background image

 

3

 

instrument panel. This knob, labelled “ALTERNATE AIR”, should be pulled out if significant 
airframe icing happens to be encountered during flight

 

No fuel priming is required for engine start 

and furthermore, as we will see, there is no mixture 

control to be taken into consideration. 

 
Perhaps the most interesting part is the fact that the required fuel is diesel (DIN

EN590), which may 

be obtained at any car station-service and which is considerably cheaper than the usual aviation 

gasoline. It is unfortunate that, at least presently, few airports (if any) are equipped to provide diesel 

fuel. However, as said previously, the TAE 125-01 operates equally well on Jet A1 fuel (ASTM

1655), 

which is normally available at any major or regional airport. On the other hand, 

assuming that 

diesel fuel would ever be used, one must remember that the fuel temperature in the tank 
must be closely monitored, before takeoff as well as during flight to avoid formation of 

paraffin 

(see below). 

 

At any rate, 

keep in mind that whenever a refuelling stop is required elsewhere than at the 

home base, make sure that you don’t plan a stop at an airfield where these fuel types are 

not available! 
 

THE TAE 125-01 ENGINE AND ITS PROPELLER 

 

Although most light aircraft engines feature four or six horizontally opposed cylinders, the TAE 125- 

01, also referred to as the CENTURION 1.7, has four cylinders in line with double overhead camshaft 

(DOHC). In fact, the engine is based on the Mercedes Series A automotive design. 
 

Another major difference is that, unlike most light aircraft engines which are 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 includes a 

turbocharger. 

 
Let us first clarify the term “double overhead camshaft”, and have a few words about the 

turbocharger: 

 

Double overhead camshaft 

 
Without digging in the constructional details of engines, recall that each cylinder is fitted with (at 

least) two valves: the inlet valve and the exhaust valve. Incidentally, the 

TAE 125-01 features four valves per cylinder: two for the inlet, two for the exhaust. The four valve 

configuration contributes amongst other things to a lesser fuel consumption and to an improved 

quality of the exhaust gases. All these valves are driven by cams (NL: nokken) located on a shaft, the 

so-called camshaft (NL: nokkenas) which is itself driven by the crankshaft (NL: krukas). 
 

The camshaft can be located either in the lower part of the engine, close to the crankshaft (NL: 

onderliggende nokkenas), or higher up, close to the cylinder head, in which case one talks about an 

overhead camshaft (NL: bovenliggende nokkenas), or OHC, operating all inlet and exhaust valves in 

the required sequence. Double overhead camshaft, or DOHC, means that two overhead camshafts are 

used: one which operates all inlet valves and one which operates all exhaust valves. 
 

Turbocharger 

 

A turbocharger is in fact a form of supercharger and has the very same purpose, namely to increase 

the amount of air flowing in the induction system, thus increasing the manifold air pressure (MAP), 

and consequently the total power output of the engine. Note that with the TAE 125-01 installed, the 

 
 

Deutsche Industrie Norm 

American Society for Testing and Materials 

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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