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3070800-73 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
3070800-73 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly
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A740C - Aircraft Tool Supply Aircraft Jack With AT-JPR2
A740C - Aircraft Tool Supply Aircraft Jack With AT-JPR2
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3070800-74 - Honeywell Aerospace Turbine Engine Main Fuel Control Assembly

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3070800-74 – Honeywell Aerospace Main Fuel Control (MFC) Assembly

Available now through the AirParts Aero marketplace.

Overview Section

The Honeywell 3070800-74 is a high-precision Main Fuel Control (MFC) unit, also known as a Fuel Control Unit (FCU). Engineered for the Honeywell TFE731 turbofan engine series, the -74 dash number represents one of the most advanced and mature hydro-mechanical configurations in the 3070800 lineage.

This assembly acts as the engine's "primary analog processor," metering fuel with extreme accuracy by balancing pilot input (Power Lever Angle) against real-time atmospheric data: Compressor Discharge Pressure (P3) and Inlet Temperature (T2). The -74 variant is specifically designed for high-performance airframes, offering refined internal porting and calibrated bellows to ensure stable thrust management and surge protection in all flight envelopes.

Key Features Section

  • Advanced 3D Cam Logic: Features a precision-ground internal cam profile that optimizes fuel scheduling for smoother throttle transitions and superior linearity.

  • Refined Surge Protection: Utilizing high-sensitivity pneumatic bellows, the -74 reacts instantaneously to changes in P3 air density, shielding the engine from compressor stalls during rapid power transients.

  • High-Altitude Stability: Engineered to maintain stable engine speeds (N2) at extreme altitudes, preventing "RPM hunting" and ensuring consistent governing in thin air.

  • Hardened Metering Components: Includes specialized surface treatments on internal valves to mitigate "stiction" caused by varied fuel qualities and environmental contaminants.

  • Integrated Mechanical Fail-Safe: Features a built-in overspeed governor that physically limits fuel flow to protect the engine core from structural damage.

  • Ruggedized OEM Housing: Housed in a high-integrity aluminum alloy body designed to withstand the vibration and thermal loads of the Accessory Gearbox (AGB) mounting.

Technical Specifications Section

SpecificationDetail
Part Number3070800-74
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 3070800-74 is a mission-critical component for several prominent business jets utilized in the AirParts Aero inventory:

  • Beechcraft Hawker 800 / 800XP: Found in specific engine configurations requiring the -74's refined scheduling for TFE731-5R powerplants.

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

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

  • Learjet 35A / 36A: Used in high-utilization environments where throttle responsiveness and reliability are paramount.

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) and compares it to the pilot's request. If the $P_3$ sensing line is restricted by carbon or moisture, the 3070800-74 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" procedure. 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 3070800-74 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 3070800-74 lies in its Pneumatic Signal Dampening Architecture. In high-pressure turbine engines, the $P_3$ air signal can be highly turbulent. The -74 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 3070800-74 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 "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 3070800-74 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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