Page 293 - (KU)01-75GAJ-1.5 - Change 1
P. 293

INTRO


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



                           Q1  ARE ALL GENERATORS STILL INOPERATIVE?                                         ACAWS


                              NO     B.  Icing conditions........................................ Exit immediately  GROUND


                              EoP    &   'LYHUW                                        7R QHDUHVW VXLWDEOH DLU¿HOG
                                                                                                            TAKEOFF
                                                                NOTE

                                           Full functionality of the pilot CNI-MU remains;
                                           however, only digitally displayed navigation data                FIRE/SMK
  NORM                                     is available.

                                                                NOTE                                        PRES/OXY

                                           The GHC must be used to change UHF 1 or
                                           VHF 1 radio transmit source selections. The ICS                 ENG/PROP
                                           control panels are failed.

                                                                NOTE                                           FUEL

                                           The IFF transponder is inoperative.
                                                                                                               AAR
                                     D.  Performance data.................................................. Review

                                           Compute performance data for inoperative anti-skid in
  SPEC                              NOT FOR FLIGHT                                                             ELEC
                                           WKH SODQQHG ODQGLQJ FRQ¿JXUDWLRQ
                                                                NOTE
                                                                                                               HYD
                                           Trim and anti-skid are inoperative. Consider
                                           ODQGLQJ LQ WKH FXUUHQW ÀDS FRQGLWLRQ WR PLQLPL]H
                                           elevator trim forces.                                            FLT CTRL

                                     Once below 10,000 feet MSL:
                                                                                                              GEAR
                                     E.  Nacelle shutoff switches........................................ CLOSE

                                           When below 10,000 feet MSL, select all engine nacelle            DOR/RMP
                                           shutoff switches to CLOSE to depressurize the aircraft.
  PERF

                                                                NOTE
                                                                                                            JETTISON
                                           :LWK WKH ORVV RI DOO JHQHUDWRUV  WKH RXWÀRZ YDOYH
                                           closes completely and the cabin pressurizes
                                           at approximately 6,000 feet per minute until                     LANDING
                                           regulated by the safety valve at maximum
                                           differential pressure. When below 10,000 feet,
                                           selecting all nacelle shutoff switches to CLOSE                  DITCHING
                                           allows the cabin to depressurize at approximately
                                           1,500 to 1,700 feet per minute. Approximately 10
                                           minutes is required for the cabin to completely                  BAILOUT
                                           depressurize from maximum differential pressure
  OPER                                     LQ WKLV FRQ¿JXUDWLRQ                                             FAULT LG

                            Use, copying and/or disclosure is   1 -253
                            governed by the statement on the
                            title page of this document.  BACK                                               CHARTS
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