Lycomin 0-360, 10-360, HO-360, TIO-360, AIO-360 Operator's Manual

...
-Lycoming
OPERATOR’S MANUAL
REVISION
REVISION NO. PUBLICATION PUBLICATION PUBLICATION
60297-12-4
PREVIOUS REVISIONS
July 1989
March 1990
1-5, 1-6; 2-9,2-10,2-11, 2-12,
2-13; Added page 3-18A, 3-29; 5-4
May 1996
1-5, l-6, l-7; 2-2, Added page 2-2A/B; 2-9, 2-10, 2-11, 2-12, 2-13, 2-14; 3-12, Added page
3-12A/B; 3-14, Added page 3-14A/B; 3-15, 3-16, Added pages 3-16A, 3-16B; 3-17,3-l& 3-26, Added pages 3-26A/B, 3-4OAJB; 3-50, Added pages 3-5OA, 3-50B; 3-51
0, HO, IO, AIO, NO. DATE
HIO, TIO-360
Series 60297-12 April 1989
CURRENT REVISIONS
April 1998
3-5
3-3,3-4, Adds page 3-4AD3
Lycoming
OPERATOR'S MANUAL
REVISION
REVISION NO. PUBLICATION
60297-12-5
The page(s) in this revision
the operator's manual.
PREVIOUS
July 1989 December 1999
March
1-5, 1-6; 2-9,
2-13;
Added page
5-4
May 1996
1-5, 1-6, 1-7; 2-2A/B; 2-13, 2-14; 3-12, Added page 3-12A/B; 3-14A/B; 3-15, pages 3-16A, 3-16B; 3-17, 3-18, 3-26, Added pages 3-26A/B, 3-40A/B; 3-50, Added pages 3-50A,
2-9, 2-10,
3-14, Added
3-50B;
HIO, TIO-360
SERIES 60297-12 April 1989
replace, add to, or delete
REVISIONS
3-5
1990 2-13;
2-10, 2-11, 2-12,
3-18A; 3-29;
2-2, Added
3-16,
3-51
page
2-11, 2-12,
page
Added
PUBLICATION
CURRENT
1-7; 2-2A,
Adds page 3-40B; 8-1
Adds page
3-12, 3-15, 3-23, 3-40A,
PUBLICATION
current pages in
REVISIONS
2-2B; 2-10,
April
3-3, 3-4, Added
1998
page 3-4A/B
0, HO, I0, AIO, HIO,
Textron Lycoming Part Number: 60297-12
© 1989, 1999 Textron Lycoming. All Rights Reserved
Lycoming and "Powered by Lycoming" are trademarks or registered
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TIO-360 Series Operator's
Manual:
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TEXTRON
OPERATOR'S
REVISION
MANUAL
REVISION
60297-12-6
page(s)
The
operator's
the
PREVIOUS
1-5, 1-6;
Added
2-13; 5-4
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3-50B;
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NO.
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PUBLICATION
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3-5
page
May 1996
2-2,
2-10,
3-12,
3-14,
3-15,
3-50, Added
Added page
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3-16B;
pages
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1998
, HO, IO,
TIO-360
HIO,
SERIES
2-11, 2-12,
3-18A;
Added
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2-11,
Added
Added
Added
3-17,
3-26A/B,
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AIO,
replace,
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PUBLICATION
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60297-12
or delete
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CURRENT
May 2000
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Adds
PUBLICATION
DATE
April
current
REVISIONS
3-12B;
page
1989
pages
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in
1-7;
2-10,
3-40A,
December
2-2A,
2-13, Added
Added
3-12, page
1999
page
3-15,
3-40B;
2-2B;
3-23,
8-1
0,
HO, IO, AIO,
Textron Lycoming
HIO, TIO-360
Part Number:
Series
Operator's
60297-12
Manual:
O 1989, 2000
Lycoming
trademarks
All
brand and product names
trademarks
Textron Lycoming.
and "Powered by Lycoming"
of Textron
or registered
Lycoming.
trademarks
For additional information:
Mailing address:
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Lycoming 652 Oliver Street Williamsport,
PA 17701
Phone:
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of their respective
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U.S.A.
