DA 62 AFM Airplane Description
If MÄM 62-254 is installed:
One fuel probe measures the fuel quantity in each auxiliary tank. The indication is provided
by the G1000 flight display. Information about fuel consumption can be found in
Chapter 5 -PERFORMANCE.
When one auxiliary pump is defective, the fuel stored in the related auxiliary fuel tank
is not available. For use of the remaining fuel pump refer to to Section 4B.12 - L/R FUEL
TRANSFER FAIL. The flight plan must be amended accordingly.
The auxiliary pumps are electrically connected to the LH MAIN BUS and protected by
a 7.5 A circuit breaker.
Doc. No. 11.01.05-E Rev. 0 11-Jan-2019 Page 7 - 49
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