1998 Sea-Doo SPX, GS, GSX Limited, XP Limited, GTS, GTI & GTX Limited PWC Repair Manual (P/N 219 100 068)
426 Pages • Printable PDF • 79.32 MB • Download
Sea-Doo Models Covered & Key Technical Specifications
Models: SPX, GS, GSX Limited, XP Limited, GTS, GTI, GTX Limited
Models & Model Codes:
SPX — 5838/5839
GS — 5626/5844
GSX Limited — 5629/5845
XP Limited — 5665/5667
GTS — 5819
GTI — 5836/5841
GTX Limited — 5837/5842
Sub-models / Variants: 717 Engine (GS, GTS, GTI), 787 Engine (SPX), 947 Engine (GSX Limited, XP Limited, GTX Limited)
Model Year: 1998
Transmission: Direct drive (all covered models)
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Engine displacement: 781.6 cc (787 Engine)
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Cooling system pressure test: 34 kPa (5 PSI), for 717 and 787 engines
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Jet pump impeller clearance: 1.0 mm (0.040 in) maximum allowable tolerance
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Starter nominal output: 0.6 kW (12 V rated), for 717 and 787 engines
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Cylinder head bolt torque: 15 N•m (11 lbf•ft), then 34 N•m (25 lbf•ft), following the specified tightening sequence, for 947 engine
Sea-Doo Manual Features & Selected Content Preview
Official Bombardier shop manual for the 1998 Sea-Doo SPX, GS, GSX Limited, XP Limited, GTS, GTI, and GTX Limited personal watercraft, P/N 219 100 068. Its 14 sections cover maintenance, troubleshooting, mechanical repair, electrical testing, and model-specific technical data.
Searchable Workshop Text and Model Wiring Diagrams
Text search and diagram detail: Workshop text is searchable, but the model wiring diagrams have no searchable text layer. Embedded bookmarks provide access to the main sections and individual model diagrams; the legacy MAIN MENU link points to a separate file. Small connector numbers and wire codes require zooming, and each model’s wiring diagram spans two pages.
One printable English PDF with 426 pages, including both covers, the copyright page, nine preliminary pages, and seven wiring-diagram divider pages.
Rotax Engine, Electrical, and Jet-Pump Service
The following selected coverage highlights outline the main workshop areas. Other topics include seat-cover replacement and hull-insert repair.
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Engine repair: Step-by-step engine removal and installation, top-end and bottom-end disassembly, internal inspection, rotary-valve timing, and RAVE valve adjustment.
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Fuel and oil injection: Mikuni carburetor rebuilding and synchronization, fuel-system pressure testing, oil-pump adjustment, bleeding, and delivery checks.
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Cooling and maintenance: Cooling-circuit diagrams, flushing and lubrication, water-flooded engine recovery, storage procedures, and the periodic inspection chart.
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Electrical troubleshooting: Ignition, charging, and starting-system tests, starter overhaul, DESS self-diagnosis, and model-specific wiring diagrams.
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Jet-pump overhaul: Impeller and wear-ring inspection, shaft-bearing and seal replacement, pump pressure testing, and drive-system service.
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Steering and trim: Steering-cable replacement and alignment, reverse-system adjustment, and Variable Trim System service for the applicable models.
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Hull and suspension: Fiberglass and gelcoat repairs, jet-pump support sealing, and XP Limited direct action suspension removal and inspection.
Written primarily for manufacturer-trained watercraft technicians already familiar with Sea-Doo service and maintenance procedures, this manual assumes access to the specified hand tools and special service tools.
Engine Overhaul and Variant Differences
The Rotax 717 and 787 use rotary-valve induction; the 947 uses reed valves. RAVE coverage distinguishes the exhaust-pressure-operated arrangement from the MPEM-controlled system on the 947.
Inspection procedures address cylinder taper, piston-to-cylinder clearance, ring end gap, combustion-chamber volume, and crankshaft alignment. Component-specific torque tables, fluid capacities, exploded views, and torquing-sequence illustrations support reassembly.
The engine leakage diagnostic flow chart helps distinguish cooling-system, crankcase, and rotary-valve-shaft sealing faults before teardown. The documented leak-test kit procedures apply to the 717 and 787; the manual defers the 947 kit update to a separate service bulletin.
Incorrect indexing of the crankshaft and counterbalance shaft can cause engine vibration and premature wear. Defective assembled crankshafts are referred to a specialized repair shop or replacement.
Carburetor, Lubrication, and Cooling Checks
Fuel-system schematics distinguish the single- and twin-carburetor layouts. The carburetor chapter includes diaphragm leakage, needle-valve, pop-off pressure, and accelerator-pump checks, with model-specific calibration data.
Oil-injection coverage extends to pump synchronization and measured delivery testing. Cooling-system information explains the different engine circuits and the water-flow regulator used with the 787 and 947; its factory calibration is not intended to be modified.
When servicing the fuel system or ignition components, follow the manual’s fuel-leak checks and electrical-isolation precautions.
Electrical Diagnosis and MPEM Functions
Starting-system troubleshooting separates battery, switch, solenoid, wiring, and MPEM faults from starter-motor faults before removal. Ignition testing includes static and dynamic checks rather than relying on resistance measurements alone.
The timing correction chart supports programmer-based ignition adjustment on the 787 and 947. DESS coverage includes basic and advanced diagnostic beep charts; safety-lanyard programming refers to the separate MPEM programmer guide.
Pump Alignment, Reverse, and Suspension
Engine/jet-pump alignment procedures identify the required support plates and alignment shaft, including P/N 295 000 141. Drive-system coverage distinguishes carbon-ring and seal-carrier arrangements.
Reverse adjustments are separated for the GTS and GTI/GTX Limited layouts. VTS procedures cover the SPX, GSX Limited, and XP Limited, while the XP Limited suspension section adds shock-absorber inspection and spring-handling requirements.
Selected Rotary-Valve Clearance and Oil-System Test Data
For the 717 and 787, rotary valve-to-cover clearance is 0.25–0.35 mm (0.010–0.014 in). The rotary-valve chapter explains that insufficient clearance can cause overheating, while excessive clearance can cause hard starting.
The oil-injection system pressure test specifies 21 kPa (3 PSI), maintained for at least 10 minutes with the reservoir full. This is a separate test from the engine and jet-pump leakage checks.
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