1997 Sea-Doo SP/SPX/GS/GSI/GSX/GTS/GTI/GTX/XP/HX Service Manual (428 P.)

Factory service documentation covers 717D (66 kW), 717 (70 kW), 787 (82 kW), and 947 (110 kW) engines with complete maintenance, troubleshooting, and rebuild procedures for all 1997 Sea-Doo watercraft models.

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Document Details

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Document Number / Seller:
23308 / Harold Grant
File Size:
68.98 MB
File Type:
ZIP
Language:
English
Pages:
428
Printable:
Yes
Estimated Download Time:
1.41 Minutes
Delivery Format:
Digital (PDF) - Instant Access
Category:
Personal Watercraft (PWC)
Brand:
Sea-Doo
Reviewed and Approved:
Jan 21, 2025
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Models Covered & Key Technical Specifications

Sea-Doo SP, SPX, GS, GSI, GSX, GTS, GTI, GTX, XP, HX — 1997

Procedural Guide & Technical Directory Record.

  • Published Production Rate: The 717D engine corresponds to 717 cm³ (43.7 cu in) displacement volume Margin.
  • Measured Physical Specs: Crankshaft assembly fasteners sets 95 N·m (70 lbf·ft) torque requirement Protocol.
  • Approved Output Quality: Peak horsepower is rated at 110 kW (147 hp) for the 947 engine Architecture.
  • Reference Fill Levels: Standard fuel tank volume achieves 48 liters (12.7 US gallons) capacity Norms.
  • Fundamental Assembly Gap: Impeller shaft radial play determines 0.05 mm (.002 in) maximum tolerance Bounds.
  • Universal Print Rate: Oil injection pump delivery yields 4.5 mL per 100 engine revolutions Topology.

Professional Workshop Service Manual & Technical Specifications

Specialized Reference Training Manual: Personal Watercraft (PWC) 1997 Sea-Doo Service Manual: SP 5879 / SPX 5834 / GS 5821 / GSI 5822 / GSX 5624 / GTS 5818 / GTI 5841 / GTX 5642 / XP 5662 / HX 5882 Repair-Index

Maintenance-Category: Sea-Doo SP, SPX, GS, GSI, GSX, GTS, GTI, GTX, XP, HX models // Architecture-Focus: 2-stroke engine / Jet pump propulsion // Series-Validation: 717D, 717, 787, 947 engine configurations with rotary valve intake control systems.

Performance-Element Operational-Logic Architecture
Engine Systems Rotary valve timing procedures, magneto CDI ignition, top end/bottom end overhaul Complete specifications provided
Fuel & Lubrication Mikuni carburetor adjustment, oil injection pump calibration, fuel system pressurization See Chapter 5-6
Propulsion Assembly Impeller clearance measurement, wear ring replacement, drive shaft alignment Documented in Chapter 8
Electrical Components DC-CDI ignition timing, charging system testing, starter motor disassembly Complete diagnostic procedures
Cooling Architecture Serial cooling circuit, water flow regulator valve calibration, RAVE system Chapter 4 specifications

Outlining the operational framework across maintenance procedures, the document addresses troubleshooting protocols, specifies engine configurations, details fuel system components, and catalogs propulsion mechanisms with systematic cross-referencing throughout all technical chapters.

Quality checks are addressed for cylinder head torque sequences, piston ring gap measurements, and crankshaft deflection tolerances across all displacement variants. The engine section documents complete disassembly procedures for 717 cm³ and 787 cm³ powerplants, including specialized tooling requirements for magneto flywheel removal and rotary valve timing verification. Cooling system maintenance is addressed in dedicated chapters covering water injection fitting calibration, temperature sensor diagnostic procedures, and tuned pipe pressurization testing protocols.

The troubleshooting chapter addresses diagnostic flow charts for ignition spark verification, fuel delivery problems, and starting system failures with resistance value specifications. Testing requirements are specified for battery charging coil output, trigger coil continuity, and MPEM self-diagnostic modes using Bombardier ignition tester equipment. The propulsion system documentation includes impeller/wear ring clearance specifications with maximum 1.0 mm tolerance limits, jet pump housing pressurization procedures at 70 kPa, and drive shaft deflection measurement techniques.

The manual documents torque specifications for the crankshaft assembly to ensure proper thermal expansion compensation, with values ranging from 24 N•m for cylinder head fasteners to 145 N•m for magneto flywheel retention across different engine configurations.

FAQ

What values are **calibrated** for the 787 engine displacement and compression ratio? keyboard_arrow_down

787 cm³ (48.0 cu in) displacement with 8.2:1 compression ratio defines the 787 engine specifications, delivering 82 kW (110 hp) output for models including SPX, GSX, and GTX.

Assess the **applicable** torque specifications for crankshaft assembly fasteners? keyboard_arrow_down

95 N·m (70 lbf·ft) for crankshaft assembly fasteners, 40 N·m (30 lbf·ft) for connecting rod bolts, and 40 N·m (30 lbf·ft) for cylinder head bolts according to primary torque specifications chart.

What components require the **exact** 34 kPa (5 PSI) pressurization during leak testing? keyboard_arrow_down

34 kPa (5 PSI) maximum pressure applies to engine cooling system testing, bottom end and top end verification, and fuel system pressurization checks as specified in diagnostic procedures.

Confirm the **specific** oil injection pump delivery rate at maximum RPM? keyboard_arrow_down

4.5 mL per 100 engine revolutions at maximum RPM ensures precise lubrication across all operating conditions through the technical fuel injection oil pump capacity system.

What tools are **designated** for measuring impeller shaft radial clearance tolerances? keyboard_arrow_down

0.05 mm (.002 in) maximum radial play measured with dial gauge positioned at shaft end close to threads, requiring V-blocks and indicator setup per jet pump inspection procedures.

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Reviews (3)

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Rated 4 out of 5 stars
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The detailed breakdown of each system is impressive. I contacted support with a question, and they were very responsive!
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This manual has everything you need to keep your Sea-Doo in top shape. The troubleshooting sections are particularly helpful!