570-323-6181 570-327-7268 570-327-7101
regular
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at:
are
Monday
Time
OPERATOR'S
MANUAL
Lycoming
0-360, HO-360, 10-360
AIO-360,
HIO-360
& TIO-360
SERIES AIRCRAFT ENGINES
6th Edition
No. 60297-12
Part
Approved by F.A.A.
September,
Printed in U.S.A.
1999
TEXTRON
LYCOMING
ATTENTION
OPERATOR'S
MANUAL
OWNERS,
MAINTENANCE
This operator's
specifications,
it. Such maintenance periodic inspections owners,
Lycoming contained in
refer to these for
should
Neglecting maintenance
loss. Also,
exceeded, happen. Consult
SERVICE BULLETINS,
Although the
publication,
of through which are available factory L114 for subscription
and detailed
pilots and
powered aircraft.
to follow
procedures
if power
for any reason;
your local
information
users
Lycoming
by subscription.
OPERATORS,
PERSONNEL
description
manual contains
information on
procedures
are also included.
maintenance
Modifications
Lycoming
overhaul manuals;
such procedures.

SAFETY WARNING

the operating
can result
and speed
damage FAA approved
contained in this
are urged
Service Bulletins,
from all Lycoming
Consult the
information.
SPECIAL NOTE
a
how to operate
that may
be required
This manual
personnel
instructions
in poor engine
limitations
to the engine and
responsible
maintenance
INSTRUCTIONS,
to keep
abreast
Instructions
latest edition
AND
of the
in conjunction
is intended
and repair
maintenance
and to carry
performance
specified
in this
personal injury
facility.
AND
manual is up-to-date
of later information
and Service Letters
distributors or from the
of Service Letter
engine,
and maintain
for use by
for care
procedures
personnel
out periodic
and power
manual
LETTERS
its
with
of
are
are
can
at time
No.
illustrations, pictures
The typical interpreted
of the
as examples
ii
subject
and drawings
matter they
of any specific
shown in
portray;
in no instance
engine, equipment
this publication
they to be
are
or part thereof
are
TEXTRON
LYCOMING
OPERATOR'S
MANUAL
Proper
operation
Textron
by operations. specially and as
tain order
vice
are evaluate
vice be satisfy ty
designed
recommended.
important
It is
various
minimize
to
methods
also
It is
all
not
or
might
involved.
themselves
be jeopardized
will
service
all aircraft
of
Lycoming
Some
Warnings
that
important
inclusive.
advise
done
be
Acordingly,
IMPORTANT
is essential
repair
and
engines.
effective
are
service
these
of
task.
the
for
most
that
to note
Cautions
and
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risk
the
damage
may
understand
to
Textron
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or
thoroughly
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trade
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the
anyone
service
the
SAFETY
The
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These
Textron
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the
that
Lycoming
of
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who
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procedure
NOTICE
increase
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special
Lycoming
or
these
service
a
their
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for
require
tools
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or
render
Warnings
could
consequences
safety
they
service
methods
which injury
all conceivable
safe,
the
recommended
performing
the use
be used
must
publications
be carefully
of improper
use
it unsafe.
and
possibly
not
in which
ways
procedure
select.
must
nor aircraft
reliable
service
tools
of
when
con-
read
ser-
Cautions
know,
ser-
may
that
first safe-
in

WARRANTY

NEW AND
RECIPROCATING
WHAT TEXTRON LYCOMING PROMISES YOU
(LIMITED)
REMANUFACTURED
AIRCRAFT
ENGINE
THIS LIMITED
WARRANTY
IS EXCLUSIVE
AND IN LIEU
OF ALL
OTHER
WARRANTIES
AND REPRESEN-
Textron
Lycoming warrants each workmanship testing. The date
change basis,
in material Lycoming Lycoming's then
Lycoming distributor
the part of Textron This warranty
been subject to accident manual. cause of the
such alterations
THIS TATIONS, EXPRESS
LIMITED
AND TRADE USAGE. CLAIM, TORT TEXTRON CABLE TO
appearing
of first operation
Textron Lycoming's
of the engine
or workmanship.
will also
bear the cost
current Removal and Installaton
Any
engine or part so repaired
The engine
must have received normal
within 30 days of the appearance of the
Textron Lycoming's
Textron
Textron
LIMITED
ANY IMPLIED WARRANTY
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WARRANTY
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THIS WARRANTY
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RECIPROCATING
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within one
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Such repair
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for labor in connection
or replaced will be entitled
YOUR OBLIGATIONS
use and service. You
warranty does not cover
or used, adjusted,
OR IMPLIED
above are your exclusive
product failure between
the right to deny
altered, handled, maintained
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the warranty
application
the construction of
previously sold.
