- Serial number
- 560-5563
- Year built
- 2005
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 23, 2005
- Certificate issued
- December 21, 2015
- Expires
- December 31, 2028
- Mode S code
- A73252
- Registered owner
- Tulsa Xls LLC
- Location
- Tulsa, OK
- Owner type
- LLC
Cessna 560XLTCDS A22CEAirframe · Cessna 560XLTCDS E00059ENEngine · Pratt & Whitney Canada PW545 series
From the FAA registry file of October 20, 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. Not a compliance determination.
| 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. Matched the same way as ADs.
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 N563CSMatched by N-number and event date. 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 N563CSMatched by N-number and event date. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Cessna 560XL aircraft
Service difficulty reports · 13
SDR 9JLA2022121632678Pressure Switch · defectiveTHE FLIGHT CREW REPORTED A STABILIZER MISCOMPARE ANNUNCIATOR ILLUMINATED WHEN COMMANDING FLAPS 0 TO 15 FOLLOWED THE QRH WHICH LED THE CREW PULLING THE STAB CONTROL CIRCUIT BREAKER. HYDRAULIC PRESSURE ANNUNCIATOR WAS FLASHING DUE TO STAB NOT MOVING. THE LANDINGSDR 9JLA2022102832674Overheat Sensor · defectiveTHE FLIGHT CREW REPORTED THAT THE APU SHUTS DOWN WHEN BLEED AIR LOAD WAS APPLIED. THE MAINTENANCE TEAM VERIFIED DISCREPANCY AND FOUND THE APU INLET TEMP SENSOR DEFECTIVE. THE SENSOR WAS REMOVED AND REPLACED WITH A NEW UNIT. OPS CHECKS WERE SATISFACTORY, AND THSDR 9JLA2022101432669Circuit Breaker · failedTHE FLIGHT CREW REPORTED THAT THE POWER BRAKE CIRCUIT BREAKER WOULD TRIP INTERMITTENTLY. THE MAINTENANCE BASE DETERMINED THAT THE POWER BRAKE CIRCUIT BREAKER WAS DEFECTIVE. THE CIRCUIT BREAKER WAS REMOVED AND REPLACED WITH A NEW BREAKER. OPERATIONAL CHECKS WERSDR 9JLA2022082332666Fire Loop · faultyTHE MAINTENANCE TEAM DISCOVERED DURING POSTFLIGHT CHECKS THE APU FIRE ANNUNCIATOR WOULD NOT ILLUMINATE DURING TEST. THE APU SYSTEM WAS DISABLED AND THE MAINTENANCE WAS DEFERRED, OPERATIONS CONTINUED UNDER MEL 49-20-01. DURING THE MAINTENANCE CORRECTIVE ACTIONSSDR 9JLA2022081132664Pcb · defectiveTHE MAINTENANCE TEAM DISCOVERED DURING PREFLIGHT CHECKS THAT THE APU FIRE LED LIGHT WAS INOP DURING APU FIRE TEST. THE SYSTEM FAULT WAS DEFERRED UNDER MEL 49-20-01 AND OPERATIONS WERE CONTINUED UNTIL MAINTENANCE COULD BE SCHEDULED. THE MAINTENANCE PROVIDER TRSDR 9JLA2022071232657Brake Assy · leakingDURING POST FLIGHT CHECKS THE MAINTENANCE TEAM DISCOVERED BRAKE FLUID LEAKING FROM THE BRAKE BOOST PUMP FILTER HOUSING. THE MAINTENANCE TEAM REMOVED AND REPLACED THE BRAKE BOOST PUMP FILTER HOUSING O-RING PER THE AMM. LEAK CHECKS WERE SATISFACTORY AND THE AIRCSDR 9JLA2021100717376Boot · leakingTHE FLIGHT CREW REPORTED THE RIGHT SIDE HORIZONTAL STABILIZER PNEUMATIC BOOT FAILS TO INFLATE AND HAS ASSOCIATED YELLOW MASTER CAUTION WHEN IN AUTO OR MANUAL MODES. CREW NOTED A BUBBLE AND AREA NOT INFLATING ON UPPER INBOARD AREA OF BOOT. THE MAINTENANCE TEAM SDR 9JLA2021090817375Relay · faultedTHE FLIGHT CREW REPORTED THE LEFT IGNITOR WOULD NOT TURN OFF INDICATING THAT THE CADENCE OF IGNITOR FIRING IS NOT NORMAL. THE MAINTENANCE VENDOR TROUBLESHOT AND REPLACED THE LEFT ENGINE IGNITION RELAYS KZ051, KZ053 AND KZ055. ENGINE GROUND RUNS WERE SATISFACTOSDR 9JLA2021090217373Relay · faultyTHE FLIGHT CREW REPORTED THAT DURING STARTING OF THE LEFT ENGINE FOR FLIGHT THE IGNITORS WOULD NOT TURN OFF. THIS CAUSED THE CREW TO SHUT THE ENGINE DOWN AND CANCELLING THE FLIGHT. THE MAINTENANCE TEAM DETERMINED THE KZ051 (P/N M6106/19-012) WAS DEFECTIVE. A NSDR 9JLA2021082017373Relay · failedTHE FLIGHT CREW REPORTED THE LEFT ENGINE IGNITORS WOULD NOT TURN OFF. THE MAINTENANCE TEAM DETERMINED THAT THE KZ051 RELAY CONTROLLING THE SYSTEM WAS AT FAULT. THE RELAY WAS REPLACED WITH A NEW UNIT AND OPERATIONAL CHECKS WERE SATISFACTORY. THE AIRCRAFT WAS RESDR 9JLA2021061817366Solenoid · multiple failTHE FLIGHT CREW REPORTED THAT DURING CLOSING THE CABIN DOOR FOR FLIGHT THE CABIN DOOR ANNUNCIATOR REMAINED ILLUMINATED. THE SCHEDULED FLIGHT WAS CANCELLED. THE MAINTENANCE VENDOR REPLACED THE DEFECTIVE MAIN DOOR VENT SOLENOID WITH AN NEW SOLENOID RIGGED AND RESDR 9JLA2021020411098Switch · defectiveTHE FLIGHT CREW REPORTED THAT THE LANDING GEAR WARNING HORN WOULD NOT TEST ON ROTARY CHECK. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THAT THE ROTARY TEST SWITCH WAS DEFECTIVE. THE SWITCH WAS REPLACED WITH A NEW UNIT. OPERATIONAL CHECKS WERE SATISFACTOSDR 9JLA2017083113068Solenoid · inoperativeTHE FLIGHT CREW REPORTED THAT DURING THE MAIN CABIN DOOR CLOSURE FOR FLIGHT THEY RECEIVED AN WARNING ANNUNCIATOR THAT THE MAIN CABIN DOOR VENT DOOR WAS INOPERATIVE. THE CABIN DOOR VENT SOLENOID WAS FOUND TO BE DEFECTIVE AND WAS REPLACED WITH A NEW UNIT.