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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Document Details

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Document Number / Seller:
29188 / Donna Murphy
File Size:
29.18 MB
File Type:
PDF
Language:
English
Printable:
Yes
Category:
Aircraft
Last updated / verified
Oct 16, 2025

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.

FAQ

Specify the **applicable** lubrication requirements for the Piper Seneca II? keyboard_arrow_down

100 hours is the standard lubrication interval for most components, including main gear pivot points and bellcrank assemblies. Refer to specific lubrication charts for detailed requirements.

What are the **exact** testing parameters for the hydraulic system? keyboard_arrow_down

2000 to 2500 psi is the operational pressure range for the gear type hydraulic pump, with a primary thermal relief valve maintaining pressure up to 2350 ± 50 psi.

Calculate the **specific** diagnostic procedures for control surface balance? keyboard_arrow_down

80 hours is the recommended interval for checking control surface balance. This involves using a fabricated rigging tool and bubble protractor to ensure static balance within specified limits.

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Reviews (4)

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Rated 4 out of 5 stars
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I found the troubleshooting section particularly helpful. The download process was smooth, and support was quick to respond to my questions.
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This manual has everything from inspections to maintenance procedures. Highly recommend it!
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The service manual is incredibly detailed and easy to follow. It covered everything I needed for maintenance!