Raytheon Beechcraft Bonanza Series Maintenance Manual V35B F33A F33C A36 A36TC B36TC – P/N 36-590001-9A23
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Comprehensive factory maintenance manual for Beechcraft Bonanza models V35B, F33A, F33C, A36, A36TC, and B36TC. Provides complete manufacturer service instructions, overhaul and replacement time limits, 100-hour and annual inspection checklists, lubrication schedules, fluid capacities, airframe standard practices, and ground handling procedures.
Description
Raytheon Beechcraft Bonanza Series Maintenance Manual Overview
The Raytheon Beechcraft Bonanza Series Maintenance Manual V35B F33A F33C A36 A36TC B36TC – P/N 36-590001-9A23 is the authoritative technical reference prepared in accordance with GAMA Specification No. 2 and meeting the intent of ATA Specification 100. This manual covers factory-level servicing, inspections, scheduled maintenance, and airframe standard practices across classic and modern Bonanza models. Whether supporting routine line servicing, complying with Title 14 CFR periodic checks, or executing comprehensive airframe component maintenance, this Raytheon Beechcraft Bonanza shop manual delivers precise technical procedures, exact torque values, and rigorous inspection criteria straight from the aircraft manufacturer.
File Details
- Manual Type: Aircraft Maintenance Manual
- Brand: Raytheon Aircraft Company / Beechcraft
- Models Covered: Bonanza V35B, F33A, F33C, A36, A36TC, and B36TC
- Part Number: 36-590001-9A23 (Base P/N: 36-590001-9)
- Publication Issue Date: May 9, 1980
- Revision Date: Revision A23, Dated June 28, 2002
- Language: English
- Page Count: 736 pages
- Format: Digital PDF
Chapters Covered
- Introduction: GAMA/ATA Chapter Index Guide, Supplementary Publications List, Vendor Publication Cross-Reference, and Complete Master Alphabetical Index
- Chapter 5 — Time Limits / Maintenance Checks:
- 5-10-00 Overhaul and Replacement Schedule (Landing Gear, Power Plant, Flaps and Flight Controls, Fuel System, Instruments, Electrical System, Miscellaneous)
- 5-20-00 Scheduled Maintenance Checks: Electric Propeller Deicer (50-Hour and 100-Hour Guides)
- 5-20-00 Turbocharger Inspections (25-Hour, 50-Hour, and 100-Hour Guides for EA-1 and After)
- 5-20-00 Models E33C and F33C Acrobatic Category 50-Hour Spin Inspection Schedule
- 5-20-00 100-Hour or Annual Inspection Guide & FACTS Program Guidelines (Models A36 and B36TC)
- 5-20-00 Comprehensive 100-Hour / Annual Inspection Checklist (Operational, Power Plant, Cabin and Baggage, Wings and Carry-Through, Nose Gear, Main Gear, Empennage, and General)
- Chapter 6 — Dimensions and Areas:
- 6-00-00 Principal Aircraft Dimensions and 3-View Drawings (F33A, F33C, V35B, A36, A36TC, B36TC)
- 6-00-00 Fuselage, Wing, Vertical Fin, and Stabilizer Fuselage Stations Diagrams
- Chapter 7 — Lifting and Shoring:
- 7-00-00 Jacking Procedures: Three-Point Jack Setup, Tail Tie-Down Ballast, and Pad Locations
- 7-00-00 Main Wheel Jacking Procedures and P/N 35-590006 Axle Jack Adapter Usage
- 7-00-00 Aircraft Hoisting Procedures and P/N 35-590064-1 Sling Assembly Rigging
- Chapter 8 — Leveling and Weighing:
- 8-00-00 Longitudinal Plumb-Bob Leveling and Lateral Carry-Through Bubble Leveling
- Chapter 9 — Towing and Taxiing:
- 9-00-00 Manual Towing via P/N 36-590015 Hand Tow Bar and Lower Torque Knee Tow Pins
- 9-00-00 Tractor/Tug Towing via P/N 45-590075 Tow Bar and Steering Turn Angle Limits
- 9-00-00 Taxiing Precautions, Flap Retraction, and Cowl Flap Cooling Configurations
- Chapter 10 — Parking, Mooring, Storage, and Return to Service:
- 10-00-00 Parking Brake Settings, Thermal Expansion Cautions, and Mooring Tie-Down Practices
- 10-00-00 Control Column Lock Pin Assembly Installation and Retention
- 10-00-00 Flyable Storage (7 to 30 Days), Temporary Storage (30 to 90 Days), and Indefinite Storage Preservation
- 10-00-00 Engine Preservation, Cylinder Desiccant Plugs, and Complete Return-to-Service De-Preservation
- Chapter 11 — Required Placards and Markings:
- 11-00-00 Model Designation Placard Locations and Interior FAA Placard Verification
- 11-20-00 Exterior Placards: Jack Points, Tow Limits, Strut Servicing, Wing Bolt Lubrication, Fuel Fillers (50, 80, and 108 Gallon Systems), and ELT Switch Panels
- Chapter 12 — Servicing:
- 12-10-00 Replenishing Systems: Fuel Cell Filling, Sump and Cell Draining, Fuel Screens, and Inverted Flight Sponge Reservoir (Model F33C)
- 12-10-00 12-Quart Engine Oil Wet Sump Servicing, Spin-Off Oil Filter Replacement, and Drain Adapters
- 12-10-00 Air Conditioning System: Depressurization, Recovery, Evacuation to 125 Microns, R-12 and R-134a Charging, and Compressor Oil Level Dipstick Measurement
- 12-10-00 Hydraulic Brake Reservoir Servicing with MIL-H-5606 Fluid
- 12-10-00 High-Pressure Breathing Oxygen System Charging (1850 ± 50 psi at 70°F) Across Aircraft Serial Variations
- 12-20-00 Scheduled Servicing: Tire Inflation Pressures, 28.25-Volt External Power Rules, and 24-Volt 110 Ah Battery Servicing
