Beechcraft Bonanza A36 Pilot's Operating Handbook and FAA Approved Airplane Flight Manual
This Pilot's Operating Handbook for Beech Bonanza A36 covers serials E-1946, E-2104, E-2111 thru E-3629 and E-3631 thru E-3635. PN 36-590002-37B
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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
Build Years: 1983–2006
Serial Numbers: E-1946, E-2104, E-2111–E-3629, E-3631–E-3635
Technical Data:
- 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
Beechcraft Manual Features & Content Preview
Beech Bonanza A36 Pilot's Operating Handbook
- Covers 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
- Original Raytheon Aircraft publication P/N 36-590002-37B, revised January 2006
- Contains 432 pages of operational data, flight limitations, emergency procedures, and normal operating sequences
- Accessible from your device as soon as the order is placed
- OCR text layer lets you jump to a torque spec by keyword
- Document structure aligns with GAMA Handbook Specification No. 1 requirements
- Includes full aircraft weight and balance terminology plus cabin dimensions for understanding factory workshop documentation
- This revised 2006 edition serves as the FAA-approved Airplane Flight Manual for the A36 airframe, integrating specific CAA and GAMA compliance updates
Operational Scope and Flight Guidance
The 1983–2006 Beech Bonanza A36 Pilot's Operating Handbook provides standard flight procedures for the normal and utility categories. Sections detail preflight inspections, engine starting, climb performance, cruise operations, and landing techniques, while referencing essential systems like the oxygen console, heating and ventilation, and anti-collision lighting installations. The documentation organizes critical flight metrics for both VFR and IFR operational environments.
Aircraft Performance and Specification Highlights
Technical specifications document the IO-550-B 6-cylinder engine configuration and related operational limits. Maximum ramp weight is listed at 3663 lbs in the certification data. The document covers propeller pitch settings, fuel capacity of 80 gallons, and maximum structural weights for baggage compartments. The center of gravity limits are defined for landing gear extended configurations. Engine oil capacity for the A36 is documented at 12 quarts. The landing gear warning horn is inoperative when the battery switches are turned off. Maximum Demonstrated Crosswind for the A36 is 17 knots. This 432-page FAA-approved manual provides the primary operational data for the 1983–2006 Beech Bonanza A36, documenting flight limits, emergency handling, and standard procedures for the Raytheon-built airframe.
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