N845JS
Registered owner: THESE PRETZELS ARE MAKING ME THIRSTY LLC, NC (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.
17 reports on file, 1995-01-05 – 2025-12-09.
Part: UPLOCK SWITCH — OUT OF RIG (ZONE 700) · airframe 11,861 hrs · 7,761 cycles
GEAR SELECTED UP. GEAR WOULD NOT RETRACTâ¦.STILL HAD 3 GREEN, NO RED. SUCCESSFULLY RIGGED NLG UPLOCK SWITCH, OPERATIONAL CHECK GOOD
Part: BEARING — WORN (ZONE 300 ELEV) · airframe 11,493 hrs · 7,538 cycles
ABNORMAL VIBRATION IN THE CONTROL YOKE. THE VIBRATION INCREASED AS AIRSPEED INCREASED AND DIMINISHED WHEN AIRSPEED WAS DECREASED. COMPLETED GENERAL VISUAL INSPECTION OF THE AIRCRAFT EXTERIOR INCLUDING ALL GEARS & FLIGHT CONTROLS, FOUND EXCESSIVE PLAY ON LH ELEVATOR TRIM TAB & LH & RH PRECOOLER RAM AIR INLET DOORS. REPLACED ALL HARDWARE, OPS CHECK GOOD AS PER CE560XL AMM REF CHAPTER #27-32-03 & 36-11-01.
Part: AUTOPILOT SYS — MALFUNCTIONED (ZONE 100) · airframe 11,369 hrs · 7,467 cycles
AT FRA, A/P WOULD NOT ENGAGE AND THE MESSAGE AP FAIL APPEARED. RESET AND ENGAGED THE AUTOPILOT TWICE, BUT IT FAILED IMMEDIATELY BOTH TIMES. THE AIRPLANE KEPT PITCHING UP AGGRESSIVELY, SO, MOVED THE TRIM ALL THE WAY FORWARD MANUALLY, BUT THAT DIDNâT HELP. REDUCED THE POWER AND THE AIRPLANE STARTED TO PITCH DOWN AGGRESSIVELY.BOTH PILOTS HAD TO HOLD THE YOKE IN ORDER TO MAINTAIN CONTROL AND OVERCOME THE FORCES. EVENTUALLY, WAS ABLE TO MAINTAIN SOME CONTROL BY ADJUSTING THE POWER ENOUGH TO MAINTAIN ALTITUDE AND ATTITUDE.
Earlier reports · 1995–2024 · 14 reports
2024
Part: WARNING MESSAGE — ILLUMINATED (MLG) · airframe 10,951 hrs · 7,215 cycles
THE GEAR UNLOCK LIGHT DID NOT REMAIN EXTINGUISHED AFTER GEAR AND FLAP RETRACTION. THIS LED TO THE HYDRAULIC PRESSURE AND STAB MISCOMPARE CAUTION ANNUNCIATORS ILLUMINATING.
Part: OIL SYSTEM — LOW PRESSURE · airframe 10,895 hrs · 7,180 cycles
MASTER WARNING OIL PRESSURE LOW. OIL PRESSURE READING 0. LH ENGINE
2000
Part: MASTER CYLINDER — LACK OF LUBE (BRAKE SYS) · airframe 24,732 hrs · 32,225 cycles
CAPTAIN REPORTED THE RIGHT BRAKE PEDAL AS INOPERATIVE. MAINTENANCE INSPECTED THE SYSTEM, FOUND THE MASTER CYLINDER REQUIRED SERVICING. THE MASTER CYLINDER WAS SERVICED, SYSTEM BLED, WITH ALL INDICATIONS NORMAL.
Part: MASTER CYLINDER — LACK OF LUBE (BRAKE SYSTEM) · airframe 24,682 hrs · 32,176 cycles
CAPTAIN REPORTED THE RIGHT BRAKE PEDAL HAD NO PRESSURE DURING TAXI. MAINTENANCE INSPECTED THE SYSTEM AND FOUND THE MASTER CYLINDER NEEDED SERVICING. THE MASTER CYLINDER WAS SERVICED, SYSTEM BLED, WITH ALL INDICATIONS NORMAL.
Part: FIRE LOOP — MALFUNCTIONED (ENGINE) · airframe 24,556 hrs · 32,040 cycles
LEFT FIRE DETECTOR INDICATION SYSTEM WOULD NOT TURN OFF. THE FIRE LOOP WAS REPLACED AND ALL INDICATIONS NORMAL.
