1998 Cessna Citation X Specifications and Summary
Cessna Citation X · Specifications
Overview
This document provides detailed specifications and summary information for the 1998 Cessna Citation X, specifically for aircraft N110PK with serial number 750-0040. It includes critical data on the aircraft's performance, weight, engine specifications, avionics, and maintenance status. This reference is intended for pilots, aviation enthusiasts, and potential buyers, offering insights into the aircraft's capabilities and operational history. Key highlights include engine details, weight limits, and avionics systems, making it a comprehensive resource for understanding the aircraft's features and requirements.
- Total time: 4,580 hours; Landings: 2,736
- Max ramp weight: 36,000 lbs; Max take-off weight: 35,700 lbs
- Engines: Rolls-Royce AE 3007C1; Total time since new: 4,466 hrs (engine #1), 4,381 hrs (engine #2)
- Avionics: Honeywell Primus 2000; Dual Honeywell NV-850 NAV receivers
- Maintenance per MSG-3; Last inspection: March 2, 2018, at 4,433 hours
Document
Source
Originally published by www.guardianjet.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Specifications
- Year
- 1998
- Pages
- 9
- File size
- 1.6 MB
- Publisher
- www.guardianjet.com
Specifications & performance
Extracted from this document.
Specifications
- Engine model
- Rolls-Royce AE 3007C1
- Empty weight (lb)
- 21,710
- Max takeoff weight (lb)
- 35,700
Weight & balance
- Max ramp weight (lb)
- 36,000
- Basic empty weight (lb)
- 22,320
- Max landing weight (lb)
- 31,800
- Max takeoff weight (lb)
- 35,700
Most owners only have the POH. Here's the essential set for the Cessna Citation X.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
More Cessna Citation Xmanuals & documents
- Noise Abatement Departure Procedures (NADPs)Other Documents
- Citation X Options and UpgradesPerformance Data
- 2009 Cessna Citation X Specifications and SummarySpecifications
- 2008 Cessna Citation X Specifications & SummarySpecifications
- 2008 Cessna Citation XSystems Description
- Pilot’s Guide - Guide du PilotePilot's Operating Handbook
- AAIB Bulletin: 8/2007Other Documents
- 1998 Cessna Citation XChecklist
- Cessna Citation XLS - ElectricalWiring Diagram
In this document
Aircraft Highlights
The 1998 Cessna Citation X features Rolls Royce Corporate Care, WAAS/LPV capabilities, and ADS-B Out. The aircraft has a total time of 4,580 hours and 2,736 landings. It is powered by Rolls-Royce AE 3007C1 engines, with total times since new of 4,466 hours for engine #1 and 4,381 hours for engine #2. The APU is a Honeywell Model GTCP 36-150 with a total time since new of 3,306 hours.
Weight Specifications
The maximum ramp weight for the Cessna Citation X is 36,000 lbs, with a maximum take-off weight of 35,700 lbs and a maximum landing weight of 31,800 lbs. The maximum zero fuel weight is 24,400 lbs, while the empty weight is 21,710 lbs and the basic operating weight is 22,320 lbs. The aircraft can carry a maximum usable fuel of 13,031 lbs.
Avionics and Cockpit
The avionics system is the Honeywell Primus 2000, which includes dual Honeywell AZ-840 air data computers, a Honeywell AFIS DMU, and a Honeywell Primus 2000 autopilot. The cockpit is equipped with multiple communication and navigation systems, including dual Honeywell NV-850 NAV receivers and dual Honeywell XS-852 transponders.
Maintenance Programs & Inspection Status
The aircraft is maintained per MSG-3 and operated under FAR Part 91. It is enrolled in Rolls Royce Corporate Care and Aux Advantage for APU coverage. The last inspection was completed on March 2, 2018, at 4,433 hours, with various documents detailing the maintenance history and next due dates.
Interior and Cabin Features
The interior features an executive eight-passenger layout with forward and aft 4-place clubs, a forward galley, and an aft lavatory. It includes four Rosen swivel monitors for entertainment and multiple electrical outlets throughout the cabin.
