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CEAPR DR400/135CDI User Manual

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Supplement POH DR400/120D, DR400/140B,
DR400/180R, DR400/200R, DR400/RP
Page 3 - 2 Issue 3 July 2014
ENGINE FAILURE OR LOSS OF POWER
During takeoff roll
1) Thrust Lever .............................................................................. IDLE
2) Apply brakes and hold direction. Avoid obstructions.
3) Engine Master switch ................................................................ OFF
4) Battery and ALT CB .................................................................. OFF
5) Fuel selector.............................................................................. OFF
6) Emergency ground egress ............................................. As required
Immediately after takeoff
1) Establish glide
Speed (flaps retracted) ..................................... (78 KIAS) 144 km/h
Speed (flaps T/O position) ............................... (75 KIAS) 139 km/h
2) Land straight ahead, with only small direction changes to avoid
obstructions.
3) If complete engine failure:
FADEC A/B Switch .............................................................. Force B
4) Battery and ALT switch .................................................... Check ON
When landing inevitable:
5) Engine Master ........................................................................... OFF
6) Battery and ALT CB .................................................................. OFF
7) Fuel selector.............................................................................. OFF
8) Wing flaps ........................................ T/O or Landing recommended
9) Touch down with minimum speed
10) When aircraft has stopped ..................... Emergency ground egress
WARNING: Never try to turn back to the runway, as altitude just after
takeoff is seldom sufficient.
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CEAPR DR400/135CDI Specifications

General IconGeneral
BrandCEAPR
ModelDR400/135CDI
CategoryAircrafts
LanguageEnglish

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