N578QS
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
CLIMBING OUT FLIGHT LEVEL 230 IN MCT STILL. IN ICING CONDITIONS ALL ANTI-ICE ON. AT APPROXIMATELY THREE MINUTES THE A/I ENGINE COLD L ILLUMINATED, AND DID NOT EXTINGUISH. WE INITIATED THE QRH AND ACCOMPLISH IT. THE LIGHT REMAIN ILLUMINATED THEN EXTINGUISH WITH THE L ENG BLD AIR HP SELECTED. WE EXIT ICING CONDITIONS AND PROCEED TO DESTINATION. NEXT FLIGHT WAS TO KLAS AND IT WAS IFR WITH RAIN. CORRECTIVE ACTION: REMOVED AND REPLACED #1 ENGINE INLET COWL ANT- ICE PRESSURE REGULATING SHUTOFF VALVE WITH CUSTOMER SUPPLIED UNIT IN ACCORDANCE WITH CESSNA 6B0A AMM 30-20-05. OPS AND LEAK CHECKS GOOD. INSTALLED VALVE INSPECTED BY C&L AVIATION SERVICES LLC, CERT# J2SR196J, WO# X1124, 24/DEC/2025
CABIN DOOR OPEN ANNUNCIATOR DID NOT EXTINGUISH AFTER CLOSING. THE VENT DOOR WAS NOT HEARD CLOSING. DURING ABNORMAL PROCEDURE THE CHECK HANDLE/PUSH TO OVERRIDE LIGHTS DID NOT ILLUMINATE DURING RESET. POWER UP ANOMALIES PROCEDURE DID NOT CORRECT ISSUE. REMOVED FAILED PASSENGER DOOR INNER HANDLE SWITCH SC009 PN: 8250915-1 AND INSTALLED CUSTOMER SUPPLIED NEW SWITCH PN: 8250915-1. OPS CHECK GOOD NO FURTHER DEFECTS NOTED. WORK DONE IAW AMM 52-10-16.
ACFT STARTED TO PULL RT. IT APPEARED TOTJE CREW THAT THE RT BRAKE WAS DRAGGING. . PULLED TO THE RT GOT STRONGER SO WE TOOK THE CLOSEST TAXI WAY AND THE LAST 30 FEET IT WAS OBIVIOUS WE NEEDED TO STOP. APPROX 100 YARDS OF TRAVEL FROM FIRST NOTICE TO STOPPING. REMOVED TEMP INSTALLED RH MLG WHEEL ASSEMBLY AND INSTALLED RH MLG WHEEL ASSEMBLY WITH TIRE IAW MM 32-41-02. SERVICED RT MLG TIRE IAW MM 12-13-03.
CABIN EMERG LIGHT: EMERGENCY LIGHTING ABOVE SEAT 10 ACROSS FROM MAIN ENTRY DOOR DOES NOT ILLUMINATE DURING TEST. RAN APU DURING PREFLIGHT CHECKED LIGHT AGAIN AFTER APU WAS SHUT DOWN. IT ILLUMINATED. THEN AFTER CHECKING OIL COMPLETED TEST AGAIN TO CONFIRM AND THE LIGHT WOULD NOT ILLUMINATE. // SIGNOFF // TC-FLT-33-1001 (CESSNA 680 / 680A/ 700 I EMBRAER EMERGENCY LIGHTING POWER SUPPLY BATTERY EXERCISE PROCEDURE)
EMER LIGHTS REPORTED BEING ON. // SIGNOFF// T/5 UGHTS FOUND PEDISTAL G-SWITCH TO BE TRIPPED, RESET G-SWITCH PERFORMED TC-FLT-33-1001 TO VERIFY CONDMON OF BATTERIES NO DEFECTS NOTED IAW CE-680A AMM CHAPTER 33-50-00
MAIN EXIT SIGN/LIGHT: THE EXIT SIGN OVER THE MAIN CABIN DOOR AND THE LIGHT UNDER SEAT 10 WILL NOT EXTINGUISH WITH ALL POWER REMOVED FROM THE SYSTEM. THIS IS A REPEAT WRITE UP. RESET THE FWD #1 G-SWITCH IN THE PEDESTAL. CHARGED EMEREGENCY LIGHT BATTERIES IAW NJA 'TASK CARD TC-FLT-33-1001. PERFORMED THE OPERATIONAL TEST OF THE EMERGENCY LIGHTING SYSTEM. SYSTEM OPS CHECKS GOOD AT THIS TIME. REF. CE-680A AMM 33-50-11.
NLG: UPON GEAR RETRACTION ON TAKEOFF AMBER HASHES THROUGH NOSE GEAR INDICATION FOLLOWED BY AMBER GEAR DISAGREE CAS MESSAGE. FOLLOWED QRH AND SELECTED GEAR HANDLE DOWN. LANDED THE A/C WITH NO FURTHER ISSUES. NLG DOOR ADJUSTMENT AND TEST WAS PERFORMED AND ADJUSTED AS REQUIRED SEE SQWK 4.4 OF THIS WORK ORDER FOR DETAILS. INSPECTED NLG DOOR HINGES FOR AND LOOSE HARD WARE OR CRACKS NO FAULTS FOUND. PERFORMED MULTIPLE GEAR SWINGS WITH DOORS ATTACHED AND DETACHED WHILE INEBRIATING ARES LIVE VIEW WITH NO FAULTS FOUND BOTH CHANNELS OF THE UPLOCK SWITCH ARE BEING TRIGGERED AS REQUIRED AND UP AND LOCK LIGHT ILLUMINATES AS REQUIRED. PERFORMED CHECK OF THE NLG CENTERING GEAR CENTERS AS REQUIRED WHEN HANDLE IS SELECTED GEAR UP. VERIFIED NLG STRUT SHOCK STRUT EXTENSION FOUND WITHIN LIMIT 9.72IN AND CHECKED NITROGEN SERVICING ON THE NLG STRUT BOTH HIGH AND LOW SIDE FOUND TO BE AT THE CORRECT PSI. VERIFIED HYDRAULIC ACCUMULATOR AND RESSIVOIR PRESSURE WITHIN LIMITS RESCUED ALL ACCESS GAINED AND DOWNED JACK AIRCRAFT. WORK PERFORMED IN REF TO CE-680A AMM 12-10-52, CE-680A AMM 12-10-30, 12-10-35, CE-680A AMM 52-80-05, 32-00-00,CE-680A AMM 7-10-10 AND CE-680A AMM 31-33-00.
