N104QS
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
DURING MAINTENANCE CHECK FOUND MAIN ENTRY EXIT LIGHTED SIGN INOPERATIVE.
MAIN DOOR: IN FLIGHT, PASSENGER DOOR AMBER MESSAGE ILLUMINATED ON AND OFF FOR ENTIRE FLIGHT. WE RAN THE QRH. NO PRESSURE SPIKES NOTED. FOUND INTERMITTENT CONNECTION BETWEEN PINS J AND K ON CONNECTOR P452. FOUND LOOSE SPLICE WIRE DAH0732W-22. REPAIRED SPLICE IN REFERENCE TO SPM 20-12-10. OPS CHECK GOOD AT THIS TIME. MESSAGES CLEARED AND DID NOT RETURN.
MAIN DOOR: WHILE PREPARING FOR ENGINE START WITH DOOR CLOSED .. PASSENGER DOOR CAS MESSAGE CAME ON 4 DIFFERENT TIMES. WE OPENED AND CLOSED DOOR BUT MESSAGE STILL CAME BACK. REMOVED AND REPLACED THE FORWARD AND AFT G LOCK AND THE OUTER HANDLE PROXIMITY SWITCH WIRING SPLICES. ADJUSTED AFT G LOCK PROXIMITY SWITCH TO .030 AND PERFORMED OPERATIONAL CHECKS NO FAULTS FOUND. ALL WORK DONE WITH REFERENCE TO G5000-AMM-52-70-01-00, G5000- SPM-20-16-05. RETURNED AIRCRAFT BACK TO ORIGINAL CONFIGURATION
PASSENGER DOOR AMBER CAS: DESCENDING THRU FL 180, PASSENGER DOOR AMBER CAS ILLUMINATED SEVERAL DIFFERENT TIMES, THEN REMAINED ON CONTINUOUSLY UNTIL LANDING AND PARKED. DOOR CLOSED NORMALLY AND PRESSURIZATION APPEARED NORMAL. FOUND FAULT CODE 3232117EL SEVERAL PINGS ON OMS, TROUBLESHOOT IAW WITH SMART FIX AND FOUND AFT G-LOCK HOOK IS LIKELY AT FAULT. REMOVED AFT G HOOK PROX SWITCH MT43 SWITCH IS OK TO INSTALL INSTALLED CUSTOMER SUPPLIED NEW PROX SWITCH IAW GLOBAL 5000 GVFD AMM 52-70-01 PERFORMED RIGGING OF AFT G HOOK SWITCH MT43 IAW GLOBAL 5000 GVFD AMM 52-70 PERFORMED OPERATIONAL CHECK OF PASSENGER DOOR WARNING SYSTEM 52·11-00.
MAIN ENTRY DOOR WILL NOT CLOSE WITH EITHER INSIDE OR OUTSIDE DOOR SWITCHES. WHEN EITHER SWITCH IS DEPRESSED, AFTER APPROX. :05 SECONDS, THE LOWER HINGED STEP FOLDS EXTREMELY SLOWLY, BUT DOOR MOTOR IS NOT RUNNING. REMOVED PASSENGER DOOR ACTUATOR DUE TO BURNED OUT MOTOR P/N: GS321-0591-9 S/N: G0807 AND INSTALLED REPAIRED UNIT AS LISTED ABOVE I/A/W GL5000 AMM 52-11-25. OPS CHECKED GOOD.
