N680QS
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 GEAR RETRACTION WE RECEIVED A GEAR DISAGREE L CAUTION MSG FOLLOWED BY A ADC SSEC MISCOMPARE. LEFT GEAR INDICATION DISPLAYED AN AMBER DN. FOLLOWED QRH GUIDANCE AND EXTENDED THE GEAR NORMALLY FOR A RETURN LANDING. HISTORY SHOWED LT UPLOCK SWITCH REPLACED 12/20 & NO RIGGING MENTIONED ON 12/24 POST FERRY MX EVENT. IAW ARES REVIEW ARES SHOWS THE LT MLG UPLOCK SWITCH IS UP & LOCKED FROM POWER ON, ON LT PCB. BUT SHOWS NOT UP & LOCKED ON RT PCB. ONCE GEAR HANDLE PUT IN UP POSITION, A DISAGREE BTWN BOTH PCB'S & STOPS GEAR FROM MOVING ON THAT SIDE. ONCE GEAR HANDLE PUT IN DOWN POSITION, UP & LOCKED SWITCH GOES TO CORRECT POSITION. PERFORMED ANALYSIS OF LIVE VIEW PCB WHILE MANIPULATING HARNESS & SWITCH, NO DEFECTS. PERFORMED SEVERAL GEAR SWINGS, NO FAULTS & NO ABILITY TO DUPLICATE FAULT. PERFORMED RIGGING CHKS OF SWITCH & FOUND LT UPLOCK SWITCH RIGGED INCORRECTLY. PERFORMED WIRING CHK OF SWITCH, NO FAULTS. PERFORMED WIRING CHK BTWN LT UPLOCK SWITCH TO GROUNDS & TO PCB, NO FAULTS. R & R PCB NC106 IAW AMM 24-60-40. OPS CHKD GOOD IAW AMM 24-60-40. R & R LT MLG UPLOCK SWITCH SG007 IAW MM. CONTINUITY CHECK OF NEW SWITCH, NO DEFECTS. PERFORMED MLG UPLOCK ADJUST CHK IAW MM 32-32-00. ADJUSTED LT & RT MLG UPLOCK SWITCH PLUNGERS. PERFORMED 15 MLG OPS CHKS IAW MM 32-00-00, NO DEFECTS. POWER CYCLED ACFT & 5 MLG OPS CHKS IAW MM 32-00-00, NO DEFECTS.
FLOOR EMERG EXIT LIGHT: DURING INTERIOR PREFLIGHT, DISCOVERED LAV TOE KICK LIGHT INOP CORRECTIVE ACTION: REMOVED INOP FLOOR EMERGENCY LIGHT BELOW LAV TOILET P/N: CLE327-01-30 S/N: 239006870 AND INSTALLED NEW LAV TOE KICK LIGHT P/N: CLE327-01-30 S/N: 202200000008765. OPS CHECK GOOD, NO FAULTS DETECTED AT THIS TIME. WORK PERFORMED IAW CE680A IMM 25-40-07, SEE 8130 FROM_TEXTRON AVIATION INC. CERT. # PC, TRACKING #:9070662, W0:5620732, DATED:16/JAN/2024.
WITH FIRM AND EVEN APPLICATION OF THE BRAKES, THE AIRCRAFT PULLS STRONGLY TO THE LEFT UNTIL PRESSURE IS RELEASED. WEAR PINS ON THE LEFT AND RIGHT APPEAR NORMAL. ARRIVED AT AIRCRAFT AND VERIFIED DISCREPANCV. PERFORMED BRAKE BLEED TEST AND FOUND AIR IN RH INBD MLG BRAKE. SERVICED HYDRAULIC SVSTEM TO SPEC AND PERFORMED SUCCESSFUL OPERATIONAL CHECK. WORK PERFORMED IAW CE-680A AMM 32-42-00.
