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10

 

fuel injectors in each cylinder, both systems being electrically supplied when the engine master switch 

is “ON”. 

 
The engine starting procedure is extremely simple. With the main battery switched on, the selection of 

the engine master switch to “ON” causes the glow plugs to heat up, which is indicated by the “GLOW” 

warning light momentarily illuminating. It also causes the fuel injectors to open and allow fuel under 

pressure stored in the common rail to be injected in the cylinders, the whole operation being FADEC 

controlled. As soon as the “GLOW” warning light extinguishes, and with the thrust lever in full idle 

position, engine starting may be initiated by turning the starter key. 
 

Small detail: the engine’s hobbsmeter (hourmeter) starts “counting” as soon as the engine master 

switch is selected to “ON”, whether the engine is running or not. Switching the engine master switch 

to “OFF” causes the engine to shut down.

[HOP3] 

 

CAUTION: Selecting either the battery switch or pulling the alternator circuit-breaker to 

“OFF” will not cause the running engine to stop, at least not immediately (see below). 

However, if both battery and alternator are switched off, as the FADEC is no 

longer electrically supplied, the engine will stop at once. 

If the alternator fails, 

electrical power will be provided by the battery only. The time the engine can run on 

battery alone will depend on total electrical consumption supported by the battery. 

 

ENGINE COOLING AND CABIN HEATING SYSTEMS 

 

Both these systems are closely related. As was mentioned earlier, the engine uses liquid coolant 

instead of being air-cooled. One advantage of the liquid cooling system is that shock cooling during 

descent is eliminated. The coolant is stored in a tank within the engine compartment, and is a fiftyfifty 
mixture of water and BASF Glysantin Protect Plus/G48, again a product which is only available 

through Maintenance. 

 

Prior to start engine, the pilot must check the coolant’s level. This is done by means of a yellow 

“COOLANT LEVEL” warning light. When the battery switch is selected to “ON”, it is imperative to verify 

that the warning light initially illuminates (mostly very shortly) then extinguishes. Assuming that the 
light remains illuminated, the coolant level is too low and engine starting is prohibited. Note also that 

engine starting is not allowed if the coolant temperature happens to be lower than -30°C. Incidentally, 

the same limit is also applicable to the engine oil and gearbox temperatures. 

 

Engine cooling circuit 
 

The coolant leaves the tank and is pumped into the engine where it evidently picks up heat. Upon 

exiting the engine, the coolant is directed to a three-way thermostat of which one exit is unregulated 

and relates to the cabin heating system (see below). The two other exits regulate the coolant flow 

between a so-called short circuit and/or a large circuit (also referred to as “external circuit”), 

depending on the coolant’s temperature: 
 

a) Assuming that the coolant’s temperature is less than 84°C, the coolant circulates through the short 

circuit which directs it immediately back to the engine via the pump. 

 

b) Assuming that the coolant’s temperature is between 84°C and 94°C, the coolant is caused to flow 

partly through the small circuit, partly through the large circuit. This latter circuit includes a heat 
exchanger (radiator) located on the left side of the engine, where the fluid is cooled by outside air 

coming from the left upper air intake on the front part of the cowling. This heat exchanger is divided 

in two parts, one serving the coolant’s fluid cooling, the other serving the engine oil cooling (see 

engine oil system). Upon exiting the heat exchanger, the coolant fluid is directed partly back to the 

tank, partly back to the engine. 

Versie oktober 07 

Summary of Contents for DR400/140B

Page 1: ...TENANCE MANUAL PUBLISHED BY THIELERT AIRCRAFT ENGINES GmbH Met bijzondere dank aan de collega s van de RAAC voor het ter beschikking stellen van de informatie F Gardin voorzitter NZVC Revision History...

Page 2: ...is the case in the gasoline version but solely air Typical for diesel engines is that there is no throttle valve During the induction stroke the air can freely enter the cylinder Unlike in gasoline e...

Page 3: ...air cooled the TAE 125 01 is liquid cooled This in turn results in a significant change not only in the engine s cooling system but in the cabin heating system as well see below The power plant also i...

Page 4: ...in reason for the turbocharger is to increase the volumetric efficiency of the cylinders In other words the more air can be crammed into the cylinders during the induction stroke the greater will be t...

Page 5: ...t 60 about 1960 RPM at 80 about 2140 RPM etc and at 100 2300 RPM This implies that although the pilot cannot change the propeller RPM at all the FADEC produces the most efficient blade setting for the...

Page 6: ...he electric pump Thus far the system is similar to the original one except for the fact that for takeoff and landing the electrical pump must be ON 3 Beyond the shutoff valve the fuel is ducted toward...

Page 7: ...rather straightforward its main line supplies the various engine parts with the necessary engine driven supply pump oil pressure sensor oil filter and oil temperature sensor the used oil being then r...

Page 8: ...e system the other being the standby system ready to take over automatically should the active fail FADEC A is normally the active one Both these computers are located behind the right hand part of th...

Page 9: ...cally to FADEC B Should this not be the case as made evident by the engine s abnormal behaviour the switching from FADEC A to FADEC B can be done manually by pulling the Auto FADEC Pull to Force B bre...

Page 10: ...of water and BASF Glysantin Protect Plus G48 again a product which is only available through Maintenance Prior to start engine the pilot must check the coolant s level This is done by means of a yell...

Page 11: ...ngine compartment In other words when the cabin heat shutoff knob is closed the usual cabin heat knob has no effect The open position knob pulled out is the normal position during flight VACUUM SYSTEM...

Page 12: ...CG forward The DR400 135CDI delivers greater range and at altitude greater speed than AVGASpowered Robin of equivalent sea level power ratings for a given volume of fuel Normal category Maximum ramp...

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