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3070800-45 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
3070800-45 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
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3070800-54 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
3070800-54 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
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3070800-52 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly

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3070800-52 – Honeywell Aerospace Main Fuel Control (MFC) Assembly

Available now through the AirParts Aero marketplace.

Overview Section

The Honeywell 3070800-52 is a top-tier Main Fuel Control (MFC), representing one of the most technologically refined hydro-mechanical control units for the Honeywell TFE731 turbofan engine series. The -52 dash number is specifically calibrated for high-thrust, late-model variants such as the TFE731-40, -50, and -60, which power modern, long-range business jets.

Acting as a sophisticated "analog computer," the 3070800-52 manages the entire combustion cycle. It calculates the precise fuel-to-air ratio by balancing the pilot’s Power Lever Angle (PLA) against critical environmental feedback: Compressor Discharge Pressure (P3) and Inlet Temperature (T2). This assembly is critical for ensuring that the engine provides maximum thrust while preventing destructive compressor stalls or turbine over-temperature events.

Key Features Section

  • Precision-Calibrated 3D Cams: Features an advanced internal cam architecture that provides a linear and highly predictable engine response, essential for precision flight path management and autothrottle integration.

  • High-Sensitivity Pneumatic Bellows: Utilizes the latest bellows technology to react instantaneously to P3 air density changes, providing a superior safety margin during rapid power transients.

  • Enhanced Environmental Compensation: Automatically adjusts fuel flow for varied altitudes and ambient temperatures, ensuring consistent "light-offs" in cold-soak conditions and stable governing at high altitudes.

  • Integrated Mechanical Overspeed Governor: Provides a physical fail-safe that limits fuel flow if the engine N2 speed exceeds structural safety limits.

  • Advanced Surface Treatments: Internal metering valves are treated with proprietary coatings to mitigate "stiction" and wear caused by diverse fuel types and microscopic contaminants.

  • Ruggedized Cast Housing: Constructed from a high-strength aluminum alloy designed to withstand the high-vibration and high-heat environment of the engine's Accessory Gearbox (AGB).

Technical Specifications Section

SpecificationDetail
Part Number3070800-52
ManufacturerHoneywell Aerospace
Engine ApplicationTFE731-40R, -50R, -60, and -60W variants
Input SignalsPower Lever Angle (PLA), P3 (Pneumatic), T2 (Temperature)
Control LogicHydro-mechanical with Pneumatic Feedback
Fuel CompatibilityJet-A, Jet-A1, JP-5, JP-8
WeightApproximately 18.9 lbs

Aircraft Compatibility Section

The 3070800-52 is a primary fuel management component for several high-performance business jets:

  • Dassault Falcon 900EX / 900LX: The core metering solution for the triple-engine TFE731-60 configuration.

  • Hawker 900XP: Essential for the reliability and fuel efficiency of the TFE731-50R engines.

  • Gulfstream G150: Critical for the performance and climb schedules of the TFE731-40AR powerplants.

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

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 sensing line is restricted by carbon or moisture, the 3070800-52 will sense an artificial "low air" condition and limit fuel flow, which may prevent the engine from reaching takeoff power.

Safety Warning: Installation requires a mandatory "Part Power Trim" procedure. This is a safety-of-flight ground run that synchronizes the MFC with the engine's Interstage Turbine Temperature (ITT). Failure to correctly rig the 3070800-52 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 3070800-52 lies in its Signal Dampening Architecture. In high-pressure turbofans, the $P_3$ air coming from the compressor can be turbulent. The -52 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, significantly improving the precision of autothrottle systems.

By sourcing a certified 3070800-52 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 dirty 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 3070800-52 drive shaft to prevent premature failure.

  3. Preservation Fluid: 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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