N245JX
Registered owner: DELUX PUBLIC CHARTER LLC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| DELUX PUBLIC CHARTER LLC (4DPA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
ISSUE-CREW REPORTED E2 ANTI ICE FAILâ CAUTION WHEN PERFORMING ICE TEST ON CLIMB OUT. RETURNED TO DAL DUE TO ICING IN SKX. CORR ACTION- MX FOUND PRESSURE TRANSDUCER LINE CAME DISCONNECTED. CONNECTED LINE ALL PERFORMED OPS TEST AND ALL OPS TESTS GOOD.
CREW REPORTED-ONCE WE LEVELED OFF AT 15,000 FT WE DECREASED POWER TO MAINTAIN A CERTAIN SPEED. AS SOON AS WE DECREASED OUT POWER A LOUD AND STRONG VIBRATION COULD BE FELT THROUGHOUT THE AIRCRAFT. WE ASSUMED IT WAS THE PACKS DUE TO SOME PROBLEMS LIKE PACK OVERHEAT BUT NOT ANYTHING BIG. WE RECEIVED NO WARNINGS OR CAUTIONS ON THE EICAS. THE VIBRATION AND NOISE WOULD INCREASE WITH WHEN POWER WAS ADDED AND DECREASE WHEN POWER WAS DECREASED. WE WORKED THROUGH WHAT WE THOUGHT IT WAS AND RAN THE ASSOCIATED CHECKLIST FOR IT AND NOTHING CHANGED. CORR ACTION- MX PERFORMED A GVI OF EXTERIOR NO DEFECTS NOTED. JSX DECIDED T FERRY AIRCRAFT TO MRO FOR FURTHER INVESTIGATION. MRO MX PERFORMED A FLAP ZERO RIG CHECK NO DEFECTS AND PERFORMED A LANDING GEAR DOOR GAP CHECK LH MLG DOOR REQUIRED ADJUSTMENT AIRCRAFT RTS'D.
CREW WITNESSED A HYD 1 LO QTY CREW AWARENESS ADVISORY APPEARED IN FLIGHT. FLUID QUANTITY ON HYDRAULIC SYSTEM NUMBER 1 INDICATED IN THE AMBER. DETERMINED NO MX ON STATION IN T89 SO CREW ELECTED TO RETURN TO AUS TO HAVE MX ACTION COMPLETED. CORR ACTION- MX DETERMINED SYSTEM 2 OVER SERVICED AND SYSTEM 1 LOW. MX TECH BALANCED THE SYSTEM AND SERVICED HYD SYSTEM AS REQUIRED. AIRCRAFT RELEASED
ISSUE; CREW REPORTED #1 HYD LOW MESSAGE, ABOUT AN HOUR LATER RECEIVED A #1 ENGINE DRIVEN PUMP FAIL MESSAGE WHICH WAS FOLLOWED BY #1 ELECTRIC MOTOR DRIVEN PUMP (EMDP) FAIL MESSAGE. CREW RAN QRH CONTACTED ATC AND DIVERTED TO IAH. CREW ALSO HAD TO USE THE FREE FALL HANDLE TO LOWER THE GEAR. AIRCRAFT LANDED NO FURTHER ISSUES.CORR ACTION; R&R'D BOTH #1 ENGINE DRIVEN HYD PUMP AND THE EMDP LEAK AND OPS TEST GOOD. FREE FALL REQUIRED THGE GEAR TO BE SWUNG BUT NO JACKS AVAILABLE IN IAH. JSX PINNED AND SAFETIED THE GEAR AND PERFORMED A MX FERRY TO DAL WHERE THE GEAR SWINGS WERE ACCOMPLISHED ALL CHECKS WERE ACCOMPLISHED AND CHECKED GOOD.
ENGINE #2 FIRE INDICATION IN FLIGHT DURING DESCENT. SHUT ENGINE DOWN AND USED BOTTLE A. UPON INSPECTION/TESTING, FOUND THAT THE FIRE CONTROL MODULE HAD FAILED. FIRE MODULE CONTROL UNIT WAS REMOVED AND REPLACED AND THE SYSTEM WAS OPS CHECKED GOOD. THE FIRE BOTTLE WAS ALSO REMOVED AND REPLACED DUE TO BEING USED.
APU COWLING ASSY FWD MID SKIN LAP LWR CORNER EDGE HAS CURLED UP EDGE AT STA 26461.57. STRAIGHTENED SKIN, PERFORMED HFEC NO DEFECTS NOTED AT THIS TIME. INSTALLED DOUBLER 2.1" X 2.4" REF EMBRAER TECHNICAL DISPOSITION ETD2020-145-022629 REV.:/ DTD JULY 21, 2020. AND EMB 145 SRM 53-32-17. REV 59 DTD 28 JUNE 2019.