Honeywell

TFE731

Business Aviation In Production

Technical Specifications

Thrust
20.9 kN (4700 lbf)
Bypass Ratio
2.8:1
Fan Diameter
0.716 m
Pressure Ratio
14.0:1
SFC
0.4500 lb/lbf·h
Dry Weight
340 kg
Length
1.524 m
First Run
1970
In Service
1972

Overview

The Honeywell TFE731 is one of the most successful and long-lived turbofan engines in business aviation history. First entering service in 1972, it has powered an extraordinarily wide range of business jets for more than five decades, establishing itself as the benchmark powerplant for the midsize business jet category. With thrust ratings from approximately 3,500 lbf to over 5,000 lbf across its many variants, the TFE731 strikes an effective balance between performance, fuel efficiency, and compact dimensions that made it the engine of choice for dozens of aircraft types from manufacturers including Dassault, Learjet, Hawker, and Israel Aerospace Industries.

The TFE731 introduced a then-novel geared fan architecture to the business jet market, using a reduction gearbox between the low-pressure turbine and the fan to allow each component to spin at its aerodynamically optimal speed. This design philosophy — later adopted by Pratt & Whitney for its PW1000G GTF family on commercial aircraft — delivers improved propulsive efficiency compared to a direct-drive architecture at the bypass ratios typical of business jets. The engine's longevity is a testament to its robust core design, which has accommodated successive upgrades in aerodynamics, materials, and engine management electronics over five decades without departing from its fundamental architecture.

Today, Honeywell continues to produce TFE731 engines and support the massive installed base of existing aircraft, making it one of the aviation industry's most enduring powerplant programs alongside the CFM56 and JT8D.

Technical Specifications

ParameterValue
Maximum Thrust20.9 kN (4,700 lbf)
Bypass Ratio2.8:1
Fan Diameter0.716 m (28.2 in)
Dry Weight340 kg (750 lb)
Length1.524 m (60.0 in)
Overall Pressure Ratio14.0:1
SFC0.450 lb/lbf·h
First Run1970
Entry into Service1972

Variants

The TFE731 family spans more than a dozen major variants across five decades of production. The original TFE731-2 (3,500 lbf) powered the Learjet 35/36 and Dassault Falcon 10. The TFE731-3 (3,700 lbf) became the engine for the Dassault Falcon 20 and Hawker 700 series. The TFE731-5 (4,300 lbf) powered the Falcon 50 tri-engine and Learjet 55. The TFE731-20/40/60 series introduced FADEC and new aerodynamics for the Falcon 900 series and Learjet 45/60. The TFE731-50R brought blended winglet compatibility and further efficiency improvements. More recent variants include the TFE731-40BR with an extended maintenance interval designed to reduce total ownership cost for high-utilization operators.

Aircraft Applications

The TFE731 has powered an exceptionally broad array of business jet types across its history. Key aircraft include the Dassault Falcon 10/20/50/900 series spanning four decades of Falcon production; the Learjet 35/36/45/55/60 family representing Learjet's primary lineup for many years; the Hawker 700/800/800XP/850XP/900XP corporate jet series; the IAI Astra/Galaxy Israeli business jets; and the CASA C-101 jet trainer in the military segment. This remarkable breadth of applications across manufacturers and continents reflects the TFE731's versatility and the confidence that airframers placed in its reliability and performance characteristics.

Development History

The TFE731 program was initiated by Garrett AiResearch (later Garrett, then Allied Signal, and ultimately Honeywell following the 1999 merger) in the late 1960s in response to growing demand for turbofan power in the emerging business jet market. The engine first ran in 1970 and received FAA certification in 1972, entering service on the Dassault Falcon 10 and Learjet 35. The geared fan concept was a defining innovation, distinguishing the TFE731 from competing engines that used direct-drive fan architectures. Over five decades, Honeywell invested in numerous product improvement programs, including advanced fan aerodynamics, low-emission combustors, FADEC integration in the 1990s, and extended-life turbine components. The engine's installed base of thousands of aircraft worldwide has made continuous support and spare parts availability a core business priority for Honeywell's aerospace division through the 21st century.