For saleSold
2007 Cessna Citation Mustang
S/N 510-0044 N300VR
Price on request
SOLD
- Passengers
- 5
- Max cruise speed
- 340 ktas
- NBAA IFR range
- 1,200 nm
- Total time
- 10,089 h
- Total landings
- 8,170
Highlights
- KTA 810 TAS (Traffic Advisory System)
- Synthetic Vision (SVT)
- USB A and C charging outlets in cockpit
- ADS-B Out
- Garmin G1000 integrated avionics
- Cescom maintenance tracking
This aircraft has been sold.
Airframe
| Total hours | 10,089 |
| Total landings | 8,170 |
Engines – Pratt & Whitney PW615F-A
| Left | Right | |
|---|---|---|
| Serial numbers | PCE-LB0147 | PCE-LB0148 |
| Total hours | 7,835 | 7,885 |
| Total cycles | 6,534 | 6,586 |
| Hours until overhaul | 289 | 295 |
Maintenance
- Doc 11 completed: July 2021
- Doc 32 completed: July 2022
- Doc 6 & 10K airframe completed: July 2024
- Doc 7, Doc 13, Doc 14, Doc 15, Doc 18, Doc 21 completed: December 2024
- Cescom maintenance tracking
Interior
- Standard five (5) passenger center club, tan with dark gray inserts leather seating, with left-hand and right-hand forward storage cabinets, dual executive writing tables, aft center console, and side-facing non-belted lav.
Exterior
- Overall Matterhorn White with black and red accents.
Features / options
- ADF
- KTA 810 TAS (Traffic Advisory System)
- Synthetic Vision (SVT)
- USB A and C charging outlets in cockpit
- ADS-B Out
Full specifications
Standard avionics
- Garmin G1000 integrated avionics suite
- Dual 10.4” PFDs
- Single 15” MFD
- Dual Garmin GMA 1347D digital audio control panels with dual comm
- Dual nav
- Dual GTX 33D Mode S transponders
- Garmin integrated FMS
- Garmin GWX 68 digital weather radar
- Garmin Class B TAWS
- Artex C406-N three-frequency ELT
- GFC 700 automatic flight control system
- RVSM capable
Performance
| Maximum cruise speed (35,000 ft / 10,668 m, mid cruise weight) | 340 ktas · 630 km/h |
| NBAA IFR range (100 nm alternate; full fuel, MTOW and max cruise) | 1,200 nm · 2,222 km |
| Takeoff distance (SL, ISA, MTOW; dry, level, hard, zero wind) | 3,110 ft · 948 m |
| Landing distance (SL, ISA, MTOW) | 2,380 ft · 725 m |
| Maximum certified ceiling | 41,000 ft · 12,497 m |
| Rate of climb – all engines | 3,010 ft/min · 917 m/min |
| Rate of climb – single engine | 870 ft/min · 265 m/min |
| Vmo from sea level to 27,120 ft | 250 kias · 463 km/h |
| Mmo at 27,130 ft (8,266 m) and above | M 0.63 (indicated) |
| Approach speed (MLW, landing configuration) | 73 kcas · 135 km/h |
| Nominal pressure differential | 8.3 psi · 0.57 bar |
Dimensions
| Overall length | 40 ft 7 in · 12.37 m |
| Overall height | 13 ft 5 in · 4.09 m |
| Wingspan | 43 ft 2 in · 13.15 m |
| Cabin length (excluding cockpit) | 117 in · 2.97 m |
| Cabin height | 54 in · 1.37 m |
| Cabin width | 55 in · 1.40 m |
Design weights and capacities
| Max ramp weight | 8,730 lb · 3,969 kg |
| Max takeoff weight | 8,645 lb · 3,921 kg |
| Max landing weight | 8,000 lb · 3,629 kg |
| Max zero fuel weight | 6,750 lb · 3,062 kg |
| Max fuel capacity (6.7 lb/gal) | 2,580 lb · 1,170 kg |
| Typical empty weight* | 5,350 lb · 2,427 kg |
| Useful load** | 3,380 lb · 1,536 kg |
| Payload with full fuel | 800 lb · 363 kg |
*Reflects standard aircraft with typical options and unusable fuel/oil. **Amount of payload and fuel that can be carried based on ramp weight.
Engines (type data)
| Engines | Two (2) Pratt & Whitney PW615F-A |
| Takeoff thrust | 1,460 lb · 6.49 kN |
| Bypass ratio | 2.2:1 |