CITATION MUSTANG SN RANGE (NM) 1,200 PASSENGERS 4 KNOTS 340 CONTACT: DAVID LEE I

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Transcription:

KNOTS 340 PASSENGERS 4 RANGE (NM) 1,200

AIRCRAFT LISTING DETAILS: Total Hours: 1550 ENGINES: Pratt & Whitney PW615F-A Left Right Total Hours: 1550 1550 AIRCRAFT HIGHLIGHTS: ADS-B Out Cessna Service Center Maintained No Damage History Fully enrolled on PowerAdvantage Plus and ProParts 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

FEATURES / OPTIONS: ADS-B Out Synthetic Vision XM Radio INTERIOR: Standard Four (4) Passenger Center Club Platinum Leather Seating with LH and RH Fwd Storage Cabinets, Dual Executive Writing Tables, Aft Center Console, and Side-Facing Non-Belted Lav. 40 Cu Ft Oxygen Bottle EXTERIOR: Overall Matterhorn White with Metallic Blue, Metallic Silver, and Black Stripes.

MAXIMUM CRUISE SPEED (35,000 ft / 10,668 m, mid cruise weight) 340 ktas 630 km/hr RATES OF CLIMB All engines 3,010 ft/min 917 m/min Single engine 870 ft/mi 265 m/m NBAA IFR RANGE (100 nm Alternate) Full fuel, max takeoff weight 1,200 nm 2,222 km AIRPORT PERFORMANCE (Dry, Level, Hard, Zero Wind) Takeoff distance (SL, ISA, MTOW) 3,110 ft 948 m Landing distance (SL, ISA, MTOW) 2,380 ft 725 m AIRSPEED LIMITS Vmo from Seal Level to 27,120 250 kias 463 km/hr Mmo at 27,130 (8,266 m) and above M.63 (indicated) STALL SPEED MLW, Landing configuration 73 kcas 135 km/hr CEILING Maximum certified 41,000 ft 12,497 m PRESSURIZATION Nominal pressure differential 8.3 psi.57 bar

2001 2010 CITATION CESSNA MUSTANG CITATION SN 510-0304 CJ2 SN 525A-0013 OUTSIDE DIMENSIONS Overall length 40 ft 7 in 12.37 m Overall height 13 ft 5 in 4.09 m Wingspan 43 ft 2in 13.15m CABIN DIMENSIONS Length (excluding cockpit) 9 ft 9 in 2.97 m Height 54 in 1.37 m 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 ENGINES Two (2) Pratt & Whitney PW615F-A Takeoff thrust 1,460 lb 6.49 kn Bypass ration 2.2 :1 *Reflects standard aircraft with typical options and unusable fuel / oil **Amount of payload and fuel that can be carried based on ramp weight

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