Page 297 - (KU)01-75GAJ-1.5 - Change 1
P. 297

INTRO


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


                            INSTRUMENTS
                                                                                                             ACAWS
                            STAND-BY INSTRUMENTS:
                                  ‡  Attitude

                                     Powered by Utility Battery bus regardless of BTRY switch               GROUND
                                     position.

                                  ‡  Airspeed/altitude (vibrator)                                           TAKEOFF

                                     Powered by Utility Battery bus regardless of BTRY switch
                                     position.                                                              FIRE/SMK
  NORM                            ‡  Magnetic compass


                                     Electrical power not required.                                         PRES/OXY
                                  ‡  Pilot and copilot inclinometers

                                     Electrical power not required.                                        ENG/PROP
                            PFD:
                                  ‡  Airspeed and altitude indications may be erroneous in icing               FUEL
                                   conditions
                                  ‡  CDI and bearing pointers not functional                                   AAR

                            PANEL CONTROLS/DISPLAYS
  SPEC                              NOT FOR FLIGHT                                                             ELEC

                                                           NOTE

                                   Functionality of operable panels (to include soft panels)                   HYD
                                   may be severely limited due to loss of associated
                                   component power.
                            FUNCTIONAL HARD PANELS:                                                         FLT CTRL
                                  ‡  GEAR (landing and taxi lights failed)

                                  ‡  HYDRAULIC (engine pump control only; all other controls failed)          GEAR
                                  ‡  3LORW DQG FRSLORW 5() 02'(  ÀLJKW GLUHFWRU IDLOHG

                                  ‡  APU                                                                    DOR/RMP
  PERF                            ‡  BLEED AIR

                                  ‡  ELECTRICAL                                                             JETTISON
                                  ‡  ENGINE START (engine 1 and 4 start valves inoperative)

                                  ‡  FADEC (PMA supplies electrical power for switches)                     LANDING
                                  ‡  ICE PROTECTION (pilot and copilot pitot heat, NESA, propeller
                                   ice protection and vertical tail pneumatic boot failed)
                                                                                                            DITCHING
                                                           NOTE
                                                                                                            BAILOUT
                                   The fuel and mode annunciator panels are powered, but
                                   not functional due to associated component failures.
  OPER                                                                                                      FAULT LG

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