SOLOY TURBINE PAC
SECTION 4
POHS CESSNA T206H/206H
NORMAL PROCEDURES
4-9
F.A.A. Approved
November 17, 2015
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
.
10. Generator Switch – ON.
11. N
1
– CHECK 59% MINIMUM. If not, turn off generator and add
power to 70% N
1
, then turn on generator.
12. Lights – As required
13. Avionics – As required
14. Wing Flaps – UP
STARTING ENGINE (With External Power)
1. Propeller – CLEAR
2. TOT 150
C or Lower
3. External Power – CONNECT to airplane receptacle
NOTE
TOT can readily be reduced to 150°C by motoring
the starter.
4. 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.
5. Start Motor Switch – START and HOLD to 58% N
1
– Positive oil
PSI indication.
6. 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
)
7. TOT and N
1
– MONITOR TOT (810
to 927
C), 10 seconds
maximum and N
1
for normal acceleration.
8. Propeller (N
P
) – CHECK rotating by 25% N
1
.
9. Transmission Oil Pressure – POSITIVE indication at completion
of the start.
10. Start Switch – RELEASE at 58% N
1
(within 25 to 60 seconds).
11. APU – DISCONNECT.
12. Generator Switch – ON.
13. N
1
– CHECK 59% MINIMUM. If not, turn off generator and add
power to 70% N
1
, then turn on generator.
14. Lights – As required
15. Avionics – As required
16. Wing Flaps – UP
UNCONTROLLED
COPY
