Engine Details

Introduced in the mid-1990s, the Trent 700 is the first of the Trent family and was developed specifically for the Airbus A330 series. It entered service in 1995 and is known for its robust widebody performance and high-thrust capability.

Full Engine Name
Rolls Royce Trent 700
Manufacturer
Rolls Royce
Engine Family
Trent

Engine Specifications

Key Specifications of This Engine Type
Thrust: 67,500–72,000 lbf
Bypass Ratio: ~5:1
Fan Diameter: 97.4 in (2.47 m)
Three-shaft design
Trent 700 Engine Details and Support

Aircraft Applications

Airbus A330-200 and A330-300 (primarily)
Competes with PW4000 and GE CF6-80E1 for same aircraft

Notable Design Features

Unique hollow titanium wide-chord fan blades — a signature Rolls-Royce innovation
Three-shaft design enhances efficiency and simplifies component stress distribution
Modular engine design allows easier maintenance on individual sections

Maintenance & Shop Visit Considerations

Engine tends to have long time on-wing but expensive SV events due to 3-shaft architecture
Fan blade health is crucial — common BSI topic
LLP management is more complex due to modular stack design
Trend in recent years for SV work to be conducted in Asia (e.g., HAECO, SIAEC)

Market Context

Most popular engine variant for the A330
Remains in demand in secondary leasing markets, especially for cargo conversions
Rolls-Royce Total Care agreements are often involved — impacts asset flexibility

Technical Records & Due Diligence Considerations

Check for TotalCare maintenance structure (records may be embedded with OEM)
Fan blade life tracking critical
LLP visibility by module
Inspect compliance with key SBs relating to turbine blades and IP compressor

Borescope (BSI) Considerations

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