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
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
Serial Numbers: E-1946, E-2104, E-2111–E-3629, E-3631–E-3635
Technical Data:
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Engine: Teledyne Continental IO-550-B, 6-cylinder, 300 hp
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Propeller: McCauley 3-blade constant-speed
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Fuel Capacity: 80 gallons total, 74 gallons usable
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Oil Capacity: 12 quarts
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Maximum Take-off Weight: 3650 lbs
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Wing Area: 181 sq ft
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Max Demonstrated Crosswind: 17 knots
Beechcraft Manual Features & Content Preview
- Applies to 1983–2006 Beech Bonanza A36 aircraft (specifically models within serial ranges E-1946, E-2104, E-2111 thru E-3629, and E-3631 thru E-3635)
- Official Raytheon Aircraft publication P/N 36-590002-37B, revised January 2006
- FAA-approved Airplane Flight Manual integrating specific CAA and GAMA compliance updates
- 432 pages of operational data, flight limitations, emergency procedures, and normal operating sequences
- Includes full aircraft weight and balance terminology plus cabin dimensions for understanding factory workshop documentation
Operational Scope and Flight Guidance
Designed for aviation mechanics and pilots, this handbook provides approved standard flight procedures for both normal and utility categories. The manual systematically details preflight inspections, engine starting, climb performance, cruise operations, and landing techniques. It also outlines critical systems, including the oxygen console, heating and ventilation, and anti-collision lighting installations. Always verify these operational metrics and emergency procedures against the latest FAA directives prior to initiating any flight operations or maintenance checks.
Aircraft Performance and Technical Specifications
The documentation outlines precise technical data for the IO-550-B 6-cylinder engine configuration. Key specifications include a maximum ramp weight of 3,663 lbs, an 80-gallon fuel capacity, and a 12-quart engine oil requirement. It clearly defines center of gravity limits for gear-extended configurations, propeller pitch settings, and maximum structural weights for baggage compartments. Crucial operational thresholds—such as the 17-knot maximum demonstrated crosswind and the specific battery dependencies of the landing gear warning horn—are clearly indexed for quick reference.
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