1947–1996 Beechcraft Bonanza 35 Series Aircraft Shop Manual, D-1 to D-10119 except D-10097 (P/N 35-590096B19)

This 1947–1996 Beechcraft Bonanza 35 Series Shop Manual, P/N 35-590096B19, covers serials D-1 through D-10119, except D-10097. Its eight sections cover airframe servicing, adjustments, component removal, repair and overhaul, wiring, inspections, and replacement schedules. This edition incorporates the March 22, 1996 revision and Temporary Revision 3-1 dated October 31, 1997.

• Flight controls: Aileron, elevator/ruddervator, rudder, and trim-system rigging, cable-tension adjustment, control-surface balancing, and serial-specific setup procedures.
• Landing gear and brakes: Retraction-system adjustment, shock-strut and shimmy-dampener overhaul, brake-master-cylinder repair, and dual-brake-system bleeding procedures.
• Fuel and powerplant: Bladder fuel-cell replacement, fuel-pump adjustment, engine removal and installation, magneto timing, and turbocharger-system testing.
• Electrical and propeller deicing: Starter and charging-system diagnosis, electric deicer tests, slip-ring checks, and Goodrich deicer-boot replacement and repair.
• Cabin systems and autopilot: Evaporative air-conditioner servicing, refrigerative air-conditioning component replacement, and New-Matic autopilot adjustment and fault diagnosis.
• Inspection and servicing: Periodic inspection guides, lubrication charts, tire-pressure and shock-strut extension specifications, and component overhaul or replacement schedules.

Written for experienced aircraft mechanics, the manual assumes familiarity with basic maintenance and omits some elementary removal and servicing instructions.

Flight-Control Rigging and Airframe Repair

The Temperature Effect on Cable Tension graphs accompany serial-specific rigging procedures. For applicable aircraft from D-5726, the instructions identify the 35-590087 rigging jig and 35-590087-9 stop, helping the mechanic select the correct setup before adjusting the controls.

Ruddervator balancing procedures address work following painting or repair. The trim-system instructions also warn that binding at the cable-to-tab-horn attachment can crack the horn.

Structural coverage includes wing, leading-edge, and main-spar removal and installation, with attachment details and torque tables. The Fuselage and Empennage Skin Plating illustration identifies the skin arrangement for airframe work.

Landing-Gear and Brake Component Overhaul

Component procedures cover landing-gear actuators, shock struts, shimmy dampeners, Paramount and Gerdes master cylinders, and Goodyear brakes with single or dual pressure cylinders. Inspection criteria accompany disassembly and reassembly, while separate sections address gear rigging and door-linkage adjustment.

The inspection guide warns that electrical gear operation with the emergency handcrank engaged can damage the worm-shaft engagement slot. Flap-actuator overhaul is included, but flap motors installed from D-9966 are replacement items rather than field-overhaul units.

Fuel-Cell Repair and Engine-Service Boundaries

The Nipple Clamp Torque Chart supports fuel-cell installation, and the repair section distinguishes permissible field patches from damage around fittings or curved areas requiring specialist repair. Fuel-system schematics distinguish tank arrangements and associated plumbing.

The Turbocharger Schematic accompanies controller, wastegate, leak-test, and critical-altitude troubleshooting information. Engine removal, installation, and on-aircraft adjustments are covered; internal engine overhaul is referred to separate Continental publications that are not included here.

The component schedules include Continental engine-overhaul guidance and its service-bulletin reference. They do not constitute a complete engine-overhaul manual.

Electrical Diagnosis and Wiring Coverage

The Electrical Utilization Load Chart identifies circuit loads, while troubleshooting tables address charging, starting, flaps, landing-gear indications, and other electrical faults. Strobe coverage includes Bullock fault tracing and Grimes lamp and power-unit servicing.

New-Matic autopilot fault charts distinguish roll, pitch, heading, and altitude-control complaints and relate them to gyro, servo, and pneumatic-system checks.

Wiring applicability: The included wiring section covers aircraft before D-9818. V35B aircraft D-9818 through D-10119, excluding D-10097, require the separate wiring-diagram manual P/N 35-590102-7, which is not included.

A Preview of Fuel-Capacity and Starter-Service Data

For D-5726 through D-6561, the Fuel Cell Capacities table lists two standard wing cells of 25 gallons each, with 22 gallons usable per cell. Optional cells are listed separately, keeping standard and optional installations distinct.

For the Prestolite starter fitted to IO-520 installations from D-7310, the service instructions specify brush replacement at 1/4 inch or less. Brush-spring tension is 32–40 ounces with new brushes installed.

PDF Navigation and Included Revision Pages

Finding procedures and diagrams: Searchable OCR text and bookmarks provide access to the main sections, indexes, and revision material. OCR errors can affect exact code searches, and small labels on denser wiring diagrams require magnification.

One printable, English-language 471-page PDF includes nine front-matter pages, one additional Section 4 revision-record page, and the two-page Temporary Revision 3-1 with its blank reverse. Both versions of printed page 3-32 are also included in that total.