N570QS
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
ON DEPARTURE OUT OF BOS AFTER SELECTING GEAR UP, GOT A YELLOW CAS- GEAR DISAGREE RT & A YELLOW X RT GEAR INDICATION. COMPLETED THE QRH PROCEDURE FOR. GEAR DISAGREE. BEGAN TROUBLESHOOTING, GATHERED MANUALS, REFERENCES, & PRIOR HISTORY. SUSPECT THAT THE ISSUE IS COMING FROM RT MLG DOWNLOCK SWITCH. BEGAN WITH METERING CHECKS & PERFORMED CONTINUITY CHECKS ON BOTH DOWNLOCK AND UPLOCK SWITCHES. BOTH SWITCHES, GROUND METERED GOOD. THEN RECONFIGURED ACFT BACK TO NORMAL CONDITION DUE TO EMERGENCY GEAR BOTTLE BEING OPERATED.AFTER. 4'0 THE RESETJACKED UP AIRCRAFT AND HOOKED UP ELECTRICAL AND HYDRAULIÃâ¡ POWER. PERFORMED THE LANDING GEAR OPERATIONAL CHECKS. ONE OUT OF THE 15 GEAR SWING NOTICED WHEN HANDLE WAS SELECTED DOWN THE RH DOWN INDICATION WENT FROM GREEN TO AMBER BACK TO GREEN FOR ABOUT A SECOND, OTHER THAN THAT ALL OPERATIONAL CHECKS WERE GOOD. THEN GAINED ACCESS TO THE DOWN LOCK SWITCH AND BEGAN TO REMOVE THE / SEALANT. AFTER WAS ABLE TO REMOVE THE SWITCH FROM THE ACTUATOR HOUSING. INSPECTED THE HOUSING AND FOUND MOISTURE AND DEBRIS INSIDE. CONTINUED WITH REPLACING THE SWITCH. PER THE MANUAL IT SAYS TO PERFORM THE LANDING GEAR DOWNLOCK SWITCH TEST FOR THIS ACTUATORS PART NUMBER. CE-680A MM 32-30-15.NEXT STEP IS TO CONTINUE WITH THE LANDING GEAR DOWNLOCK SWITCH TEST AND PROCEED WITH THOSE FINDINGS. FOLLOWING CIRCUIT BREAKERS ARE PULLED: FLIGHT HOUR METER, L FUEL BOOST, R FUEL BOOST AND, IN THE BAGGAGE L BOOST PUMP, R BOOST PMP. PANEL 316AR IS TAGGED ON TOP OF CART NEXT TO AIRCRAFT. NEXT STEP IS TO CONTINUE WITH THE LANDING GEAR DOWNLOCK SWITCH TEST AND PROCEED WITH THOSE FINDINGS. FOLLOWING CIRCUIT BREAKERS ARE PULLED: FLIGHT,HOUR.METER, L FUEL.BOOST, R FUEL BOOST AND, IN THE BAGGAGE L BOOST-PUMP, R BOOST PMP. PANEL 316AR IS TAGGED ON TOP OF CART NEXT TO ACFT.CONTINUED & PERFORMED LANDING GEAR DOWNLOCK SWITCH CONTINUITY CHECKS GOOD. ALSO PERFORMED MEASUREMENT OF DOWNLOCK SWITCH / ACTUATION LEVER AND VERIFIED IT IS WITHIN SPEC WITH A MEASUREMENT OF .50 INCH AND A SPEC OF (.48INCH +/- .05 INCH). MOVED ON AND PERFORMED CONTINUITY CHECKS FROM DOWNLOCK SWITCH CONNECTOR PG012 TO WHEEL WELL DISCONNECT CONNECTOR GOOD, VERIFIED GROUNDS ARE GOOD AND NO OPENS OR SHORTS WHILE MANIPULATING HARNESS. NEXT PERFORMED / CONTINUITY CHECKS OF RH UP-LOCK SWITCH (SG008) FROM THE