Full document text
102A BROAD STREET • GUILFORD • CONNECTICUT • 06437 • 203-453-0800 • WWW.GUARDIANJET.COM 1 1998 Cessna Citation X N110PK S/N 750-0040 Specifications and Summary 102A BROAD STREET • GUILFORD • CONNECTICUT • 06437 • 203-453-0800 • WWW.GUARDIANJET.COM 2 1998 Cessna Citation X N110PK S/N 750-0040 OFFERED AT: MAKE OFFER AIRCRAFT HIGHLIGHTS: Rolls Royce Corporate Care WAAS/LPV – FMS 6.1 ADS-B Out Aux Advantage AVAILABLE: Immediately STATUS: As of June 1st, 2019 TOTAL TIME: 4,580 LANDINGS: 2,736 ENGINES: Rolls-Royce AE 3007C1 #1 #2 Total Time Since New: 4,466 4,381 Cycles Since New: 2,592 2,634 OVERHAUL DUE: 6,311.2 6,311.3 SERIAL NUMBER: 330083 330119 (Engines enrolled on Rolls Royce Corporate) APU: Honeywell Model GTCP 36-150 (CX) Serial Number: P-122 TSN: 3,306 HOT SECTION DUE: 7,717 (APU Hours) (APU enrolled on Aux Advantage) WEIGHT: MAX RAMP WEIGHT: 36,000 Lbs. MAX TAKE-OFF WEIGHT: 35,700 Lbs. MAX LANDING WEIGHT: 31,800 Lbs. MAX ZERO FUEL: 24,400 Lbs. EMPTY WEIGHT: 21,710 Lbs. BASIC OPERATING WEIGHT: 22,320 Lbs. MAX USABLE FUEL: 13,031 Lbs. CAPABILITIES: FM Immunity 8.33 Spacing RNP-10/5/1 Enhanced Flight Mode S MNPS BRNAV VNAV Emergency Descent Mode RVSM WAAS/LPV ADS-B OUT TCAS 7.0 102A BROAD STREET • GUILFORD • CONNECTICUT • 06437 • 203-453-0800 • WWW.GUARDIANJET.COM 3 AVIONICS & COCKPIT AVIONICS: Honeywell Primus 2000 Avionics System AIRBORNE FLIGHT INFORMATION SYSTEM: Honeywell AFIS DMU (VHF and Satcom) AIR DATA COMPUTERS: Dual Honeywell AZ-840 ADC AUDIO CONTROL PANELS: Dual Honeywell AV-850A Control Panels AUTOMATIC DIRECTION FINDER: Honeywell DF-850 ADF AUTOMATIC FLIGHT INFORMATION SYSTEM: Honeywell AFIS DMU (VHF and Satcom) AUTOPILOT / FLIGHT DIRECTOR: Honeywell Primus 2000 COCKPIT VOICE RECORDER: L3 A200S CVR (120 minutes) COMMUNICATIONS: Dual Honeywell TR-833 Com Modules (8.33 MHz) DATA ACQUISITION UNIT: Dual Honeywell DA-800 DAUs DATA LOADER: Honeywell DL-950 Data Base Loader DISTANCE MEASURING EQUIPMENT: Dual Honeywell DM-850 Modules ELECTRONIC FLIGHT INFORMATION SYSTEM: Honeywell Primus 2000 5-Tube w/ Dual EICAS Flight Director Systems with 8x7” DU-870 Electronic Flight Displays EMERGENCY LOCATOR TRANSMITTER: KANNAD 406 AF 3-Frequency ELT FLIGHT GUIDANCE CONTROLLER: Honeywell GC-810 FGC FLIGHT DATA RECORDER: Provisions Only FLIGHT MANAGEMENT SYSTEM: Dual Honeywell FMZ-2000 w/ 6.1 Software GLOBAL POSITIONING SYSTEM: Dual Honeywell HG2021GD04 GPS Sensor Units HIGH FREQUENCY: Dual Honeywell KTR-953 High Frequency Receivers INTEGRATED COMM UNITS: Dual Honeywell RCZ-833M Comm Units LONG RANGE NAVIGATION: Dual Honeywell Laser Inertial Reference Units NAVIGATION: Dual Honeywell NV-850 NAV Receivers (w/ FM Immunity) RADIO ALTIMETER: Honeywell RT-300 Radio Altimeter RADIO MANAGEMENT UNITS: Dual Honeywell RM-855 RMUs SELCAL: Avtech CSD-714 Selcal Decoder TERRAIN AWARENESS AND WARNING SYSTEM: Honeywell Mark V EGPWS w/ Wind Shear Detection TRAFFIC COLLISION AVOIDANCE SYSTEM: Honeywell TCAS II TPU-67A w/ Change 7.0 TRANSPONDER: Dual Honeywell XS-852 Enhanced Mode S Transponders