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Jabiru Aircraft
Pty Ltd
Instruction & Maintenance Manual
Jabiru 2200 Aircraft Engine
Hydraulic Valve Lifter Models
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REVISION
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Dated : June 2010
Issued By: DPS
Page: 32 of 116
L:\files\Manuals_For_Products\Engine_Manuals\Transition\JEM2204-9_I&M_unsigned.docx
EITHER
– Remove each rocker cover and check that each lifter has not collapsed.
This is done by turning the crankshaft so that the valve is fully in the closed position,
then feeling the rocker by hand. There should be no free rotation of the rocker. Press
down on the pushrod end of the rocker
– the lifter should feel hard, with minimal
movement possible under thumb pressure. Note that the correct method for finding
this point is to turn the crank until the valve is fully open, then turning the crankshaft
through one complete revolution to rotate the cam lobe away from the lifter.
OR
– after the service, idle the engine, listen for loud tapping noises and feel for rough
running. This must be carried out with the cowls removed. Note that due to the need
to have a person at the controls of the aircraft, this is a two-person job.
CAUTION:
While ever the engine is running there must be a qualified person inside the aircraft,
at the controls. Under NO circumstances run the engine without a qualified person
at the controls.
Troubleshooting information is given in Section 14.1.11
Air can be caught inside the lifters after maintenance. Running the engine at a high
idle - approx 1500 RPM
– will expel the air but may take up to 15 minutes. When
fitting lifters after inspection or maintenance they should be filled by injecting oil into
the hole in the side of the lifter. Care must be taken to ensure all air is removed.
Several different hydraulic lifters have been used in Jabiru 2200 engines. The cam
P/No. fitted to the engine must be known when ordering replacement lifters. This
information can be found from the engine’s S/No. or from it’s overhaul records.
The type of lifter must be matched correctly to the cam design. Use of mismatched
parts will cause reduced engine power and possible engine damage.
Figure 7 shows identification markings on a P/No. 4A432A0D cam
– it has two “rings”
machined at the oil pump end and two small “spots” machined at the drive gear end.
Similarly, P/No. 4A430A0D cams are marked with one “ring”, and one “spot”. Engines
assembled with these cam types must use a Jabiru P/No. PE4A001 Hydraulic Lifter.
These cams are standard in engines with S/No. 22A-2850 & 22C-001 onwards.
Cams manufactured
without
any identification “rings” or “spots” must use a Jabiru
P/No. 4A294C0D Hydraulic Lifter.
The different types of Hydraulic Lifter are not marked and the difference requires
disassembly and careful measuring using a micrometer to detect. Accordingly, care
must be taken to ensure different types of lifter are not confused during maintenance.