Teledyne Continental TSIO-360-F / FB Aircraft Engine 1978 Operation and Maintenance Manual OEM (P/N X-30512)

Manual Features & Access

• Official OEM publication (Form No. X-30512, FAA approved January 1978) covering the 360-cubic inch series.
• Includes 5 performance curves and 10 detailed engine schematics mapping fuel and lubrication systems.

Getting accurate baseline data is critical when working on turbocharged flat-six architectures. This official 42-page operator's manual delivers the exact factory specifications and system overviews required for the 1978 Teledyne Continental TSIO-360-F and TSIO-360-FB aircraft engines. Available as an instant download, it puts essential diagnostic reference material directly into your hands on the hangar floor. Before initiating any maintenance procedures based on these operational parameters, always coordinate with a certified aviation technician to ensure compliance with current safety directives.

The documentation provides a deep dive into the turbocharged induction system and continuous-flow fuel injection logic. You will find complete protocols for standard starts, ground running requirements, and critical in-flight emergency responses—including specific troubleshooting logic for turbocharger failure and fuel management anomalies. It also outlines exact procedures for preheating, long-term storage, and operating within abnormal environmental conditions. Detailed schematics break down the Bendix 25 series magnetos and Ray Jay turbocharger units, taking the guesswork out of your system familiarization.

Operational Specs and Reference Data

• Rated continuous power: 200 BHP at 2575 RPM (manifold pressure set at 41.0 inches Hg at sea level).
• Maximum continuous manifold pressure: 41.0 inches Hg.
• Turbine Inlet Temperature: Continuous operation above 1650°F is strictly prohibited.
• Lubrication specs: 8-quart oil sump capacity with a normal operating temperature of approximately 170°F (SAE 50 or 30 recommended depending on ambient temperature).
• Fuel requirements: Minimum grade 100 or 100LL aviation gasoline.
• Engine weight: 393 lbs dry weight (including accessories).