CEAPR DR400/135CDI Pilot Operating Handbook

Supplement POH DR400/120D, DR400/140B,
DR400/180R, DR400/200R, DR400/RP
Page 2 - 6 Issue 3 – July 2014
ENGINE INSTRUMENT MARKINGS
The engine data of the TAE 125 installation to be monitored are
integrated in the combined engine instrument CED-125. The ranges of
the individual engine monitoring parameters are shown in the following
table.
Instrument
Red
Range
Amber
Range
Green
Range
Amber
Range
Red
Range
Tachometer
[rpm]
-
-
0-2300
-
> 2300
Oil Pressure
[bar]
0-1.1
1.2-2.2
2.3-5.2
5.3-6.0
> 6.0
Coolant
temperature [°C]
< -32
-32...
+59
60-100
101-
105
> 105
Oil Temperature
[°C]
< -32
-32...
+49
50-124
125-
140
> 140
Gearbox
Temperature [°C]
-
-
< 115
115-
120
> 120
Load
[%]
-
-
0-100
-
-
Table 2-6 Markings of the Engine Instruments
 Note: If an engine reading is in the yellow or red
range, the "Caution" lamp is activated. It only
extinguishes when the "CED-Test / confirm" button is
pressed. If this test button is pressed longer than one
second, a self-test of the instrument is initiated.
GROUNDING (EARTHING) BEFORE AND DURING FUELING
Use the engine exhaust pipe for draining static charge.

CEAPR DR400/135CDI Specifications

General

Brand	CEAPR
Model	DR400/135CDI
Category	Aircrafts
Language	English