IS EXCLUSIVE
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OFMERCHANTABILITY
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IS ALSO IN LIEU OF
FROM NEGLIGENCE
LIABILITY
OR IN TORT,
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LYCOMING
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Labor Allowance Guidebook
normal maintenance
you and Textron Lycoming,
any warranty
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is filed.
engines at any time without
AND
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GIVES RISE TO THE CLAIM
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to warranty for the
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YOU
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AND
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PURPOSE,
DEALING OR
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ALLO-
OR
IN
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WHETHER
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NOT LIMITED
this warranty
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A BREACHOF
BE LIABLE
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WARRANTY,
OR CONSEQUENTIAL OR REVENUES,
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CONTRACT
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LOSS
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be binding
upon Texron
Effective October 1, 1995
Revision 'J'
Williamsport,
Textron
Pennsylvania
Lycoming
TEXTRON
LYCOMING
OPERATOR'S
MANUAL

TABLE OF CONTENTS

Page SECTION 1 DESCRIPTION 1-1 SECTION SECTION 3 OPERATING INSTRUCTIONS 3-1
SECTION 4 PERIODIC INSPECTIONS 4-1 SECTION 5 MAINTENANCE PROCEDURES 5-1 SECTION 6 TROUBLE-SHOOTING 6-1 SECTION 7 INSTALLATION AND STORAGE 7-1 SECTION 8
2 SPECIFICATIONS
TABLES
2-1
8-1
Figure 1. 3/4 Right Side View IO-360-A1A
Figure 2. 3/4 Left Rear View - TIO-360-AlB
TEXTRON LYCOMING
DESCRIPTION
OPERATOR'S
MANUAL
Page
General .....
Cylinders ....
Valve
Operating
Crankcase . . . Crankshaft . . .
Mechanism
Connecting Rods Pistons .. Accessory
Oil Sump ....
Cooling
Induction Lubrication System
Housing
System
Systen
ng ........
m
em ........
Priming System Ignition System
. . .
. . . .
. . . . . . . . .
. . . . . . . . . . . . . . . .1 -1
. . . . . . . . . . . . . . . .1-1
. . . . . . . . . . . . . . . .1-1
. . . . . . . . . . . . . . . .1-1
. . . . . . . . . . . . . . .. 1-2
. . . . . . . . . . . . . . .. 1-2
. . . . . . . . . . . . . . .1-2
. . . . . . . . . . . . . . .1-2
. . . . . . . . . . . . . . .. 1-2
. . . . . . . . . . . . . . .. 1-2
. . . . . . . . . . . . . . .1-2
. .
. . . . . . . . . . . . . . .. 1-4
. . . . . . . . . . . . . . .. 1-4
. . . . . . . . . . . . . . .. 1-4
Model Application Table ..................... 1-5
TEXTRON
LYCOMING OPERATOR'S
MANUAL
0-360 and ASSOCIATED MODELS SECTION 1
SECTION 1
DESCRIPTION
The O, HO, 10, AIO, HIO, LIO and TIO-360 series are four cylinder,
direct drive, horizontally opposed, air cooled engines.
In referring to the location of the various engine components, the parts are described the front and the accessory
bottom located the top. Reference to the left and right side is made with the observer facing the rear of the engine. The cylinders are numbered from front to rear, odd numbers crankshaft, viewed drives is determined with the observer facing the drive pad.
The letter "L" in the model prefix denotes the reverse rotation of the
basic model. Example: model 10-360-C has clockwise rotation of the crankshaft. crankshaft. Likewise,
are opposite those of the basic
The letter
denotes that the particular
single housing. Example: All information pertinent to the 0-360-A116
will apply to 0-360-A IF6D.
