
Page 7-18 G1000 System Maintenance Manual – Diamond DA40/40F
Revision G 190-00545-01
ENGINE LEAN SYSTEM
Figure 7-10. Engine Instrument Sub Pages
6. Deactivate reversionary mode.
Table 7-1: Engine/Airframe Instrument Checks
Engine/Airframe
Indicator
Desired Reading
Manifold Air Pressure
(DA 40 Only)
Atmosphere Pressure
Tachometer 0
Fuel Flow 0
CHT Ambient*
EGT Ambient*
Oil Temperature Ambient*
Oil Pressure Approximately 0
Amps Approximately 0
Volts
Battery or GPU Voltage,
Approximately 28 Vdc
Fuel Tanks
FULL w/ full tanks, (
including
extended range tanks, if
equipped
)
Total Time in Service Total Airborne Time
*Unless engine is hot, in which case higher temps to be expected.
7. If no other service is to be performed, continue to the return-to-service checks in Section 8.
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