Powerplants 動力裝置

• Pratt & Whitney PW305A turbofans 
• Thrust: 4,600 pounds (20.46 kN) at takeoff 
• Flat-rating: ISA + 17°C (90°F) 
Powerful, steadfast and exceptionally quiet, the Pratt & Whitney PW305A turbofan engine has set new standards for business jet propulsion. Low in fuel consumption and high in thrust, these engines help give the Bombardier Learjet 60 XR （龐巴迪利爾60 XR公務(wù)機） its exceptional range and economical operation.

This reliable powerplant's Full-Authority Digital Engine Control (FADEC) noticeably reduces pilot workload. The engine's unique fan contour maximizes airflow to ensure optimum performance and efficiency. Variable compressor inlet guide vanes ensure rapid response under all conditions.

Avionics 航電

The Bombardier Learjet 60 XR （龐巴迪利爾60 XR公務(wù)機） features a Rockwell Collins Pro Line 21 avionics system.

In designing the Bombardier Learjet 60 XR （龐巴迪利爾60 XR公務(wù)機） flight deck, Bombardier engineers have created an aircraft which, pilots agree, is a pure pleasure to fly. By applying the latest flight deck design, human factors and systems technology, panel scanning has been reduced and data presentations have been simplified. This engineering effort has effectively minimized pilot workload while increasing situational awareness. Key to this are the pristine layout and sensible ergonomics of the aircraft's Rockwell Collins Pro Line 21 digital avionics suite.

The Rockwell Collins Pro Line 21 avionics suite of the Learjet 60 XR is an advanced fully integrated system. The avionics system features an Integrated Avionics Processing System (IAPS), dual Mode-S transponders and an Electronic Flight Instrumentation System (EFIS).
 
The avionics suite features include: 
• Electronic Flight Instrument System (EFIS) 
• Engine Indication System (EIS) 
• Air Data System (ADS) 
• Attitude Heading Reference System (AHRS) 
• Flight Guidance System (FGS) 
• Radio Sensor System (RSS) 
• Flight Management System (FMS) 
• Integrated Flight Information System (IFIS) 
• Weather Radar System (WXR) 
 
Installed on either side of the instrument panel are four Electronic Flight Displays; these are two Adaptive Flight Displays, AFD-3010, Primary Flight Displays (PFD), and two AFD-3010E Multifunction Displays (MFD). This system features PFD backup and radar displays for pilot and copilot, dual PFD instrumentation, dual flight guidance, dual control display units, dual air data computers, dual AHRS, and dual COMM/NAV/PULSE radios.