Supplement POH DR400/120D, DR400/140B,
DR400/180R, DR400/200R, DR400/RP
Issue 3 – July 2014 Page vii
SECTION 3
EMERGENCY PROCEDURES
ENGINE FAILURE OR LOSS OF POWER ........................................... 3-2
During takeoff roll ................................................................................... 3-2
Immediately after takeoff ....................................................................... 3-2
During flight ............................................................................................ 3-3
LANDING WITHOUT ENGINE POWER ............................................... 3-4
Restart after engine failure .................................................................... 3-5
FADEC malfunction in flight ................................................................... 3-6
ENGINE SHUT-DOWN IN FLIGHT ....................................................... 3-8
FIRE ....................................................................................................... 3-9
Engine fire on the ground, during starting ............................................. 3-9
Engine fire in flight ................................................................................ 3-9
Electrical fire ........................................................................................3-10
ROUGH ENGINE OPERATION ..........................................................3-11
Oil pressure too low .............................................................................3-11
Oil temperature too high ......................................................................3-12
Coolant temperature too high ..............................................................3-12
“Cool level” light illuminates .................................................................3-13
Gearbox temperature too high .............................................................3-13
Fuel temperature too low .....................................................................3-13
Propeller RPM too high ........................................................................3-14
Fluctuations in propeller RPM ..............................................................3-14
ICING ...................................................................................................3-14
ELECTRICAL POWER SUPPLY MALFUNCTION .............................3-16
If the “ALT” light is lit or the ammeter shows battery discharge during
normal engine operation for more than 5 minutes ...............................3-17
INADVERTENT SPIN ..........................................................................3-18
LOSS OF ELEVATOR CONTROL ......................................................3-18
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