AD 77-07-07

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AD Number:
77-07-07
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
AVCO LYCOMING Model O-320-H2AD Series Engines
Subject:
Oil Level Gage
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/20/1979
Make:
Lycoming Engines
Model:
O-320-H2AD
Product Type:
Engine
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 77-07-07
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3415

AD NUMBER:   77-07-07

SUBJECT HEADING:   AVCO LYCOMING Model O-320-H2AD Series Engines

ACTION:  

SUMMARY:  

DATES:   Effective February 20, 1979.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   77-07-07 AVCO LYCOMING: Amendment 39-2864 as amended by Amendment 39-3415. Applies to the O-320-H2AD series Lycoming engines Serial Numbers L-101-76 thru L-1049-76.
Compliance required within 50 hours in service after the effective date of this AD, unless previously accomplished.
To prevent the incorrect installation of the P/N LW-14784 or the P/N LW-15481 oil level gage modify the P/N 75675 oil filler extension by installing a P/N LW-15498 perforated sleeve as follows:
(a) Remove the P/N 75675 oil filler extension from the engine.
(b) Insert the P/N LW-15498 perforated sleeve in the oil filler extension. Make certain that the flanged end rest evenly against the recessed surface below the threads inside of the oil filler extension. Locate and mark the perforated sleeve where it protrudes through the base of the oil filler extension.
(c) After locating this position, remove the perforated sleeve from the oil filler extension and insert a length of 3/4 inch diameter steel rod into the sleeve. Place the steel rod and sleeve in a vise or other suitable holding device and with a narrow chisel cut the perforated sleeve as shown in figure 1 at the location marked per instructions of item (b) of this AD.
(d) Remove the 3/4 inch diameter steel rod and install the perforated sleeve in the oil filler extension. Bend the chiseled section of the perforated sleeve at the seam to form a tab as shown in figure 2.


(e) Install the reworked oil filler extension and perforated sleeve in the engine, making certain that the P/N 70457 gasket is properly in place between the oil filler extension and the engine crankcase. Install either P/N LW-14784 or P/N LW-15481 oil level gage. Apply lockwire as required.
(f) Upon submission of substantiating data through an FAA Maintenance Inspector, the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region, may adjust the compliance time.
(Note: AVCO Lycoming Service Bulletin No. 407A covers this subject).
Amendment 39-2864 became effective April 11, 1977.
This amendment 39-3415 is effective February 20, 1979

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