2008 Cessna Citation CJ3 Specifications and Summary

CESSNA CITATION JET · Performance Data

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Overview

This document provides specifications and a summary for the 2008 Cessna Citation CJ3, specifically for the aircraft with serial number 525B-0292. It includes detailed information on the aircraft's history, weight limits, engine specifications, avionics systems, additional equipment, maintenance programs, and interior features. The document is intended for potential buyers and aviation professionals looking for comprehensive data on the CJ3 model. Key performance metrics, weight capacities, and maintenance schedules are highlighted to assist in evaluating the aircraft's operational capabilities and requirements.

Maximum ramp weight: 14,070 lbs
Maximum takeoff weight: 13,870 lbs
Maximum landing weight: 12,750 lbs
Empty weight: 8,321 lbs
Fuel capacity: 4,710 lbs
Total time: 920 hours
Landings: 425
Engines: Williams FJ44-3A

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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: 2008
Pages: 9
File size: 1.3 MB
Publisher: www.guardianjet.com

Specifications & performance

Extracted from this document.

Specifications

Engine model: Williams FJ44-3A
Empty weight (lb): 8,321
Max takeoff weight (lb): 13,870

Weight & balance

Max ramp weight (lb): 14,070
Max landing weight (lb): 12,750
Max takeoff weight (lb): 13,870

Documentation completeness

4/7

Most owners only have the POH. Here's the essential set for the CESSNA CITATION JET.

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

The Cessna Citation CJ3 has a maximum ramp weight of 14,070 lbs, a maximum takeoff weight of 13,870 lbs, and a maximum landing weight of 12,750 lbs. The empty weight is recorded at 8,321 lbs, with a fuel capacity of 4,710 lbs. The aircraft has a total time of 920 hours and 425 landings on its engines, which are Williams FJ44-3A.

Avionics & Cockpit

The CJ3 is equipped with the Collins Pro Line 21 Avionics System, which includes dual air data computers, autopilot, and a multi-function display. It features advanced navigation systems, including GPS and DME, and is capable of displaying weather data and electronic charts. The cockpit is designed for enhanced situational awareness with multiple displays.

Maintenance Programs & Inspections Status

The aircraft is enrolled in the Williams TAP ELITE program for engines and Cessna's ProParts program for parts. Maintenance is conducted per manufacturer recommendations, with specific inspection intervals noted. The last completed inspection was on December 17, 2008, with the next due on December 31, 2014.

Interior Description

The CJ3 features a standard seating configuration with a four-place forward club and two stowable executive tables. The cabin includes high gloss wood veneer accents, indirect lighting, and a belted flushing toilet. The interior is designed for passenger comfort and functionality.

Exterior Description

The aircraft has an original paint scheme from Cessna Wichita, featuring an overall snow white color with black and silver metallic accents. This aesthetic contributes to the aircraft's professional appearance.

