Beechcraft Baron 95-B55 / 95-B55A Pilot's Operating Handbook & FAA Approved Airplane Flight Manual (P/N 96-590011-23)
370 Pages • 7.06 MB • Instant, Printable PDF
Beechcraft Models Covered & Key Technical Specifications
Models: Beechcraft Baron 95-B55, Beechcraft Baron 95-B55A
Sub-models / Variants: Special Reduced Gross Weight Configuration
Model Years: 1978–1994 (Publication revisions covering serials TC-1608 through TC-2002)
Serial Numbers: TC-1608 through TC-2002
Technical Data:
- Engine: Two Continental IO-470-L fuel-injected, air-cooled, horizontally-opposed six-cylinder
- Engine Power Rating: 260 horsepower at 2625 RPM
- Standard Fuel Capacity: 106 Gallons (100 Gallons usable)
- Optional Fuel Capacity: 142 Gallons (136 Gallons usable)
- Maximum Take-Off Weight (95-B55): 5100 lbs
- Maximum Take-Off Weight (95-B55A): 4990 lbs
- Oil Capacity: 12 quarts per engine
- Maximum Oil Pressure: 80 psi
- Minimum Take-off Oil Temperature: 75°F
- Standard Wing Area: 199.2 sq. ft.
Beechcraft Manual Features & Content Preview
- Covers 1978–1994 Beechcraft Baron 95-B55 and 95-B55A aircraft with serials TC-1608 through TC-2002
- Official OEM publication P/N 96-590011-23, revised through July 1994
- Features 64 pages of dedicated safety parameters and comprehensive performance charts
- Captures the final certification data for the 1978 original publication with 1994 revision A5
Operational Content Overview
This 370-page Pilot's Operating Handbook serves as the primary reference for all flight operations and ground handling. Whether you are running preflight checks on the ramp or reviewing protocols in the hangar, it provides the exact factory data required for the job. The document breaks down into ten divisions. You get straightforward layouts of general descriptive data, airplane limitations, and both normal and emergency procedures. Detailed system breakdowns cover the fuel, electrical, landing gear, and ice protection setups. This ensures you fully understand standard operations as well as critical responses during a system failure.
Technical Specification Highlights
The manual documents essential structural and handling limits for the TC-series airframe. It outlines weight and balance data alongside precise center of gravity boundaries required for normal category certification under CAR 3. You will also find flight load factors documented at a maximum of 4.4G for positive maneuvers, and the demonstrated crosswind component specified at 22 knots.
Systems Data and Reference Values
Engine power settings for the Continental IO-470-L are meticulously detailed. The descriptive data section lists specific manifold pressure and RPM values for take-off, cruise climb, and maximum cruise conditions. Operating limits are strict. Oil temperature caps at a maximum of 225°F, while cylinder head temperatures must stay below 460°F during flight. Minimum oil pressure sits at 30 psi. Please note that these figures strictly dictate operational boundaries. Always rely on qualified technicians and current, approved maintenance data before attempting any active mechanical work, servicing, or physical adjustments.
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