DA 42 AFM
Normal Operating
Procedures
Doc. No. 7.01.05-E Rev. 8 15-Dec-2017 Page 4A - 9
Check Procedure:
a) ELECT. MASTER ..................... ON
CAUTION
When switching the ELECT. MASTER ON, the electrically
driven hydraulic gear pump may activate itself for 5 to
20 seconds in order to restore the system pressure. Should
the pump continue to operate continuously or periodically,
terminate flight. There is a malfunction in the landing gear
system.
b) Fuel quantity ......................... check indication, verify using
alternate means (see Section
7.9.5 - FUEL SYSTEM)
c) Position lights, strobe lights (ACL) ........ check for correct function
CAUTION
Do not look directly into the anti collision lights.
d) Landing/Taxi light ..................... check for correct function
e) Stall warning/stall heat/Pitot heat ......... check
NOTE
The stall warning switch gets slightly warmer on ground only
and STAL HT FAIL is indicated on the PFD.
CONTINUED
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