Rolls-Royce

Tay

Low-Bypass Turbofan Out of Production

Technical Specifications

Thrust
67,2 kN (15.100 lbf)
Bypass Ratio
3,1:1
Fan Diameter
1,168 m
Pressure Ratio
16,0:1
SFC
0,3600 lb/lbf·h
Dry Weight
1.415 kg
Length
2,413 m
First Run
1984
In Service
1988

Overview

The Rolls-Royce Tay is a low-bypass turbofan engine developed as a modern successor to the earlier Spey engine. Designed for short-to-medium range regional jets, the Tay entered service in 1988 and became the exclusive power plant for the Fokker 100 and Fokker 70 airliners. It also found a significant role on business aviation platforms, most notably the Gulfstream IV. With approximately 800 engines produced, the Tay represents one of the most successful regional turbofan programs in European aviation history.

The Tay traces its lineage directly to the Rolls-Royce Spey, a low-bypass turbofan that powered the Fokker F28 Fellowship and BAC One-Eleven among others. Rather than a clean-sheet design, the Tay was an extensive modernisation incorporating an advanced fan, new high-pressure compressor technology, and a full authority digital engine control (FADEC) system. This evolutionary approach reduced development costs while delivering a step-change improvement in efficiency and noise compared to the Spey it replaced.

Technical Specifications

ParameterValue
Thrust (takeoff)67.2 kN (15,100 lbf)
Bypass ratio3.1:1
Fan diameter1.168 m (46.0 in)
Overall pressure ratio16.0:1
Specific fuel consumption (cruise)0.360 lb/lbf/hr
Dry weight1,415 kg (3,120 lb)
Length2.413 m (95.0 in)
First run1984
Entry into service1988

Variants

The Tay family comprises two main commercial variants optimised for their respective applications. The Tay 620-15 was the launch variant certified for the Fokker 100, rated at 61.6 kN (13,850 lbf) to match the original aircraft's performance requirements. The uprated Tay 650-15 followed, offering the full 67.2 kN (15,100 lbf) thrust, and this variant was selected for the shorter Fokker 70 as well as retrofit on later Fokker 100 aircraft requiring better hot-and-high performance. For business aviation, the Tay 611-8 powers the Gulfstream IV, with output optimised for the aircraft's long-range cruise requirements rather than the high-cycle demands of airliner service.

Aircraft Applications

The Fokker 100, a 107-seat narrow-body regional jet introduced in 1988, was designed from the outset around the Tay. The engine's rear-fuselage mounting configuration, inherited from the F28, gave the Fokker 100 a clean, uncluttered wing ideally suited for operations from shorter regional runways. The smaller Fokker 70, seating approximately 80 passengers and entering service in 1994, uses the same airframe with a shortened fuselage and relies on the Tay 650 for adequate runway performance. Outside the Fokker family, the Gulfstream IV and G400 series business jets adopted the Tay 611, giving the engine a secondary market in large-cabin long-range corporate aviation.

Development History

Rolls-Royce launched the Tay programme in the early 1980s as Fokker sought a more efficient replacement for the Spey powering its F28 Fellowship. The decision to base the new engine on Spey core architecture — combined with modern aerodynamic design for the fan and compressor — proved commercially sound. The first run occurred in 1984 at Rolls-Royce's Bristol facility, with certification and entry into service achieved in 1988 aboard the Fokker 100. Production continued until Fokker's insolvency in 1996, after which demand was sustained primarily by the Gulfstream IV business jet market. With roughly 800 units delivered, the Tay closed out production as a commercially successful but ultimately niche programme, its market bounded by the demise of its primary customer.