2009 Citation Mustang

Cessna Citation Mustang · Performance Data

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Overview

This document provides performance data and specifications for the 2009 Cessna Citation Mustang, specifically for the aircraft with serial number N603WS. It includes detailed information about the aircraft's operational history, engine specifications, weight limits, avionics systems, and maintenance programs. The document is intended for potential buyers and aviation enthusiasts who are interested in the capabilities and features of the Citation Mustang. Key performance metrics, including maximum takeoff weight and usable fuel capacity, are highlighted, along with a comprehensive overview of the avionics suite and cockpit features.

Total Time: 497.8 hours
Maximum Takeoff Weight: 8,645 lbs
Usable Fuel Capacity: 2,580 lbs
Engines: Pratt & Whitney PW615F
Avionics: Garmin G1000 with three AMLCDs
Maintenance Program: PowerAdvantage Plus Program
Last Inspection: April 3, 2012, at 450.4 hours

Document

Source

Originally published by www.guardianjet.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type: Performance Data
Year: 2009
Pages: 9
File size: 2.3 MB
Publisher: www.guardianjet.com

Specifications & performance

Extracted from this document.

Specifications

Engine model: Pratt & Whitney PW615F
Fuel capacity (gal): 2,580
Max takeoff weight (lb): 8,645

Weight & balance

Max landing weight (lb): 8,000
Max takeoff weight (lb): 8,645

Documentation completeness

3/7

Most owners only have the POH. Here's the essential set for the Cessna Citation Mustang.

Pilot's Operating Handbook / AFM
Checklist
Maintenance Manual
Parts Catalog (IPC)
Systems & Wiring
Service Bulletins
Type Certificate (TCDS)

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In this document

Specifications and Summary

The document outlines the specifications for the 2009 Cessna Citation Mustang, including total time, landings, and engine details. The aircraft has a total time of 497.8 hours and 257 landings. It is powered by two Pratt & Whitney PW615F engines, both with the same total time and cycles. The maximum takeoff weight is 8,645 lbs, the maximum zero fuel weight is 6,750 lbs, and the maximum landing weight is 8,000 lbs. Usable fuel capacity is 2,580 lbs.

Avionics & Cockpit Features

The Citation Mustang is equipped with the Garmin G1000 advanced avionics system, featuring three active matrix liquid crystal displays (AMLCDs). The system includes dual 10.4-inch primary flight displays and a 15-inch multi-function display. Key components include dual air data computers, attitude heading reference systems, and a three-axis autopilot. Additional features include synthetic vision technology, traffic advisory systems, and chart view options.

Maintenance Programs & Inspections Status

The aircraft is enrolled in several maintenance programs, including the PowerAdvantage Plus Program and Cessna ProParts Program. The document lists various inspections, their completion dates, and when the next inspections are due. For example, the last Doc 1 Inspection was completed on April 3, 2012, at 450.4 hours, with the next due at 900.4 hours.

Interior and Exterior Description

The document describes the interior as having the original FK710 Bronze interior and the exterior painted in JET GLO Snow White with accent stripes. The interior layout includes a forward cabin looking aft and an aft cabin looking forward.