WEATHER RADAR: Honeywell Primus WU-880 Weather Radar Transceiver YAW STAB COMPUTER: Dual Honeywell SZ-805 Yaw Stab Computers 102A BROAD STREET • GUILFORD • CONNECTICUT • 06437 • 203-453-0800 • WWW.GUARDIANJET.COM 4 ADDITIONAL EQUIPMENT ➢ Standby Gyro and HSI Indicator ➢ AOA Indicator/Indexer ➢ LED Wing Navigation Lights ➢ Tail Flood Light ➢ Locking Fuel Caps ➢ Dual ATSP-44 Nicad Ship Batteries ➢ EROS Oxygen Masks CABIN ENTERTAINMENT & COMMUNICATIONS ENTERTAINMENT Airshow 400 DVD Player Four Cabin Monitors COMMUNICATIONS Aircell ST-3100 Iridium Satellite Communication System (2) Aircell Phone Handsets MAINTENANCE PROGRAMS & INSPECTIONS STATUS MAINTENANCE & INSPECTIONS • Maintained Per MSG-3 • Operated FAR Part 91 • Rolls Royce Corporate Care • Aux Advantage (APU coverage) • Maintenance Tracking by CAMP/CESCOM INSPECTION LAST COMPLETED NEXT DUE Document 1 3/02/2018 @ 4,433 Hours 6,433 Hours Document 2 2/06/2019 @ 4,525 Hours 1/31/2020 Document 3 3/02/2018 @ 4,433 Hours 1/31/2020 Document 6 3/02/2018 @ 4,433 Hours 1/31/2027 Document 7 2/06/2019 @ 4,525 Hours 1/31/2020 Document 8 2/06/2019 @ 4,525 Hours 1/31/2020 Document 9 3/02/2018 @ 4,433 Hours 1/31/2020 Document 10 1/07/2018 @ 4,430 Hours 1/31/2020 Document 11 3/02/2018 @ 4,433 Hours 2/28/2021 Document 18 1/07/2018 @ 4,430 Hours 1/31/2020 Document 19 2/06/2019 @ 4,525 Hours 1/31/2020 Document 34 2/06/2019 @ 4,525 Hours 1/31/2020 Document MG 1/07/2018 @ 4,430 Hours 1/31/2020 Engine 1 Overhaul (4,500 hrs.) 1/29/2004@ 1811.2 Hours 6311.2 Hours Engine 2 Overhaul (4,500 hrs.) 4/29/2004@ 1811.3 Hours 6311.3 Hours 102A BROAD STREET • GUILFORD • CONNECTICUT • 06437 • 203-453-0800 • WWW.GUARDIANJET.COM 5 INTERIOR Forward Cabin INTERIOR DESCRIPTION Executive eight passenger interior with forward and aft 4-place clubs, forward galley with ample storage and aft lavatory. Four Rosen swivel monitors can be moved to any of the 8 passenger seat receptacle to monitor Airshow or DVD. Two electrical outlets in the cabin plus one in the lavatory and one in the cockpit. Forward Cabin looking Aft 102A BROAD STREET • GUILFORD • CONNECTICUT • 06437 • 203-453-0800 • WWW.GUARDIANJET.COM 6 INTERIOR Forward Cabin Forward Cabin looking Aft Forward Cabin looking Forward 102A BROAD STREET • GUILFORD • CONNECTICUT • 06437 • 203-453-0800 • WWW.GUARDIANJET.COM 7 INTERIOR Aft Cabin Aft Cabin looking Aft Aft Cabin looking Forward 102A BROAD STREET • GUILFORD • CONNECTICUT • 06437 • 203-453-0800 • WWW.GUARDIANJET.COM 8 GALLEY & LAVATORY Forward Galley Aft Lavatory 102A BROAD STREET • GUILFORD • CONNECTICUT • 06437 • 203-453-0800 • WWW.GUARDIANJET.COM 9 EXTERIOR EXTERIOR DESCRIPTION Painted January 2002 at Duncan Aviation, Lincoln Overall Snow White with Anisto Blue and Silver Platinum accent stripes This aircraft is being brokered by Guardian Jet, LLC. Prospective purchasers are encouraged to conduct their own independent pre-purchase inspection as
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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. 2019 06 10 / MB