Supplement POH DR400/120D, DR400/140B,
DR400/180R, DR400/200R, DR400/RP
Page 4 - 10 Issue 3 – July 2014
▲ WARNING: The whole test procedure has to be performed without
any discrepancy. In case the engine shuts down or the
FADEC lamps are flashing, takeoff is PROHIBITED. This
applies even if the engine seems to run without failure
after the test.
Note: If the test button is released before the self-test is fully
completed, the FADEC immediately resumes normal
operation.
Note: While switching from one FADEC to
another, it is normal to hear and feel a momentary surge
in the engine.
10) Thrust Lever ........................................................ FULL FORWARD,
RPM must be stabilized
load display minimum 94%
RPM 2240 - 2300
Note: The power check should be performed at a
place which is free of debris to minimize risk of damage
to propeller or other parts.
11) Thrust Lever .............................................................................. IDLE
12) Engine instruments and Voltmeter ...................................... CHECK
13) Vacuum gauge ..................................................................... CHECK
14) Flaps .................................. Full down, then back to takeoff position
15) Electrical fuel pump ..................................................................... ON
16) Radios and avionics ............................................................. ON, set
17) Thrust Lever friction control ..................................... SET as desired
18) Brakes .............................................................................. RELEASE
19) CED ......................................................... CHECK all LEDs GREEN
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