DATE RELEASED:

September 2017

TITLE:

LIO-360-B1G6 Maintenance Manual 

DOCUMENT PART NUMBER:

MM-LIO-360-B1G6

DATE RELEASED:

September 2017

TITLE:

LIO-360-B1G6 Installation and Operation Manual

DOCUMENT PART NUMBER:

IOM-LIO-360-B1G6

REPRINT OF HARTZELL ENGINE TECHNOLOGIES' SERVICE BULLETIN ASB 069

DATE:

August 29, 2017

MODELS AFFECTED:

Table 2 in this Service Bulletin

TIME OF COMPLIANCE:

Next maintenance event not to exceed 25 hours or before further flight if fuel leak found during preflight inspection

DATE:

April 10, 1987

MODELS AFFECTED:

GO-435, GO-480, IGO-480. GSO-480, IGSO-480. IGO-540, IGSO-540, VO-540. TIGO-541.

TIME OF COMPLIANCE:

At all times during engine operation including ground running.

DATE: September 30, 2002

MODELS AFFECTED

All engines listed in Table 1. All O, IO, (L)TIO or AEIO-540 engines that have had a crankshaft bolt replaced during maintenance or overhaul between November 27, 1996 and November 10, 1998.

TIME OF COMPLIANCE

Within the next ten (10) hours of operation or seven (7) days, whichever occurs first.

DATE: September 5, 2002

Lycoming Service Bulletin No. 552 requires replacement of crankshafts in some turbocharged Lycoming TIO and LTIO-540 engines rated at 300 horsepower or higher.

DATE: July 1, 2002

MODELS AFFECTED

All Lycoming aircraft engines.

TIME OF COMPLIANCE

At engine start in cold weather.

In extremely low temperatures, oil congeals, battery capacity is lowered, and the starter can be overworked. Improper cold weather starting can result in abnormal engine wear, reduced performance, shortened time between overhauls, or failure for the engine to operate properly.

Supersedes Service Bulletin No. 529 A

June 10, 2002

MODELS AFFECTED

All Lycoming aircraft engines employing new or overhauled “AN” rotary fuel pump model series RG9080, RG9570 and RG17980, including:

Supersedes Service Letter No. L180 A

Models Affected

To all Owners and Operators of Textron Lycoming Aircraft Engines

Engines in aircraft that are flown only occasionally may not achieve normal service life because of corrosion. This occurs when moisture from the air and products of combustion combine to attack cylinder walls and bearing surfaces during periods when the aircraft is not used. The procedures for combating this condition consist of coating the vulnerable surfaces with rust inhibitive compounds as herein described.

Supersedes Service Bulletin No. 545

October 2, 2001

MODELS AFFECTED

I. All Textron Lycoming TIO-540-AJ1A and IO-540-AC1A5 aircraft engines shipped from the factory before October 30, 2000, unless Kit P/N 05K23081 has been installed.

II. All Textron Lycoming TIO-540-AJ1A and IO-540-AC1A5 aircraft engines that have had Kit P/N 05K23081 installed before May 1, 2001.

TIME OF COMPLIANCE

I. Inspect within the next 10 hours of operation and replace within the next 50 hours of operation.