N830JS
Registered owner: ROSS ADVISORS LLC, FL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| EXCLUSIVE JETS LLC (3EJA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
6 reports on file, 1997-07-01 – 2026-02-06.
Part: SWITCH — DIRTY (THRUST REVERSERS) · airframe 10,696 hrs · 6,735 cycles
ON DEPARTURE AT 2000 FEET T/R LIGHT ARM, AND UNLOCKED CAME ON, WITH ASSOCIATED HYDRAULIC PRESSURE CAS MESSAGE. CLEANED AND INSPECTED TR SWITCHES, FUNCTION CHECK, NDF
Part: THRUST REVERSER — FAULTED (ZONE 400) · airframe 10,408 hrs · 6,571 cycles
AT ABOUT 14,000 FEET. THE THRUST REVERSER ARM LIGHT CAME ON, WITH ASSOCIATED MASTER CAUTION, AND MASTER WARNING, AND HYDRAULIC PRESSURE. TROUBLE SHOT THRUST REVERSER SYS AND COULD NOT DUPLICATE ISSUE
Part: PRESSURE SWITCH — FAILED (ZONE 800) · airframe 10,306 hrs · 6,512 cycles
COULD NOT CONTROL AIRCRAFT CABIN PRESSURE DURING CLIMB IN MANUAL MODE AND DUMP SWITCH ON USING THE CABIN ALTITUDE UP AND DOWN SWITCH. R&R DOOR SEAL DIFFERENTIAL PRESSURE SWITCH.
Part: SWITCH — FAILED (ZONE 800) · airframe 10,306 hrs · 6,512 cycles
ON CLIMB OUT GOT AT KGPI HAD A DOOR SEAL STEADY YELLOW CASS MESSAGE. REMOVED AND REPLACED DOOR SEAL DIFFERENTIAL PRESSURE SWITCH P/N P18M-30 S/N 5313. INSTALLED "INSPECTED" PRESSURE SWITCH P/N 18M-30 S/N 2527.
Part: WARNING MESSAGE — ILLUMINATED (ZONE 800) · airframe 10,177 hrs · 6,431 cycles
DURING CRUISE FLIGHT AT FL400, WE RECEIVED A CAS MESSAGE âCABIN DOOR. PERFORMED OPERATIONAL AND LEAK CHECKS ON MAIN CABIN DOOR SEAL IAW CESSNA MODEL 560XL AMM 52-10-04, NO DEFECT NOTED. TESTS GOOD.
Part: ENGINE — LOW TORQUE (LEFT ENGINE)
LEFT ENGINE FAILED TO MAKE TARGET TORQUE 98 PERCENT. RUN-UP FAILED TO DUPLICATE.