N220QS
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
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.
3 reports on file, 2023-08-16 – 2026-01-16.
Part: BULB — BURNED OUT (ZONE 200) · airframe 8,982 hrs · 4,925 cycles
RIGHT FORWARD EMERGENCY LIGHT INOP. R & R DEFECTIVE FORWARD EMERGENCY LIGHT BULB AND PERFORMED OPS CHECKS, NO DEFECTS NOTED. WORK DONE IAW MM 33-51-04. LENS IS SEALED AND CURED.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 7,004 hrs · 3,816 cycles
PARKING BRAKE: WHEN COMING INTO LAND ON APPROACH THE PARKING BRAKE SOV CASS AND ANTI SKID INOP CASS ILLUMINATED WHILE ON APPROACH AND WENT ON AND OFF THREE TIMES! WE WENT AROUND AND RAN THE CHECKLIST WHICH ALOUD US TO LAND WITH USING NO BRAKES AND ONLY THE TRS! THE LIGHTS WENT OUT UPON LANDING AND WE HAD NO FURTHER EVENTS!
Part: DETECTOR — DEFECTIVE (OVERSPEED) · airframe 6,877 hrs · 3,741 cycles
FLAPS FAIL AMBER CAS: UPON SELECTING FLAPS 20° TO COMMENCE APPROACH, THE AMBER COLORED FLAPS FAIL CAS MESSAGE ILLUMINATED . FLAPS DID NOT MOVE FROM THE FULLY RETRACTED POSITION. QRH PROCEDURES FOR FLAPS FAIL AMBER CAS MESAAGE WERE COMPLETED. NO CHANGE IN FLAP POSITION ONSERVED. FLAPS FAIL APPROACH QRC AND FLAPS FAIL LANDING QRC WERE COMPLETED. SUCCESSFUL ZERO FLAP LANDED CONDUCTED AT LOS ANGELES INTERNATIONAL AIRPORT // SIGNOFF // GAINED ACCESS TO REMOVED OUTBOARD FLAP HINGE FAIRING AND OUTBOARD FLAP BUTE DOOR. REMOVED AND REPLACED L/H ASYMMETRY/OVERSPEED DETECTOR UNIT AND REPLACED WITH A REPAIRED UNIT. PERFORMED OPERATIONS CHECK OF THE FLAP SYSTEM, NO DEFECT NOTED. SYSTEM OPERATIONS CHECKED GOOD. WORK PERFORMED IAW CL-650 AMM 27-51-07-000-801¿ AND 27-51-07-720-801. INSTALLED ASYMMETRY/OVERSPEED DETECTOR UNIT WAS REPAIRED AT MOOG AIRCRAFT GROUP, CERTIFICATE NUMBER ND13344K, UNDER WORK ORDER NUMBER 5800712969, DATED 19 JUN, 2023. GAINED ACCESS TO REMOVED OUTBOARD FLAP HINGE FAIRING AND OUTBOARD FLAP BUTE DOOR REMOVED AND REPLACED R/H ASYMMETRY/OVERSPEED DETECTOR UNIT AND REPLACED WITH A REPAIRED UNIT. PERFORMED OPERATIONS CHECK OF THE FLAP SYSTEM, NO DEFECT NOTED. SYSTEM OPERATIONS CHECKED GOOD. WORK PERFORMED IAW CL-650 AMM 27-51-07-000-801¿ AND 27-51-07-720-801. INSTALLED ASYMMETRY/OVERSPEED DETECTOR UNIT WAS REPAIRED AT MOOG AIRCRAFT GROUP, CERTIFICATE NUMBER ND13344K, UNDER WORK ORDER NUMBER 5800712125, DATED 24 FEB 2023.