Full document text

1445 BOSTON POST ROAD • GUILFORD • CONNECTICUT •06437 •203-453-0800• WWW.GUARDIANJET.COM 1 2008 Cessna Citation CJ3 N329BH S/N 525B-0292 Specifications and Summary 1445 BOSTON POST ROAD • GUILFORD • CONNECTICUT •06437 •203-453-0800• WWW.GUARDIANJET.COM 2 2008, Cessna Citation CJ3 N329BH S/N 525B-0292 OFFERED AT: $5,195,000 USD HISTORY: One owner since new Always hangared No known damage history AVAILABLE: IMMEDIATELY STATUS: As of February 1, 2014 TOTAL TIME: 920 LANDINGS: 425 ENGINES: Williams FJ44-3A #1 #2 Total Time Since New: 920 920 Cycles Since New: 425 425 Hot Section Due: 2000 2000 Overhaul Due: 4000 4000 SERIAL NUMBER: 141607 141606 (Engines Enrolled on William’s TAP ELITE program) WEIGHT: MAX RAMP WEIGHT: 14,070 Lbs. MAX TAKE-OFF WEIGHT: 13,870 Lbs. MAX LANDING WEIGHT: 12,750 Lbs. MAX ZERO FUEL: 10,510 Lbs. EMPTY WEIGHT: 8,321 Lbs. FUEL CAPACITY: 4,710 Lbs. CAPABILITIES: RVSM 8.33 Spacing FM Immunity Steep Approach 1445 BOSTON POST ROAD • GUILFORD • CONNECTICUT •06437 •203-453-0800 •WWW.GUARDIANJET.COM 3 AVIONICS & COCKPIT AVIONICS: (Collins Pro Line 21 System) AIR DATA COMPUTER: (2) Collins ADC-3000 Air Data Computer ALTITUDE HEADING REFERENCE SYSTEM: (2) Collins AHC-3000 AHRS AUTOPILOT: Collins Pro Line 21 Integrated Avionics System BROADCAST WEATHER: XM WX Satellite Weather Data receiver displayed on MFD (subscription required) COCKPIT VOICE RECORDER: L3 Communications FA2100 / 120 minutes COMMUNICATIONS: (2) Pro Line 21 CNS Radios with dual VHF-4000 transceivers and dual Collins RTU-4220 Radio Tuning Units DISTANCE MEASURING EQUIPMENT: (1) Pro Line 21 CNS Radios by Collins include single DME-4000 ELECTRONIC FLIGHT INFORMATION SYSTEM: Collins Pro Line 21 with 3-Tube Integrated System ELECTRONIC CHARTS: Jeppesen Electronic Charts are displayed on MFD (subscription required) EMERGENCY LOCATOR TRANSMITTER*: ARTEX C406-N three frequency ELT which interfaces with FMS to transmit last known aircraft position FLIGHT DIRECTOR: Collins Pro Line 21 Integrated Avionics System with dual Collins FCG-3000 Flight Guidance Computers FLIGHT MANAGEMENT SYSTEMS/GLOBAL POSITIONING SYSTEMS: (1) Collins FMS-3000 with GPS-4000A, both lateral and vertical modes and (1) Garmin GPS-500W FMS which serves as a second, independent FMS using its own internal GPS sensor with advisory vertical navigation data. HIGH FREQUENCY RADIO: Provisions Only for Collins HF 9000 RADIO ALTIMETER: (1) Collins ALT-4000 Radar Altimeter STANDBY FLIGHT DISPLAY: JET GH-3000 Standby Gyro TRAFFIC COLLISION and AVOIDANCE SYSTEM: Collins TTR-4000 (TCAS II) with Change 7 TERRAIN AWARENESS AND WARNING SYSTEM*: Honeywell Mark VIII EGPWS (TAWS A) TRANSPONDER*: (2) TDR-94D Mode S Diversity Transponders with Enhanced Surveillance capability. *[NOTE: This option is required to meet European regulations]  VHF NAVIGATION: (2) Pro Line 21 CNS Radios by Collins include dual NAV-4500 receivers WEATHER RADAR: Collins RTA-800 Weather Radar System 1445 BOSTON POST ROAD • GUILFORD • CONNECTICUT •06437 •203-453-0800 •WWW.GUARDIANJET.COM 4 AVIONICS DESCRIPTION Collins Proline 21 Avionics System is an integrated Flight Director/Autopilot and EFIS system utilizing three 8”x10” Color Liquid Crystal Displays (LCD). The Primary Flight Displays (PFD) are located on the pilot’s and copilot’s panel with an Enhanced Multi- Function Display (MFD) on the center panel. All displays are capable of providing compass, radar information, and engine parameters. The MFD has enhanced capabilities and is able to display a variety of graphical information. The weather display may be overlaid on either the arc or map format. The PFD’s also display lateral navigation information in conjunction with the compass information. Vertical deviation, distance, display, autopilot/flight director annunciations, and navigation bearings are also displayed on the PFD. Dual Collins AHC-3000 Attitude Heading Reference Systems supply attitude and magnetic or true heading information to the PFD.. Engine parameters will be displayed at the top of the MFD, including N1, N1 reference, thrust mode, ITT, ignition selected annunciation, N2, oil temp, oil pressure, fuel quantity, fuel flow and fuel temperature. Below the engine display is a window which may display extended FMS data or an integrated electronic checklist. The lower portion of the MFD displays navigation in either a full compass rose, partial compass arc, present position (PPOS) map format or a planning map format. Situational awareness presentations (weather detection, TAWS, and TCAS) may be overlaid on either the arc or PPOS map formats. Temperatures (TAS, RAT, SAT and ISA deviation) are displayed at the bottom of the MFD. Electronic approach and taxi charts and uplinked graphical weather may also be displayed on the MFD. The Collins Flight Management System FMS-3000 provides multiple waypoint navigation solution blended from available GPS, VOR, and DME sources, suitable for en-route, terminal, and non-precision approach navigation. Both lateral and vertical modes may be displayed on the Flight Director and may be fully coupled to the autopilot. Airway flight planning, plain language identifiers and airport communication and navigation frequency lookup features are included. Present position referenced geopolitical and airspace boundaries, and airways may be overlaid on any of the FMS formats. The CDU-3000 (Control Display Unit) provides an alternate method for controlling the radio sensors, in lieu of the RTU-4210s (Radio Tuning Units). An optional Performance Data Base is available which will enable ground-based predicted performance, including automatic computation of takeoff reference speeds. 1445 BOSTON POST ROAD • GUILFORD • CONNECTICUT •06437 •203-453-0800 •WWW.GUARDIANJET.COM 5 ADDITIONAL EQUIPEMT & COMMUNICATIONS ADDITIONAL EQUIPMENT EROS Crew Oxygen Mask & Smoke Goggles Locking Fuel Caps Devore Tail Logo Lights Precise Flight Pulse Light System with TCAS II interface

