Page 107 - (KU)01-75GAJ-1.5 - Change 1
P. 107

INTRO


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


                                                  1.2.3 ADVISORIES                                    B
                                                                                                             ACAWS
                                    Alert/Condition                    Crew Action
                              A/C PNL FAIL                                                            C
                             MC has lost communication with   SOFT PANEL, AIR COND.......... Utilize        GROUND
                             the AIR COND panel.                                                      D
                              A/C PNL FAULT                                                                 TAKEOFF

                             MC has detected an invalid     SOFT PANEL, AIR COND......................   E
                             switch/knob/etc. input from the   ............................... Utilize (as required)
                             AIR COND panel.                                                                FIRE/SMK
  NORM                        A/I AIR TEMP LOW                                                        F

                             Ice protection is on and the   HP........................................... Increase
                             BA/ECS has determined that                                              G      PRES/OXY
                             there is not enough bleed air      Advance at least two engines to
                             supply from the engines for ice    minimum HP shown on the power
                             protection.                        setting schedule in Chapter 12        H    ENG/PROP
                                                                (Required Power vs Altitude For
                                                                Two Engines During Anti-Icing/
                                                                Deicing Operations chart) or exit     I
                                                                icing conditions. The schedule                 FUEL
                                                                is 1,300 HP above 20,000 feet,
                                                                incrementally reducing power          L
                                                                by 100 HP every 5,000 feet until               AAR
                                                                reaching 5,000 feet when 750 HP
                                                                should be maintained.                M
  SPEC                              NOT FOR FLIGHT                                                             ELEC
                                                                If the scheduled HP is set,
                                                                EOHHG DLU VXSSO\ ZLOO EH VXI¿FLHQW    N
                                                                DQG ÀLJKW LQ LFLQJ FRQGLWLRQV LV
                                                                permissible, even if the A/I AIR               HYD
                                                                TEMP LOW (A) ACAWS does not          O
                                                                clear.
                              AA TACAN BCN BEARING FAIL                                               P     FLT CTRL
                             EGI 1 26 Vac TACAN synchro     Air-to-air TACAN Inverse Beacon
                             reference is lost.             Mode is not functional. All other EGI
                                                            attitude and navigation functions are     R       GEAR
                                                            operational.
                              ADC 1 (or 2) DEGRADED                                                   S     DOR/RMP

                             Respective Static Pressure     CADC (fully functional) (Pilot PFD data
  PERF                       Transducer Unit (SPTU) has     source)…...…..........................…. Select
                             failed.                                                                  T
                                                            Autopilot (pilot’s side)….........… Engage      JETTISON
                                                            CADC (degraded) (Copilot PFD data
                                                            source).....................................… Select  U
                                                                                                            LANDING

                                                                           NOTE                       V
                                                                In RVSM airspace, notify  ATC               DITCHING
                                                                of RVSM equipment failure and        W
                                                                comply with instructions.
                                                                                                            BAILOUT
                                                                                                      X

  OPER                                                                                                      FAULT LG

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