111.11,
.41
••
411
STARTING ENGINES (CONT)
d. Monitor the following:
(1)
Fan Speed
(Nl)
- Increasing
as
Turbine Speed (N2)
increases.
(2)
Turbine Temperature (fIT) -
Max.
860°C.
(3)
OIL
PRESS - Indication within
10
seconds.
(4)
Fuel Row.
e. At approximately 45%
or
50% Turbine Speed
(N2),
the starter
will automatically disengage. Check:
(1)
AIR
IGN
Ught - Out.
(2)
Starter Engaged Ught
(if
installed) - Extinguished.
If
starter· engaged light remains illuminated, refer
to
STARTER
ENGAGED UGHT
REMAINS
IU..UMINATED
AFfER
START,
Section
IV.
If
engine does
not
start, adhere
to
the
following
cooling
periods between starting attempts.
After Start
Attempt
Wait
1
One
Minute
2
One
Minute
3 Fifteen Minutes
4
One
Minute
5
One
Minute
6
One
Hour
The
above cycle may
then
be repeated.
+12.
START
-GEN
Switch - GEN
at
Idle.
E~
On aircraft 35-067 thru
35-147
and 36-018 thru
36-035,
set
BAT
1 or
BAT
2 switch
to
OFF prior
to
set-
ting the START-GEN switch to GEN. Prior to starting
the second engine or,
in
the case of single engine taxi,
when ammeter reads less than
175
amps - Both bat-
tery switches - On.
+ 13. DC VOLTS and AMPS - Check generator output.
14. Spoileron/Spoiler Check:
eAircraft 35-067 thru
35-142
and 36-018 thru 36-035 when not
incorporating
SB 35/36-27-7:
a.
Raps
- Check,
DN.
b. Control Wheel - Center.
c.
SPOlLERON RESET Switch - Hold On. Rotate control
wheel.
AUG
AIL
light
will
illuminate. Release SPOlLERON
RESET switch.
FAA
APPROVED
4-30-76
REISSUED
2-25-81,
CHANGE
10
2-19
I
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