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8-33. Exhaust ports and other openings should be closed with suitable covers.
8-34. All exposed cadmium plated and machined surfaces should be liberally coated with soft-film, corrosion preven-titive compound, MIL-C-16173, Grade 2.
8-35.Although the above procedure should prevent corro-sion under favorable conditions it is recommended that the engine be periodically inspected for evidence of corro-sion. If corrosion should be present, the affected partshould be cleaned and the engine represerved. Also, engines preserved by the above procedures are not ade-quately protected for extended periods of storage. If at the end of 60 days it is found that the engine must remain in storage it must be represerved.

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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