N572QS
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
UPON DEPARTURE AFTER FLAP RETRACTION AT ABOUT 1000' NOTICED A STRONG BURNING SMELL IN COCKPIT AREA. DID NOT SEE SMOKE, LOOKED BACK IN CABIN AREA AND ALSO DID NOT SEE SMOKE, DID NOT GET ANY CAS MESSAGES NOR AUDIO WARNINGS , JUST A STRONG BURNING ODOR THAT STAYED UNTIL AFTER LANDING , AT WHICH TIME THE ODOR DIMINISHED BUT DID NOT ENTIRELY DISSIPATE. RESEARCHED PREVIOUS MAINTENANCE DONE AND THE MM DOES NOT CALL OUT FOR 'AIR DUCT BURN IN'. LOOKED UP NJA COMPLY 365 AND FOUND TC-68A-21-181006MR3 ENVIRON CONTROL SYS BLEED AIR DUCT BURN OUT. ACCOMPLISHED TC-68A-21-181006MR3 ENVIRON CONTROL SYS BLEED AIR DUCT BURN PROCEDURE. REMOVED HEPA FILTER & INSTALLED NEW UNIT IAW M/M 21-70-10. OPS CHKD GOOD.
ACCOMPLISHED REMOVAL OF CORROSION TO AFFECTED AREAS OF VERTICAL STABILIZER. INSPECTED THE REMAINING MATERIAL USING ULTRASONIC TESTING AND EDDY CURRENT FOR CRACKS. NO CRACKS NOTED. ACCOMPLISHED DOUBLER REPAIR TO ONE NOTED LOCATION AND RESTORED FINISH TO ALL SURFACES. ALL WORK ACCOMPLISHED IAW NETJETS RFTS-117010 REV 0 DATED: 21APR26 - N572QS (680A-0113) LH & RH VERTICAL STABILIZER CORROSION.
DISBONDS ON THE UPPER WINGS BETWEEN THE OUTBOARD END OF STRINGERS AND THE COMMON SKIN DOUBLERS. THE SKIN AND COMMON DOUBLERS MAY ALSO EXHIBIT A GRADUAL DEVIATION FROM CONTOUR IN THESE REGIONS. THE EXTENT OF THE DEFECT IS LOCATED USING ULTRASONIC INSPECTION AND CORRECTED BY ADDING FASTENERS AND ADHESIVE TO THE DISBONDED AREAS. REFERENCE FIELD REPAIR SR-680A-ATA57-47522 REV- DATED: 05/MAR/2025.
EMERGENCY LIGHT INOP UNDER LAV TOE KICK PANEL. GAINED ACCESS TO LAV RH VANITY EXIT INDICATOR TO CHECK FOR VOLTAGE AND PROPER INSTALLATION OF EXIT LIGHT ASSY. IAW AMM 33-50-00. ACCOMPLISHED OPS CHECK OPS CHECK GOOD.
CABIN EMERG LIGHT: FORWARD EMERGENCY LIGHTS WILL NOT EXTINGUISH. VISUALLY INSPECTED #1 AND #2 BATTERY COMPARTMENT, NO DEFECT NOTED. VISUALLY INSPECTED ALL THE BREAKERS OF THE JBOX FROM THE CARGO BAY AREA NO DEFECT NOTED. REMOVED PANEL #244BR FROM THE COCKPIT AND RESET G SWITCH AND REINSTALLED PANEL #244BR EMERGENCY LIGHTS EXTINGUISHED IAW AMM 33-50-11. PUT SOME LOAD ON THE CIRCUIT, HYD PUMPS TURNED ON, ALL THE LIGHT, AND MADE A FULL CYCLE OF THE FLAP (ELECTRICAL), OPS CHECK GOOD.
FUSELAGE STRUCTURE: A VIBRATION ON THE FLOOR, UNDER OUT FEET AND ON THE GLARESHIELD IN COCKPIT WAS OBSERVED IN OUR CLIMBOUT @15000' AND ONCE LEVEL AT 17000' IT CONTINUED AS SPEED INCREASED TO @270KTS. WE SLOWED TO @250 AND IT SEEMED TO GET A LITTLE BETTER BUT VIBRATION STILL APPEARED TO BE THERE. AT FL300 VIBRATION WAS NOT AS PRONOUNCED AND AS WE DESCENDED AT SPEED 280 THE VIBRATION FELT LIKE IT HAD DIMINISHED CONSIDERABLY, AND PARTICULARLY AT LOWER ALTITUDES. IT IS TO NOTE THAT OUR FIRST LEVEL OFF ON DEPARTURE AT 2000' WE DID NOT FEEL ANYTHING UNTIL THE MID- TEENS (ALTITUDE). A CURSORY CHECK OF SYSTEM SYNOPSIS OR ENGINE READINGS DID NOT REVEAL ANYTHING OUT OF THE ORDINARY
CABIN EMERG LIGHT: LAV EMER LIGHT AND LAV "EXIT" EMER LIGHT WILL NOT EXTINGUISH. /// CORRECTIVE ACTION /// VERIFY DISCREPANCY FOUND EMERGENCY LIGHT ON LAV ON. RESET LAV EMERGENCY LIGHT BATTERY G-SWITCH AND RUN THE AIRCRAFT FOR 2 HOURS TO TOP CHARGE EMERGENCY LIGHT BATTERY ALL WORK IAW CESSNA 680 AMM REF 33-50-00.
L/H MLG ACTUATOR SIDE BRACE FITTING (PN: 6922928-3) IS GOUGED FROM CONTACT WITH THE ACTUATOR. GOUGE IS ON THE INTERNAL SURFACE THAT DOES NOT HAVE A PROTECTIVE WEAR PLATE INSTALLED. IT WAS REPAIRED PER TEXTRON AVIATION ENGINEERING MEMO DQ32221M1 DATED NOV 3, 2021. THE REPAIR WAS DEEMED MINOR IN SCOPE.
THE NOSE LANDING GEAR WHEEL WELL IS CRACKED ON LH AND RH SIDES AT APPROXIMATELY FS 75. CRACK DAMAGE IS TYPICALLY SEEN ON THE TOP WEB PN: 7413133-10, LH DOUBLER PN: 7413133-15, RH DOUBLER PN: 7413133-16, AND FRAME PN: 7413133-59. REPAIR ACCOMPLISHED IAW TEXTRON AVIATIONS INC. STANDARD REPAIR SR-680A-ATA53-25890. REPAIR IS MAJOR IN SCOPE AND APPROVED BY FAA FORM 8100-9 SUBMITTAL LETTER NO. 20-0804 DATED 06/01/2020.
R/H MLG ACTUATOR SIDE BRACE FITTING (PN: 6922928-4) IS GOUGED FROM CONTACT WITH THE ACTUATOR. GOUGE IS ON THE INTERNAL SURFACE THAT DOES NOT HAVE A PROTECTIVE WEAR PLATE INSTALLED. IT WAS REPAIRED PER TEXTRON AVIATION ENGINEERING MEMO DQ32221M1 DATED NOV 3, 2021. THE REPAIR WAS DEEMED MINOR IN SCOPE.
RH ENGINE AGB REAR COVER HAS MULTIPLE AREAS OF CORROSION.
LH ENGINE AGB REAR COVER HAS MULTIPLE AREAS OF CORROSION.