Operational
specifications
Cylinders - The cylinders are
the two major heads are made from combustion chamber. the head barrels ground and
as installed in the airframe.
and the opposite side of
from the rear, is clockwise.
Therefore, LIO-360-C
"D" used as the 4th or 5th
aspects of engines are the same
for the
along with housings to form
have deep
honed to a specified
the rotation of the accessory
basic model
parts, head and barrel, screwed
integral cooling
drive end the rear. The
on the right. The direction
NOTE
model as listed in Section 2
model employs dual magnetos
will apply.
of conventional air cooled construction
an aluminum alloy casting with
Rocker shaft bearing supports
finish.
Thus, the power take-off end
the engine where the shroud
has counter-clockwise rotation
character in the model suffix
and performance curves and
the rocker boxes. The cylinder
fins and the
sump section is the
of rotation of the
Rotation for accessory
drives of the LIO-360-C
of this manual.
housed in a
and shrunk together. The
a fully machined
are cast integral with
inside of the
tubes are
of the
with
barrels are
is
1-1
TEXTRON LYCOMING OPERATOR'S MANUAL
SECTION
1 0-360
and ASSOCIATED MODELS
Valve Operating Mechanism
above and parallel
to the crankshaft. The camshaft tappets which operate valve rockers
are supported on full floating
bear against hardened
means
of
split keys.
- A conventional type camshaft
the valves through push rods and
steel shafts. The valve springs
steel seats and are retained
on the valve stems by
actuates hydraulic
is located
valve rockers. The
Crankcase - The crankcase assembly consists of two reinforced aluminum alloy
castings, fastened together
mating surfaces
of the two castings are joined
by means of studs, bolts and nuts.
without the use of a gasket,
The
and the main bearing bores are machined for use of precision type main
bearing
Crankshaft - The steel
Connecting Rods
sections the caps on the crankshaft
inserts.
crankshaft is made from a chrome
forging. All bearing
journal surfaces are nitrided.
- The connecting rods are
from alloy steel forgings.
They have replaceable bearing
crankshaft ends and bronze bushings
ends are retained by two bolts
nickel molybdenum
made in the form of "H"
in the piston ends. The
and nuts through
inserts in
bearing
each cap. Pistons - The pistons
pin is
of a full floating Depending three Consult the piston
Accessory
casting
on the cylinder
or four rings
latest revision
and ring combinations.
Housing
and is fastened
sump. It forms
Oil Sump (Except
oil suction riser
Crankcase
screen, mounting
and intake
Covers (-A10
top and bottom
screens, oil
connection suction
scavenge line
for a breather
line.
are machined from an aluminum
type with
a plug located
assembly, pistons
and may
employ
either half
of Service Instruction
- The accessory
housing is made
to the rear of the
a housing for the oil pump
-AIO Series)
- The sump incorporates
pad for carburetor
pipe connections.
Series) - Crankcase
of the engine. These covers
connections.
line and
the lower cover
alloy. The piston
in each end of
may be
wedge or
No.
crankcase and
machined for either
full wedge
1037 for proper
from an aluminum
the top rear of
the pin.
rings.
the
and the various accessory drives.
an
or fuel
covers
are employed
oil drain plug,
injector, the intake
on the
incorporate oil suction
The top cover
a connection for
incorporates
an oil
a
1-2
TEXTRON LYCOMING
OPERATOR'S
MANUAL
0-360 and ASSOCIATED
Cooling
Baffles cylinder augmentor
Induction
equipped
for model application. mixture system, which
insuring a more
in the cylinder
are
model 10-360-B1A
injector. (See Table 1 for model application.) The fuel injection system schedules fuel
place
the TIO-360 series engines. Automatic waste gate control of the
turbocharger provides constant air density to the fuel injector inlet from
seal level to critical altitude.
barrel float type equipped
cut-off.
System - These
are provided to build up a
fins. The air is
to each
sump. From
by individual
Lycoming 10-360,
equipped with
at the intake ports. A turbocharger
A brief description of the carburetors and fuel injectors follows: The Marvel-Schebler MA-4-5 and HA-6 carburetors are of the single
usually
tubes
System
with either
cylinder is
is integral with
uniform vaporization
a Bendix type
flow in proportion
MODELS
engines are then exhausted
located
Lycoming
a float
Particularly good distribution
the riser the fuel-air
intake pipes.
