N434QS
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
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.
8 reports on file, 2021-02-08 – 2026-07-19.
Part: WINDSHIELD — NO DISCREPANCY (ZONE 200) · airframe 6,606 hrs · 5,064 cycles
ON CLIMB OUT, NOTICED WHAT LOOKS TO BE A HAIRLINE CRACK IN CENTER PANE OF THE CAPTAIN`S WINDSHIELD. LOOKS LIKE THE CRACK EXTENDS FROM THE A-PILLAR TO THE CENTER OF THE WINDSHIELD. RETURNED TO DAL FOR FURTHER INSPECTION. COMPLETED INSPECTION OF CAPTAINS WINDOW, CLEANED WINDOW NO CRACKS DETECTED IAW MM 56-11-00.
Part: BATTERY — UNKNOWN (ZONE 200) · airframe 7,311 hrs · 5,679 cycles
EMERGENCY LIGHTS STAY ON WHEN EMERGENCY LIGHT ARE IN ARM POSITION. SHUT AIRPLANE DOWN, DISCONNECTED GPU. TURNED BATTERIES BACK ON, STARTED AN ENGINE, SAME ISSUE, EMERGENCY LIGHTS STAYING ON WHEN SWITCH IS IN ARM POSITION. TROUBLESHOOT AND FOUND NO DISCREMPENCIES. REPLACED 2 EMERGENCY BATTERIES PER MCC OPS CHECKED GOOD
Part: POWER SUPPLY — FAULTY · airframe 6,013 hrs · 4,615 cycles
EMER EMER LIGHT NOT ARM CAS MESSAGE REMAINS ON WITH EMERGENCY LIGHT SWITCH IN ARM POSITION. REMOVED AND REPLACED FWD AND AFT EMERGENCY POWER SUPPLY IAW AMM33-52-01. ALL OPS CHECK GOOD NO CAS MESSAGES PRESENT.FWD E-BATTERY TESTED BY RADIANT POWER CORP., REF.FORM 8130-3, FTN:64038.
Part: LIGHT — UNKNOWN (CABIN) · airframe 4,246 hrs · 3,258 cycles
CABIN EMERG LIGHT: EMER LIGHTS BEGAN TO BLINK IN FLIGHT. ONLY REMEDY WAS TO TURN OFF EMER LIGHTS. PERFORMED NJA TC-505-33-200403 DATED 04/23/20 EMER LIGHT TOP CHARGE. INSPECTED ALL EMER LIGHTS AND NONE WERE FLICKERING. PERFORMED OPS CHECK OF LIGHTING TWICE AND NO FLIKERING. WORK DONE !AW NJA TASK CARDS AND MM 33-52-01.
Part: NONE — NONE · airframe 2,155 hrs · 1,669 cycles
MAIN DOOR: UPON OPENING MAIN CABIN DOOR , IT FALLS DOWNWARD WITH EXCESSIVE FORCE CAUSING EXTREME VIBRATION OF DOOR HANDLES. ***VERIFIED FAULT PERFORMED ADJUSTMENT OF MAIN CABIN DOOR OPENING SPEED I/A/W PHENOM 300 AMM 52-10-00-820-804-A AND MAIN DOOR AFT TELESCOPING ROD IAW PHENOM 300 AMM 52-12-25-820-801-A. NO FURTHER DEFECTS FOUND AT THIS TIME
Part: SUPPORT — OUT OF ADJUST (PAX DOOR) · airframe 1,787 hrs · 1,380 cycles
MAIN DOOR: MED REQUIRES ADDITIONAL EXCESSIVE FORCE TO OPEN BEYOND 1/2 WAY. TELESCOPING SUPPORTS APPEAR UNEVEN DURING EXTENSION.
Part: SUPPORT — MALFUNCTIONED (PAX DOOR) · airframe 1,787 hrs · 1,380 cycles
MAIN DOOR: MED REQUIRES ADDITIONAL EXCESSIVE FORCE TO OPEN BEYOND 1/2 WAY. TELESCOPING SUPPORTS APPEAR UNEVEN DURING EXTENSION. // SIGNOFF // SMOOTHED TELESCOPING~ ROD, APPLIED WIRICANT, OPS OLECK GOOD, REF PHENOM 300 AMM 52-12·23
Part: BATTERY PACK — DEFECTIVE · airframe 1,434 hrs · 1,124 cycles
CABIN EMERG LIGHT: UNDER NORMAL ELECTRICAL POWER, WITH THE EMERGENCY LIGHT SWITCH IN THE ARM POSITION, ALL EMERGENCY LIGHTS ARE ILLUMINATED.///SIGN-OFF///REMOVED AND REPLACED EMERGENCY BATTERIES ON RH RACK AND COCKPIT. IAW EMB AMM 33-52-01-01-010. OPS CHECK GOOD.