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

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Beechcraft Models Covered & Key Technical Specifications

Models: 95-B55, 95-B55A

Sub-models / Variants: Special Reduced Gross Weight Configuration

Model Years: 1978–1994 (1978, 1979, 1980, 1981, 1982, 1983, 1984, 1985, 1986, 1987, 1988, 1989, 1990 1991, 1992, 1993, 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.

Technical Specifications
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Document Number / Seller:
28268 / Donna Brown
File Size:
7.06 MB
File Type:
PDF
Language:
Pages:
370
Printable:
Yes
Category:
Aircraft
Last updated / verified
Aug 11, 2026

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
  • Delivers essential PDF troubleshooting and diagnostic reference data
  • Streamlines maintenance to fix and repair systems

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. For aviation mechanics and DIYers, having these specifications centralized prevents unnecessary tear-downs and significantly speeds up 100-hour inspections. You avoid costly shop visits by following clear step-by-step instructions for servicing the main and nose gear shock struts, replenishing the shimmy damper fluid, and cleaning the induction air filters.

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. Visually, the reference material leaves no room for ambiguity. It features precise Airplane Three-View drawings, a detailed Fuel System Schematic, an Environmental Schematic, a complete Lubrication Points Diagram, and an Altimeter Correction chart.

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. When undertaking any repair on the 95-B55, mechanics must be aware of specific model pitfalls. For example, inadvertently operating the landing gear electrically while the manual handcrank remains engaged can severely damage the retract mechanism. Furthermore, after an emergency gear extension, never reset the switches or circuit breakers until the airframe is securely supported on jacks, as the gear might retract instantly on the ground. 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.

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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