Pilatus PC-12 NGX, Pilot'S Information Manual

Page: 156 / 625

Air Start - With starter 3-5-02
continued
3. NG............................................... Check NG < 5%
4. EEC CH A (Essential Bus
L
C3)
circuit breaker.............................
PULL
5. EEC CH B (Avionic 1 Bus
L
R1)
circuit breaker.............................
PULL
6. EEC CH A (Essential Bus
L
C3)
circuit breaker.............................
PUSH, wait for 1 second
7. EEC CH B (Avionic 1 Bus
L
R1)
circuit breaker.............................
PUSH
If EPECS Fail persists:
8. Aircraft......................................... Make a Forced Landing - 3-9-02
WARNING
DO NOT ATTEMPT AN ENGINE START WITH EPECS FAIL DISPLAYED.
If no EPECS Fail displayed:
9. PCL............................................. Idle
10. PROP LOW SPEED switch........
(if installed).................................. PUSH (set to ON, if not active)
11. Engine switch.............................. RUN
12. FUEL EMERG shut off................ Full in
13. BAT 1 and BAT 2 switches.......... ON
14. Air start envelope........................ Check (Refer to Fig. 3-5-1 )
15. IGNITION switch......................... ON
16. STARTER switch......................... PUSH momentarily
17. ITT and NG................................. Monitor
When engine has relit NG >64.5%:
18. IGNITION switch......................... AUTO
19. FUEL PUMP switches................. AUTO
20. GEN 1 and GEN 2...................... Check volts and amps
21. Electrical equipment.................... As required
Continued on next page
Section 3 - Emergency Procedures (EASA Approved)
Air Start
Pilot's Operating Handbook Report No: 02406
Issue date: Mar 06, 2020
Page 3-5-2
12-C-A15-40-0305-00A-141U-A
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