WITH EMER LTS IN OFF POSITION, BOTH WING INSPECTION LIGHTS, MAIN ENTRANCE EXIT LIGHT, AND SEAT 3 OVERHEAD AND FLOOR LIGHTING ALL REMAINED ON. REMOVED AND REPLACED BATTERY PACK IAW 680A AMM 33-50-01. OPS CHECK GOOD
CABIN EMERG LIGHT: THE LIGHT OVER SEAT 3 WILL NOT GO OUT. *** CORRECTIVE ACTION *** ACCOMPLISHED EMERGENCY LIGHTS OPERATIONAL TEST AND RECHARGE OF EMERGENCY LIGHT BATTERIES. ALL EMERGENCY LIGHTING OPERATIONAL CHECKS ARE GOOD AT THIS TIME. NO FAULTS FOUND. ALL WORK DONE IAW CESSNA MODEL 680A AMM CHAPTER 33-00-00.
LEFT EXTERIOR EMERG LIGHT: THE LEFT EXTERIOR EMERG LIGHTS WILL NOT GO OUT *** CORRECTIVE ACTION *** ACCOMPLISHED EMERGENCY LIGHTS OPERATIONAL TEST AND RECHARGE OF EMERGENCY LIGHT BATTERIES. ALL EMERGENCY LIGHTING OPERATIONAL CHECKS ARE GOOD AT THIS TIME. NO FAULTS FOUND. ALL WORK DONE IAW CESSNA MODEL 680A AMM CHAPTER 33-00-00.
MAIN EXIT SIGN/LIGHT: THE MAIN EXIT SIGN LIGHT WILL NOT GO OUT *** CORRECTIVE ACTION *** ACCOMPLISHED EMERGENCY LIGHTS OPERATIONAL TEST AND RECHARGE OF EMERGENCY LIGHT BATTERIES. ALL EMERGENCY LIGHTING OPERATIONAL CHECKS ARE GOOD AT THIS TIME. NO FAULTS FOUND. ALL WORK DONE IAW CESSNA MODEL 680A AMM CHAPTER 33-00-00.
RIGHT EXTERIOR EMERG LIGHT: THE RIGHT EXTERIOR EMERG LIGHT WILL NOT GO OUT. *** CORRECTIVE ACTION *** ACCOMPLISHED EMERGENCY LIGHTS OPERATIONAL TEST AND RECHARGE OF EMERGENCY LIGHT BATTERIES. ALL EMERGENCY LIGHTING OPERATIONAL CHECKS ARE GOOD AT THIS TIME. NO FAULTS FOUND. ALL WORK DONE IAW CESSNA MODEL 680A AMM CHAPTER 33-00-00.
THE RIGHT BRAKE PEDAL FEELS SPONGY. WHEN TAXIING THE AIRPLANE PULLS TO THE LEFT WHEN APPLYING EVEN BRAKE PRESSURE TO THE LEFT AND RIGHT BRAKE PEDALS. AS BRAKE PEDAL PRESSURE IS INCREASED THE AIRPLANE PULLING TO THE LEFT IS MORE PRONOUNCED. PUSHING THE RIGHT BRAKE PEDAL FURTHER THAN THE LEFT BRAKE PEDAL IS REQUIRED TO INCREASE THE PRESSURE TO THE RIGHT BRAKE TO ALLOW THE AIRPLANE TO TRACK STRAIGHT. THIS WAS VERIFIED WITH THE LEFT PILOT SEAT POSITION AND THE RIGHT PILOT SEAT POSITION. REMOVED AND REPLACED BRAKE METERING VALVE. IAW CE-680A AMM 32-42-25. OPS CHECK GOOD.
NR 3 GSD FAILED IN FLIGHT. LANDING GEAR WAS EXTENDED MANUALLY AND BOTTLE WAS BLOWN. REMOVED GSD AND INSTALLED REPAIRED GSD IAW AMM 42-10-07. PERFORMED GSD SOFTWARE CONFIGURATION UPLOADS IAW AMM 31-40-00.