- 12-20-00 Oleo Shock Strut Servicing with MIL-H-5606 Fluid and Nitrogen/Air Inflation Dimensions
- 12-20-00 Nose Gear Shimmy Damper Fluid Level Depth Check Wire Measurement and Rebuilding
- 12-20-00 Roton Seat Recline Lock Disassembly, Cleaning, and Lubrication
- 12-20-00 Exterior Finishes, Urethane Paint Waxing, Acrylic Plastic Window Cleaning, and Interior Plastic Care
- 12-20-00 Chart 1 Servicing Intervals and Chart 2 Lubrication Schedule (Details A through T)
- 12-20-00 Special Maintenance Tools, Wing Bolt Socket Wrenches, Rigging Check Fixtures, and Cable Gauges
- Chapter 20 — Standard Practices — Airframe:
- 20-00-00 Airframe Maintenance Procedures and Disconnection Identification Rules
- 20-01-00 Torque Wrench Formulas, Adapter Offset Calculations, and Fastener Charts (Chart 1 Fine Thread, Chart 2 Coarse Thread Shear)
- 20-02-00 Electrostatic Discharge Sensitivity (ESDS) Handling, Classifications, Grounding Workstations, and Packaging Rules
- 20-03-00 Electrical Bonding and Grounding: Direct/Indirect Bonding, Surface Preparation, Bonding Jumpers, and Hardware Stacks
This technical publication equips certificated A&P mechanics, avionics technicians, repair stations, and owner-operators with standard maintenance practices, detailed scheduled checklists, exact fluid requirements, and critical component life limits required to maintain airworthiness across the entire Beechcraft Bonanza fleet.
Scheduled Inspections, Life Limits & FACTS Maintenance Program
The manual establishes strict operational, 50-hour, 100-hour, and annual inspection protocols. It outlines the computerized Factory Aircraft Comprehensive Tracking System (FACTS) program used for factory tracking on Models A36 and B36TC. Life-limited airframe and power plant items are specified with exact overhaul intervals, including a 2,000-hour replacement on nose gear retract rod rod-ends, 4,000-hour landing gear actuator overhaul, 2,000-hour flap actuators and flexible drive shafts, 10-year fuel selector valve replacement, 10-year fuel cell reservoir foam insert renewal, and mandatory wing-attach bolt structural inspections. For aerobatic category operators flying the E33C or F33C in spins, a dedicated 50-hour spin inspection provides precise reaming limits and bolt torque requirements for rudder pedal bellcranks, stabilizer attachment spars, and elevator torque fittings.
Ground Handling, Servicing & Lubrication Schedules
Detailed ground handling instructions ensure aircraft protection during towing, tie-down, and shop movement. The manual details hand-towing procedures using tow bar P/N 36-590015, tug towing using P/N 45-590075, turn limit warnings, and the three-point jacking protocol requiring tail ballast to prevent nose-over. Chapter 12 details fluid capacities and servicing procedures for the 12-quart wet sump oil system, MIL-H-5606 brake fluid reservoir, R-12 and R-134a air conditioning circuits, and 1850 psi aviator’s breathing oxygen cylinders. The comprehensive Lubrication Schedule (Chart 2, Details A through T) identifies every grease fitting, rod end, pulley, hinge, and drive mechanism across the airframe, specifying MIL-G-81322, MIL-G-23827, and Aeroshell lubricants at clear 100-hour, 300-hour, 600-hour, and 900-hour intervals.
IMAGES PREVIEW
Airframe Standard Practices & Technical Torques
Chapter 20 delivers foundational shop guidelines covering standard aerospace hardware and electrical handling. Standard torquing procedures provide exact mathematical formulas for calculating true torque when using wrench adapters or spring scales. Comprehensive fastener torque charts provide values for both fine-thread fasteners and coarse-thread shear bolts. Electrostatic Discharge Sensitivity (ESDS) practices safeguard modern avionics, defining static-dissipative workstations, grounding wrist straps, and packaging protocols. In addition, detailed electrical bonding standards ensure low-resistance structural grounding across aluminum, stainless steel, and titanium airframe components.
Professional Aviation Capability & Instant PDF Delivery
Whether you are performing an annual inspection, rebuilding a shimmy damper, rigging control cables, or servicing landing gear shock struts, the Raytheon Beechcraft Bonanza Series Maintenance Manual V35B F33A F33C A36 A36TC B36TC – P/N 36-590001-9A23 delivers the verified factory technical data required to keep your aircraft fully compliant and airworthy. Using official procedures guarantees adherence to manufacturer tolerances, preserves aircraft market value, and maintains maximum flight safety. Delivered as an instant, fully downloadable digital PDF, this manual provides immediate access with no shipping wait. Compatible with iPads, tablets, laptops, and desktop computers, it allows seamless zooming on detailed schematics and full printing of inspection checklists for the maintenance hangar.
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