N968CR
Cessna 525A Citation CJ2 (CJ2)
Cessna (Textron Aviation)
4 Hours
Duration of Flight
1550 NM
Range
410 MPH
Max Speed

Gallery




Basic Information
Airframe
Data valid as of 2024-10-07| Date | From | To | Flight Time | Status |
|---|---|---|---|---|
| 2025-11-25 | N/A | N/A | N/A | ✓ Landed |
| 2025-11-25 | N/A | N/A | N/A | ✓ Landed |
| 2025-11-25 | N/A | N/A | N/A | ✓ Landed |
| 2025-11-25 | N/A | N/A | N/A | ✓ Landed |
AI Summary
Cessna 525A Citation CJ2 (CJ2)
Overview
2002 Cessna 525A (Citation CJ2), MSN 525A0110. Registered to BANK OF UTAH TRUSTEE, Salt Lake City, UT. Certificate action dated Oct 7, 2024; airworthiness originally dated 2002-11-14; registration expiration 2031-07-31.
Specifications
- Engines: 2× Williams FJ44-2C (2400 lbf each)
- Range: 1550 nm
- Cruise: 410 kts
- Seats: 8
- Ceiling: 45000 ft
Operations & Cabin
6–8 passenger executive club seating with forward refreshment/galley and belted lavatory (typical CJ2 layouts) Executive club seating, forward refreshment center, belted aft lavatory; specific fit for this airframe not publicly detailed in listings consulted. Avionics: Collins Pro Line 21 (typical for CJ2 installations / common retrofit)
Model & Market Context
This entry documents airframe N968CR, a 2002-built Cessna 525A Citation CJ2 with serial number 525A0110. The aircraft is manufactured by Cessna (Textron Aviation) and is registered in the US. Ownership is held by BANK OF UTAH TRUSTEE as a trust based in Salt Lake City, UT, US, reflecting a trustee-held ownership structure rather than a single individual operator. The airframe's known registry status and trustee ownership are the primary public disposition details for this specific aircraft.
The cabin for this Cessna 525A Citation CJ2 follows typical CJ2 layouts and is outfitted for executive transport with 6–8 passenger executive club seating with forward refreshment/galley and belted lavatory (typical CJ2 layouts). Avionics fit is noted as Collins Pro Line 21 (typical for CJ2 installations / common retrofit), aligning this airframe with modernized cockpit capabilities common to CJ2 operators. With a range of 1,550 nm and cruise speed near 410 kts, the aircraft is configured for short- to medium-range business missions; trustee ownership in Salt Lake City, UT, US indicates its administrative base, while registry in the US governs its operating certification and airworthiness oversight. Powerplant configuration of twin Williams FJ44-2C engines informs routine maintenance planning and parts support considerations typical for this engine type.
The airframe is an example of the Cessna 525A Citation CJ2 family produced by Cessna (Textron Aviation), representing the light-cabin, short-to-medium range business jet niche typified by the given performance figures. With seating for 8, a 45,000 ft ceiling and a 1,550 nm mission radius, the platform is positioned for corporate point-to-point trips and owner/operator trust operations. The combination of the Collins Pro Line 21 avionics suite and twin Williams FJ44-2C engines frames typical maintenance, avionics support, and resale considerations for this specific CJ2 airframe.
Aircraft Comparison
| Parameter | N968CR | 23NG | N100AR |
|---|---|---|---|
| Serial Number (MSN) | 525A0110 | 680-0527 | 560-5241 |
| Year Manufactured | 2002 | 2014 | 2002 |
| Duration of Flight | 4 Hours | 7 Hours | 4 Hours |
| Range | 1550 NM | 3190 NM | 1839 NM |
| Max Speed | 410 MPH | 460 MPH | 433 MPH |
| Aircraft Class | Under 12,500lbs | Over 20,000lbs | 12,500-19,999lbs |
| Service Ceiling | 45000 ft | 47000 ft | 45000 ft |
| Max Passengers | 8 | 9 | 13 |
| Cabin Comfort | No items found. | No items found. | No items found. |