Air Compressor Specifications; Fuel System Specifications - Mercury 200 OptiMax Jet Drive Service Manual

Direct Fuel Injection

Air Compressor Specifications

Air compressor type
Air compressor output
Displacement
Cylinder bore
Cylinder bore taper (maximum)
Cylinder bore out of round (maximum)
Cylinder bore type
Stroke
Piston type
Piston diameter
Ring end gap
Top ring
Middle ring
Bottom ring
Reed stand open (maximum)

Fuel System Specifications

Fuel lift pump pressure at idle
Normal
Maximum
Fuel lift pump amps
Low‑pressure boost pump pressure at idle
Low‑pressure boost pump amps
High‑pressure fuel pump pressure
Air pressure
Fuel/air differential
High‑pressure fuel pump amp
High‑pressure fuel pump ohm resistance
Fuel injector ohm resistance
Direct injector ohm resistance
Page 3B-2
Air Compressor Specifications
Fuel Lift Pump Specifications
Low‑Pressure Boost Pump Specifications
Fuel System Specifications
Reciprocating piston
Single cylinder, oil lubricated, water‑cooled
655 ± 14 kPa (95 ± 2 psi)
116 cc (7.07 cid)
65.0 mm (2.559 in.)
0.025 mm (0.001 in.)
0.025 mm (0.001 in.)
Cast iron
34.9 mm (1.374 in.)
Aluminum
64.97 ± 0.010 mm (2.5578 ± 0.0004 in.)
0.15–0.25 mm (0.006–0.0010 in.)
0.15–0.25 mm (0.006–0.0010 in.)
0.10–0.35 mm (0.004–0.014 in.)
0.25 mm (0.0010 in.)
6.9–13.8 kPa (1–2 psi)
69 kPa (10 psi)
1–2 A
41–62 kPa (6–9 psi)
751.5 ± 14 kPa (109 ± 2 psi)
655 ± 14 kPa (95 ± 2 psi)
103.5 kPa (15 psi)
10–14 A
1.0–1.8 Ω
1.8 ± 0.1 Ω
1.3 ± 0.3 Ω
90-8M0050731 MAY 2011
1–2 A