Tecnam P2006T, Aircraft Flight Manual

Page: 409 / 508

GARMIN G950 IFDS – SMP
FOR DIGITAL CONFIGURATION
Page SSMP4-26
Section 4 – Normal procedures
CHECKLISTS
Ed.4, Rev.0
3.10 C
RUISE
1
LH and RH Propeller Lever
SET to 1900-2250 RPM
CAUTION
Throttles MAP decrease should be made before propeller speed reduction below
2200 RPM, as, contrariwise, Propeller Lever increase RPM should be set be-
fore engine Throttle Levers are advanced.
2
Engine parameters check (LH and RH)
 Oil temperature:
90°

110 ° C.
 CHT:
90°

110 °C
 Oil pressure:
2 - 5 bar.
 Fuel pressure:
2.2 – 5.8 psi
*2.2 – 7.26 psi (0.15 – 0.50 bar)
*applicable for fuel pump part no.893110 and no.893114
3
Carburettor heat as needed
(see also instructions addressed on Section 3, Para.
7.4)
WARNING
Deselect and do not use Auto Pilot if possible icing condition area is inadvert-
ently entered.
4
Fuel balance and crossfeed
check as necessary
3.10.1 CONVERTER BOX TURN ON
1 LH and RH AUX FIELD
ON
2 Converter Box
Check enabled (no fail lamps)
3 Mission systems
Use as required
3.10.2 CONVERTER BOX TURN OFF
1 Mission systems
Shut down as necessary
2 LH and RH AUX FIELD
OFF
3 Green lamps on switch panel
Check OFF