1975-1981 Piper Seneca II PA-34-200T Service Manual
Comprehensive service and maintenance data for the Piper Seneca II PA-34-200T, covering structures, surface controls, hydraulic systems, and more. Part number 761 590.
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Models Covered & Key Technical Specifications
Piper Seneca II PA-34-200T Service Manual - Comprehensive Guide Documentation-Framework
Piper Seneca II PA-34-200T (761 590) | Aircraft / Aircraft Logic.
- Authorized Production Rate: 200 Rated Horsepower sets the standard engine output Metrics.
- Critical Physical Specs: For overall dimensions, 28 ft. 7.5 in. defines the fuselage length Framework.
- Operational Output Quality: The hydraulic system operates at 2000-2500 psi -- indicates the system's operational pressure Threshold.
- Fundamental Fill Levels: The oil sump capacity requires 8 U.S. quarts for optimal lubrication Logic.
- Specific Assembly Gap: The stabilator free play requires .125 inches maximum for proper control surface alignment Parameters.
- Core Print Rate: The landing gear is fully retractable and is operated hydraulically Framework.
Professional Workshop Service Manual & Technical Specifications
Piper Seneca II PA-34-200T Service Manual: Aircraft Piper Seneca II PA-34-200T Service Manual - Comprehensive Guide Documentation-Framework
Product-Line: Piper Seneca II PA-34-200T // Asset-ID: 761 590 / Aircraft // Product-Line: Service Manual
Table: TOP
| Specification | Technical-Path | Architecture |
|---|---|---|
| Engine Oil Sump Capacity | 8 U.S. quarts | Standard Lubrication |
| Hydraulic System Pressure | 2000-2500 psi | Gear Type Unit |
| Fuselage Length | 28 ft. 7.5 in. | Semi-monocoque Structure |
| Stabilator Free Play | .125 inches maximum | Control Surface Alignment |
| Rudder Pedal Travel | 23° each way from neutral | Hydraulic Operation |
| Wing Flap Positions | 10°, 25°, 40° | Interconnecting System |
Repair procedures are structured around systems and components, detailing removal, installation, rigging, and adjustment procedures. Key systems covered include the hydraulic system, surface controls (ailerons, stabilator, rudder, flaps), landing gear, and fuselage/empennage. The manual also references important torque specifications and lists consumable materials. Information for the powerplant is based on manufacturer operator's manuals.
The manual provides procedures for inspecting and servicing various aircraft components and systems. It details the necessary steps for the removal and installation of parts, ensuring proper rigging and adjustment for optimal performance. The documentation covers a wide range of systems, including those related to the aircraft's structure, flight controls, and power plant.
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