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Engine Overhaul Manual
Jabiru Aircraft
Pty Ltd
Jabiru 2200 & 3300 Aircraft Engines
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ISSUE
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6 7
Dated : 28/10/2014
Issued By: AS
Page: 164 of 201
L:\files\Manuals_For_Products\Engine_Manuals\Overhaul_Manual\JEM0001-7_Overhaul_Manual_DRAFT_(29_10_14).docx
9.5.1 Oil Pump Clearance Measurement:
Figure 202
– Oil Pump Details
9.6 Electrical System Specifications
Table 13
– Electrical System Specifications
Ignition
All Coils
Strong & continuous spark required with 8mm
gap when tested using coil tester (Figure 27)
Coil to flywheel gap
0.27mm
to
0.30mm
Ignition harness resistance
6.7 K
Ω per 300mm length
Ignition magnet Strength (see Figure 203)
1.5
– 2.5kg.
Alternator
Coil resistance: early 2200 (10 Pole)
0.5 Ω to
1.1 Ω
Coil resistance: Parallel Wound 12-Pole.
0.2 Ω to
0.5
Ω
Coil resistance
–
Series Wound 12-Pole (per Document AVDALSR087)
1.4 Ω to
1.9 Ω
Coil earth resistance
Infinite
A.C. output: early 2200 (10 Pole)
30.0 VAC at 3000 RPM
A.C. output: (parallel wound 12 pole)
30.0 VAC at 3000 RPM
A.C. output
–
(series wound 12 pole per Document AVDALSR087)
Up to 40.0 VAC at 3000 RPM
D.C. output
Up To 14.3 VDC at 3000 RPM
Tachometer
Coil resistance
160
Ω to
170
Ω
Gap, flywheel tags to sender
0.40mm
– 0.50mm