AIO-360, HIO-360 and TIO-360
which is equipped with
designed to be
pressure and force the air through
to the atmosphere
at the rear
or pressure
type
obtained
the oil sump
RSA fuel injector,
to air
with a manual mixture control
of the
0-360 and
through the
of fuel
mixture
flow and fuel vaporization
is mounted as an integral
cowling.
HO-360
type
and is submerged
and aiding in
a Simmonds type 530 fuel
SECTION 1
cooled by air pressure.
through gills
series engines
carburetor.
center
is distributed
with the exception
Table
See
of the fuel-air
zone induction
cooling the oil
series engines
and an idle
the
or
are
1
in oil,
to each
of
takes
part of
The Marvel-Schebler MA-4-5AA carburetor is of the single barrel float type with automatic pressure altitude mixture control. This carburetor is equipped with
The Bendix-Stromberg horizontal enrichment valve and an automatic mixture control unit. It is equipped with an idle cut-off and a manual mixture control. The AMC unit works independently of, and in parallel with, the manual mixture control.
idle cut-off but does not have
PSH-5BD is a
carburetor, incorporating
a manual mixture control.
pressure operated, single barrel an airflow operated power
1-3
TEXTRON
LYCOMING
OPERATOR'S
MANUAL
SECTION
The Bendix measuring convert differential) makes
The This continuous
valve
to each
mixture
the manual of injected control to engine.
Lubrication
wet sump
contained
and accessory
air
the
air force into
when
fuel flow
Simmonds
1. A
fuel
2. A
3. Four fuel This system
pump
throttle
ports by
intake valve
control
mixture
fuel to
"Idle Cut-Off"
System
lubrication
within
(A10-360
is of the
housing.
1
RSA type
flow and
proportional
flow system
body
flow nozzles.
is throttle actuated.
the nozzles.
position.
the
series).
dry sump
fuel injection
using the
a fuel
applied
assembly.
across the
type 530 is a
has
assembly.
The system
port in
response
Complete
control
- (All
which permits
suit all
results
models except
system
accessory
The AIO-360
type. A double
0-360
air flow signal
force. This
fuel metering
to
air flow.
continuous flow
three separate
Fuel is
to throttle
flexibility
operating
in a
is actuated
housing.
series
and
ASSOCIATED
system
is based
in a stem
fuel force
components:
injected into the
continuously
position,
of operation
the adjustment
conditions.
complete
AIO-360
by an
is designed
scavenge
on the
type regulator
section
series).
(jetting system)
fuel injection
delivers
engine speed
Moving
cut-off of
The full
impeller
for aerobatic
pump
is installed
MODELS
principle
(fuel
pressure
system.
engine intake
metered
is provided
of the amount
the mixture
fuel and
fuel to
the
pressure
type pump
flying
on the
of to
by
Priming
employing
System
a carburetor.
system.
Ignition
Consult
Counterweight
of the
System
Table
model
crankshafts
- Provision
-
Dual ignition
1 for model
System
- Models
number (example:
with pendulum
for a primer
Fuel
injected
is
application.
designated
type
counterweights
system
engines
furnished
by the numeral
0-360-A1G6)
is provided
on all
do not require
by
two Bendix
6 in
are
equipped
attached.
engines
a priming
magnetos.
