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7

 

As for the difference between the DI and IDI, here again, both have their own advantages and 

disadvantages. For instance, amongst other things, the DI tends to produce more noise, more 

vibrations and more harshness than the IDI. On the other hand, the DI gives way to a lesser fuel 
consumption than IDI. However, the use of the common rail technology, which seems to be only 

applicable for DI, tends to combine the advantages of both DI and IDI. 

 

FUEL SYSTEM 

 

With the TAE 125-1 installed, only two draining points are to be found, a main tank drain valve and a 
fuel drain valve. 

 

OIL SYSTEMS 

 

The TAE 125-1 includes two separate oil systems, one for the engine, and one for the gearbox, each 

system requiring its own very specific type of oil. Be aware that these oils are not available at the BP 
refuelling services at Antwerp/Deurne airport, and must be obtained through Maintenance. 

 

The engine oil system 

 

Let us first emphasize that, according to the “Supplement”, 

the only approved oils are Shell EP 

75W90 API GL-4 and Shell Spirax GSX 75W-80 
 

The engine oil system is a wet oil sump system containing up to 6 litres. A wet sump system means 

that the oil is stored in the engine’s casing rather than in a tank (in which latter case one talks about a 

dry sump system). The oil level can be checked by means of a dipstick located on the upper center 

nose cowling. It should not be less than 4.5 litres, as indicated by the level being between two red 

markers at the extremity of the dipstick . The maximum engine oil consumption should not exceed 0.1 
litres/hour. 

The system is 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 returned partly by gravity, partly via a so-called catch-tank and associated gear 

pump, back into the sump. An additional oil line supplies the turbocharger, and also drains into the 
catch-tank. 

 

Downstream of the oil filter, a thermostat ensures that whenever the oil temperature is lower than 

78°C, the oil streams directly to the engine and the turbocharger. If the temperature is between 78°C 

and 94°C, the oil is partly directed to an oil cooler adjacent to the cooling fluid’s heat exchanger (see 

below), then further through the normal path. Above 94°C, all of the oil goes through the oil cooler, 
thus ensuring a maximum oil temperature of 140°C. 

 

Note that, although the maximum oil pressure is normally 6 bar, when starting in cold weather 

conditions, it is allowed to build up to 6.5 bar for up to 20 seconds. Assuming a low oil pressure 

condition, this will activate the “OIL” warning on the original annunciator panel. 

 
The gearbox oil system 

 

This is also a wet sump system, the oil being used for lubrication and cooling of the gearbox, as well 

as for the propeller’s constant speed unit. The gearbox oil is not the same as the engine oil: according 

to the “Supplement”, the Shell EP 75W90 API GL-4 type is solely to be used. 

 
The system contains only 1 litre. The oil level can be checked by means of a viewer located behind a 

small panel at the left lower front side of the engine cowling. 

 

Note:   Although the engine and gearbox oil pumps are said to be engine driven, in fact 

they are one single unit, known as a combined system, driven by the gearbox. 

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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