TM 1-1510-225-10 2-109 Section X.  LIGHTING 2-73.  EXTERIOR LIGHTING. Exterior lighting consists of navigation lights, two strobe     beacons,     three     white     strobe     lights,     two recognition  lights,  two  ice  lights,  two  tail  floodlights, and an entry light.  Refer to Figure 2-32 for details and locations. a.   Navigation  Lights.     One  navigation  light  is located  on  the  aft  end  of  the  aft  portion  of  the  vertical stabilizer   and   one   standard   navigation   light   on   the outside  of  each  wing  tip.    The  navigation  lights  are controlled    by,    and    the    circuit    is    protected   by,   a 5-ampere    circuit    breaker    switch,    placarded     NAV, located on the pilot's subpanel. b.  Strobe   Beacons.       One   strobe   beacon   is installed on the underside of the fuselage, and another is  installed  on  top  of  the  horizontal  stabilizer.    These lights   are   cont rolled   by,   and   a   10-ampere   circuit- breaker  switch,  placarded    BEACON,  located  on  the pilot's subpanel protects their circuits. c.   Strobe   Lights.       One   white   strobe   light   is installed  on  each  wing  tip  and  one  is  installed  on  the tail.      A   5-ampere   circuit-breaker   switch,   placarded STROBE,   located   on   the   pilot's   subpanel   controls these lights and protects their circuits. NOTE Landing lights are not automatically turned off when the landing gear is retracted. d.  Landing   Lights.      Dual   landing   lights   are mounted  on  the  nose  gear  assembly.    The  lights  are controlled  by,  and  the  circuits  are  protected  by,  two 10-ampere circuit-breaker switches placarded LANDING  LEFT   and  LANDING   RIGHT,  located  on the pilot's subpanel.  A green advisory light, placarded LDG / TAXI LIGHT, located on the aircraft annunciator panel, indicates illumination of the landing lights. NOTE The  taxi  light  is  not  automatically  turned off when the landing gear is retracted. e.   Taxi Light.  A single taxi light is mounted on the  nose  gear  assembly.    The  taxi  light  is  controlled by, and the circuit is protected by, a 15-ampere circuit- breaker switch, placarded  TAXI,  located  on  the  pilot's subpanel.    A  green  advisory  light,  placarded  LDG /   TAXI LIGHT, located on the aircraft annunciator panel indicates the illumination of the taxi light. f.    Ice Lights.   The ice lights are controlled by, and   the   circuit   is   protected   by,   a  5-ampere   circuit- breaker switch, placarded ICE, on the pilot's subpanel. g.  Recognition   Lights.       A   white   recognition light is mounted in the leading edge of each wing tip.   The recognition lights are controlled by, and the circuit is protected by, a 7-1/2-ampere circuit-breaker switch, placarded RECOG, located on the pilot's subpanel. h.  Tail Floodlights  R .  A white tail floodlight is mounted on the outboard underside of each horizontal stabilizer    to    illuminate    each    side    of    the    vertical stabilizer.    The  tail  floodlights  are  controlled  by,  and the   circuit   is   protected   by,   a   7-1/2-ampere   circuit- breaker switch placarded TAIL FLOOD, located on the pilot's subpanel. i.    Entry   Light.      A   flush-mounted    floodlight, located forward of the flap on the bottom surface of the left wing, provides illumination of the ramp area around the  airstair  door.    The  threshold  light  switch  that  is located   just   inside   the   cabin   door   on   the   forward doorframe  controls  the  entry  light.   The  entry  light  will extinguish    automatically    when    the    cabin    door    is closed. 2-74.  INTERIOR LIGHTING. a.   Cockpit Lighting. (1)   Master   Panel   Lights   Switch.      A   switch placarded   MASTER   PANEL   LIGHTS   ON   /    OFF, located on the overhead control panel controls cockpit lighting.      Refer   to   Figure   2-31   for   interior   lighting switches and locations. (2)   Overhead  Flood  Lights.    Two  overhead floodlights are installed in the cockpit to provide overall illumination  of  the  entire  cockpit  area.    The  lights  are controlled by a rheostat switch placarded OVERHEAD FLOODLIGHTS BRT / OFF, located on the overhead control   panel.      The   overhead   floodlights   circuit   is protected by a 7-1/2-ampere circuit breaker placarded SUB  PNL,  OVHD  &  CONSOLE  located  on  the  right sidewall circuit breaker panel. (3)   Instrument  Indirect  Lights.    Lights  in  the glareshield  provide  indirect  lighting  to  the  instrument panel.  The instrument indirect lights are controlled by a rheostat switch placarded  INSTRUMENT INDIRECT LIGHTS, BRT /  OFF, located on the overhead control panel.  The instrument indirect light circuit is protected by    a   5 -ampere    circuit    breaker    placarded    INSTR INDIRECT, located on the right sidewall circuit breaker panel.