Part: MASTER CYLINDER — LOW (BRAKE PEDAL) · airframe 24,554 hrs · 32,038 cycles
CAPTAIN REPORTED THE RT CAPTAINS BRAKE PEDAL HAD NO PRESSURE. MAINTENANCE INSPECTED THE SYSTEM, SERVICED THE BRAKE MASTER CYLINDER, BLED THE SYSTEM. OPS CHECKED OK.
Part: HARNESS — BROKEN (LT ENGINE) · airframe 24,549 hrs · 32,033 cycles
CREW RETURNED TO THE FIELD AFTER THE LEFT ENGINE EGT STARTED TO FLUCTUATE. MAINTENANCE GROUND RAN WITH SRL OFF, NO FLUX NOTED. THE SYSTEM WAS DEFERRED. THE SYSTEM WAS INSPECTED AND FOUND A WIRE BROKEN AT THE ENGINE EGT SHORT LEAD. THE WIRE WAS REPLACED, ENGINE GROUND RAN WITH FLUCTUATIONS NOTED.
1998
Part: WINDOW — CRACKED (BS 187)
AIRCRAFT RETURNED TO FIELD DUE TO OUTER CABIN PANE AT SEAT 2A CRACKED AFTER TAKEOFF. THE OUTER PANE AND SEAL WERE REPLACED. (M)
1995
Part: CONNECTOR — DIRTY (RT ENGINE)
FLT NR 4145 - AFTER DEPARTURE, RIGHT ENGINE HAD LARGE FLUCTUATIONS IN RPM, EGT AND TORQUE. REDUCED POWER AND ENGINE STABILIZED, RETURNED TO FIELD. CLEANED CANNON PLUGS ON RIGHT ENGINE TORQUE SIGNAL CONDITIONER. GROUND RUN AND OPERATIONAL CHECK OF ENGINE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: TORQUE IND — FLUCTUATION (RT ENGINE)
FLT NR 4101 - ON CLIMB-OUT RIGHT ENGINE EXPERIENCED AN EGT AND TORQUE FLUCTUATION WITH SRL COMPUTER DEFERRED. RETURNED TO PIT, CONDUCTED GROUND RUNS ON ENGINE IAW MM 71-00-00. OPERATIONAL CHECK GOOD. UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M)
Part: ENGINE — MALFUNCTIONED (LT/RT)
FLIGHT NR 4032 - AIRCRAFT RETURNED TO GATE AFTER FLIGHT CREW NOTICED TORQUE FLUCTUATION BOTH ENGINES PRIOR TO TAKEOFF. PIT/MX CONDUCTED ENGINE GROUND RUNS IAW MM 71-00-00. OPS CHECK GOOD. UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M)
Part: PITOT TUBE — ICED UP (LEFT)
FLT 4094 - DURING TAKEOFF ROLL, CAPTAIN'S AIRSPEED INDICATOR STOPPED AT 68 KNOTS. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AIRCRAFT AND DISCOVERED ICE ACCUMULATION IN CAPTAIN'S PITOT TUBE, THEY THEN ACTIVATED PITOT HEATER SYSTEM TO THAW ICE FROM SYSTEM. CONDUCTED HIGH SPEED TAXI, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: DOWNLOCK SWITCH — DEFECTIVE (RT MLG)
FLT 4019 - DURING APPROACH AND PREPARATION FOR LANDING WHEN SELECTING GEAR DOWN, CREW NOTICED AN UNSAFE GEAR INDICATION ALL 3 LANDING GEAR LEGS. F/O VISUALLY CONFIRMED MAIN LANDING GEARS WERE DOWN AND LOCKED. NO EMERGENCY WAS DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND A DEFECTIVE DOWNLOCK MICROSWITCH RT MLG - REMOVED AND REPLACED DEFECTIVE COMPONENT. AIRCRAFT RETURNED TO SERVICE.
Part: PITOT HEAD — INOPERATIVE (LT FWD FUSELAGE)
FLT 4076 - DURING TAKEOFF ROLL, CAPTAIN NOTICED AIR SPEED INDICATOR REMAINED AT ZERO, TAKEOFF WAS ABORTED, AIRCRAFT RETURNED TO GATE. OUT STATION MAINTENANCE PREHEATED PITOT/STATIC SYSTEM TO MELT ANY POSSIBLE ICE ACCUMULATION IN PITOT HEAD. AIRCRAFT RETURNED TO SERVICE.