- Registered owners
- Corporate Flight Management Inc DBAContour Aviation
- Location
- Smyrna, TN
- Owner type
- Corporation
- Serial number
- 560-5252
- Year built
- 2002
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- May 17, 2002
- Certificate issued
- December 16, 2025
- Expires
- December 31, 2032
- Mode S code
- A63F77
Cessna 560XLTCDS A22CEAirframe · Cessna 560XLTCDS E00059ENEngine · Pratt & Whitney Canada PW545 series
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada PW545 model are included below.
On this page
Airworthiness directives that may apply · 20
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1994 | 1 |
|---|---|
| 1998 | 1 |
| 2000 | 2 |
| 2001 | 2 |
| 2003 | 1 |
| 2006 | 2 |
| 2007 | 1 |
| 2010 | 2 |
| 2012 | 2 |
| 2013 | 2 |
| 2014 | 2 |
| 2017 | 1 |
| 2020 | 1 |
| 2023 | 1 |
| 2025 | 1 |
| 2026 | 1 |
See all 23 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
Airframe · Cessna 560XL
SAIB AIR-21-15R1Navigation SystemSAIB CE-10-29R1Lights Aft Side Ledger Divider LightSAIB NM-10-13Navigation: Flight Management SystemEngine · Pratt & Whitney Canada PW545 series
SAIB 2024-06Oil Servicing Issues on Pratt & Whitney Canada PW545 Series EnginesHistorical bulletins · 2
NTSB investigations
No NTSB investigations matched to N501UPMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Cessna 560XL aircraft
FAA incident reports
No FAA accident or incident reports matched to N501UPMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Cessna 560XL aircraft
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CVGA2025090603001Shuttle Valve · defectiveON APPROACH HAD NOSE GEAR UNSAFE INDICATION. NOSE GREEN LIGHT DID NOT TEST EITHER. LANDING GEAR UNSAFE EMERGENCY PROCEDURE USED TO BLOW DOWN LANDING GEAR. UNEVENTFUL LANDING. REMOVED NOSE GEAR HYDRAULIC SHUTTLE VALVE P/N 98120 SN 2046 AND INSTALLED OVERHAULED SDR CVGA20240103001Unknown · unknownEMERGENCY DECLARED ON LANDING. ON APPROACH GEAR DOWN SELECTED, R/H MAIN GEAR LIGHT DID NOT ILLUMINATE AND RED UNLOCK LIGHT WAS ILLUMINATED. DECLINED THE APPROACH CLEARANCE TO RUN THROUGH THE CHECKLIST COMPLETELY TO INCLUDE BLOWING THE NITROGEN BOTTLE. NEITHER SDR O2GA2020091850102Bracket · bentDURING CRUISE FLIGHT FELT A BANG FOLLOWED BY A RED LANDING GEAR UNLOCK ANNUNCIATOR AND HYDRAULIC PRESSURE ANNUNCIATOR LIGHT. EMERGENCY DECLARED. FOLLOWED CHECKLIST, LOWERED GEAR AND DIVERTED TO KPIT, LANDING WAS UNEVENTFUL. AIRCRAFT WAS FERRIED TO THE KGSOSDR O2GA2020091025101Shimmy Dampener · damagedAFTER TAKE-OFF THE LANDING GEAR RED UNLOCK LIGHT REMAINED ILLUMINATED, THE HYDRAULIC LIGHT WAS ILLUMINATED, AND THE STAB MIS-COMPARE LIGHT WAS ALSO ILLUMINATED. AFM CHECKLIST WAS FOLLOWED, EMERGENCY WAS DECLARED, AND DIVERSION WAS MADE TO AN ALTERNATE AIRPORTSDR O2GA2020072750101Position Switch · out of adjustSTAB MIS-COMPARE ANNUNCIATOR ILLUMINATED WHEN FLAP SELECTOR WAS SELECTED TO ZERO POSITION. AIRSPEED WAS BELOW 