- Registered owners
- 5437 Holdings LLCWagnew LLC
- Location
- Houston, TX
- Owner type
- Co-owned
- Serial number
- 560-5015
- Year built
- 1998
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 30, 1998
- Certificate issued
- April 6, 2026
- Expires
- April 30, 2033
- Mode S code
- A727A6
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 N560HNMatched 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 N560HNMatched 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 · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 9JLA2016110710774Computer · faultyWHILE IN THE CRUISE STAGE OF FLIGHT AT FL 410 THE FLIGHT CREW EXPERIENCED AN ENGINE FAILURE OF THE NR ENGINE. THIS OCCURRED AS THEY CAME OUT OF CROSS FEED GOING FROM THE LEFT TANK TO THE RIGHT ENGINE. THE ENGINE JUST FLAMED OUT, AND N2 ROLLED ITSELF BACK TO 11SDR 9JLA2016112210769Pcb · defectiveFLIGHT CREW REPORTED THAT DURING FLIGHT THEY RECEIVED A STAB MISCOMPARE ANNUNCIATOR ILLUMINATED AND WOULD NOT EXTINGUISH AFTER SEVERAL CYCLES OF THE FLAPS. TROUBLESHOOTING IDENTIFIED THE TWO-POSITION HORIZONTAL STAB PCB N2017 DEFECTIVE. THE PCB WAS REPLACED WISDR 9JLA2016102010768Circuit Board · failedTHE FLIGHT CREW REPORTED INTERMITTENT TROUBLE WITH THE NR 1 ENGINE NOT STARTING. MAINTENANCE TROUBLESHOT AND FOUND THE START CONTROL PCB WAS DEFECTIVE. THE DEFECTIVE PCB WAS REMOVED AND A NEW PCB INSTALLED P/N 6318324-5SDR 9JLA2014031103596Processor · defectiveCREW REPORTED THE TCAS SYS FAILED IN FLIGHT. TROUBLE SHOT & FOUND THE TCAS PROCESSOR DEFECTIVE. REPLACED THE PROCESSOR WITH A MODIFIED CONDITION UNIT. FUNCTIONAL TEST SATISFACTORY.SDR 9JLA2014030703590Computer · failedCREW REPORTS THAT IN FLIGHT AT FL270 AN ATT & HDG FAIL INDICATION WAS DISPLAYED ON THE PILOTS PFD. FMS HAS AHRS NR 1 INPUT FAIL, AHRS HDG FAIL DISPLAYED AS MSG. REPLACED THE NR 1 AHRS COMPUTER & INSTALLED A REPAIRED UNIT.SDR 9JLA2014021703590Ahrs · defectiveCREW REPORTED THAT IN FLIGHT AT FL270 THEY RECEIVED A ATT & HDG FAIL ON PILOTS PDF & FMS HAD AHRS 1 INPUT FAIL, AHRS HDG FAIL MASSAGES. TROUBLESHOOTING FOUND THE NR 1 AHRS DEFECTIVE, THE DEFECTIVE UNIT PN 142185-1100 SN 1135 WAS REMOVED & A REPAIRED UNIT WAS SDR 9JLA2014013003586Hydraulic Line · failedAFTER ARRIVING AT THEIR DESTINATION & DURING THEIR POST FLIGHT INSPECTION THEY NOTED FLUID LEAKING FROM AN AFT FUSELAGE DRAIN & DETERMINED THAT IT WAS HYD FLUID. HYD RETURN LINE LOCATED IN THE HYD FILTER PANEL AREA FAILED CAUSING THE LEAK. THE FAILED HYD RETSDR 9JLA2014013003583Uplock · stiffAFTER DEPARTURE & THE GEAR WAS RETRACTED THE RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED, INDICATING THAT ONE OR MORE OF THE LG WERE NOT IN THE UP POSITION. THE LG WAS CYCLED SEVERAL TIMES & EACH TIME FAILED TO RETRACT PROPERLY. THE GEAR WAS EXTENDED & SINCE SDR 9JLA20131217545Carbon Seal · defectiveDURING THE POST FLIGHT CHECKLIST ON DEC 10TH IT WAS DISCOVERED THAT THE OIL LEVEL FOR THE NR 1 ENG WAS BELOW THE INSPECTION SIGHT GLASS WITH OIL STREAKING PRESENT IN THE BYPASS DUCT. THE TROUBLESHOOTING FOR THE DEC 10TH OIL LEAK EVENT FOUND THAT THE OIL LEAK WSDR 9JLA2013120403577Display · inoperativeTHE CREW REPORTED THAT THE MULTI-FUNCTION DISPLAY WAS INOPERATIVE. THE MFD WAS REMOVED PN 7014300-901 SN 96031332 & A REPAIRED UNIT WAS INSTALLED. FUNCTIONAL CHECKS WERE SATISFACTORY IAW CITATION 560XL AMM 34-26-00.SDR 9JLA2013081603573Switch · faultyFLIGHT CREW REPORTED THAT THE "ACC DOOR UNLOCK", TAIL ANNUNCIATOR LIGHT ILLUMINATED. MX TROUBLESHOOTING IDENTIFIED THE AFT BAGGAGE DOOR AFT SWITCH WAS DEFECTIVE PN A4-1130. INSTALLED A NEW SWITCH. REF: WDM 33-20-01. FUNCTIONAL CHECKS SATISFACTORY.
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.