Page 538 - (KU)01-75GAJ-1.5 - Change 1
P. 538

INTRO


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


                         3.8 FLAPS-UP OPERATION
                                                                                                             ACAWS
                         3.8.1 FLAPS-UP TAKEOFF

                          1. WING FLAP CNTL electronic circuit breaker (ECB 485)....................Pull    GROUND
                          2. FLAPS lever...........................................................................20 %

                          3.  Take off using normal procedures including the normal target pitch            TAKEOFF
                          DWWLWXGH DQG WDNHRII WULP VHWWLQJV  5HIHU WR  .8      *$-     IRU ÀDSV XS
                          performance.
                             :KHQ DERYH )866  UDLVH WKH )/$36 KDQGOH  ,I WKH ÀDSV DUH WR                    FIRE/SMK
  NORM                    remain stationary, leave ECB 485 pulled.

                                                                                                            PRES/OXY
                         3.8.2 FLAPS-UP LANDING
                                    NOT FOR FLIGHT
                                                        NOTE
                                                                                                           ENG/PROP
                              The GCAS ‘‘TOO LOW FLAP’’ message will occur during
                              WKH ÀDSV XS DSSURDFK XQOHVV LW LV LQKLELWHG E\ WKH )/$3
                              INHIBIT selection on the AMU GCAS page.                                          FUEL
                          1. Determine High Speed Landings procedure requirements.

                             ([WHQG GRZQZLQG DQG EDVH OHJV WR     SHUFHQW RI D QRUPDO ÀDSV                     AAR
                          GRZQ WUDI¿F SDWWHUQ  )O\ D VKDOORZ DSSURDFK  HVSHFLDOO\ DW KHDYLHU
                          JURVV ZHLJKWV  WR DYRLG ODQGLQJ IDVW  'R QRW H[HFXWH D ODUJH ÀDUH WR
  SPEC                    DYRLG ÀRDWLQJ WR D ORQJ ODQGLQJ DQG WRXFKLQJ GRZQ DW DQ H[WUHPH                      ELEC
                          pitch attitude.
                          3. After touchdown, hold nosewheel off the runway, if necessary,
                          until below the 139-knot ground speed limit.                                         HYD

                          4.  Check for B indications in the HP gauges and for airspeed less
                          than 145 KTAS prior to moving the power levers to GND IDLE.
                                                                                                            FLT CTRL

                                                      CAUTION
                                                                                                              GEAR
                              'R QRW EULQJ WKH SRZHU OHYHUV EHORZ ÀLJKW LGOH DW JUHDWHU
                              than 145 KTAS. This can result in all four engine generators
                              tripping off line because of an over frequency condition.                     DOR/RMP
  PERF                        All ac electrical power will be lost resulting in the loss of
                              antiskid protection and increased landing distances. If hard
                              braking is being applied when ac power is lost, main tires                    JETTISON
                              could blow resulting in possible loss of directional control
                              and damage to the gear doors and surrounding structure.
                                                        NOTE                                                LANDING

                              If only three Bs are present after touchdown, all power levers can
                              be moved to GND IDLE, but anticipate a possible minor swing                   DITCHING
                              away from the engine with no B. Reverse engines normally,
                              based on BETA indications. If more than one B is not present
                              on operating engines, it is most likely because the airspeed is
                              too fast. Continue slowing and wait for the Bs if runway length is            BAILOUT
                              not critical. If runway length is critical, execute a go-around. An
                              additional landing at the correct speed should be attempted.
  OPER                                                                                                      FAULT LG

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