200 KYS. EMERGENCY DECLARED BY ATC AND DIVERTED TO ALTERNATE DESTINATION. MAINTENANCE ADJUSTED THE HORIZONTAL STABILIZER POSITION SWITCH. GROUND OPERASDR O2GA2020070250101Printed Ckt Board · inoperativeSTAB MIS-COMPARE ANNUNCIATOR ILLUMINATED AFTER FLAP RETRACTION DURING INITIAL CLIMB. AIRSPEED LIMITS WERE NOT EXCEEDED. HYD PRESS ANNUNCIATOR REMAINED ILLUMINATED UNTIL GEAR EXTENSION FOR LANDING. EMERGENCY WAS DECLARED AND AFM CHECKLIST PROCEDURE WAS FOLLOSDR O2GA202001190101Uplock Switch · defectiveON CLIMB OUT RED GEAR UNLOCK LIGHT ILLUMINATED FOLLOWED BY 'HYD PRESS' ANNUNCIATOR. FOLLOWED CHECKLIST, DIVERTED TO MCO, AIRPORT EMERGENCY RESCUE TEAM NOTIFIED AND WERE STANDING BY. LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED THE LEFT AND NOSE GEAR UP-LOCK SWSDR O2GA2019012450101Engine · overtempRIGHT ENGINE FIRE ANNUNCIATOR ILLUMINATED IN FLIGHT. FOLLOWED CHECKLIST AND LIGHT EXTINGUISHED. EMERGENCY DECLARED AND DIVERTED TO KDAL. MAINTENANCE REPLACED 4 DEFECTIVE BLEED AIR WIGGINS CLAMPS. DURING ENGINE RUNUP AND OPERATIONAL CHECK NOTED RIGHT ENGINE ITTSDR O2GA2016120650101Brake Sys · contaminatedAIRCRAFT HAD TO BE REPOSITIONED POST MAINTENANCE FOR FUELING. WHEN CHOCKS WERE PULLED AIRCRAFT STARTED MOVING AND WOULD NOT STOP USING NORMAL BRAKING. EMERGENCY BRAKE APPLIED TO STOP AIRCRAFT WITHOUT ANY FURTHER INCIDENT. CIRCUIT BREAKERS FOR POWER BRAKES AND SDR O2GA2016120150101Control Valve · defectiveDURING PREFLIGHT INSPECTION, THE ACM OVERHEAT ANNUNCIATOR ILLUMINATED WHILE APU WAS RUNNING. E6/E5 FAULT CODE ON TEMPERATURE CONTROLLER. SMOKE IN COCKPIT OBSERVED. MAINTENANCE TROUBLESHOT THE DISCREPANCY TO A FAULTY RIGHT COCKPIT TEMPERATURE CONTROL VALVE. INSDR O2GA2016011350101Hinge Pin · backed outAIRCRAFT HAS BAD VIBRATION THROUGH YOKE & RUDDER PEDALS. VIBRATION GETS MUCH WORSE WITH INCREASE IN AIRSPEED. POWER SETTINGS MODE MADE NO DIFFERENCE. TROUBLE SHOT THE DISCREPANCY TO A DEFECTIVE RUDDER LOWER TRIM TAB HINGE PIN THAT BACKED OUT CAUSING THE VIBSDR O2GA2015121050101Unknown · malfunctionedAFTER TAKEOFF THE FLAPS WOULD NOT RETRACT TO 0*. DURING FLIGHT ALL OTHER HYD SYS WORKED. ACFT DIVERTED BACK & AFTER LANDING THE FLAPS WOULD NOT RETRACT TO 0*. ON POST FLIGHT NOTICED FLAP STUCK IN 7* POSITION. ACFT WAS INSPECTED & FERRIED WITH THE FLAPS AT SDR O2GA2015090450101Actuator · defectiveON CLIMB OUT, WHEN FLAPS WERE SELECTED UP THE STAB MISCOMPARE & HYD PRESS ANNUNCIATOR LIGHTS REMAINED ILLUMINATED. CREW COMPLETED THE STAB MISCOMPARE LIGHT ON ABNORMAL CHECKLIST & DIVERTED BACK. DURING THE RETURN & COMPLETING THE CHECKLIST THE HYD PRESS & GE
STCs that may be installed · 114
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Cessna 560XL
STC ST01305WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.STC ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC ST01823WIInstallation of Garmin GTS Traffic Sensor with Garmin GTX 3000 Mode S Transponders with ADS-B Out.