TM 1-1510-218-10 2-119 the  individual  warning  annunciator  lights.    Table  2-12 provides    a    list    of    causes    for    illumination    of    the individual    caution/advisory    annunciator    lights.        In frontal view, both panels present rows of small opaque rectangular   indicator   lights.      Word  printing  on  each indicator  identifies  the  monitored  function  situation  or fault  condition,  but  cannot  be  read  until  the  light  is illuminated.   The bulbs of all annunciator panel lights are   tested   by   activating   the   ANNUNCIATOR   TEST switch,   which   is   located   on   the   right   side   of   the caution/advisory  panel.    The  system  is  protected  by two  5-ampere  circuit  breakers,  placarded   ANN  PWR and  ANN  IND,  on  the  overhead  circuit  breaker  panel, Figure   2 -16.       The   annunciator   system   lights   are dimmed when the MASTER PANEL LIGHTS switch is actuated and the pilot's flight instrument lights are on.   The    lights    are    automatically    reset    to    maximum brightness if any of the following conditions exist. (1)   The main aircraft power (both dc generators) are off. (2)   The  INST  INDIRECT  LIGHTS  switch  is on. (3)   The  MASTER PANEL LIGHTS switch is off. (4)   The  MASTER PANEL LIGHTS switch is ON and the PILOT INST LIGHTS switch is OFF. b.  Annunciator Panels  D2  T . NOTE  T2 On    C-12T2     aircraft     equipped     with     the Aviation     Night     Vision     Imaging     System (ANVIS), the annunciator lighting is ANVIS green  and  ANVIS  yellow .    Both  pilot  and copilot  sides  have  a  master  warning  light (ANVIS   yellow)   and   master   caution   light (ANVIS    green)    with    a    PRESS    TO    TEST switch located in the right inboard subpanel section. The warning annunciator panel is located in the glareshield    immediately    above    the    fire extinguisher system controls on the instrument    panel.       The    caution/advisory panel is located on the subpanel.   In other respects,   the   annunciator   panels   are   as described in the following paragraph. Table 2-11.  C-12  Warning Annunciator Panels NOMENCLATURE COLOR CAUSE FOR ILLUMINATION AIRCRAFT EFFECTIVITY C  D1 #1 FUEL PRESS Red Fuel pressure failure on left side. All #2 FUEL PRESS Red Fuel pressure failure on right side. All L BL AIR FAIL Red Left  bleed  air  warning  line  has  melted  or  failed  indicating possible loss of #1 engine bleed air. All R BL AIR FAIL Red Right bleed air warning line has melted or failed, indicating possible loss of #2 engine bleed air. All ALT WARN Red Cabin altitude exceeds 12,500 feet. All INST AC Red No AC power to engine instruments. All AP TRIM FAIL Red Trim won’t run or running opposite direction commanded. All #1 CHIP DETR Red Contamination of #1 engine oil detected. All #2 CHIP DETR Red Contamination of #2 engine oil detected. All D2 T1 ALT WARN Red Cabin altitude exceeds 12,500 feet. All INSTR AC Red No AC power to engine instruments. All #1 FUEL PRESS Red Fuel pressure failure on left side. All A/P TRIM FAIL Red Trim won’t run or running opposite direction commanded. All A/P DISC Red Autopilot is disconnected. All #2 FUEL PRESS Red Fuel pressure failure on right side. All