N921AP
Cessna 525A CitationJet CJ2 (525A (CJ2))
Cessna (Textron Aviation)
4 Hours
Duration of Flight
1500 NM
Range
418 MPH
Max Speed

Gallery



Basic Information
Airframe
Data valid as of 2025-11-26No flight history available
Flight records for this aircraft have not been tracked yet.
AI Summary
Cessna 525A CitationJet CJ2 (525A (CJ2))
Overview
2003 Cessna 525A CitationJet CJ2, MSN 525A0137. Photographed at KDAN (2012) and I75 (2024). Public spotting and type-specific references identify this airframe as a CJ2 model (525A).
Specifications
- Engines: 2× Williams FJ44-2C (2400 lbf each)
- Range: 1500 nm
- Cruise: 402 kts
- Seats: 8
- Ceiling: 45000 ft
Operations & Cabin
Typical 6–8 place executive club layout with forward refreshment center and belted aft lavatory Executive leather seating, dual/club seating possible, small refreshment center, belted lavatory; specific interior on this airframe not documented in public listing Avionics: Collins Pro Line 21 (typical fit for CJ2 airframes)
Model & Market Context
The airframe bearing registration N921AP is a Cessna 525A CitationJet CJ2 built in 2003 with serial number 525A0137 by Cessna (Textron Aviation). Public records for this specific airframe’s ownership timeline and operator/home base are not published. There are no publicly provided notable registry actions or detailed valuation and condition highlights for this individual aircraft in the supplied dataset. The entry data identifies the airframe to the model level and construction serial but omits operator and market appraisal details.
The cabin for this airframe is described as a typical 6–8 place executive club layout with a forward refreshment center and a belted aft lavatory, supporting executive transport missions and short‑to‑medium range point‑to‑point operations. The avionics fit cited for CJ2 airframes is the Collins Pro Line 21, which supports contemporary navigation, communication and flight management capabilities common to light business jets of this configuration. Typical mission profiles for this configuration include corporate point‑to‑point travel within the stated 1,500 nm range and operations to flight levels approaching the 45,000 ft ceiling; specific operator base, route history, and unique amenities for N921AP are not published. Maintenance considerations follow twin‑engine light jet practice centered on the Williams FJ44 engine maintenance programs and airframe inspection cycles customary to Cessna Citation airframes.
As a Cessna 525A CitationJet CJ2, this airframe belongs to the light, fixed‑wing multi‑engine Citation family produced by Cessna (Textron Aviation), offering a blend of modest cabin capacity (8 seats) and transcontinental‑regional capability (approximately 1,500 nm range and 402 kts cruise). The combination of the Williams FJ44‑2C powerplants and Collins Pro Line 21 avionics positions the type for continued demand in the light business jet segment where operators value efficiency, climb performance to 45,000 ft, and a compact executive cabin. Resale and maintenance considerations for this serial typically follow common Citation CJ2 practices tied to engine program status, avionics upgrades, and documented maintenance history, which for N921AP are not published.
Aircraft Comparison
| Parameter | N921AP | 23NG | N100AR |
|---|---|---|---|
| Serial Number (MSN) | 525A0137 | 680-0527 | 560-5241 |
| Year Manufactured | 2003 | 2014 | 2002 |
| Duration of Flight | 4 Hours | 7 Hours | 4 Hours |
| Range | 1500 NM | 3190 NM | 1839 NM |
| Max Speed | 418 MPH | 460 MPH | 433 MPH |
| Aircraft Class | 12,500 to 20,000lbs | 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. |