Textron Lycoming IO-540 Series User Manual

TEXTRON
LYCOMING
OPERATOR'S
MANUAL
SECTION
3
0-540
&
10-540
SERIES
(3)
Landing
Approach
- In
making
an approach
for a
landing,
car-
buretor
air
heat
should
generally
be
in
the
"Full
Cold"
position.
However,
if icing
conditions
are
suspected,
the
"Full
Heat"
should
be applied.
In the
event
that
full
power
need
be
applied
under
these
conditions,
as for
an
aborted
landing,
the
carburetor
heat
should
be
returned
to
"Full
Cold"
prior
to
full
power
application.
See
the
air-
craft
flight
manual
for
specific
instructions.
9.
ENGINE
FLIGHT
CHART
-
Fuel
Requirements
-
0-540
MODELS
*Aviation
Grade
Fuel
-B
Series
-A3D5,
-E Series
-A,
-G,
-H
Series
-F,
-J,
-LSeries
80/87
Octane,
Minimum
91/96
Octane,
Minimum
91/96
or 100/1OOLL
Octane,
Minimum
100/1OOLL
Octane,
Minimum
10-540
MODELS
-C*,-D,-N,-VSeries
-A,
-B,
-E,
-G,
-J,
-K,
-L,
-M,
-P,
-R,
-S,
-T,
-W,
-AA,
I -AB,-ACSeries
91/96
or 100/100LL
Octane,
Minimum
100/1OOLL
Octane
Minimum
* -
Refer
to
the
latest
edition
of
Service
Instruction
No.
1070.
NOTE
Aviation
grade
1OOLL
fuels
in
which
the
lead
content
is
limit-
ed to
2
c.c. per
gal.
are
approved
for
continuous
use
in the
above
listed
engines.
3-10
Revised
January
1999

Textron Lycoming IO-540 Series Specifications

General

Brand	Textron
Model	Lycoming IO-540 Series
Category	Engine
Language	English