2
TFE731-50R Turbofan Engine Proven, Reliable, Durable Turbofan Power OUTSTANDING PERFORMANCE AND WORLD CLASS RELIABILITY WITH A LOWER COST OF OWNERSHIP

Proven, Reliable, Durable Turbofan Power - Honeywell · Proven, Reliable, Durable Turbofan Power ... Net Thrust TSFC Takeoff, Sea Level, ... TFE731-50R Turbofan Engine Honeywell Aerospace

Embed Size (px)

Citation preview

Page 1: Proven, Reliable, Durable Turbofan Power - Honeywell · Proven, Reliable, Durable Turbofan Power ... Net Thrust TSFC Takeoff, Sea Level, ... TFE731-50R Turbofan Engine Honeywell Aerospace

TFE731-50R Turbofan Engine

Proven, Reliable,Durable Turbofan Power

OUTSTANDING PERFORMANCE AND WORLD CLASSRELIABILITY WITH A LOWER COST OF OWNERSHIP

A60-0916-000-001 FINAL.qxp 1/31/2007 12:21 PM Page 1

Page 2: Proven, Reliable, Durable Turbofan Power - Honeywell · Proven, Reliable, Durable Turbofan Power ... Net Thrust TSFC Takeoff, Sea Level, ... TFE731-50R Turbofan Engine Honeywell Aerospace

PerformanceNet Thrust TSFC

Takeoff, Sea Level, Static (Available to 78°F) 5000 lb 0.424

Max Cruise, 40,000 ft, Mach 0.8, ISA 1116 lb 0.685

A60-0916-000-001February 2007© 2007 Honeywell International Inc.

The TFE731-50 is designed to meet operator requirements for lower operating costs,

increased performance and improved durability, reliability and maintainability. In addi-

tion to improved core and LP spool component technologies, the TFE731-50 includes

70 individual design and material enhancements. A new N1 Digital Electronic Engine

Control (DEEC) with hydromechanical back-up, integral sync, and APR is also a stan-

dard feature.

TFE731-50R Turbofan Engine

Honeywell Aerospace

1944 E. Sky Harbor Circle

Phoenix, AZ 85034

Domestic: 1.800.601.3099

International: 1.602.365.3099

www.honeywell.com

Design Data

Basic Engine Weight: 978 lb

Bypass Ratio: 3.6

Bleed Air Flow: 10% Core Flow (max)

Airflow: 157 lbs/sec

Service Ceiling: 51,000 ft

Airstart: 37,500 ft

Starting: Electric

Accessory Power Extraction: 45 hp(max)

A60-0916-000-001 FINAL.qxp 1/31/2007 12:22 PM Page 2