Teledyne Continental TSIO-360-F / FB Aircraft Engine 1978 Operation and Maintenance Manual

1978 Teledyne Continental TSIO-360-F & FB Operator's Manual

• This operator manual covers the 1978 Teledyne Continental TSIO-360-F and TSIO-360-FB aircraft engines, documenting operational specifications, fuel injection management, and turbocharger system parameters
• Official OEM publication Form No. X-30512, FAA approved January 1978
• Contains 5 performance curves, 10 engine schematics including fuel and lubrication systems, and comprehensive operating limit tables for various power settings
• Accessible from your device as soon as the order is placed
• Permanent availability in your purchase account — no re-buy required
• Laid out for standard letter and A4 printing
• OCR text layer lets you jump to a torque spec by keyword
• This 1978 edition serves as the primary technical reference for the specific TSIO-360-F and FB engine configurations, detailing the operation of the turbocharged induction system for the 360-cubic inch series

Engine Operation and System Documentation

The 1978 Teledyne Continental TSIO-360-F and TSIO-360-FB aircraft engine manual provides technical oversight for the turbocharged flat-six engine architecture. Chapters detail start procedures, ground running requirements, and in-flight emergency protocols, including specific guidance for turbocharger failure and fuel management. The text presents instructions for preheating, storage and removal from storage, and abnormal environmental operation. System descriptions explain the continuous-flow fuel injection logic, wastegate adjustment, and the specific lubrication requirements of the Bendix 25 series magnetos and Ray Jay turbocharger units.

Operational Specs and Reference Data

This manual provides extensive technical data to define operating thresholds and maintenance intervals. The engine oil sump capacity is rated at 8 quarts, with recommended SAE 50 or 30 oil grades depending on ambient temperature. The rated continuous power is documented as 200 BHP at 2575 RPM, with manifold pressure set at 41.0 inches Hg at sea level. The document includes detailed performance charts for fuel consumption, altitude limits, and fuel pump inlet pressures. Reference data includes:

• Minimum fuel grade is 100 or 100LL aviation gasoline.
• Normal oil temperature range is documented at approximately 170°F.
• Engine dry weight with accessories is listed as 393 lbs.
• Maximum continuous manifold pressure is 41.0 inches Hg.
• Continuous operation at Turbine Inlet Temperature above 1650°F is prohibited.

Reference only — always consult a certified technician before performing service on this equipment. An official 42-page Teledyne Continental Motors OEM operator manual covering the 1978 TSIO-360-F and TSIO-360-FB aircraft engines, documenting performance, lubrication, and emergency procedures for the turbocharged opposed-piston engine series.