1996 Sea-Doo SP/SPI/SPX/XP/HX/GTS/GTI PWC Shop Manual

Technical reference for all 1996 Sea-Doo models including Rotax engine teardown, jet pump service, and electrical diagnostics. Complete OEM shop procedures with torque specs and part numbers.

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Document Details

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Document Number / Seller:
24903 / Nancy Crawford
File Size:
16.76 MB
File Type:
PDF
Language:
English
Pages:
315
Printable:
Yes
Category:
Personal Watercraft (PWC)
Last updated / verified
Jan 5, 2026

Models Covered & Key Technical Specifications

Sea-Doo SP / SPI / SPX / XP / HX / GTS / GTI — 1996 Systematic Technical Dossier | PWC Engine Repository.

  • Nominal Feed Speed: Idle speed is set to 1500 RPM when watercraft is in water, defining operational baseline Framework.
  • Prescribed Size Parameters: For 587 engine, 1.2–1.8 mm (.047–.071 in) squish gap corresponds to combustion chamber clearance Threshold.
  • Calibrated Imaging Specs: Piston / cylinder wall clearance for 587 engine is 0.05–0.07 mm (.002–.0028 in), specifying bore tolerance Mapping.
  • Documented Fluid Capacity: Jet pump oil reservoir dictates 90 mL (3.0 U.S. oz) capacity using synthetic 75W90 GL5 polyolester oil Configuration.
  • Defined End Play: Maximum impeller shaft end play limits 0.12–0.54 mm (.005–.021 in) radial displacement Benchmarks.
  • System Processing Speed: Engine rev limiter is standardized to 6550 ± 50 RPM for 587 engine, 7000 ± 50 RPM for 717 engine Range.

Professional Workshop Service Manual & Technical Specifications

Thorough Technical Manual: Personal Watercraft (PWC) Sea-Doo SP/SPI/SPX/XP/HX/GTS/GTI Standards-Vault

Model-Portfolio: Sea-Doo SP (5876), SPI (5878), SPX (5877), XP (5858/5859), HX (5881), GTS (5817), GTI (5865/5866) // Technical-Domain: Rotax 587/717/787 Engine Logic, Bombardier Formula Pump Propulsion, CDI/DC-CDI Ignition Systems // Subsystem-Focus: Multi-engine service specifications, jet pump architecture, RAVE exhaust valve function documentation.

Documentation Section Coverage Category Reference Material
Engine Systems Rotax 587, 717, 787 platform configurations with top/bottom-end assemblies Complete specifications provided
Propulsion & Drive Jet pump disassembly, impeller wear ring clearance, drive shaft alignment, reverse system procedures See Chapters 09-01 through 09-04
Electrical & Controls Magneto, CDI/DC-CDI ignition, charging system, DESS security module, variable trim system Documented specifications included

Systematizing the service groups into Engine (top/bottom-end, rotary valve, exhaust), Cooling System (Serial Cooling, water injection, elbow fittings), Fuel System (carburetors, oil injection pump synchronization), Electrical (magneto systems, ignition timing, starting motor), Propulsion (jet pump, drive system, reverse mechanism), and Steering (handlebar assembly, trim systems), the manual provides comprehensive technical information across seven primary powerplant configurations and seven distinct watercraft models.

Strategic Nexus

Engine rebuild procedures are documented for the 587 and 717 engines featuring Rotax Capacitor Discharge Ignition systems with integrated multi-purpose electronic modules, while the 787 engine incorporates a digital DC-CDI system with separate rear electrical box mounting and RAVE (Rotax Adjustable Variable Exhaust) automatic valve control. Logical system documentation includes crankshaft deflection measurement procedures, piston-to-cylinder wall clearance verification, squish gap establishment using solder methodology, and rotary valve timing specifications with opening/closing angle references for each engine platform. The manual documents torque specifications for critical fasteners to ensure proper gasket seal integrity throughout engine assembly and reassembly operations.

