~~liUED~U
II~
1111111
••••••
ENGINE ICE INGESTION (CONT)
b.
If
either engine flames out, airstart in accordance with
ENGINE
AlRSTART procedure, Section
m.
After restart,
repeat
step
5,
but stay below engine
speed
at
which engine fBrned out.
c.
If
ice damage
has
been
experienced, land
as
soon
as
practical
and within limitations of operating capacity of engine
as
defined by this procedure.
After landing, inspect engine for damage
any
time inad-
vertent icing conditions have been encountered.
ENG ICE
UGHT
ILLUMINATED
A failure of the nacelle heat
system
(bleed air) is indicated by illumination of
the
amber
Lor
R ENG ICE light. Two types
of
failures are annunciated with
these lights.
The
first
is
an
uncommanded application of nacelle heat, and
the
second is a
failure
of
nacelle heat
to
activate when commanded.
Affected Engine:
4-2
1. NAC
HT
Crcuit
Breaker
(Main
Bus) -
Pull
and/or
reset.
U Ught
remains
illuminated:
2
.•
1/
associated NAC
HEAT
switch
is
OFF,
Engine RPM - Reduce
to
minimum required.
·1/
associated NAC
HEAT
switch
is On, Engine RPM - Increase
to
improve airflow.
Ay
out of icing conditions
if
possible.
FAA
APPROVED 4-30-76
REISSUED
2-25-81, CHANGE
10
To Next Page
Loading...