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Heads UP Technology PBS-250 Passenger Briefing System Concord 42-amp hour Lead acid Battery SafeFlight Angle of Attack Indexer Ground Com Dispatch Switch Voice Annunciator Davtron Chronometer Sheepskin for Pilot’s seats 110V AC outlet in the cockpit Seat Back Pockets Left Hand Belted Flushing Toilet CABIN ENTERTAINMENT & COMMUNICATIONS Aircell ST-3100 Iridium Satellite Phone System Two Handsets, one in the cockpit and one in the cabin AvVisor Cabin Display System (2) 110V cabin OUTLETS MAINTENANCE PROGRAMS & INSPECTIONS STATUS MAINTENANCE & INSPECTIONS  Engines enrolled in William’s TAP ELITE program  Parts Enrolled in Cessna’s ProParts program  Enrolled in CAMP/CESCOM  Maintained per Manufacturer’s Recommended Schedules INSPECTION (Interval) LAST COMPLETED NEXT DUE Document 9 (72 Month) 12/17/2008 12/31/2014 Document 16 (48 Months / 2400 Hours) 12/15/2012 12/31/2016 or 3193 Hours Document 22 (36 Months / 1200 Hours) 12/17/2012 12/31/2015 or 1810 Hours 1445 BOSTON POST ROAD • GUILFORD • CONNECTICUT •06437 •203-453-0800 •WWW.GUARDIANJET.COM 6 INTERIOR Aft Cabin INTERIOR DESCRIPTION Standard CJ3 seating configuration with the four place forward club, with 2 stowable Executive Tables. The left and right side ledges are High Gloss Wood Veneer with leather accent and the Hardware is brushed aluminum. All seats (except #3) have optional seat back pockets. Directly aft of the forward club seats are two forward facing seats. The cabin lighting includes PSU Indirect Lighting and Dropped Aisle Accent Lighting. The Cabinetry is Gloss Laminate. The storage cabinet aft of the Pilot’s seat features a cabin information system. The Flight Deck includes sheepskin pilot seats with 110VAC electrical outlet. Passenger seats are fireblocked. The aft cabin includes an optional Left Side Belted Flushing Toilet with stowable (pocket) privacy doors. Aft Cabin looking Forward 1445 BOSTON POST ROAD • GUILFORD • CONNECTICUT •06437 •203-453-0800 •WWW.GUARDIANJET.COM 7 INTERIOR Forward Cabin Forward Cabin looking Aft Mid Cabin looking Forward 1445 BOSTON POST ROAD • GUILFORD • CONNECTICUT •06437 •203-453-0800 •WWW.GUARDIANJET.COM 8 GALLEY & LAVATORY Forward Galley looking aft Aft Lavatory with belted toilet 1445 BOSTON POST ROAD • GUILFORD • CONNECTICUT •06437 •203-453-0800 •WWW.GUARDIANJET.COM 9 EXTERIOR EXTERIOR DESCRIPTION (Original Paint, Cessna Wichita, December 2008) Overall Snow White with Black Metallic and Silver Metallic accents 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. 02/01/2014 /SS

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