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CEAPR DR400/135CDI Pilot Operating Handbook

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Supplement POH DR400/120D, DR400/140B,
DR400/180R, DR400/200R, DR400/RP
Issue 3 July 2014 Page 1 - 1
SECTION 1
DESCRIPTION
OVERALL DIMENSIONS
Wing span ................................................................ (28 ft 7.3 in) 8.72 m
Overall length ...............................................................(23 ft 8 in) 7.20 m
Overall height ........................................................... (7 ft 3.79 in) 2.23 m
Propeller ground clearance ............................................... (9.5 in) 0.26 m
ENGINE
Engine manufacturer ........................................... Technify Motors GmbH
Engine models ........................................ TAE 125-01 or TAE 125-02-99
The TAE 125-02-99 is the successor of the TAE 125-01. Both engine
variants have the same power output and the same propeller speeds but
different displacement. While the TAE 125-01 has 1689 ccm, the TAE
125-02-99 has 1991 ccm.
Both engine variants are liquid cooled in-line four-stroke 4-cylinder
engines with DOHC (double overhead camshaft) and are direct Diesel
injection engines with common-rail technology and turbocharging. Both
engine variants are controlled by a FADEC system. The propeller is
driven by a built-in gearbox (i = 1.69) with mechanical vibration damping
and overload release. The engine variants have an electrical self-starter
and an alternator.
WARNING: The engine requires an electrical power source for
operation. If the main battery and alternator fail
simultaneously, the engine will operate for a very limited
time on FADEC backup battery power (TAE 125-02-99
installation).
Therefore, it is important to pay attention to indications of
alternator failure.

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CEAPR DR400/135CDI Specifications

General IconGeneral
BrandCEAPR
ModelDR400/135CDI
CategoryAircrafts
LanguageEnglish

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