8-36.Represervation Run. The represervation run should be accomplished under the same conditions as the run-in after overhaul except that only the followin time schedule must be followed.
TABLE 8-3
RECOMMENDED REPRESERVATION SCHEDULE
RPM LOAD TIME (MINUTES)
1200 1800 2400 Normal Rated Prop. Load Prop. Load Prop. Load See Table 8-1 5 5 5 15
8-37. Preservation and Storage. Float Type Carburetors. Carburetor shall be emptied of all residual gasoline and the throttle locked in the closed position.
TABLE 8-4
TEST PROPELLER CONFIGURATION
TEST TEST TEST
ENGINE PROPELLER PROPELLER PROPELLER
MODELS P/N ADAPTER P/N BOLTS P/N
0-320-H 64802 64980 64983
0-360-E 64803 64981 64984
LO-360-E ST-298 64981 64984
OVERHAUL MANUAL LYCOMING 76 SERIES AIRCRAFT ENGINES
SECTION 9
TABLE OF LIMITS
This section of the manual has been reserved for the Special Service Publication No. SSP-1776 Part I, Table of Limits and Tightening Torque Recommendations.
Upon receipt of the owner's registration card, attached in the front of this manual, at Lycoming, a copy of the Special Service Publication SSP-1776 Part I will be forwarded to the registered owner.
The SSP-1776 Part I should then be inserted in the manual at this location.
Also, the return of the registration card will assure the owner that for a period of three (3) years all future revi-sions to this publication and the Table of Limits will automatically be forwarded.
Lycoming
SERVICE TABLE OF LIMITS
AND
TORQUE VALUE
RECOMMENDATIONS
NOTICE
The basic Table of Limits, SSP2070 (including SSP2070-1, SSP2070-2, SSP2070-3 and SSP2070-3A) has been completely revised and reissued herewith as SSP1776. It is now made up of the following four parts, each part contains five sections.
PART I DIRECT DRIVE ENGINES (Including VO and IVO-360)
PART II INTEGRAL ACCESSORYDRIVE ENGINES
PART III GEARED ENGINES
PART IV VERTICAL ENGINES (Excluding VO and IVO-360)
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