TM 1-1510-224-CL
2.
ENG START switch - START-IGNITION. IGN ON
annunciator
should
illuminate
and
FUEL
PRESS
annunciator should extinguish.
3.
CONDITION lever (after N1 RPM stabilizes above 13%
minimum) - LOW IDLE.
4.
TGT and N, - Monitor (TGT 10000 C maximum).
5.
Oil pressure - Check (60 PSI minimum).
6.
ENG START switch - OFF after TGT peaks.
7.
AC and DC GPU units - Disconnect (check aircraft
external power and mission external power annunciators
extinguished).
8.
CONDITION lever - HIGH IDLE. Monitor TGT as
CONDITION levers are advanced.
9.
PROP levers - HIGH RPM.
10.
#1 and #2 INVERTER switches - ON. Check
INVERTER annunciators extinguished.
11.
GENERATOR switch (1) - RESET, then ON.
12.
Current limiters - Check.
13.
GENERATOR switch - RESET, then ON.
14.
BEACON lights switch - OFF, then as required.
BEFORE TAXIING
* 1.
BRAKE deice switch - Check and set as required.
Ensure both bleed air valves are open.
* 2.
CABIN AIR MODE and TEMP controls - Set as desired.
*.3.
AC/DC power - Check.
H4. AUTO PLT POWER switch - ON.
*5.
AVIONICS MASTER POWER switch - ON.
* 6. # 1 and # 2 EFIS POWER switches - ON.
*7.
Mission panel - Set.
* 8.
Pilot's and copilot's EFIS TEST switches - As required.
Verify indications.
H9. Automatic flight control system - Perform as required.
H10. Avionics - Check and set as required.
11.
Weather radar/LSS - SBY.
12.
Flaps - Check.
N-6
