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Side-by-side aircraft model specifications (max across variants).
| Spec | Cessna Aircraft Company 525C | Bell Textron Citation CJ4 |
|---|---|---|
| ICAO type | C25C | C25C |
| MTOW | 7,700 kg | 7,700 kg |
| Range | 2,165 nm | 2,165 nm |
| Cruise speed | — | — |
| Service ceiling | 45,000 ft | 45,000 ft |
| Max seats | 9 | — |
| Length | 16 m | 16 m |
| Wingspan | 15 m | 15 m |
The Cessna Aircraft Company 525C has a range of 2,165 nm; the Bell Textron Citation CJ4 has a range of 2,165 nm.
The Cessna Aircraft Company 525C has a maximum take-off weight of 7,700 kg, compared with 7,700 kg for the Bell Textron Citation CJ4.
The Cessna Aircraft Company 525C is ICAO type C25C; the Bell Textron Citation CJ4 is ICAO type C25C.