TM 1-1510-224-10 TEST position. Check that annunciator     panels,     FIRE     PULL handle annunciators, MASTER CAUTION, and MASTER WARNING annunciators are illuminated. b. MASTER   CAUTION and   MASTER WARNING  annunciators  Press  and release.    Both  annunciators  should extinguish. 8-14.  FIRST ENGINE START (BATTERY START). NOTE Do   not   start   engines   until   after   the INS  is  placed  into  the  NAV  mode  or OFF, as required. Starting procedures are identical for both engines. 1. INS - OFF. 2. EXTERIOR LTS switches - As required. 3. Propeller area - Clear. 4. ENG  START  switch  -   START-IGNITION. IGN ON annunciator should illuminate and FUEL PRESS annunciator should extinguish. NOTE False   fuel   flow   indications   may   be observed   with   the   starter   engaged and   the   CONDITION   lever   in   FUEL 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  (15  minute minimum). 5. CONDITION lever (after N₁ RPM stabilizes   above   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, initiate Abort Start procedure and discontinue start. Enter     the     peak     temperature     and duration on DA Form 2408-13-1. 6. TGT    and    N1    Monitor    (TGT    1000°    C maximum). 7. Oil pressure Check (60 PSI minimum). 8. ENG START switch OFF after TGT peaks. 9. CONDITION   lever   HIGH   IDLE.      Monitor TGT as CONDITION lever is advanced. 10. GENERATOR switch RESET, then ON. * 8-15.  SECOND ENGINE START (BATTERY START). 1. GENERATOR  DC  LOAD  Verify  less  than 50%. 2. Propeller area Clear. 3. ENG    START    switch    START-IGNITION. IGN ON annunciator should illuminate and FUEL PRESS annunciator should extinguish. 4. CONDITION lever (after Nl RPM stabilizes above 13% minimum) LOW IDLE. 5. TGT    and    Nl    Monitor    (TGT    1000°    C maximum). 6. Oil pressure Check (60 PSI minimum). 7. ENG START switch OFF after TGT peaks. 8. CONDITION  levers  HIGH  IDLE.    Monitor TGT as CONDITION lever is advanced. CAUTION Monitor oil temperature closely during ground operation with propellers in FEATHER due to lack of air flow over oil cooler. 9. PROP levers HIGH RPM. 10. INVERTER switches ON, check INVERTER annunciators off. 8-16