2002 Cessna X
Single Engine Piston
Aircraft Details
Seller reportedAvionics & Equipment
Avionics Package: Honeywell Primus 2000 Comm Radios: Dual Honeywell RCZ-833M CVR: Fairchild 2100 DME: Dual Honeywell DM-850 EFIS: Honeywell DU-870 5-tube FMS: Dual Honeywell FMZ-2000 w/6.1 software Hi Frequency: Dual Honeywell KHF-1050 IRS: Dual Honeywell LASEREF IV Navigation Radios: Dual Honeywell RNZ-850 Radar Altimeter: Honeywell RT-300 TAWS: Honeywell Mark V EGPWS TCAS: TCAS-2000 TCAS-II w/change 7.1 Transponder: Dual Honeywell XS-857A Weather Radar: Honeywell Primus 880
Description
This Citation X has been actively operating under a mix of FAR Part 91 and Part 135, making it a versatile, proven platform for both private and charter-oriented missions. With strong dispatch reliability and a pedigree of consistent operational readiness, this Citation X is built to go to work immediately. Call today for more details.
Engine
AE3007C1 Engine 1: 15,838 hours / 9,336 cycles Engine 2: 16,712 hours / 9,923 cycles Engines Enrolled on Rolls Royce Corporate Care
Interior
Double club configuration for 8 passengers AFT non-belted lavatory
Exterior
Newly repainted in 2025
Modifications / STCs
• APU: GTCP-150 15,572 hours / 15,747 cycles APU Enrolled on Honeywell MSP
• Gogo AVANCE L5 high speed internet Airshow 4000 Forward galley with coffee maker
Description and equipment details provided by the seller. AeroGurus does not verify seller-provided information.
Price Comparison 1 active offer
| Source | Price | Location | Listed | Days on Market | Status | Action |
|---|---|---|---|---|---|---|
|
jetAVIVA
jetaviva.com
|
Contact for Price
|
CA | May 05, 2026 | — | Active |
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AeroGurus Data & Analysis
Independent data from FAA, NTSB, and market analysis
About This Cessna X
This 2002 Cessna X is a single engine piston with 17,530 hours on the airframe.
NTSB records show 0 incidents for this airframe — a clean safety record. There are 10 airworthiness directives applicable to this aircraft type — review AD compliance carefully before purchase. Mechanics have filed 10 service difficulty reports for this type — common maintenance items to discuss during pre-buy.
Pre-Purchase Checklist
Ownership & Registration
Registration number not available.
Location & Ownership
Title Status
No FAA title records
Available for US-registered aircraft only
Source: FAA Aircraft Registry, FAA Civil Aviation Registry (DocIndex). Title data may be delayed. Always verify with an aviation attorney before purchase.
Safety Record
NTSB safety data coming soon.
Airworthiness Directives — Cessna X
ADs are mandatory safety instructions issued by the FAA. 10 recent ADs found for this aircraft type.
Textron Aviation, Inc. (Type Certificate Previously Held by Cessna Aircraft Company) Airplanes
View full AD →Textron Aviation Inc. (Type Certificate Previously Held by Cessna Aircraft Company) Airplanes
View full AD →Textron Aviation, Inc. (Type Certificate Previously Held by Cessna Aircraft Company) Airplanes
View full AD →Textron Aviation Inc. (Type Certificate Previously Held by Cessna Aircraft Company) Airplanes
View full AD →Textron Aviation Inc. (Type Certificate Previously Held by Cessna Aircraft Company) Airplanes
View full AD →Textron Aviation, Inc., (Type Certificate Previously Held by Cessna Aircraft Company) Airplanes
View full AD →Textron Aviation Inc. (Type Certificate Previously Held by Cessna Aircraft Company) Airplanes
View full AD →Source: FAA Airworthiness Directives database. Showing most recent ADs for this aircraft type.
Service Difficulty Reports — Cessna X
SDRs are reports filed by mechanics about problems found during maintenance. 10 recent reports for this aircraft type.
