Pilatus PC-12 NGX, Pilot'S Information Manual

Page: 161 / 625

Engine Torque Engine Torque 3-6-04
continued
If torque above 44.3 psi:
2. PCL............................................. Reduce power
If Engine Torque or Engine Torque remains:
3. Aircraft......................................... Land as soon as possible, using
minimum power. If possible always retain
glide capability, to the selected landing
airfield, in case of total engine failure
---------- END -----------
Engine ITT Engine ITT 3-6-05
1. ITT............................................... Check ITT indication
If ITT above 850 ºC:
Note
For hot/high environment ground operations, momentary ITT peak in the transient
range may be expected during engine acceleration.
2. PCL............................................. Reduce power
If Engine ITT or Engine ITT remains:
3. Aircraft......................................... Land as soon as possible, using
minimum power. If possible always retain
glide capability, to the selected landing
airfield, in case of total engine failure
---------- END -----------
Engine Oil Press Engine Oil Press 3-6-06
1. Oil................................................ Check OIL P PSI indication
If Engine Oil Press or Engine Oil Press is confirmed:
2. NG............................................... Check NG above 72%
3. Torque......................................... Reduce to below 24 PSI
If Engine Oil Press or Engine Oil Press remains:
4. Aircraft......................................... Land as soon as possible, using
minimum power. If possible always retain
glide capability, to the selected landing
airfield, in case of total engine failure
---------- END -----------
Section 3 - Emergency Procedures (EASA Approved)
Engine Emergencies
Pilot's Operating Handbook Report No: 02406
Issue date: Mar 06, 2020
Page 3-6-3
12-C-A15-40-0306-00A-141A-A
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