Full document text

2009 Citation Mustang N603WS S/N510-215 Specifications and Summary 2 2009 CITATION MUSTANG N603WS – S/N510-0215 OFFERED AT: $2,345,000 HISTORY: No Damage History OPERATED: Part 91 AVAILABLE: IMMEDIATELY TOTAL TIME: (Times as of June 26, 2012) TTAF: 497.8 LANDINGS: 257 ENGINES: Pratt & Whitney PW615F Left Right SNEW: 497.8 497.8 Cycles: 257 257 Serial Number: LB0451 LB0448 Engines are enrolled in Cessna’s PowerAdvantage+ Program WEIGHT (Lbs): MAX T/O WEIGHT: 8,645 . MAX ZERO FUEL WGT: 6,750 MAX LANDING WGT: 8,000 USABLE FUEL: 2,580 . CAPABILITIES:  RVSM  WAAS  FM Immunity  8.33 kHz Channel Spacing for Comms 3 AVIONICS & COCKPIT AVIONICS The Citation Mustang features the Garmin G1000 advanced avionics system, a large-format glass cockpit with integrated sensors and lightweight modular avionics. The system presents to the crew all the flight, navigation, and situational inputs as well as aircraft systems information for a precise picture of the total flying environment. Three active matrix liquid crystal displays (AMLCDs) designed with high resolution, wide viewing angles and clear sunlight readability, comprise the windows into Garmin’s sophisticated G1000 system. Complete flight system functionality and a three axis autopilot ease the workload for one or two pilots. The Garmin G1000 avionics system and flight guidance package and the Mustang consists of the following components: • Dual 10.4-inch (diagonal) AMLCD Control Display Units with integrated Terrain Awareness System (TAWS B) utilized as Primary Flight Displays (PFD) – Garmin GDU 1040A • Single 15-inch (diagonal) AMLCD Control Display Unit with integrated TAWS B utilized as a Multi-Function Display (MFD) – Garmin GDU 1500 • Dual Engine/Airframe Interface Units – Garmin GEA 71 • Dual digital Air Data Computers (ADC) – Garmin GDS 74B • Dual digital Attitude Heading Reference Systems (AHRS) – Garmin GRS 77 • Dual Magnetometers – Garmin GMU 44 • Dual Integrated Avionics Units with VHF Nav/Com, GPS receivers, and Flight Directores – Garmin GIA 63W • Single Distance Measuring Equipment (DME) receiver – Honeywell KN 63 • Dual digital Audio Control Panels – Garmin GMA 1347D 4 AVIONICS, COCKPIT & OTHER FEATURES (Continued) • Single Remote Flight Management System (FMS) / MFD control keyboard – Garmin GCU 475 • Three Axis Automatic Flight Control System (AFCS) – Garmin GFC 700 with Garmin GMC 710 Module Controller • Single Mode S Diversity Transponder with Elementary Surveillance and Traffic Information System (TIS) – Garmin GTX 33D • Single Mode S Non-diversity Transponder with Elementary Surveillance and TIS – Garmin GTX 33 • Single four-color Weather Avoidance Radar – Garmin GWX 68 • Single Satellite Data Link Weather Transceiver – Garmin GDL 69A • Single Electric Standby Attitude Indicator – Mid Continent Instruments 4200 • Single electromechanical Standby Airspeed Indicator – Aerosonic 261440 • Single electromechanical Standby Altimeter - Aerosonic 162350 • Single Emergency Locator Transmitter (ELT) – Artex C406N COCKPIT & OTHER FEATURES  Dual Cockpit Sun Visors  Smoke Goggles  Eros Crew Oxygen Masks  Synthetic Vision: Garmin’s Synthetic Vision Technology provides a virtual picture of the terrain ahead on the G1000 PFDs. The system utilizes the powerful G1000 central flight management computer, a detailed terrain data base and precision WAAS-enhanced GPS navigation to present a synthetic virtual picture of the terrain, obstructions and the airports ahead. The presentation includes a flight path symbol showing the projected flight path  Chart View: The Chart View Option adds the ability to show approach charts, SIDs, STARs, and airport diagrams as moving maps on the Multi-Function Display (MFD). Aircraft position is graphically overlaid in the plan view format. A profile view may also be shown, and both formats may be zoomed and panned. Chart View in integrated with the FMS to automatically load charts according to the flight plan. A database subscription is required.  Traffic Advisory System: The Honeywell KTA-870 system provides traffic surveillance from 2NM to 40 NM. Up to 45 aircraft can be tracked while displaying up to 30 of the most threatening. Three levels of intruders are identified: non-threat, proximity intruder and Traffic Advisory (TA). Aural traffic advisories are issued through the aircraft audio system and visually displayed on the MFD and the PFD inset maps.  XM Radio: The XM Satellite Radio service features digital quality stereo audio of over 150 channels including news, sports, talk, and commercial free music. The system adds individual headset jacks with volume control in the sidewalls at each passenger seat. The signal is received through the GDL69A datalink weather transceiver and is available throughout the Continental U.S.. Channels may be tuned by the cockpit MFD of by the remote channel selector located in the armrest between the aft cabin seats. A subscription with XM is required.  Oxygen Bottle 40 Cu. Ft.: This bottle replaces the smaller 22 cubic foot oxygen bottle (Note: Required for Part 135 operations) 5 MAINTENANCE PROGRAMS & INSPECTIONS STATUS MAINTENANCE & INSPECTIONS  PowerAdvantage Plus Program  Cessna ProParts Program  CESCOM/CAMP Mx Tracking Program INSPECTION LAST COMPLETED NEXT DUE Doc 1 Inspection 04/03/2012 @ 450.4 Hrs. 900.4 Hrs. Doc 6 Inspection 04/03/2012 @ 450.4 Hrs. 04/30/2013 Doc 7 Inspection 04/21/2011 @ 275.2 Hrs. 04/30/2013 Doc 8 Inspection 12/05/2011 12/31/2014 Doc 13 Inspection 04/03/2012 @ 450.4 Hrs. 04/30/2013/900.4 Hrs. Doc 14 Inspection 04/03/2012 @ 450.4 Hrs. 04/30/2013/1350.4 Hrs. Doc 15 Inspection 04/21/2011 @ 275.2 Hrs. 04/30/2013/1625.2 Hrs. Doc 16 Inspection 04/03/2012 @ 450.4 Hrs. 04/30/2015/1800.4 Hrs. Doc 17 Inspection 04/03/2012 @ 450.4 Hrs. 04/30/2015/2250.4 Hrs. Doc 18 Inspection 04/03/2012 @ 450.4 Hrs. 04/30/2015/2700.4 Hrs. Doc 20 Inspection - 05/31/2013/2700.4 Hrs.

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Doc 21 Inspection 04/03/2012 @ 450.4 Hrs. 04/30/2013 6 INTERIOR Forward Cabin INTERIOR DESCRIPTION (Original FK710 Bronze Interior) Fwd Cabin looking Aft 7 INTERIOR Forward Cabin Fwd Cabin looking Aft Aft Cabin looking fwd 8 EXTERIOR EXTERIOR DESCRIPTION (Original paint by Cessna) JET GLO Snow White with accent stripes JET GLOW Platinum Charcoal Gray 10492 and Maroon 10700 This aircraft is being brokered by Guardian Jet, LLC. Prospective purchasers are encouraged to conduct their own independent pre-purchase inspection as Guardian Jet, LLC makes no representations as to the airworthiness of the aircraft or the accuracy of the above information. Specifications subject to verification upon inspection. Aircraft subject to prior sale. 2012 09 05 /LG 9

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