TM 1-1510-262-10
d. PROP SYNC switch -- OFF.
e. Engine instruments -- Check instruments for protective glass and static readings. (DC instruments
should show the needle parked at the minimum travel position.)
13. Copilot s instrument panel -- Check and set.
a. MIC switch -- HEADSET.
b. HDG AHRS #2 -- NORM.
c. ADF -- BOTH
d. PFD -- Check screen is clean and inclinometer ball centered and full of luid.
e. APR-39 Power -- OFF and MODE 1/2 as required.
f. APR-44 Power -- OFF
g. MFD -- Check screen is clean.
h. Weather Radar Control Panel MODE select -- OFF.
14. Mission panel switches and circuit breakers -- As required.
15. Subpanels -- Check and set.
a. CABIN PRESS DUMP switch -- OFF
b. Pressurization controls -- As required.
c. LANDING , TAXI , and RECOG light switches -- OFF.
d. LDG GEAR CONTROL switch -- Recheck DN.
e. CABIN LIGHTS switch -- As required.
f. PILOTS STATIC AIR SOURCE -- NORMAL.
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.
16.
AC and DC GPU -- As required.
* 17.
BATTERY switch -- ON.
18.
DC power -- Check (22 VDC minimum for battery, 28 VDC maximum for GPU starts).
19.
Pilots chronometer -- Check and set.
20.
Copilots chronometer -- Check and set.
*8-15. FIRST ENGINE START (BATTERY START).
1. EXTERIOR LTS switches -- As required.
2. Propeller area -- Clear.
3. ENG START switch -- START IGNITION . IGN ON annunciator should illuminate and FUEL PRESS
annunciator should extinguish.
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 se-
quence must be repeated after allowing the engine to come to a complete stop (15-minute minimum).
NOTE
False fuel low indications may be observed with the starter engaged and the CONDITION lever in
FUEL CUTOFF.
4. CONDITION lever (after N 1 RPM stabilizes above 13% minimum) -- LOW IDLE.
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