N145QS
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| NETJETS AVIATION, INC. (DXTA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
LINING UP FOR TAKEOFF WE GOT AN AMBER CAS MESSAGE "R EMER DOOR" AND AN EMER DOOR OPEN ICON ON THE AIRCRAFT STATUS PAGE. POST FLIGHT WE OBSERVED THE EXTERIOR EMERGENCY DOOR HANDLE IS NOW PUSHED INWARD. ON ARRIVAL TO ACFT, INSPECTED EMERG EXIT DOOR HANDLE FROM OUTSIDE & VERIFIED HANDLE TO BE PUSHED INWARD. INSPECTED INNER HANDLE & FOUND HANDLE TO BE OUT OF LOCKED POSITION. OPENED EMERG EXIT & INSPECTED. NO DEFECTS. REINSTALLED EMERG EXIT & VERIFIED CASS MESSAGE EXTINGUISHED. INSPECTED BOTH OUTER HANDLE WAS FLUSH & INNER HANDLE SEATED. INSERTED GROUND LOCKING PIN, NO ISSUES. INTERIOR PANELS WERE FLUSH. ALL WORK COMPLETED IAW MM 52-21-00. OPS CHKD SAT.
CABIN SMOKE: SMOKE IN THE CABIN AND COCKIT FOLLOWED BY L PAC FAIL AMBER CAS MSG. OCCURED ON TAXI OUT. // SIGNOFF // REMOVED AND REPLACED L PACK AIR CYCLE MACHINE IAW GL6000 AMM 21-52·09. OPS CHECKS AND LEAK CHECKS GOOD. P/N OFF: GG431-2010-3"S/N OFF: 01315- P/N ON: GG431-2010·3'S/N ON: 01564.-
1 HYDRAULIC RESERVOIR: DURING TAKEOFF ROLL. HYD 1 LO QTY CAS CAME ON FOLLOWED BY HYD 1 LO PRESS. TAKEOFF WAS ABORTED. FURTHER INVESTIGATION FOUND HYD 1 RES LEVEL SHOWED 0%. ALSO HYD FLUID IS VISIBLE UNDER LEFT ENGINE. REMOVED AND REPLACED #1 HYDRAULIC SYSTEM PRESSURE HOSE ASSY P/N GD478-1126-1 WITH NEW HOSE ASSY P/N GD478-1126-1. REMOVED AND REPLACED #1 HYDRAULIC SYSTEM RETURN HOSE ASSY P/N AR1048-16 WITH NEW HOSE ASSY P/N AR1048-16. REMOVED AND REPLACED #1 HYDRAULIC SYSTEM CASE DRAIN FILTER P/N AC014F8 WITH CUSTOMER SUPPLIED NEW FILTER P/N ACC314F8. REMOVED AND REPLACED #1 HYDRAULIC SYSTEM PRESSURE FILTER P/N ACC314F12 WITH CUSTOMER SUPPLIED NEW FILTER P/N ACC314F12. SERVICED AND BLED HYDRAULICS. OPS AND LEAK CHECK GOOD. REINSTALLED FWD. LOWER PYLON ACCESS PANEL 412 AB. NO FURTHER DEFECTS NOTED. ALL WORK DONE IAW GL6000 AMM 29-12-21, 29-12-13, 29-10-00, 29-12-25.
MAIN DOOR WILL NOT CLOSE USING INTERIOR OR EXTERIOR SWITCHES. SIGNOFF. REPLACED FAILED PASSENGER DOOR ACTUATOR P/N GS321-0591-9 S/N F0455 AND INSTALLED THE DOOR ACTUATOR, IAW AMM 52-11-25-4000/000-801. PERFORMED A SATISFACTORY OPERATIONS CHECK, IAW BD 700 AMM 52-11-00-710-801.
MAIN CABIN DOOR MOTOR ACTUATOR FAILED TO BRAKE DURING OPENING OF THE CABIN DOOR WHILE THE AIRCRAFT WAS IN MAINTENANCE. DOOR EXTENDED AT A RAPID UNCONTROLLED RATE AND DAMAGED THE DOOR STRUTS AFTER REACHING FULL EXTENSION.
HORIZ STAB FAIL ANNUNCIATOR LIGHT ILLUMINATED INFLIGHT. T/S SYSTEM FOUND LT HEAT HORN IN-OP. REMOVED AND REPLACED LT HEATER HORN WITH NEW OPS CHECKS GOOD ALL WORK IAW MM 30-11-00.
WITH AUTOPILOT CONNECTED RED (AP PITCH TRIM FAIL) ANNUNICTOR ILLUMINATED. WITH AP ON WE HEARD AN INTERMITTENT CLICK ( LIKE WHEN A CB POPS) BUT ALL CB'S ARE IN. [07-23-07] COMPLETED COMPLETE TRIM SYSTEM OPERATIONAL CHECK IN NORMAL EMERGENCY AND AUTO-PILOT. ACCESSED PITCH TRIM ACTUATOR CLEANED, LUBED AND OEPRATED ACTUATOR NO DEFECT NOTED AT THIS TIME ALL WORK IAW 400XP 27-40-00 & 12-20-00.
AFTER LANDING, THE LEFT WHEEL ASSEMBLY WAS SMOKING AND GIVING OFF HEAVY ODOR OF HOT BRAKES OR HOT RUBBER. NO NOTICEABLE CONTROL ISSUES DURING TAXI AFTER LANDING. INSPECTED LT WHEEL AND BRAKE ASSY WITH NO DEFECTS NOTED. PERFORMED TAXI CHECK WITH NO SMOKE OR ODORS NOTED. OK FOR CONTINUED SERVICE. REF HAWKER 400XP M/M 32-40-00.
RT MLG DOWN AND LOCKED LIGHT DID NOT ILLUMINATE WHEN GEAR SELECTED DOWN. RAN THE CHECKLIST, ALTERNATE GEAR EXTENSION PROCEDURE WAS NOT NECESSARY. LANDED WITHOUT INCIDENT AND THE LIGHT CAME BACK ON STEADY AFTER TOUCH DOWN. REPLACED RH MAIN GEAR DOWN LOCK SWITCH WITH NEW CUSTOMER SUPPLIED SWITCH. ADJUSTED DOWN LOCK SWITCH AND CYCLED GEAR NUMEROUS TIMES, OPS TEST GOOD. ALL WORK IAW 400XP MM 32-10-00 AND WIRING 32-61-00
AFTER GEAR HANDLE WAS SELECTED UP, GREEN NOSE INDICATION REMAINED ILLUMINATED, IT SOUNDED LIKE THE NOSE GEAR WAS STILL DOWN. LANDING WAS UNEVENTFUL. JACKED AIRCRAFT, INSP NLG AREA. OPERATED GEAR CYCLE 15 TIMES. OPENED NLG DOORS, DISCONNECTED DRAG STRUT. INSP STRUT & ATTACHING COMPONENTS. CHECKED FREEDOM OF MOVEMENT. NO DISCREPANCIES NOTED. RECONNECTED DRAG STRUT & GEAR DOORS. CYCLED GEAR THROUGH SEVERAL TIMES. CHECKED EMERGENCY GEAR LOWERING & STRUT SERVICING WITH NO DEFECTS. WORK ACCOMPLISHED IAW HAWKER 400XP MM 32-20-00.