LIGHT MAINTENANCE MANUAL

TFE731-5/-5AR/-5R (ATA NUMBER 72-02-75)

CAUTION: DO NOT EXCEED MANUFACTURER’S RECOMMENDED DUTY CYCLE FOR STARTER.

2.A. (4) Every four weeks, with inlet and tailpipe plugs removed, motor engine with starter sufficiently to achieve N1 rotation, observing manufacturers recommended duty cycle for starter.

(5)Repeat Steps (2) and (3).

(6)It is recommended that digital electronic engine control (DEEC) (76-10-02) be placed in air-tight bag containing desiccant for storage.

B.Installed Engine Preservation Instructions (More Than Six Months)

CAUTION: THE COMPRESSOR SECTION SHALL NOT BE SPRAYED WITH ANY CORROSION-PREVENTIVE COMPOUND. NO HYDRO- CARBONS OR OILS, INCLUDING DE-ICING/ANTI-ICE FLUID SHALL EVER BE SPRAYED INTO INLET, EXHAUST, SCOOPS, VENTS, AND DRAINS DURING ENGINE OPERATION. UNCON- TROLLED COMBUSTION COULD BE A POSSIBLE RESULT. AVOID OPERATING ENGINE DURING AIRCRAFT DE-ICING.

(1)Disconnect fuel control discharge line between oil temperature regulator (fuel/oil cooler) and fuel control and connect a line to the fuel control discharge port to drain overboard.

(2)Disconnect fuel supply line at inlet connection on fuel pump and connect supply of oil. Supply oil under two to five pounds per square inch pressure.

CAUTION: DO NOT EXCEED MANUFACTURER’S RECOMMENDED DUTY CYCLE FOR STARTER-GENERATOR.

(3)De-energize ignition system. Advance power lever to idle position. Motor fuel control until clean oil flows from overboard drain line. Fuel control may be motored by motor- ing engine, observing motoring procedures established by the particular installation.

(4)Stop motoring engine, disconnect oil supply lines from fuel inlet port on fuel pump and cap inlet port. Allow residual oil to drain from fuel control and lines, then disconnect overboard drain line and reconnect fuel line between fuel control and fuel/oil cooler.

NOTE: Use of corrosion-preventive compound in the engine lubrication sys- tem for preservation is not required. Specified engine lubricating oil is a satisfactory corrosion preventive.

(5)Wipe all fuel and oil from engine. Secure warning tags to engine and as required to indicate preservation procedures have been performed and that engine shall not be operated except as noted until depreservation procedures are performed. Maintain engine motoring record indicating engine shall be motored every four weeks.

(6)Install inlet and tailpipe plugs.

72-00-00 Page 304

Jan 31/00

E Honeywell International Inc. Do not copy without express permission of Honeywell.

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Honeywell TFE731-5-5AR -5R manual Light Maintenance Manual

TFE731-5-5AR -5R specifications

The Honeywell TFE731-5-5AR and TFE731-5R are advanced turbofan engines widely recognized for their performance and reliability in the business aviation sector. Offering a blend of efficiency and power, these engines are engineered to meet the demands of modern aircraft, contributing to fuel economy and reduced operational costs.

One of the main features of the TFE731-5-5AR engine is its high thrust-to-weight ratio. This allows for superior climb performance and overall aircraft agility, essential for competitive operations. The engine produces a thrust rating of up to 4,500 pounds, making it suitable for a variety of business jets. The TFE731-5R version offers similar performance but with modifications tailored to specific aircraft requirements.

Technologically, the TFE731 engines incorporate advanced materials and manufacturing techniques that enhance durability while minimizing maintenance needs. Their design includes a fan system with swept blades, which improves aerodynamic efficiency, resulting in lower specific fuel consumption. This focus on modern aerodynamics translates into significant operational savings over the engine's lifecycle.

Another notable characteristic of the TFE731-5-5AR is its quiet operation. Designed with noise reduction technologies, these engines comply with the strict noise regulations present in many urban environments, making them a popular choice for operators who prioritize environmental compliance. The TFE731-5 series has also received certifications that affirm its low emissions, aligning with global initiatives to reduce the aviation industry's environmental impact.

In terms of reliability, the TFE731 engine family is renowned for its robust performance under varying operational conditions. A proven track record of dependability ensures that operators can complete missions with confidence, minimizing downtime and maintenance costs. The engine features a modular design, which simplifies repairs and maintenance, allowing for quicker turnarounds and increased aircraft availability.

Overall, the Honeywell TFE731-5-5AR and TFE731-5R engines represent a pinnacle of innovation in turbofan technology, combining power, efficiency, and reliability. With their state-of-the-art features, advanced materials, and commitment to environmental responsibility, they continue to be a top choice for business jet operators around the globe. As the aviation industry evolves, these engines set a benchmark for performance and sustainability in the world of private aviation.