- Registered owner
- Tsc Aircraft LLC
- Location
- Saint Louis, MO
- Owner type
- LLC
- Serial number
- 560-5671
- Year built
- 2006
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 12, 2006
- Certificate issued
- February 10, 2020
- Expires
- February 28, 2030
- Mode S code
- A25678
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 19
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 |
| 2006 | 2 |
| 2007 | 1 |
| 2010 | 2 |
| 2012 | 2 |
| 2013 | 2 |
| 2014 | 2 |
| 2017 | 1 |
| 2020 | 1 |
| 2023 | 1 |
| 2025 | 1 |
| 2026 | 1 |
See all 22 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 PW545B
SAIB 2024-06Oil Servicing Issues on Pratt & Whitney Canada PW545 Series EnginesHistorical bulletins · 2
NTSB investigations
No NTSB investigations matched to N25PPMatched 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 · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 9JLA2023041338728Unknown · unknownTHE MAINTENANCE TEAM FOUND DURING POST-FLIGHT CHECKS HYDRAULIC FLUID DRIPPING FROM THE LEFT MAIN LANDING GEAR WHEEL WELL. THE MAINTENANCE TEAM FOUND HYDRAULIC FLUID DRIPPING FROM THE LEFT EMERGENCY GEAR SHUTTLE VALVE. THE SHUTTLE VALVE WAS REMOVED, AND ALL THESDR 9JLA2022071938701Trim System · failedTHE FLIGHT CREW REPORTED THE PITCH TRIM DID NOT WORK WITH AUTO-PILOT ELECTRIC PITCH TRIM ON BOTH THE LEFT AND RIGHT SIDE BELOW 200KTS ON DESCENT. OPERATIONS WERE CONTINUED UNDER MEL 27-31-01. THE BASE MAINTENANCE TEAM DETERMINED THE ELEVATOR ELECTRIC TRIM MOTOSDR 9JLA2021121727643Relay · failedTHE FLIGHT CREW REPORTED THAT PILOTS SIDE PRIMARY FLIGHT DISPLAY POWERS UP WHEN AIRCRAFT BATTERY SWITCH IS TURNED TO THE ON POSITION. THE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE LEFT AVIONICS CONTACTOR (KZ001) WAS AT FAULT. THE CONTACTOR WAS REPLACED WSDR 9JLA2021090827639Battery Pack · inoperativeTHE MAINTENANCE TEAM DISCOVERED DURING MAINTENANCE CHECKS THAT THE FORWARD EMERGENCY LIGHT BATTERY INOPERATIVE. THE MAINTENANCE TEAM REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK WITH AN OVERHAULED UNIT. OPS CHECKS WERE SATISFACTORY. THE AIRCRASDR 9JLA2021073027637Wire · damagedTHE FLIGHT CREW REPORTED THAT DURING THE INITIAL CLIMB OUT THROUGH APPROXIMATELY 10000 FT MSL THE 5A LEFT WINDSHIELD CIRCUIT BREAKER TRIPPED, AND THE "WINDSHIELD FAULT - L" CAUTION ANNUNCIATOR ILLUMINATED. THE FLIGHT CREW RAN THE QRH PROCEDURE TO RESET CIRCUITSDR 9JLA2021051827629Check Valve · leakingTHE FLIGHT CREW REPORTED DURING PREFLIGHT CHECKS THE LOWER (L) PRE-CHECK LEVER WAS LEAKING FUEL. THE PLANNED FLIGHT WAS CANCELLED. THE MAINTENANCE VENDOR REMOVED AND REPLACED THE PRE-CHECK VALVE ASSEMBLY WITH A NEW UNIT. OPERATION AND LEAK CHECKS WERE SATISFACSDR 9JLA2020121827618Tube · damagedIT WAS DISCOVERED DURING A ROUTINE CHECK SOOT AROUND THE ACCESS PANEL FURTHER INVESTIGATION DETERMINED THAT THE LEFT ENGINE RUDDER-BIAS BLEEDAIR LINE HAD A HOLE CAUSED BY PROLONGED CONTACT WITH CAMLOCK RECEPTACLE FOR PANEL 321AAL IN THE AFT BAGGAGE BAY. P/N 66SDR 9JLA2020120227617Switch · faultyTHE FLIGHT CREW REPORTED THAT THE STABILIZER WOULD NOT FUNCTION DURING THE DESCENT FOR LANDING. THE LANDING WAS UNEVENTFUL. THE MAINTENANCE VENDOR DETERMINED THAT THE AIRSPEED SWITCH PN D45C-24 WAS FAULTY. A NEW AIRSPEED SWITCH WAS INSTALLED. OPERATIONS CH
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.
Earlier aircraft with this N-number · 1
This aircraft carried N25PP before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.