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3070800-64 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
3070800-64 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
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3070800-74 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
3070800-74 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
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3070800-73 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly

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3070800-73 – Honeywell Aerospace Main Fuel Control (MFC) Assembly

Available now through the AirParts Aero marketplace.

Overview Section

The Honeywell 3070800-73 is a high-precision Main Fuel Control (MFC) unit, often referred to as a Fuel Control Unit (FCU). Engineered for the Honeywell TFE731 turbofan engine series, the -73 dash number represents a specialized, late-generation hydro-mechanical configuration.

This assembly serves as the engine's primary "analog computer," metering fuel with extreme precision by balancing pilot input (Power Lever Angle) against real-time atmospheric data: Compressor Discharge Pressure (P3) and Inlet Temperature (T2). The -73 variant is a critical component for ensuring that the engine provides maximum thrust while preventing destructive compressor stalls, over-speeds, or turbine over-temperature events.

Key Features Section

  • Advanced Hydro-Mechanical Logic: Translates complex pneumatic and mechanical signals into exact fuel metering through an internal system of 3D cams and bellows.

  • Refined Transient Management: Features a specialized internal cam profile that ensures smooth, predictable engine acceleration even at high-density altitudes.

  • Superior Altitude Compensation: Automatically adjusts the fuel-to-air ratio as the aircraft climbs, maintaining optimal combustion efficiency and preventing "rich blowout" in thin air.

  • Integrated Mechanical Governor: Provides a physical fail-safe N2 overspeed protection, physically limiting fuel flow should the engine attempt to exceed structural RPM limits.

  • 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.

  • SB Compliance: As a modern dash-number in the 3070800 lineage, the -73 often incorporates hardware improvements that address "stiction" and bellows longevity issues found in earlier models.

Technical Specifications Section

SpecificationDetail
Part Number3070800-73
ManufacturerHoneywell Aerospace (formerly Garrett/AlliedSignal)
Engine ApplicationTFE731-3, -4, and -5 Series variants
Input SignalsPower Lever Angle (PLA), P3 (Pneumatic), T2 (Temperature)
Control LogicHydro-mechanical / Pneumatic Feedback
Fuel CompatibilityJet-A, Jet-A1, JP-5, JP-8
WeightApproximately 18.8 lbs

Aircraft Compatibility Section

The 3070800-73 is critical for several prominent aircraft utilizing the TFE731 engine series:

  • Beechcraft Hawker 800 / 800XP: Found in specific engine configurations requiring the -73's refined scheduling.

  • Cessna Citation III / VI / VII: Essential for the reliability of the -3 and -4R engine configurations.

  • Dassault Falcon 50 / 900: Utilized for precise thrust management across the multi-engine flight profile.

  • CASA C-101 Aviojet: Used in military trainer applications where throttle responsiveness is paramount.

Technical Applications & Safety

The MFC is a closed-loop feedback system. It continuously compares the pilot's requested power against the actual work the engine is doing ($P_3$ pressure). If the $P_3$ sensing line is restricted by carbon or moisture, the 3070800-73 will sense an artificial "low air" condition and limit fuel, which may prevent the engine from reaching takeoff power.

Safety Warning: Installation requires a mandatory "Part Power Trim" check. This ground-run calibration ensures the engine’s Interstage Turbine Temperature (ITT) is synced with the MFC's fuel schedule. Failure to properly rig the 3070800-73 can lead to "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 3070800-73 lies in its Pneumatic Signal Dampening Architecture. In high-pressure turbine engines, the $P_3$ air signal can be highly turbulent. The -73 variant utilizes internal dampening orifices to "smooth" these pressure pulses before they reach the sensitive bellows. This ensures a rock-steady power setting even in turbulent flight conditions, preventing the "RPM hunting" often seen in poorly maintained or uncalibrated units.

By choosing a certified 3070800-73 through AirParts Aero, you ensure that 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 "lazy" engine acceleration.

  2. Drive Spline Integrity: Inspect the drive splines on the accessory gearbox for "red dust" (fretting). Apply the specified high-pressure lubricant to the 3070800-73 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, internal steel bellows can corrode, causing the unit to fall out of calibration.


Specifications
Cage Code 99193
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