- Serial number
- 560-5646
- Year built
- 2006
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- August 29, 2006
- Certificate issued
- July 28, 2021
- Expires
- July 31, 2028
- Mode S code
- A5F840
- Registered owner
- Whitefish Investment Partners LLC
- Location
- Frisco, TX
- Owner type
- LLC
From the FAA registry file of October 20, 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. Not a compliance determination.
| 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. 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 PW545B
SAIB 2024-06Oil Servicing Issues on Pratt & Whitney Canada PW545 Series EnginesHistorical bulletins · 2
NTSB investigations
No NTSB investigations matched to N484JCMatched 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 N484JCMatched 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 · 2
SDR 2008FA0000553Line · rupturedHYDR FLEXIBLE LINE TO THE LT LANDING GEAR DOOR ACTUATOR RUPTURED DURING FLIGHT. LOSS OF FLUID CAVITATED LT AND RT ENG DRIVEN HYDR PUMPS. LINE RUPTURED IN SIDEWALL NEAR SWAGED END FITTING FOR CONNECTOR. PRESSURE IS 3000 PSI CONSTANT. NO LANDING GEAR ACTUATISDR 2008FA0000552Line · rupturedHYDR FLEXABLE LINE TO RT MLG DOOR ACTUATOR RUPTURED DURING FLIGHT. LOSS OF FLUID CAVITATED RT AND LT ENGINE DRIVE HYDR PUMPS. LINE RUPTURED IN SIDEWALL NEAR SWAGED END FITTING FOR CONNECTOR. PRESSURE IS 3000 PSI CONSTANT. NO LANDING GEAR ACTUATION WAS IN P