Beechcraft Bonanza A36: E-1946, E-2104, E-2111 thru E-3629 and E-3631 thru E-3635 Pilot's Operating Handbook and FAA Approved Airplane Flight Manual (P/N 36-590002-37B)

432 Pages • 6.54 MB • Instant, Printable PDF

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Beechcraft Models Covered & Key Technical Specifications

Models: Beech Bonanza A36

Sub-models / Variants: E-1946, E-2104, E-2111 thru E-3629, E-3631 thru E-3635

Years: 1983–2006 (1983, 1984, 1985, 1986, 1987, 1988, 1989, 1990, 1991, 1992, 1993, 1994, 1995, 1996, 1997, 1998, 1999, 2000, 2001, 2002, 2003, 2004, 2005, 2006)


  • Engine: Teledyne Continental IO-550-B, 6-cylinder, 300 hp

  • Propeller: McCauley 3-blade constant-speed

  • Fuel Capacity: 80 gallons total, 74 gallons usable

  • Oil Capacity: 12 quarts

  • Maximum Take-off Weight: 3650 lbs

  • Wing Area: 181 sq ft

  • Max Demonstrated Crosswind: 17 knots

File & Download Details
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Listing ID / Seller:
25164 / Patricia Harris
File Size:
6.54 MB
File Type:
PDF
Language:
English
Pages:
432
Printable:
Yes
Manual details last updated and verified:
Sep 17, 2026

Beechcraft Manual Features & Content Preview

This factory publication is the Beech Bonanza A36 Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual, not a complete shop repair manual. It is suited to pilots and owners who need approved operating, loading, performance, and routine-servicing information for the covered A36 serials. Mechanics can use it for airplane-specific limitations and servicing context, but internal repair and overhaul work requires the separate maintenance publications.

  • Factory document coverage: A 432-page PDF of Raytheon P/N 36-590002-37B, reissued November 2002 and revised January 2006 as P/N 36-590002-37B2 / Revision B2. Coverage is limited to A36 serials E-1946, E-2104, E-2111 through E-3629, and E-3631 through E-3635. Its organization follows GAMA Handbook Specification No. 1 through Revision 2.

  • Approved operating procedures: Provides preflight, external-power and engine-start procedures; takeoff, climb, cruise, EGT-based leaning, descent, landing, balked-landing, shutdown, oxygen-system, cold-weather, and icing guidance.

  • Emergency and abnormal operations: Covers engine failure and fire, rough running, propeller overspeed, an engaged starter, alternator failure, electrical smoke or fire, manual landing-gear extension, induction icing, blocked static sources, instrument-air failure, unlatched doors, and emergency exits.

  • Performance and loading references: Supplies normal- and alternate-system calibration data, takeoff and landing charts, climb planning, cruise-power tables, range and endurance profiles, weighing instructions, loading forms, moment limits, and useful-load moment tables.

  • Aircraft and system descriptions: Details the IO-550-B powerplant, constant-speed propeller, fuel and electrical systems, retractable landing gear, flight controls, cabin doors and seating, heating and ventilation, optional oxygen equipment, pitot-static system, instrument-air system, annunciators, and interior and exterior lighting.

  • Included supplemental material: Contains UK-operation and CAA pages, the reduced-external-noise supplement, standby instrument-air installation, cabin-door handle placard, Pool Aviation low-voltage material, and a dual Garmin GNS 430 flight-manual supplement. Several of these inserts and the included equipment and weight-and-balance records are assigned specifically to aircraft serial E-2788.

Operational Scope and Serial Differences

The handbook brings the limitations, required placards, kinds-of-operation equipment list, normal checklists, and immediate-action emergency procedures together in the approved flight-manual format. Serial-specific distinctions are preserved rather than treated as one configuration. These include the landing-gear warning horn used through E-2467, except E-2458, versus the horn and GEAR UP annunciator arrangement for E-2458 and E-2468 onward. Separate fuel-selector placards apply before and after E-3047, while later-airplane or service-kit compliance can also change the performance corrections and fuel-flow information used.

The installed supplements are not blanket approvals for every airplane in the main serial range. Their applicability depends on the equipment, modifications, registration basis, and aircraft-specific records for the airplane being operated.

Performance, Weight and Balance, and Technical Views

Descriptive data covers certified weights, fuel and oil capacities, propeller specifications, cabin and entry dimensions, baggage volumes, center-of-gravity terminology, and instrument markings. The weight-and-balance section explains weighing, loading calculations, seating and baggage stations, moment-envelope checks, and equipment-list use. Because this PDF contains completed records for E-2788, another airplane requires its own current equipment list and approved weight-and-balance data.

Useful visual references include the Airplane Three View, Typical Instrument Panel Illustration, Engine Instrument Panel Illustration, Seat Change Schematic, Fuel System Schematic, and Heating and Ventilating System Schematic. Performance charts cover airspeed and altimeter correction, stall speed, wind components, takeoff, climb, cruise, range, endurance, and landing.

Servicing Scope and Repair Cautions

Section 8 addresses inspection periods, towing, parking, tie-down and jacking, storage, external power, fuel strainers, oil and filter changes, battery care, tires, shock struts, the shimmy damper, brakes, induction and instrument-air filters, oxygen servicing, alternator precautions, magnetos, cleaning, approved oils, consumable materials, and lamp replacement. It does not provide full structural repair, component disassembly, engine overhaul, or electrical wiring-diagram coverage. Those repairs belong in the separately listed Bonanza Series Maintenance Manual, Parts Catalog, and Wiring Diagram Manual.

The servicing cautions are component-specific. Reversed polarity, an open alternator circuit, or improperly grounded regulator terminals can seriously damage the charging system and connected electrical equipment. High-pressure washing can unseat engine seals, strip lubricant from trim-tab hardware, remove grease from landing-gear components, and force moisture into the structure. Alteration and repair work must be performed by properly licensed personnel, and limited pilot-performed preventive maintenance still requires the applicable regulations and maintenance instructions.

Technical Safety Notice
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This official OEM document is intended for professional technicians and skilled operators. Performing service on mechanical equipment involves inherent risks. By purchasing, you acknowledge that RepairLoader provides original manufacturer data for informational purposes. Always prioritize safety: use correct tools, wear protective gear, and consult a certified professional if you are uncertain of any procedure.

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