection zones are visible from the cargo
                                   FRPSDUWPHQW ÀLJKW VWDWLRQ  ,FH DFFXPXODWLRQ ZLOO EHJLQ                   FIRE/SMK
  NORM                             to melt/shed when  TAT is maintained above 10º C.
                                   Depending on the amount and type of accumulation,
                                   EHWZHHQ    WR    PLQXWHV VKRXOG EH VXI¿FLHQW WR FOHDU                    PRES/OXY
                                   most buildups from the leading edge surfaces. Ice on the
                                   nose radome may take longer. The unprotected inboard
                                   wing section can be used as a conservative guide for
                                   clearing of ice on the empennage.                                       ENG/PROP

                            B.  Affected ice protection zone procedure.......................... Accomplish
                                                                                                               FUEL
                                 Comply with each procedure that applies if ice accumulation is
                                 suspected on one or more ice protection zones.
                                                                                                               AAR
                            (End of Procedure)

  SPEC                              NOT FOR FLIGHT                                                             ELEC
                            1.12.5.2 Wing (One or More Zones) Ice Accumulation


                                                                                                               HYD
                                                         WARNING

                                                                                                            FLT CTRL
                                   Stalls with an asymmetric ice buildup on the wings may
                                   result in an uncontrollable rolling tendency which may
                                   occur prior to stick pusher activation.                                    GEAR

                            A.  Approach and Threshold airspeed...................................... Increase
                                                                                                            DOR/RMP
                                  Approach and Threshold Airspeed Correction Table
  PERF                             FLAP SETTING         SPEED CORRECTION

                                                                                                            JETTISON
                                        0%                   + 20 knots, do not add gust factor
                                        50%                  + 10 knots, do not add gust factor
                                                                                                            LANDING
                                        100%                 + 6 knots, add gust factor up to 10

                                                             knots cumulative total
                                                                                                            DITCHING
                            B.  Touchdown airspeed..................................... Increase (as required)
                                 )RU DOO ÀDS FRQ¿JXUDWLRQV  DGG WKH JXVW IDFWRU WR WRXFKGRZQ VSHHGV         BAILOUT
                                 in accordance with the Performance Manual.

  OPER                      (End of Procedure)                                                              FAULT LG

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