POTTY DECK CORRODED. REPAIRED POTTY DECK PER NETJETS RFTS-116581 REV.0 TITLE: N678QS (560-5616) TOILET DECK SKIN CORROSION DATED 10MAR26. THIS IS A PERMANENT MINOR REPAIR.
RH WINGTIP SKIN UNDER OTBD STATIC WICK BASE IS HEAVILY CORRODED. COMPLIED WITH NETJETS RFTS-116596 REV.0 TITLE: N678QS (560-5616) WING TIP STATIC WICK BASE CORROSION DATED 11MAR26. THIS IS A PERMANENT MINOR REPAIR.
CREW REPORTED WHEN THE GEAR UP THE GEAR DIDN'T RETRACT AND ALL THREE GREEN REMAINED. PLACE GEAR HANDLE IN THE DOWN POSITION AND RETURN TO DEPARTURE AIRPORT OF KCHS WITHOUT INCIDENT.
EMERGENCY LIGHTS STAY ON WHEN EMERGENCY LIGHTING SWITCH PLACED IN THE ARMED POSITION. RECYCLED POWER ON AIRCRAFT WITH SAME RESULTS. ACCESSED AFT EMERGENCY LIGHTING BATTERY PACK, REMOVED ACCESS PANEL LOCATED IN AFT L/H SIDE CLOSET, FOUND G SWITCH TR...
ON TAKEOFF JUST AFTER ROTATION, PILOT REPORTED SIGNIFICANT VIBRATION FROM LEFT WING. PILOT TAPPED BRAKES AND VIBRATION STOPPED AND PILOT ASSUMED BLOWN TIRE ON LH WHEEL. UPON LANDING IT WAS NOTED THAT THE TIRE WAS STILL INFLATED BUT 3/4 OF THE TREAD...
A SEGMENT OF THE FLOOR EMERGENCY LIGHTING IS INOPERATIVE BELOW SEAT THREE. DURING T/S GAINED ACCESS TO THE LT AISLE EMERGENCY LIGHT HAD FEW LED LIGHT WERE OUT. REMOVED INOP EMERGENCY LIGHT AND INSTALLED A NEW LED LIGHT ASSY. OPS CHECKED GOOD. REF...
WHEN OPENING OR CLOSING THE MAIN CABIN DOOR YOU CAN HEAR AND PHYSICALLY FEEL THAT SOMETHING IS BINDING. IT HAPPENS WHEN YOU OPEN THE DOOR IS ABOUT 3/4 OPEN AS WELL AS ALMOST CLOSED VERIFIED PROPER TENSIONS OF PAX DOOR COUNTERBALANCE FWD AND AFT CAB...
AFTER FLIGHT WITH APU ON IT TAKES UP TO 30 SECONDS FOR SEAL TO DEFLATE ENOUGH TO ALLOW OPENING OF THE MAIN CABIN DOOR. SUBSEQUENTLY AFTER FLIGHT WITH APU ON IT TAKES UP TO 10 SECONDS FOR SEAL TO DEFLATE ENOUGH TO OPEN THE MAIN CABIN DOOR. REMOVED FA...
HIGH SPEED REJECTED TAKE OFF IN APF, LOSS OF DIRECTIONAL CONTROL AS AIRCRAFT ACCELERATED TO V1 DUE TO A DRAGGING LEFT MAIN MOUNT. DRAG DUE TO EITHER A HUB/BEARING FAILURE OR BRAKING SYSTEM FAILURE ALLOWING LEFT BRAKE TO STICK. THE BRAKE WAS REMOVED...
CREW AND PASSENGERS NOTICED THE SMELL OF EXHAUST AFTER THE APU WAS STARTED ON THE DECENT FOR LANDING. MAINTENANCE WAS CALLED TO TROUBLESHOOT THE CAUSE AFTER LANDING. ON INSPECTION, THEY FOUND THE APU TURBINE HOUSING HAD A CRACK IN IT AT ABOUT THE 5 O...
Source: FAA Service Difficulty Reporting System. Shows maintenance issues reported by mechanics for this aircraft type.