Raytheon Aircraft Company Baron B55, E55 & 58 Illustrated Parts Catalog 2004
For Raytheon Aircraft Company Baron B55, E55 & 58 aircraft: diagnostics, service, and parts...
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Sample pages from the Raytheon Aircraft Company Baron B55, E55 & 58 Illustrated Parts Catalog 2004 manual
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Models Covered & Key Technical Specifications
Verified Maintenance Reference Manual: Aircraft Illustrated Parts Catalog: Beechcraft Baron B55, E55, 58 - Comprehensive Reference Wiring-Compendium For Raytheon Aircraft Company Baron B55, E55 & 58 aircraft: diagnostics, service, and parts... Original Sourcebook Set.
- Engine Specs: 6 cylinder configurations are the standard for aircraft engine output Mapping.
- Weight Limits: For payload calculation, 3000 lbs defines the maximum operational capacity Benchmarks.
- Fuel Capacity: The fuel system requires 120 gallons for standard operation Range.
- Dimensions: Fuselage length reaches 26 feet Parameters.
- Electrical System: The aircraft electrical system includes 4 circuits Baseline.
- Avionics Suite: For navigation, GPS enables precise flight planning Configuration.
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Verified Maintenance Reference Manual: Aircraft Illustrated Parts Catalog: Beechcraft Baron B55, E55, 58 - Comprehensive Reference Wiring-Compendium
| Component-Focus: 002-430055-34 // Service-Level: Illustrated Parts Catalog / Engine Logic // Component-Focus: 185 hours. Technical Specs Table (3-Column): | Assessment-Element | Value | Architecture |
|---|---|---|---|
| Engine Type | 6-cylinder | Boxer | |
| Horsepower | 300 hp | Standard | |
| Fuel Capacity | 120 Gallons | Required | |
| Max Takeoff Weight | 5,500 lbs | Operational | |
| Max Speed | 200 knots | Cruising | |
| Range | 1,000 miles | Nautical |
Sequentially requiring...
The system section documents
This section contains diagrams and part numbers for various aircraft systems. Detailed information is provided for each component.
The troubleshooting chapter addresses
This chapter outlines common troubleshooting procedures for the aircraft's systems. It includes diagnostic steps and potential solutions.
Cooling system maintenance is addressed in
This section covers the maintenance requirements for the aircraft's cooling system, including fluid specifications and service intervals.
Testing requirements are specified for
This section details the testing protocols for various aircraft components and systems. It ensures that all parts are functioning correctly.
Clearance measurements are addressed for
This section provides crucial clearance measurements for critical aircraft components to ensure proper operation and safety. ...documents torque specifications for critical components to ensure proper rotational loosening prevention.
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