1962 Beechcraft Bonanza Model 35 Thru G35 Parts Catalog

Beechcraft Bonanza Model 35 Thru G35 Parts Catalog

• Covers 1960–1962 Beechcraft Bonanza Model 35 thru G35 airframes, detailing structural, flight control, and mechanical assembly components.
• Official Beech Aircraft Corporation publication 35-590028 B (first reissue September 15, 1960; revised November 16, 1962).
• Contains 137 figures with exploded-view diagrams and assembly breakdowns keyed to numerical part references.
• Essential reference material to identify correct components before starting any repair work.
• Available as an instant download immediately after purchase.
• Fully indexed, searchable PDF ensures quick navigation across all chapters and appendices.
• Documents the full D1 through D4865 serial number range.

Component and System Documentation

This comprehensive parts catalog details the complete Beechcraft Bonanza Model 35 series, including the A35, B35, C35, D35, E35, F35, and G35 variants. It breaks down the entire aircraft into an organized group assembly structure. You will find complete part breakdowns for the fuselage, wing, empennage, landing gear, and flight control systems. Need to identify components for the main landing gear retraction system or the engine power plant installation? Each chapter provides detailed, exploded-view diagrams of assemblies, sub-assemblies, and detail parts to speed up your workflow on the shop floor. An extensive model and serial number code list guarantees accurate part selection for specific aircraft configurations.

Specification and Reference Data

Technical reference data within this publication highlights critical assembly-specific details. For instance, it lists torque limits for the landing gear retract mechanisms at 48 N-m and specific rotational force limits of 60 N-m for other major components. The structural integrity of the airframe is documented through a breakdown of 77 individual parts within the fuselage structure assembly alone. The manual also outlines environmental operating parameters, noting an optimal range of 15–30 C for equipment functionality. When sourcing replacement parts or planning a major repair, cross-referencing this manual prevents costly ordering mistakes. Always verify part numbers and assembly structures against current aviation safety directives before returning an aircraft to service, as outdated or incorrectly identified components can compromise structural integrity.