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3070800-26 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
3070800-26 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
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3070800-32 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
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3070800-27 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly

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3070800-27 – Honeywell Aerospace Main Fuel Control (MFC) Assembly

Available now through the AirParts Aero marketplace.

Overview Section

The Honeywell 3070800-27 is a high-precision Main Fuel Control (MFC) unit, often referred to as a Fuel Control Unit (FCU). It is a sophisticated hydro-mechanical computing device designed for the Honeywell TFE731 turbofan engine series. The -27 configuration represents a specific calibration standard, often utilized in high-performance business jet applications that require refined fuel scheduling for various altitude and temperature envelopes.

The 3070800-27 acts as the "analog brain" for the engine, coordinating fuel flow based on pilot command (Power Lever Angle), compressor discharge pressure ($P_3$), and engine intake temperature ($T_2$). By precisely metering fuel, the MFC ensures the engine accelerates and decelerates within safe limits, preventing compressor stalls, over-speeds, and turbine over-temperature events.

Key Features Section

  • Precision Hydro-Mechanical Governing: Uses a system of flyweight governors and pneumatic bellows to maintain stable engine speeds ($N_2$) regardless of changes in altitude or ambient temperature.

  • Optimized Acceleration Schedule: Controls the rate of fuel increase during power transients to ensure the engine accelerates as quickly as possible without exceeding the surge limit of the compressor.

  • Altitude Compensation: Automatically adjusts the fuel-to-air ratio as the aircraft climbs into thinner air, maintaining optimal combustion efficiency.

  • Environmental Resilience: Housed in a rugged, cast-aluminum body designed to operate in the high-vibration and high-heat environment of the engine accessory gearbox (AGB).

  • Internal Fail-Safes: Includes a mechanical "ultimate overspeed" shut-off to protect the engine core in the event of a primary governor failure.

  • Calibrated for TFE731 Series: Specifically tuned for the geared turbofan architecture, ensuring the responsiveness required for corporate jet maneuvers.

Technical Specifications Section

SpecificationDetail
Part Number3070800-27
ManufacturerHoneywell Aerospace (Garrett/AlliedSignal)
Engine ApplicationTFE731-2, -3, -4, and -5 variants
Input SignalsPower Lever Angle (PLA), $P_3$ (Pneumatic), $T_2$ (Temperature)
Fuel CompatibilityJet-A, Jet-A1, JP-5, JP-8
Control MethodHydro-mechanical (Pneumatic Sensing)
Weight~17.8 lbs (Nominal)

Aircraft Compatibility Section

The 3070800-27 is found on several iconic business jets that rely on the TFE731's performance:

  • Dassault Falcon 50 / 900: Critical for the three-engine reliability and thrust management of these long-range jets.

  • Hawker 800XP / 850XP: Often utilized in configurations optimized for mid-size transcontinental missions.

  • Learjet 31A / 35A / 45: Provides the rapid throttle response required for the Learjet’s high-performance flight envelope.

  • Cessna Citation VII: Core fuel metering component for the TFE731-4R engines.

Technical Applications & Safety

The MFC is a "closed-loop" mechanical system. It senses the actual work the engine is doing (via $P_3$ compressor air pressure) and compares it to what the pilot is asking for via the throttle. If the $P_3$ sensing line is leaking or the internal bellows are damaged, the engine may fail to reach takeoff power or may "hunt" for a stable RPM.

Safety Warning: FCU Rigging is a safety-of-flight procedure. If the 3070800-27 is replaced, the technician must perform a "Part Power Trim" check to ensure the engine's ITT (Interstage Turbine Temperature) and RPM stay within limits. Failure to correctly rig the FCU can result in an engine that "overshoots" its temperature limits during a rapid throttle advance, leading to permanent turbine blade damage.

Technical Engineering Insight

The engineering value of the 3070800-27 lies in its Torsional Drive Shaft and Dampening. The unit is driven by a splined shaft from the accessory gearbox. To prevent engine vibration from "chattering" the internal metering valves, the -27 utilizes a fluid-dampened drive interface. This ensures that the fuel flow remains smooth and steady, preventing the "hunting" or RPM oscillations that can occur with lower-quality or worn-out fuel controls.

By choosing a certified 3070800-27 through AirParts Aero, you ensure the unit has been bench-tested on a specialized fuel stand to verify its Acceleration Schedule. This test ensures that when the throttles are advanced, the engine responds linearly and safely every time.

Installation & Maintenance Addendum

  1. $P_3$ Filter Replacement: Always replace the $P_3$ (Compressor Discharge) air filter whenever the MFC is replaced. A clogged filter will cause the engine to be "lazy" during acceleration.

  2. Seal Integrity: Use new O-rings for the fuel inlet and outlet ports. Even a minor weep can lead to high-pressure fuel spraying on hot engine components.

  3. Preservation: If the 3070800-27 is removed for storage, it must be filled with preserving oil (MIL-PRF-6081) to prevent the internal steel bellows from corroding or losing their calibration.


Specifications
Cage Code 99193