Structured Benchmarks

Drivetrain specifications are addressed in propulsion chapters detailing jet pump component inspection, impeller/wear ring clearance limits (maximum 1.0 mm), needle bearing radial play tolerance (0.05 mm maximum), and drive shaft deflection measurement techniques using V-block support. Service sections cover Bombardier Formula Pump architecture with single-stage axial flow design, crown spline transmission configuration, and nozzle angle adjustment parameters. The document includes reference data for impeller identification by pitch angle (ranging from fixed 18.8° to progressive pitch configurations), bearing installation methodology using specialized installer tools, and seal positioning requirements with lip orientation specifications.

Structured Interface

Reassembly procedures are specified for fuel system pressurization testing at 34 kPa (5 PSI) sustained pressure, oil injection system pressure testing at 21 kPa (3 PSI), and jet pump housing pressurization verification at 70 kPa (10 PSI) maximum. System documentation encompasses diaphragm carburetor specifications for Mikuni BN-38/BN-40I models with integrated fuel pump verification, needle valve pop-off pressure ranges varying by watercraft model (21-56 PSI), and low-speed screw adjustment sequences. The manual provides cooling system flushing procedures, antifreeze solution specifications for seasonal winterization, and water injection elbow fitting calibration data with stamped identification numbers and inlet/outlet diameter measurements.

Diagnostic Protocol

Service intervals are documented for periodic inspection at 10-hour, 25-hour, 50-hour, and 100-hour service cycles, with component-specific maintenance frequencies including spark plug replacement, carburetor adjustment, fuel filter/oil filter inspection, steering system verification, and variable trim system functional testing. Troubleshooting guidance addresses engine starting failure scenarios, misfiring conditions, performance loss at higher RPM ranges, and abnormal noise origination from propulsion systems. The document includes diagnostic procedures for ignition timing verification using stroboscopic timing lights, static test procedures with degree wheel positioning, and dynamic test methodology at specific RPM thresholds (6000 RPM for 587/717 engines, 3500 RPM for 787 engine).

Systematic Framework

Component locations are identified for magneto housing access, armature plate positioning, engine support mount configuration with shim documentation, battery removal sequence by cable polarity order, and jet pump support mounting on hull structures. The manual provides detailed wiring diagram references organized by section number, electrical connector color-coding documentation for MPEM and ignition system circuits, and safety lanyard switch verification procedures for DESS anti-theft system functionality. System descriptions include reverse gate spring tensioning, variable trim motor worm gear engagement, steering stem arm keyway alignment, and handlebar assembly installation with integrated throttle cable routing through bilge support structure.

Specialized service information documents carburetor synchronization for twin-carburetor engine configurations, impeller removal using heat application (150°C target) with Loctite bond breaking methodology, wear ring installation using arbor press force or hammer-strike progression technique, and bearing/seal installer tool operation to achieve precision depth positioning within lubrication reservoir zones. Reference sections detail oil injection system operation with variable-rate pump flow curves, battery hydrometer testing for specific gravity measurement, and charging system current output specifications ranging from 4 amperes (587/717) to 5 amperes (787) at 5500 RPM engine speed.

FAQ

Specify the **applicable** jet pump oil capacity for all models. keyboard_arrow_down

90 mL (3.0 U.S. oz) of SEA-DOO synthetic 75W90 GL5 polyolester oil is the standard reservoir capacity that must be filled slowly to allow complete housing fill during assembly.

What is the **exact** ignition timing specification for the 587 engine? keyboard_arrow_down

2.41 mm (.095 in) BTDC is the required ignition timing measurement, verified by positioning the TDC gauge in the MAG side spark plug hole and rotating the PTO flywheel accordingly.

Calculate the **specific** flywheel nut torque requirement for the magneto installation. keyboard_arrow_down

145 N•m (107 lbf•ft) must be applied to the MAG flywheel nut after Loctite 242 is applied to the crankshaft taper, with anti-seize lubricant used on the fastener.

What values are **designated** for cooling system monitoring beeper activation across all engines? keyboard_arrow_down

96-99°C (205-210°F) is the temperature threshold at which the monitoring beeper activates, and this specification applies universally to all engine variants regardless of displacement or configuration.

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The manual is incredibly detailed and easy to follow. I had a smooth download process, and the support team was quick to respond to my questions. Highly recommend this for any Sea-Doo enthusiast!