the suffix
with
TEXTRON
LYCOMING OPERATOR'S
MANUAL
0-360 and
-A1A, -A2A,
-A4A
-A1C,-C2D
-A1D, -A2D,
-A4D, -A2E
-A1F,
-A1G,
-A1G6
-A1H,
-A1H6
-AlP,
-C4P
-A4K, -C1F, -C4F
-A4M
-A4N
-B1A, -B2A, -C1A,
-C1G, -C2A
-B1B, -B2B, -C1C,
-C2C
-C1E, -C2E, -A4M
-C2B
-D1A, -D2A
-D2B
-F1A6
-A1AD, -A3AD,
-A5AD
ASSOCIATED
Model
0-360
-A3A,
-A3D,
-A2F, -A1F6
-A2G,
-A2H,
-A4P, -B2C,
-A4G,
-A4J
MODELS
TABLE 1
MODEL APPLICATION
Left**
S4LN-21 S4LN-20
S4LN-200 S4LN-204
S4LN-200 S4LN-204 S4LN-1227 S4LN-1209
S4LN-1227 S4LN-21 4273
4373 4371
4371 4251
S4LN-21
S4LN-200 4051 S4LN-21 S4LN-21
S4LN-200 4191
D4LN-3021
Right**
S4LN-1209 S4LN-204 4270
4370 4370 4370 4251
S4LN-20
S4LN-204 4050 S4LN-20 S4LN-20 S4LN-204 4191
SECTION 1
Carburetor
MA-4-5
PSH-5BD
MA-4-5 MA-4-5
HA-6 HA-6 HA-6
MA-4-5
HA-6 MA-4-5 MA-4-5
MA-4-5
MA-4-5
MA-4-5
PSH-5BD
MA-4-5
MA-4-5
HA-6
MA-4-5
*-
Models with
* * -
See
latest
netos.
Revised May
counterclockwise
edition
of Service
1996
rotation
Instruction
employ
No.
1443
S4RN
for
series.
alternate
mag-
1-5
TEXTRON
LYCOMING
OPERATOR'S
MANUAL
SECTION
Model
0-360 (Cont.)
-A1F6D,
-A1G6D
-G1A6
-J2A
-A1A
-B1A
-B1B
-C1A
-A1A, -B1A, -B1B
I -AB, -C1A
-C1B
-D1A
-E1AD
-E1BD,
-A1A,
-B1C
-A1B,
-A1C,
-A1D6, -B1E, -B2E
-A3B6
-B1A
-B1D,
-A1LD
HO-360
HIO-360
-F1AD
IO-360
-A2A,
-A2B,
-A2C,
-C1A
1
-B1B,
-A1B6
-C1B
0-360 and ASSOCIATED
TABLE
MODEL
1 (CONT.)
APPLICATION
Left**
D4LN-3021
D4LN-3021 4251 4251 4347 4370
S4LN-200 S4LN-200 S4LN-200 4347
S4LN-200 S4LN-200 S4LN-1208 S4LN-1208
D4LN-3021 D4LN-3200
S4LN-200
S4LN-1227 S4LN-1208 S4LN-1227 4372 S4LN-200 S4LN-200
Right**
S4LN-204 S4LN-204 S4LN-200 4370
S4LN-200 S4LN-204 S4LN-1209 S4LN-1208
S4LN-204 S4LN-1209 S4LN-1209 S4LN-1209 4370 S4LN-204 S4LN-204
MODELS
Carburetor
MA-4-5 HA-6 HA-6 MA-4SPA
MA-4-5AA
PSH-5BD PSH-5BD
HA-6 Fuel Injector
RSA-5AB1 RSA-5AD1 RSA-5AD1 RSA-7AA1 RSA-5AB1 RSA-5AB1
RSA-5AD1 RSA-5AD1 RSA-5AD1 RSA-5AD1 RSA-5AD1 530 RSA-5AD1
* - Models ** - See latest edition of Service netos.
with counterclockwise
1-6
rotation
Instruction No. 1443 for
employ
S4RN series.
Revised
alternate mag-
May 1996
TEXTRON LYCOMING OPERATOR'S MANUAL
0-360 and ASSOCIATED MODELS SECTION
TABLE I (CONT.)
MODEL APPLICATION
Model
10-360 (Cont.)
