TM 1-1510-224-10 q. BATTERY switch - As required. r. GENERATOR switches (2) - OFF. s. # 2 ENG START switch - OFF. t. # 2 AUTO IGNITION switch - Off. * 4. Fuel panel switches - Check. a. STANDBY PUMP switches (2) - Off. b. AUX XFER switches (2) - AUTO. c. CROSSFEED switch - OFF. 5. Magnetic     compass     -     Check     for     fluid, heading, and current correction card. CAUTION Movement     of     the     POWER     levers below   the   flight   idle   gate   with   the engines  not  operating  may  result  in bending and damage to control linkage. * 6. Pedestal controls - Set. a. POWER levers - IDLE. b. PROP levers - FEATHER. c. CONDITION levers - FUEL CUTOFF. d. Flaps - As required. * 7. Pedestal extension switches - Set. a. Avionics - As required. b. RUDDER BOOST switch - On. c. ELEV TRIM switch - On. 8. LANDING GEAR ALTERNATE EXTENSION pump handle - Stowed. 9. Free  air  temperature  gage  -  Check.    Note current reading. 10. Pilot's instrument panel - Check and set. a. MIC switch - HEADSET. b. GYRO switch - SLAVE. c. SYM GEN REV switch - NORMAL. d. Flight instruments - Check instruments     for     protective     glass, warning flags, and static readings. e. PROP SYN switch - OFF. f. Engine instruments - Check instruments  for  protective  glass  and static readings. 11. Copilot's   instrument   panel   -   Check   and set. a. Flight instruments - Check instruments     for     protective     glass, warning flags, and static readings. b. MIC switch - HEADSET. c. GYRO switch - SLAVE. d. SYM GEN REV switch - NORMAL. 12. Mission panel switches and circuit breakers - As required. a. ANT ORIDE switch - AUTO ROTATE. b. MISSION CONTROL switch - OFF. 13. Subpanels - Check and set. a. ENG   FIRE   TEST    switches    (2)    - OFF. b. CABIN    PRESS    DUMP    switch    - OFF. c. Pressurization controls - As required. d. LANDING,  TAXI, and   RECOG  light switches - OFF. e. LDG GEAR CONTR switch - Recheck DN. f. CABIN LIGHTS switch - As required. g. PILOTS   STATIC   AIR   SOURCE   - NORMAL. CAUTION Do   not   use   alternate   static   source during  takeoff  and  landing  except  in an     emergency.          Instruments     will show    a    variation    in    airspeed   and altitude   when   using   alternate   static source. 14. AC and  DC GPU - As required. * 15. BATTERY switch - ON. 16. DC  power  -  Check  (22  VDC  minimum  for battery,     28     VDC     maximum     for     GPU starts). 17. Annunciator panels - Test as follows: a. ANNUNCIATOR     TEST switch - Hold to 8-15