
G1000 System Maintenance Manual – Diamond DA40/40F Page 4-7
190-00545-01 Revision G
Table 4-1. Maintenance Intervals, Cont.
Item Description/Procedure
Manual
Section No.
Interval
Engine/Airframe Sensors
MAP Sensor (DA40
ONLY)
Removal & Replacement:
For DA 40 Aircraft:
Refer to the G1000/DA40 Installation
Drawing, 005-00304-00 for drawings
(Ref STC #SA01254WI-D).
For DA 40 F Aircraft:
Refer to the Diamond Airplane Maintenance
Manual and OAM 40-222.
N/A
On Condition
Oil Pressure Sensor
Oil Temperature
Sensor
Fuel Pressure Sensor
(DA40 ONLY)
Tach Sensor
Fuel Flow Sensor
CHT Probes (Qty 4)
EGT Probes (Qty 4)
Alternator Current
Sensor
Fuel Tank Quantity
Sending Units –
G1000 Fuel Tank
Recalibration
Should one or both fuel quantity transducers
fail, replace according to instructions in
Diamond DA 40 Aircraft Maintenance
Manual. The new replacement fuel quantity
probe(s) must be re-calibrated.
4.6
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