TM 1-1520-240-CL
P-8
5. Remaining three AUX FUEL PUMPs Check
as in step 4, except check R AUX PRESS light
on, then off, for R AUX FUEL PUMP switches.
714A FADEC Reversionary system Check First
flight of the day.
1. FADEC 1 and 2 PRI-REV switches PRI.
2. NR% switch 100%.
3. FADEC 1 Check as follows:
a. FADEC 1 PRI-REV switch REV.
b. FADEC 1 INC - DEC switch DEC. Check
for decrease in No. 1 engine N1 and torque,
and corresponding increase in No. 2 engine
N1 and torque.
c. FADEC 1 INC - DEC switch INC. Check
for increase in No. 1 engine N1 and torque,
and corresponding decrease in No. 2 engine
N1 and torque.
d. FADEC 1 PRI-REV switch PRI.
4. Repeat check for FADEC 2.
Transponder Check and Set.
1. Move the MASTER switch from OFF to STBY.
If the aircraft is so equipped, observe that the
STBY light on the aircraft advisory panel comes
on. Also, note that the NO GO light is on.
2. Allow 2 minutes for warmup.
3. Select the codes assigned for use in modes 1
and 3/A by depressing and releasing the
pushbutton for each switch until the desired
number shows.
4. Operate the PRESS-TO-TEST feature of the
lamp indicators.
5. Place the ANT switch BOT.
6. Move the MASTER switch from STBY to
NORM.
7. Hold the M-11 switch to TEST, observe that the
TEST/GO indicator lights.