-B2F, -B2F6
-BIF,
-B4A, -K2A S4LN-21
-CIC, -CIC6, -CID6
-CIE6, -CIF, -FIA S4LN-1227 S4LN-1209 RSA-5ADI
-EIA S4LN-1208
-DIA,
-AID S4LN-21 S4LN-204 RSA-5ADI
-L2A 4371 4371 RSA-5AD1
-MIA,-BIG6 4371 4370 RSA-5ADI
-CIG6 4345
-AIB6D, -A3B6D,
-J1AD, -J1A6D D4LN-3021 RSA-5ADI
-AID6D, -A3D6D D4LN-3000 RSA-5AD1 AIO-360
-AIA, -A2A
-AIB, -A2B, -B1B S4LN-1227 S4LN-1209 RSA-5AD1
TIO-360
-A1 A, -A1 B, -A3B6
-C1A6D D4LN-3021
Left**
S4LN-1227
S4LN-1227 S4LN-1209
S4LN-1208 S4LN-1209
S4LN-1208 S4LN-1209
Right** Fuel
S4LN-1227 S4LN-20
S4LN-1209 RSA-5ADI
4345
Injector
RSA-5ADI RSA-5ADI RSA-5ADI
RSA-5AD1
RSA-5ADI
RSA-5ADI
* - Models with counterclockwise rotation employ S4RN series. ** - See latest edition of
magnetos. Engine models with letter "D" as 4 or 5* character in suffix denotes
dual magnetos in single housing. Basic models employing -21 or -
1227 (impulse coupling magnetos) use D4LN or D4RN-3021. Basic models employing -200 D4LN or D4RN-3000. Example - Basic model 10-360-C1C uses S4LN-1227 and S4LN-1209, therefore model 10-360-CICD would employ
Revised December 1999 1-7
D4LN-3021.
Service Instruction No. 1443
and -1208 (retard breaker magnetos)
for alternate
use
TEXTRON
LYCOMING
OPERATOR'S
SPECIFICATIONS
Specifications
O-360-A,-B,-C,-D,-F HO-360-A,-B IO-360-A,-B,-C,-D,-E,-F,-J,-K AIO-360-A,-B HIO-360-A,-B HIO-360-C,-D HIO-360-E,-F
TIO-360-A,-C
Accessory Drives.........................................2-8
Detail
Dimensions............................................2-10
Weights
Engines ................................................
......................................
............................................
.............................
...........................................
...........................................
...........................................
.............................
..........................................
MANUAL
2-1 2-2 2-3 2-4 2-4 2-5 2-6 2-7
2-9
TEXTRON
LYCOMING OPERATOR'S
MANUAL
0-360 and ASSOCIATED MODELS SECTION 2
SECTION 2
SPECIFICATIONS
0-360-A, -C, -F SERIES*
FAA Type Certificate ..................
Rated horsepower
Rated speed, RPM ....................
Bore, inches ...........
Stroke, inches Displacement, cubic Compression ratio
Firing order ...........
Spark occurs, degrees
Valve rocker clearance
Propeller drive ratio ...................
Propeller
*0-360-C2D only.
drive rotation (viewed
....................
......................
inches ...............
....................
BTC ...............
(hydraulic tappets
from rear) ..
Take-off rating 180 HP @
collapsed)
2900 RPM and 28 in. hg.
SPECIFICATIONS
0-360-B,
Type Certificate ..................
FAA
Rated horsepower ....................
Rated speed, RPM ....................
Bore, inches .......................
Stroke, inches ......................
Displacement, cubic inches ...............
Compression ratio ....................
Firing order .......................
Spark occurs, degrees Valve rocker clearance (hydraulic tappets collapsed) Propeller drive ratio Propeller drive rotation
BTC ...............
...................
(viewed from
-D SERIES
rear) .....
.......... 286
.......... 180
.......... 2700
......... 5.125
......... 4.375
......... 361.0
......... 8.5:1
........ . 1-3-24
........... 25
........ 028-.080
.......... .1:1
....... Clockwlse
.......... 286
.......... 168
.......... 2700
......... 5.125
......... 4.375
......... 361.0
......... 7.2:1
........ 1-3-24
........... 25
........ 028-.080
...........
....... Clockwise
1:1
2-1
TEXTRON LYCOMING
OPERATOR'S
MANUAL
SECTION
2 0-360
and ASSOCIATED
SPECIFICATIONS
O-360-J2A
FAAType
Rated
Certificate
horsepower Rated speed, RPM Bore, inches Stroke,
...........................................
inches..........................................
Displacement, Compression Firing order
Spark Valve
Propeller
Propeller
ratio
............................................
occurs, degrees
rocker clearance
drive
drive rotation
....................................
