Beechcraft Baron 95-B55 / 95-B55A Pilot's Operating Handbook & FAA Approved Airplane Flight Manual

Beechcraft Baron 95-B55 Pilot's Operating Handbook

• 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
• Includes 64 pages of dedicated safety information and comprehensive performance charts
• Delivered as a direct download the moment payment clears
• Indexed PDF search covers every chapter and appendix
• Stored against your account so you can retrieve it after a hard-drive loss
• This 1978 original publication with 1994 revision A5 captures the final certification data for the TC-series 95-B55 build

Operational Content Overview

This 370-page Beechcraft Baron 95-B55 pilot handbook provides the primary reference for all flight operations. It segments information into ten distinct divisions, ranging from general descriptive data and airplane limitations to normal and emergency operating procedures. The document includes detailed instructions for preflight inspections, engine starting, taxiing, and in-flight operation. Coverage extends to systems descriptions for fuel, electrical, landing gear, and ice protection, ensuring the operator understands both standard usage and emergency system responses. The manual also incorporates weight and balance data, center of gravity limits, and a specific section on safety information relevant to the normal category certification under CAR 3.

Technical Specification Highlights

Systems Data and Reference Values

Engine power settings for the Continental IO-470-L are documented in the descriptive data section, listing specific manifold pressure and RPM values for take-off, cruise climb, and maximum cruise conditions. Oil temperature for the Beechcraft Baron 95-B55 is limited to a maximum of 225°F. Cylinder head temperature for the 95-B55 is restricted to a maximum of 460°F during flight. Minimum oil pressure for the Beechcraft Baron 95-B55 is specified at 30 psi. The handbook lists the maximum demonstration crosswind component at 22 knots. Flight load factors for the 95-B55 are documented at 4.4G for positive maneuvers. All service data shown here is for reference only — qualified technicians and the original OEM documentation remain the authoritative source for any hands-on work. This official 370-page Beechcraft OEM handbook covers the 95-B55 and 95-B55A, providing all necessary flight, limitation, and systems data for the TC-1608 through TC-2002 airframe series.