EMERGENCY LIGHTING: EXTERIOR AND INTERIOR EMERGENCY LIGHTING DOES NOT WORK WHEN ON GROUND POWER OR BATTERY. IN OFF POSITION EMERGENCY LIGHTING NOT ARMED CAS MESSAGE ILLUMINATES, IN ARM POSITION EMERGENCY LIGHT INTERIOR LIGHTS BLINK FOR ONE SECOND, IN THE ON POSITION INTERIOR AND EXTERIOR EMERGENCY LIGHTS DO NOT WORK.///SIGN-OFF///RESET THE EMERGENCY LIGHTING INERTIA SWITCH. IAW CE680A AMM 33-50-11. OPS CHECK GOOD.
THE ACCESSORY GEARBOX REAR COVER IS CORRODING ON THE FLANGES AND AROUND BOLT HOLES. ACCOMPLISHED STEPS (1) THRU (4) OF THE REPAIR OF CORROSION OR PITTING ON ABG MOUNT PADS AND EXTERNAL SURFACES. INSPECT AGAIN AND REPEAT STEPS (1) THRU (4) AT EVERY AIRCRAFT MINOR INSPECTION UNTIL A PERMANENT REPAIR IS PERFORMED IAW P&WC 306D1 MM 72-60-01 REV. 17.1. PER NETJETS A, REINSPECTION ALIGNS WITH THE 1A (800 HR) AIRFRAME INSPECTION.
THE ACCESSORY GEARBOX REAR COVER IS CORRODING ON THE FLANGES AND AROUND BOLT HOLES. ACCOMPLISHED STEPS (1) THRU (4) OF THE REPAIR OF CORROSION OR PITTING ON ABG MOUNT PADS AND EXTERNAL SURFACES. INSPECT AGAIN AND REPEAT STEPS (1) THRU (4) AT EVERY AIRCRAFT MINOR INSPECTION UNTIL A PERMANENT REPAIR IS PERFORMED IAW P&WC 306D1 MM 72-60-01 REV. 17.1. PER NETJETS A, REINSPECTION ALIGNS WITH THE 1A (800 HR) AIRFRAME INSPECTION.
CABIN EMERG LIGHT: ON PREFLIGHT WHEN ARMING EMERGENCY LIGHTS SWITCH TO ARM THEY DO NOT COME ON . BY MOVING THE SWITCH TO ON EMER LIGHTS DO COME ON . FOUND G SWITCH TRIPPED ON #1 EMERGENCY BATTERY, RESETT G SWITCH, LIGHTS WENT OUT, CHARGED BATTERY FOR 2 HOURS, PERFORMED EMERGENCY LIGHTING ADJUSTMENT TEST I.A.W CE·680A M/M CHAP 33-50-00, OPS CHECK SATISFACTORY, CONTACTED NJA AMCC WITH RESULTS WAS ADVISED AIRCRAFT IS O.K TO RELEASE.
MAIN EXIT SIGN/LIGHT: THE MAIN CABIN DOOR EXIT LIGHT AND THE LIGHT UNDER SEAT 10 REMAIN ILLUMINATED WITH BATTERIES DISCONNECTED AND EMERGENCY LIGHT SWITCH OFF. OPEN
WITH THE EMERGENCY LIGHT SWITCH IN THE ARM POSITION, THESE LIGHTS DO NOT ILLUMINATE: EXIT SIGN AT REAR OF CABIN, READING LIGHT OVER LAV, TOE KICK LIGHT UNDER LAV, EXIT INDICATOR ON FRONT OF LAV & THE READING LIGHT OVER THE COUCH SEAT. SIGN OFF. CHECKED AND RESEATED FUSES ON ALL FOUR EMERGENCY LIGHTS BATTERIES, EMERGENCY LIGHTS OPERATIONS CHECK GOOD IN ON POSITION WITH A/C BATTERIES DISCONNECTED. OPERATIONS CHECK GOOD, IAW CITATION MODEL 689A AMM 33-50-00.
EMERGENCY EXIT LIGHTS INOPERABLE WITH COLD AIRCRAFT. NO LIGHTS FUNCTION WITH EMERGENCY LIGHT SWITCH IN ARM. REMOVED ALL FOUR EMERGENCY LIGHT BATTERIES, INSTALLED THREE REPAIRED, AND ONE MODIFIED. CUSTOMER SUPPLIED EMEERGENCY LIGHT BATTERIES. PERFORMED DIRECT CHARGE. OPERATIONS CHECK GOOD. ALL WORK PERFORMED, IAW CITATION MODEL 580A AMM 33-50-06.
LEFT HORIZONTAL STAB O/B RIB COMMON TO PANEL 351AC LOWER FLANGE IS CRACKED. REFERENCE ENGINEERING MEMO DQ25863M1. HORIZONTAL STABILIZER TRAILING EDGE REPAIR DATED MAY 27, 2020.
HORIZONTAL TRAILING EDGE RIB REPAIR (LEFT SIDE). ENGINEERING REPAIR LETTER DQ25863M1 DATED 5/27/2020.