SOLOY TURBINE PAC
SECTION 4
POHS CESSNA U/TU 206G
NORMAL PROCEDURES
4-7
F.A.A. Approved
November 17, 2015
STARTING ENGINE
1. Propeller – CLEAR
2. TOT 150
C or Lower
NOTE
TOT can readily be reduced to 150°C by motoring the starter.
3. Start Motor Switch – MOTOR and HOLD to 12 – 15% N
1
based
on temperatures listed below.
NOTE
Starter Duty Cycle is located in Amplified Procedures.
4. Start Motor Switch – START and HOLD to 58% N
1
– Positive oil
psi indication.
5. Fuel Cutoff Control – RUN (IN) AT:
N
1
RPM
Temp
C (
F)
15% .................................... Above 7
(45
)
13% ............................ -18 to +7
(0 to 44
)
12% ................................... Below -18
(0
)
6. TOT and N
1
– MONITOR TOT (810
to 927
C), 10 seconds
maximum and N
1
for normal acceleration.
7. Propeller (N
P
) – CHECK rotating by 25% N
1
.
8. Transmission Oil Pressure – POSITIVE indication at completion
of the start.
9. Start Switch – RELEASE at 58% N
1
(within 25 to 60 seconds).
10. APU – DISCONNECT if used.
11. Generator Switch – ON.
12. N
1
– CHECK 59% MINIMUM. If not, turn off generator and add
power to 70% N
1
, then turn on generator.
13. Lights – As required
14. Avionics – As required
15. Wing Flaps – UP.
ABORTED START PROCEDURE
1. Fuel Cutoff Control – CUTOFF (OUT)
2. Start Motor Switch – MOTOR 10 to 30 seconds
3. TOT – MONITOR
4. Perform corrective maintenance action if required.
UNCONTROLLED
COPY