HYDRAULIC SYSTEM QUANTITY INDICATION: DURING CRUISE FLIGHT AT FL 430, THE HYDRAULIC QUANTITY DISPLAYED AMBER DASHES ALONG WITH OTHER (EICAS MESSAGES STAB TRIM MONITOR, ENG CONTL FAULT L, FUEL FILTR BYPASS L, AND DASHED OIL TEMP). APPROXIMATELY 5-10 LATER THE HYD VOLUME INDICATION RETURNED. STAB TRIM MONITOR WARNING: DURING CRUISE AT FL 430 THE STAB TRIM MONITOR EICAS MESSAGE DISPLAYED INTERMITTENTLY FOR APPROXIMATELY 5 TO 10 MINUTES THEM EXTINGUISHED. FUEL DISTRIBUTION: DURING CRUISE FLIGHT, AT FL430 AND VMC, FUEL FILTER L EICAS MESSAGE DISPLAYED. COMPLIED WITH QRH WITH NO FURTHER INCIDENT. LEFT ENGINE ENGINE OIL TEMPERATURE INDICATION: AT FL 430 DURING CRUISE FLIGHT AND WITH OTHER EICAS MESSAGES (STAB TRIM MONITOR, ENG CONTL FAULT L, FUEL FILTR BYPASS L, AND DASHED HYD VOLUME INDICATOR) THE OIL TEMP INDICATION DISPLAYED AMBER DASHES. OIL TEMP REAPPEARED APPROXIMATELY 5-10 MINUTES WHEN WE TURNED AND DESCENDED TOWARDS OUR DIVERT AIRPORT. A/I STAB COLD R AMBER CAS: AT 430 CRUISE FLIGHT THE A/I STAB COLD R CAS MESSAGE DISPLAYED. REMOVED #2 GEA 7100 DUE TO ENG CNTRL FAULT L AMBER CAS. REMOVED P/N 011-D2635-01. S/N 3QS005705. ENGINE RUNS WITH NO DEFECTS NOTED AT THIS TIME. WORK PERFORMED WITH REF. TO MODEL 680A AMM 31-40-15
MAIN DOOR WOULD NOT OPEN. AFTER DEPRESSING THE RED BUTTON IN THE HANDLE NO AUDIABLE DISENGAGE CLICK SOUND WAS HEARD. HANDLE WOULD NOT MOVE. AFTER SHUTTING THE PLANE COMPLETELY DOWN TO TO A DARK CABIN. THE DOOR WORKED AS NORMAL. "CORRECTIVE ACTION" REMOVED CABIN DOOR STEP'S VISUALLY INSPECTED CABIN DOOR WIRING HARNESS FOUND NO DEFECTS, VERIFIED NO POWER AT SOLENOID. VERFIED OPERATION OF SOLENOID ROTARY SWITCH. REINSTALLED CABIN DOOR STEPS REF CE680A M/M 52-10-50. REMOVED AND REPLACED PCB CARD CED MONITOR NC105 OPS CHECK GOOD.
WOW MISCOMPARE AMBER CAS: UPON RETRACTING GEAR ON DEPARTURE THE GEAR DISAGREE L/R, WOW MISCOMPARE, AND ONE OTHER FORGOTTEN CAS MESSAGE ILLUMINATED. ALSO, THE LEFT AND RIGHT MAIN GEAR INDICATION WAS AMBER DN. THE NOSE GEAR WAS UP AND NORMAL. ACCOMPLISHED X2 AND N2 ABNORMAL CHECKLIST AND HAD 3 GREEN DN GEAR. LANDED AND THATS WHEN WOW MISCOMPARE DISAPPEARED. DURING POSTFLIGHT I NOTICED SOME STRANGE ODOR COMING FROM LEFT MAIN GEAR.//CORRECTIVE ACTION//REMOVED AND REPLACED CUSTOMER SUPPLIED NOSE SQUAT SWITCH IAW CE-680A M/M CH 32-60-01. OPERATIONAL CHECKS GOOD.