Beechcraft Bonanza Model 35 H35, J35, K35, M35, N35, P35, V35 & V35TC, V35A & V35A-TC Illustrated Parts Catalog
Technician-level documentation for Beechcraft Bonanza H35, J35, K35, M35, N35, P35, V35 & V35TC, V35A & V35A-TC – includes part numbers, detailed illustrations, and cross-references for a complete service history. Publication 35-590015-9C.
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Sample pages from the Beechcraft Bonanza Model 35 H35, J35, K35, M35, N35, P35, V35 & V35TC, V35A & V35A-TC Illustrated Parts Catalog manual
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Models Covered & Key Technical Specifications
Consolidated Procedure Assembly Manual: Aircraft Genuine Beechcraft Model 35: H35, J35, K35, M35, N35, P35, V35 & V35TC, V35A & V35A-TC - Illustrated Parts Catalog OEM-Documentation
Structured Dossier Overview Resource | Series Segment. System Load Capacity: 7 units are configured at the assembly baseline. Core Environmental Range: For optimal operation, 18-26°C establishes the operational framework. Specific RPM Specs: Represents the maximum operational throughput. Critical Installation Footprint: The external dimensions require 1.75m x 1.0m for baseline placement. Universal Threaded Fastener Data: Indicates the standard torque requirements. Technical Voltage Specs: Thresholds maintain 12V for operational parameters.
Professional Workshop Service Manual & Technical Specifications
Consolidated Procedure Assembly Manual: Aircraft Genuine Beechcraft Model 35: H35, J35, K35, M35, N35, P35, V35 & V35TC, V35A & V35A-TC - Illustrated Parts Catalog OEM-Documentation
Diagnostic-Area: Comprehensive Parts Lists // Operational-Scope: Aircraft / Bonanza Logic // Diagnostic-Area: Technical Details.
| TOP | Component | Diagnostic-Logic | Architecture |
|---|---|---|---|
| Wing | Main Section Structure | 2-97 | |
| Fuselage | Structure | 7 | |
| Seat Assembly | Pilot's Seat | 13A | |
| Control System | Aileron Control | 21 | |
| Door | Baggage Door | 11 | |
| Cabin | Upholstery and Soundproofing | 15 |
Cataloging major assemblies into logical frameworks. Diagnosis Procedures Documented: Adjustment procedures are detailed for landing gear and flap systems, ensuring proper alignment and function. Timing procedures are documented for engine controls and flight systems, crucial for synchronized operation. Technical notes are provided for critical structural components and aerodynamic surfaces, offering essential context. Quality checks are addressed for electrical systems and instrument panels, ensuring reliable functionality. The flap system section documents operation and maintenance procedures for all flap motors and actuators. The rudder system section details the necessary components for pedal and control linkage assembly, including critical torque specifications to ensure proper axial load stability. ...documents torque specifications for control systems to ensure proper axial load stability.
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