Page 545 - (KU)01-75GAJ-1.5 - Change 1
P. 545

INTRO


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


                            4.1 PERFORMANCE DATA
                                                                                                             ACAWS
                            The tabular performance data provided in this section is referred
                            to as tab data. This tab data is a subset of the data available in the
                            Performance Manual. Tab data should be used in conjunction with the             GROUND
                            GDWD LQ WKH 3HUIRUPDQFH 0DQXDO IRU ÀLJKW SODQQLQJ

                            7KH &1, 08 72/' LV DQ DGYLVRU\ V\VWHP  72/' VSHHGV DQG GLVWDQFHV                TAKEOFF
                            WKDW DUH FULWLFDO IRU ÀLJKW VDIHW\ PXVW EH FURVV FKHFNHG EHIRUH &1, 08
                            72/' LV XVHG IRU ÀLJKW RSHUDWLRQV  7KH FULWLFDO &1, 08 72/' LV YHUL¿HG
                            E\ FURVV FKHFNLQJ DJDLQVW WKH WDE GDWD  :KHQ WKH FULWLFDO &1, 08 72/'           FIRE/SMK
  NORM                      GDWD LV YHUL¿HG WKH UHPDLQGHU RI WKH &1, 08 72/' PD\ DOVR EH XVHG

                            7KH  WDNHRII  WDE  GDWD  FRQVLVWV  RI  5RWDWLRQ  6SHHG   9     2EVWDFOH         PRES/OXY
                                                                                    R
                                    NOT FOR FLIGHT
                            &OHDUDQFH 6SHHG  9  2%6   DQG 5HIXVDO 'LVWDQFH  7KH WDE GDWD 5HIXVDO
                            Distance is based on refusal initiated at V  and the use of reverse thrust
                                                                    R
                            RQ WZR  V\PPHWULF HQJLQHV  7KH WDNHRII WDE GDWD LV DSSOLFDEOH IRU              ENG/PROP
                            SHUFHQW ÀDSV DQG QRUPDO WDNHRII WHFKQLTXH RQO\

                            The landing tab data consists of  Threshold Speeds and Landing                     FUEL
                            *URXQG  5ROO   7KUHVKROG  6SHHGV  DUH  SURYLGHG  IRU  DOO  ÀDS  VHWWLQJV
                            /DQGLQJ *URXQG 5ROO GDWD LV SURYLGHG IRU     SHUFHQW ÀDSV  QRUPDO DQG
                            maximum effort techniques. The Landing Ground Roll data is based on                AAR
                            the use of reverse thrust on two, symmetric engines.

  SPEC                      7KH       SHUFHQW  IDFWRU  QRUPDOO\  DSSOLHG  WR  WKH  WDLOZLQG  FRPSRQHQWV        ELEC
                            has been accounted for in the calculation of the Refusal Distance and
                            Landing Ground Roll.  Therefore, the reported tailwind component
                            should be used with the tab data.                                                  HYD

                            7KH &1, 08 FDQ SURGXFH 72/' IRU FRQGLWLRQV WKDW DUH RXWVLGH WKH UDQJH
                            RI WKH WDE GDWD  7R YDOLGDWH &1, 08 72/' IRU WKH IROORZLQJ VLWXDWLRQV           FLT CTRL
                            XVH  WKH  &1, 08  72/'  YHUL¿FDWLRQ  SURFHGXUH  LQ  WKH  3HUIRUPDQFH
                            0DQXDO  &KDSWHU
                                                                                                              GEAR
                                  t  Takeoff or landing RCR less than 12.


                                  t  7DNHRII 56& JUHDWHU WKDQ                                               DOR/RMP
  PERF
                                  t  3UHVVXUH DOWLWXGH JUHDWHU WKDQ       IHHW
                                                                                                            JETTISON

                                                           o
                                                                                o
                                  t  7HPSHUDWXUH OHVV WKDQ    & RU JUHDWHU WKDQ     C.
                                                                                                            LANDING
                                  t  V  or Touchdown Speed is increased for wind gust increment.
                                     R
                                  t  &URVVZLQG FRPSRQHQW JUHDWHU WKDQ    NQRWV IRU WDNHRII  RU              DITCHING
                                   NQRWV IRU ODQGLQJ   DQG WKH YDOXH IRU 9   RU 7RXFKGRZQ 6SHHG
                                                                         R
                                   plus the gust increment falls in the caution area of the respective
                                   crosswind chart and is increased.                                        BAILOUT
                                  t  7DLOZLQG JUHDWHU WKDQ   NQRWV XS WR    NQRWV
  OPER                                                                                                      FAULT LG

                                                              -
                            Use, copying and/or disclosure is   43
                            governed by the statement on the
                            title page of this document.  BACK                                               CHARTS
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