Tecnam P2010 - Page 436

AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV3-19
Section 3 – Emergency procedures
POWERPLANT EMERGENCIES
Ed. 1, Rev.0
7. INFLIGHT ENGINE RESTART
7.1. PROPELLER WINDMILLING
1.
Master switch ………………………………
Check ON
2.
Fuel pump ………………………………….
ON
3.
Fuel quantity indicator ……………………..
CHECK
4.
Fuel Selector ……………………………….
SWITCH TANK
5.
Throttle Lever ……………………………..
Minimum 1cm. above IDLE
6.
Propeller Lever……………………………..
Full forward
7.
Mixture ……………………………………
FULL rich
8.
Throttle lever ………………………………
SET as required
In case of unsuccessful engine restart:
 Land as soon as possible applying Forced landing procedure.
(See Para 11)
In case of successful engine restart:
 Land as soon as possible
In case of engine shutdown, propeller will keep windmilling and
will not stop, preventing the use of ignition key. Engine inflight
restart must be performed without using ignition key with propel-
ler windmilling in order to avoid possible engine damages.
Typical indication of a potential engine shutdown, with windmill-
ing propeller, will be RPM running sub-idle below 600-500 RPM,
to be confirmed by other engine instrument (OIL Pressure, CHT,
EGT running down abnormally).
Inflight engine restart may be performed during 1g flight anywhere
within the normal operating envelope of the airplane.
After engine restart, if practical, moderate propeller rpm to al-
low the temperatures for stabilizing in the green arcs.