(e) PROP lever (engine to be feath-
FEATHER. Time to
feather must not exceed 10 sec-
onds from windmilling at 2000
RPM to no rotation in the feath-
(f) Engine cleanup.
(1) CONDITION lever - FUEL
(2) AUTO IGNITION switch -
(3) AUTOFEATHER switch -
(4) GEN switch - OFF.
(5) PROP SYN switch - OFF.
(g) Engine restart.
Airstarts using the starter assist procedures will
momentarily cause the loss of all electronic flight
instrument system (EFIS) data. The engine restart
during flight (no starter assist procedure), or turn-
ing EFIS power off prior to a starter assisted
restart, should normally be performed