Pilatus PC-12 NGX, Pilot'S Information Manual

Page: 219 / 625

Loss of Digital Fuel Quantity Indication 3-16-07
continued
If Fuel Flow digital indication is invalid:
3. Fuel state.................................... Monitor analogue Fuel Quantity on Fuel
window or the digital fuel indication on
Systems Summary window
Note
Continued flight is possible without digital Fuel Quantity (QTY) providing analogue
fuel quantity is operating correctly.
---------- END -----------
LH Fuel Pump RH Fuel Pump 3-16-08
On ground:
1. Aircraft......................................... Do not take off
--- END ---
In flight:
1. FUEL PUMP switches................. AUTO
2. FUEL PUMP circuit breaker (on
affected side) (Essential Bus
L
J1
or Essential Bus
L
H1)..................
Reset
3. FUEL PUMP switch (on affected
side)............................................ ON
After 10 seconds:
4. FUEL PUMP switch (on affected
side)............................................ AUTO
5. Fuel state.................................... Monitor
If fuel imbalance with affected pump failed ON and affected tank lower:
6. Aircraft......................................... Carry out Fuel Balance Fault and/or Fuel
Imbalance - 3-16-04 procedure
If fuel imbalance with affected pump failed OFF and affected tank lower:
7. Aircraft......................................... Both automatic and manual fuel
balancing available
Continued on next page
Section 3 - Emergency Procedures (EASA Approved)
Fuel System
Pilot's Operating Handbook Report No: 02406
Issue date: Mar 06, 2020
Page 3-16-7
12-C-A15-40-0316-00A-141A-A
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GENERAL
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