Robin DR400/120D - Page 48

Supplement POH DR400/120D, DR400/140B,
DR400/180R, DR400/200R, DR400/RP
Page 2 - 10 Issue 3 – July 2014
Figure 2-4 Near the CED
FUEL
E = 0
¼ = 25
½ = 50
¾ = 75
F = 100
( LITERS )
TEST / A C K
Figure 2-5 Near their respective gauges or switches
ENGINE
CAUTION
ALT
FUEL
LOW
LEVEL
FADEC
A
FADEC
B
FLAPS
DOWN
PITOT
HEATING
COOLANT
LEVEL
Figure 2-6 Annunciator Lights at the Top of the Instrument Panel
PRISE DE
PARC
AUSSENBORD
STROMANSCHLUSS
EXTERNAL
POWER
12 V
Figure 2-7 If installed, at the access door to the external power recep-
tacle behind the wing on the aircraft's right side.
 Note: The receptacle has "one way only" feature for polarity
protection.