Cessna C525A Citation, CJ2+
1.5.1Engines
The FJ44-3A-24 is a twin spool co-rotating, axial flow turbofan engine with medium bypass ratio, mixed exhaust and high cycle bypass ratio. The engines produce approx. 2400 pounds of flat-rated static thrust at take-off power at sea level and ambient temperature of 22 degrees Celsius.
For more information refer to chapter 1.4 – CJ1+
1.5.2Avionics / Cockpit Layout
1.5.3Dimensions
1.5.4Flight Controls
For more information refer to chapter 1.4 – CJ1+
1.5.5Hydraulic System
For more information refer to chapter 1.4 – CJ1+
1.5.6Fuel System
For more information refer to chapter 1.4 – CJ1+
Difference: Useful fuel capacity: 3.960 lbs.
1.5.7Weight & Balance
Refer to AFM, Weight and Balance Data, Section VI.
- Max Ramp Weight: 12.625 lbs
- Max Take Off Weight: 12.525 lbs
- Max Landing Weight: 11.252 lbs
- Max Zero Fuel Weight: 9.700 lbs
- Standard Empty Weight: 7.550 lbs
- Useful Load: 4.975 lbs
- Useful Fuel Capacity: 3.960 lbs
1.5.8Limitations
Refer to Chapter 2 LIMITATIONS