TM 55-1510-222-10 b. Annunciation test switch Hold to TEST position. Check   that   the   annunciation   panels,   fire   pull   handle annunciators,    marker    beacon    annunciators,    antenna azimuth  indicator,  master  caution,  and  master  warning annunciators are illuminated.  Release switch and check that    all    annunciators    except    those    in    step    (a)    are extinguished. NOTE The Marker Beacon lights will illuminate only if the Avionics Master is turned ON/EXT PWR as applicable. c. MASTER  CAUTION  and  MASTER  WARNING annunciators   Press   and   release.      Both   annunciators should extinguish. 8-14.* FIRST ENGINE START (BATTERY START). NOTE The   engines   must   not   be   started until  after  the  INS  is  placed  into  the NAV mode or OFF, as required. Starting    procedures    are    identical    for    both    engines except that second engine generator is kept off line after the second engine start.  This allows performance of the current limiters check.  When making a battery start, the right   engine   should   be   started   first.   A   crewmember should   monitor   the   outside   observer   throughout   the engine start procedures. 1. Exterior lights switches As required. 2. Propeller area Clear. 3. #2    ignition    and    engine    start    switch    START IGNITION.  #2 IGN ON annunciation should illuminate   and   associated   FUEL   PRESS   light   should extinguish. NOTE False   fuel   flow   indications   may   be observed   with   the   starter   engaged and the condition lever in cutoff. CAUTION If  ignition  does  not  occur  within  10 seconds after moving condition lever to   LOW   IDLE,   initiate   Abort   Start procedure.        If    for    any    reason    a starting  attempt  is  discontinued,  the entire    starting    sequence    must    be repeated after allowing the engine to come  to  a  complete  stop  (1  minute minimum). 4. Condition   lever   (after   N.      RPM   passes   13% minimum) LOW IDLE. CAUTION Monitor  TGT  to  avoid  a  hot  start.    If there   is   a   rapid   rise   in   TGT,   be prepared   to   abort   the   start   before limits  are  exceeded.  During  starting, the maximum allowable TGT is 1000° C   for   5   seconds.      If   this   limit   is exceeded, use Abort Start procedure and   discontinue   start.      Enter   the peak   temperature   and   duration   on DA Form 2408-13. 5. TGT and N.  Monitor (TGT 1000°  C Maximum). 6. Oil pressure Check (60 PSI minimum). 7. #2  ignition  and  engine  start  switch  OFF  after TGT peaks. 8. Condition  lever  HIGH  IDLE.    Monitor   TGT  as the condition lever is advanced. 9. Generator switch RESET, then ON. 8-15.* SECOND ENGINE START (BATTERY START). 1. Propeller area Clear. 2. #1    ignition    and    engine    start    switch    START IGNITION.  #1 IGRN ON annunciation should illuminate and associated FUEL PRESS light should extinguish. 3. Condition   lever   (after   N.   RPM   passes   13% minimum) LOW IDLE. 4. TGT and N, Monitor (TGT 1000°  C maximum). 5. Oil pressure Check (60 PSI minimum). 6. #    ignition  and  engine  start  switch  OFF  after TGT peaks. 7. Condition levers HIGH IDLE. 8. Power levers GROUND FINE. 9. Propeller levers Retard to feather detent. 10. BATTERY   CHARGE   annunciation   Check   on. Annunciation should extinguish within 5 minutes following a normal engine start on battery. 11. Inverter switches ON, check INVERTER annunciators off. 12. Second  engine  generator  switch  RESET,  then ON. 13. Beacon light Reset.  then on. 8-10