MAIN DOOR PRIMARY SEAL: AFTER TAKE OFF WE GOT A PASSENGER DOOR CAS. THE CAS FLASHED ON AND OFF SEVERAL TIMES AND THE PLANE WOULD NOT PRESSURIZE AT ALL.//CORRECTIVE ACTION// RE-RIGGED MAIN CABIN DOOR HANDLE PROX SWITCH, REPLACED FOOTBALL SPLICE DUE TO BROKEN WIRE. OPERATIONAL TEST CARRIED OUT ON MAIN DOOR OPS TEST GOOD REF GL 5000 AMM 52-70-01
MAIN DOOR: "PASSENGER DOOR" CAS MESSAGE CAME ON MULTIPLE TIMES IN FLIGHT, INCLUDING YELLOW DOOR SYMBOL ON SYNOPTIC PAGE. PRESSURE DIFFERENTIAL REMAINED NORMAL. PERFORMED GENERAL VISUAL INSPECTION OF MAIN CABIN DOOR, NO FAULTS NOTED. OPERATED DOOR THROUGH SEVERAL CYCLES . NO FAULTS FOUND, VERIFIED PROPER GAP AT EACH CABIN DOOR PROX SENSORS. ALL PROX SENSOR GAPS FOUND TO BE WITHIN ALLOWABLE TOLERANCE. PRESSURIZED ACFT WITH CABIN DOOR CLOSED AND MONITORED FOR FAULTS. NO FAULTS NOTED. MAIN CABIN DOOR AND DOOR WARNING SYSTEM FOUND TO OPERATE NORMALLY AT THIS TIME. IAW GL5OOOGVFD M/M 52-70-01, 52-11-00 AND 21-00-00
MAIN DOOR: PASS DOOR AMBER CAS CAME ON 9 TIMES AND WENT OUT EACH TIME MX CODE 3231117EL///SIGN-OFF///FOUND LOWER SWITCH OUT OF RIG. RIGGING FOUND TO BE 0.056. TECHS RERIGGED TO 0.039 INCH SPECIFIED TOLERANCE RANGE 0.030-0.050 INCH. OPS CHECK GOOD. IAW GL-5000 AMM 52-70-01.
MAIN DOOR: AFTER ROTATION PASSENGER DOOR AMBER CAS MESSAGE ILLUMINATED. DOOR SCHEMATIC ALSO CONFIRMED DOOR UNLOCK CONDITION . CAS MESSAGE CYCLED ON AND OFF FOR ENTIRE 15 MINUTE FLIGHT. FLEW UP TO 5000 FT FOR TERRAIN CLEARANCE AND THE AIRCRAFT DID NOT PRESSURE AT ALL DURING THE FLIGHT. UPON LANDING DOOR HANDLE CONFIRMED IN LOCKED POSITION. POWERED A/C AND WAITED FOR OMS TO LOAD. RECORDED FAULT CODE 3231117EL. RESEARCHED SFP AND FOUND FAULT POINTING TO SENSOR MT43 AFT G HOOK PROX SWITCH. ACCESSED SWITCH AND CHECKED GAP (APPROX 0.030) AND CHECKS GOOD. NOTICED SENSOR HEAD HAD SOME METAL DEBRIS. CLEANED SENSOR AND TARGET. OPERATED DOOR SEVERAL TIMES AND NO FAULTS. REMOVED SPLICE AND CHECKED WIRING, CHECKS GOOD. RE SECURE SPLICES AND ACCESS PANELS. OPERATED DOOR SEVERAL MORE TIMES AND CHECKS GOOD. WORK DONE IN REF GL5000 MM 52-70-01. NO ADJUSTMENT OR RIGGING WAS PERFORMED ON MED
CABIN FAILED TO PRESSURIZE IN FLIGHT. AIR COULD BE HEARD LEAKING PAST THE DOOR SEAL. COMPLIED WITH RIGGING CHECK WITH NO DEFECTS NOTED. IAW AMM 52-11-00 ALSO PERFORMED MULTIPLE OPERATIONAL TEST WITH NO DEFECTS NOTED. PERFORMED SATISFACTORY ACFT PRESSURIZATION ALL WORK DONE IAW AMM 52-11-00 & 21-31-00.
RIGHT POWER OUTLET IN GALLEY, BELOW OVEN CONTROLS, SPARKED & BURNED ANY DEVICE THAT WAS PLUGGED INTO IT. REMOVED DEFECTIVE GALLEY OUTLET & INSTALLED A NEW OUTLET. BEFORE INSTALLATION NOTICED THAT THE WIRES DID NOT MATCH TO THE LABELS GOING TO THE OUTLET. FOUND THAT THE WIRES WERE NOT LABELED CORRECTLY BUT ARE CONNECTED TO THE OUTLET CORRECTLY IAW WIRING DIAGRAM. REMOVED DEFECTIVE GFCI & INSTALLED NEW GFCI . OPS CHECKED GOOD. WORK PERFORMED IAW MM 24-00-00.