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3070800-52 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
3070800-52 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
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3070800-63 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
3070800-63 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
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3070800-54 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly

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3070800-54 – Honeywell Aerospace Main Fuel Control (MFC) Assembly

Available now through the AirParts Aero marketplace.

Overview Section

The Honeywell 3070800-54 is a high-precision Main Fuel Control (MFC) unit, also categorized as a Fuel Control Unit (FCU). Engineered for the Honeywell TFE731 turbofan engine series, the -54 dash number represents a specialized, late-generation configuration. It is a hydro-mechanical "analog computer" designed to provide peak fuel metering accuracy for the high-thrust variants of the TFE731 family.

This assembly acts as the central command for engine combustion. It monitors pilot input via the Power Lever Angle (PLA) and cross-references it with critical environmental sensors: Compressor Discharge Pressure ($P_3$) and Inlet Temperature ($T_2$). The -54 variant is specifically calibrated to handle the increased airflow and thermal requirements of modern turbofan operations, ensuring smooth power transients and stable governing at all altitudes.

Key Features Section

  • Advanced Hydro-Mechanical Logic: Utilizes a complex internal system of bellows and 3D cams to calculate the optimal fuel flow for any given flight condition.

  • Optimized for High-Altitude Cruise: Features refined pneumatic sensing technology to ensure stable engine speeds ($N_2$) and prevent RPM "hunting" in thin air.

  • Precision Acceleration Schedules: Engineered to provide rapid, linear throttle response while maintaining a maximum safety margin against compressor surges.

  • Hardened Internal Metering Valves: Incorporates advanced surface treatments to resist "stiction" and wear caused by diverse fuel types or microscopic contaminants.

  • Integrated Mechanical Governor: Provides a fail-safe $N_2$ overspeed protection, physically limiting fuel flow to protect the engine core from structural damage.

  • Ruggedized Cast Housing: Constructed from a high-integrity aluminum alloy designed to dissipate heat and withstand the intense vibrations of the Accessory Gearbox (AGB) mounting.

Technical Specifications Section

SpecificationDetail
Part Number3070800-54
ManufacturerHoneywell Aerospace
Engine ApplicationTFE731-40, -50, and -60 Series variants
Input SignalsPower Lever Angle (PLA), $P_3$ (Pneumatic), $T_2$ (Temperature)
Fuel CompatibilityJet-A, Jet-A1, JP-5, JP-8
Control LogicHydro-mechanical with Pneumatic Override
WeightApproximately 18.7 lbs

Aircraft Compatibility Section

The 3070800-54 is a critical component for high-performance business jets utilizing the TFE731 geared turbofan:

  • Dassault Falcon 900EX / 900LX: Essential for the fuel management of the TFE731-60 series turbofans.

  • Hawker 900XP: Found in the high-efficiency TFE731-50R engine configurations.

  • Gulfstream G150: Core component for the TFE731-40AR powerplants, providing reliable transcontinental performance.

  • Dassault Falcon 50EX: Utilized in the upgraded -40 series engine installations for enhanced climb performance.

Technical Applications & Safety

The MFC operates as a closed-loop feedback system. It continuously monitors the "work" the engine is doing via the $P_3$ signal. If the $P_3$ sensing line is restricted by carbon or moisture, the 3070800-54 will sense an artificial "low air" condition and limit fuel flow, which can prevent the engine from reaching takeoff power.

Safety Warning: FCU installation requires a mandatory "Part Power Trim" procedure. This is a safety-of-flight task performed on the ground to synchronize the MFC with the engine's Interstage Turbine Temperature (ITT). Failure to correctly rig the 3070800-54 can result in "Hot Starts" or over-temperature events that can cause permanent, multi-million dollar damage to the turbine's hot section.

Technical Engineering Insight

The engineering value of the 3070800-54 lies in its Pneumatic Signal Dampening. In high-pressure engines, the $P_3$ air can be highly turbulent. The -54 variant uses precision-drilled orifices to dampen these pressure "pulses" before they reach the sensing bellows. This ensures a rock-steady power setting even in turbulent flight conditions, which is vital for the accuracy of modern autothrottle systems.

By choosing a certified 3070800-54 through AirParts Aero, you ensure the unit has been bench-tested on a computer-controlled fuel stand to verify its Acceleration and Deceleration Schedules match the Honeywell master engineering curve.

Installation & Maintenance Addendum

  1. $P_3$ Filter Replacement: Always install a new $P_3$ air filter when replacing the MFC. A clogged filter is the most common cause of "sluggish" engine response.

  2. Drive Spline Integrity: Inspect the drive splines on the accessory gearbox for "red dust" (fretting). Apply the specified high-pressure lubricant to the 3070800-54 drive shaft to ensure longevity.

  3. Preservation: If the unit is removed and stored, it must be filled with MIL-PRF-6081 preservation oil. If left dry, the internal steel bellows can corrode, causing the unit to fall out of calibration.


Specifications
Cage Code 99193
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