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3070800-42 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
3070800-42 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
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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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3070800-45 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly

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3070800-45 – Honeywell Aerospace Main Fuel Control (MFC) Assembly

Available now through the AirParts Aero marketplace.

Overview Section

The Honeywell 3070800-45 is a high-precision Main Fuel Control (MFC) unit, often referred to as a Fuel Control Unit (FCU). This assembly is a sophisticated hydro-mechanical "analog computer" designed for the Honeywell TFE731 turbofan engine series. The -45 dash number is a modern configuration specifically calibrated for high-performance variants, providing refined fuel scheduling and transient response for global business jet operations.

The 3070800-45 serves as the primary intelligence for engine thrust management. It continuously calculates the optimal fuel-to-air ratio by monitoring pilot input (Power Lever Angle) and cross-referencing it with real-time environmental data: Compressor Discharge Pressure ($P_3$) and Inlet Temperature ($T_2$). This ensures the engine operates at peak efficiency while remaining safely within its thermal and structural limits.

Key Features Section

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

  • Optimized Transient Response: Features a refined acceleration schedule that allows for crisp, linear throttle response while maintaining a maximum safety margin from the compressor surge line.

  • High-Altitude Governing Stability: Utilizes ultra-sensitive pneumatic bellows to maintain stable engine speeds at high flight levels, preventing "RPM hunting" in thin air.

  • Integrated Overspeed Protection: Features a mechanical flyweight governor that acts as a fail-safe, physically limiting fuel flow should the engine exceed structural RPM limits.

  • Hardened Internal Components: Designed with advanced surface treatments on internal metering valves to resist "stiction" and wear caused by varying fuel qualities and environmental contaminants.

  • Ruggedized Cast Housing: Constructed from a high-strength aluminum alloy designed to withstand the intense vibration and heat found in the engine accessory gearbox (AGB) environment.

Technical Specifications Section

SpecificationDetail
Part Number3070800-45
ManufacturerHoneywell Aerospace
Engine ApplicationTFE731-20, -40, -50, and -60 Series
Input SignalsPower Lever Angle (PLA), $P_3$ (Pneumatic), $T_2$ (Temperature)
Control ModeHydro-mechanical / Pneumatic Feedback
Fuel CompatibilityJet-A, Jet-A1, JP-5, JP-8
WeightApproximately 18.7 lbs

Aircraft Compatibility Section

The 3070800-45 is a critical component for several of the most advanced business jets in the AirParts Aero inventory:

  • 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.

  • Learjet 40 / 45 / 45XR: Provides the precise thrust management required for the Learjet’s high-performance flight profile.

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

Technical Applications & Safety

The MFC operates as a closed-loop feedback system. It senses the actual work the engine is performing (via $P_3$ compressor air) and compares it to the pilot's command. If the $P_3$ sensing line is restricted by carbon or moisture, the 3070800-45 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 ground-run calibration ensures the engine’s Interstage Turbine Temperature (ITT) is correctly synced with the MFC's fuel schedule. Failure to properly rig the 3070800-45 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 3070800-45 lies in its Signal Dampening Architecture. In modern high-pressure engines, $P_3$ air can be turbulent. The -45 variant utilizes internal dampening orifices to smooth these pressure pulses before they reach the sensitive bellows. This ensure a rock-steady power setting even in turbulent flight conditions, which is vital for the accuracy of modern autothrottle systems.

By sourcing a certified 3070800-45 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 Maintenance: 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 3070800-45 drive shaft to ensure longevity.

  3. Preservation: If the unit is removed for storage, 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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