........................................
...............................
inches ................................
cubic
.......................................
.................................
BTC
(hydraulic tappets
collapsed)
ratio ......................................
(viewed
from rear)
..................
SPECIFICATIONS
HO-360-A,
FAAType
Certificate
Rated horsepower
speed, RPM
Rated
....................
inches
Bore,
....................................
........................................
.......................................
Stroke, inches...........................................
Displacement, Compression
order
Firing
Spark occurs, Valve rocker
Propeller
Propeller
cubic inches ................................
........................................
ratio
............................................
................................
degrees
clearance
drive ratio
drive
BTC
(hydraulic
......................................
rotation
(viewed from
-C
........................
tappets
collapsed)
rear) ..................
MODELS
286
145
thru 2700
2400
5.125
3.875
361.0
8.5:1
1-3-2-4
25
.......... 028-.080
1:1
Clockwise
286
180
2700
5.125
4.375
361.0
8.5:1
1-3-2-4
25
..........
028-.080
1:1
Clockwise
2-2
Revised
May 1996
TEXTRON LYCOMING OPERATOR'S MANUAL
0-360 and ASSOCIATED MODELS SECTION 2
^
FAA Type Certificate .................................... 286
* Rated horsepower ........................................ 180
Rated speed, RPM
Bore, inches .................... .................... 5.125
Stroke, inches.........................................4.375
Displacement, cubic inches .............................. 361.0
Compression
Firing order ......................................... 1-3-2-4
Spark occurs, degrees BTC ................................. 25
Valve rocker clearance (hydraulic Propeller drive ratio
Propeller drive
FAA Type
Rated horsepower ........................................ 160
Rated speed, Bore,
inches ......... .............................
Stroke, inches .........................................
Displacement, cubic
* Compression ratio ...................................... 8.5:1
Firing order ........................................ 1-3-2-4
Spark occurs, Valve rocker
Propeller drive ratio ..................................... 1:1
Propeller drive
ratio .....................................
rotation (viewed from rear) ..............
Certificate ...................
RPM ......................................
degrees
clearance (hydraulic tappets
rotation (viewed from rear)
........SPECIFICATIONS
HO-360-B SERIES
......................................
tappets collapsed) ........
......................................
SPECIFICATIONS
10-360-L2A*
inches ..............................
BTC .................................
2900
8.5:1
028-.080
1:1
Clockwise
................
collapsed) ....... .028-.080
.............. Clockwise
1E10
2400
5.125
4.375
361.0
25
I * - This engine has an alternate rating of 180 HP at 2700 RPM.
I
Revised December 1999
2-2A
TEXTRON LYCOMING
OPERATOR'S
MANUAL
SECTION 2
0-360 and ASSOCIATED
MODELS
SPECIFICATIONS
10-360-B 1G6, -M 1A*
FAA
Type Certificate .........
Rated horsepower .......................................
Rated
speed, RPM
Bore,
inches .........................................
Stroke,
inches .........................................
Displacement, cubic Compression
......................................
inches ...........................
ratio ......................................
Firing order .........................................
Spark occurs, degrees BTC Valve
rocker clearance Propeller drive Propeller drive
* - This
ratio ......................................
rotation (viewed
engine has
an alternate
.................................
(hydraulic
from rear)
rating of 160
...................
tappets collapsed)
..............
HP at 2400
.......
.. 1E10
180
2700
5.125
4.375
... 361.0
8.5:1
1-3-2-4
25
028-.080
1:1
Clockwise
RPM.
10-360-CIG6
FAA Type Certificate Rated horsepower Rated
speed, RPM .....................................
Bore,
inches ..................................
Stroke, Displacement, Compression
inches ............................
cubic inches
ratio .....................................
..................................
........................................
..............................
........
IEIO
200
2700
5.125
4.375
361.0
8.7:1
Firing order ......................................... 1-3-2-4
Spark occurs, Valve rocker clearance, Propeller Propeller
degrees BTC ................................
(hydraulic tappets collapsed)
drive ratio
......................................
drive rotation (viewed from
20
...... 028-.080
1:1
rear) .............. Clockwise
2-2B
Added
December
1999
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