WHEEL WELL CONNECTOR THRU THE UP-LOCK SWITCH, CONTINUITY CHECKS FAILED, SWITCH HAS HIGH RESISTANCE ON ALL PINS IN BOTH UP AND LOCKED OR UN-LOCKED DIRECTIONS, NEEDS TO BE REPLACED. INFORMED TEXTRON AND MCC (ERIC HOLCOMB & BILL WILLIAMS2) OF FINDINGS, THEU ELECT TO REPLACE BOTH THE / DOWN-LOCK SWITCH AND UP-LOCK SWITCHES. PLACED PARTS ON ORDER. REMOVED DOWN-LOCK SWITCH(SG002) PN: 6-0373-3 SN: NA, AND INSTALLED, RIGGED, SEALED AND SAFE-TIED REPLACEMENT SWITCH PN: 6-0373-3 SN: NA. NEED TO CONTINUE WITH GEAR SWINGS AND OPERATIONAL CHECKS. WORK DONE IN REF TO 680A AMM CH 32-30-15. VOLT METER USED SN: 86140167 CAL DUE 14 JUL 2026 NEED TO REPLACE RH UP-LOCK SWITCH, RIG AND OPS CHECKS GEAR SWINGS (POO) NEED TO PERFORM OPERATIONAL CHECKS OF RH DOWN LOCK SWITCH GEAR SWINGS FOLLOWING CIRCUIT BREAKERS ARE PULLED: FLIGHT HOUR METER, L FUEL BOOST, R FUEL BOOST AND, IN THE BAGGAGE L BOOST PUMP, R BOOST PMP. PANEL 316AR IS TAGGED ON TOP OF CART NEXT TO AIRCRAFT. WHILE REMOVING THE RH UP LOCK SWITCH THE SCREWS WERE VERY-WORN 'AND CORRODED, CAUSING THE SCREWS TO STRIP WHEN ATTEMPTING TO TAKE OFF. HAD TO USE VICE GRIPS IN AN AREA WITH VERY LIMITED SPACE, AFTER SOME.TIME WAS ABLE TO REMOVE THE STRIP SCREWS.
LEFT NOSE SECTION OF AIRCRAFT WAS STRUCK BY WINGTIP OF TAXIING AIRCRAFT CAUSING DAMAGE TO THAT SECTION. COMPLIED WITH NETJETS RFTS 114245 REV.0. PERFORMED 10X DETAILED VISUAL INSPECTION (DVI) ON THE INTERNAL AND EXTERNAL FUSELAGE SKIN AND ADJACENT STRUCTURE PER AC43.13-1 B, CHAPTER 5 SECTION 2 TO VERIFY THERE IS NO CRACKS, DAMAGED FASTENERS, OR ADDITIONAL DAMAGE OTHER THAN WHAT HAS BEEN PREVIOUSLY REPORTED, NO ADDITIONAL DISCREPANCIES WERE NOTED. APPLIED REPAIR ADHESIVE TO INNER STRUCTURE DISBOND AND ALLOWED ADHESIVE TO CURE PER MANUFACTURERS INSTRUCTIONS. PICTURE(S) OF TEMP REPAIR PROVIDED TO MCC.
OVER WING EMERGENCY EXIT ESCAPE LIGHT IS INOP. COMPLIED WITH NJ MEL PROCEDURES. CORRECTIVE ACTION: REPLACED OVER-WING EMERGENCY EXIT LIGHT IAW CE-680A AMM 33-50-20 OPS CHECK GOOD
EMERGENCY LIGHTING: EMERGENCY LIGHTS FAILED PREFLIGHT TEST. COMPLIED WITH EMER/ABNORMAL PROCEDURE TO CHARGE BATTERIES. SECOND ATTEMPT FAILED ALSO. IN ON POSITION, ALL LIGHTS ASSOCIATED WITH NUMBER 1 BATTERY PACK ARE INOP. CORRECTIVE ACTION: REMOVED #1 EMER UGHT PWR SUPPLY. OPS CHECK GOOD. IAW CE680A AMM 33-50-06.
AFTER 2 CHARGING CYCLES OF 30 MINUTES EACH, EMER LIGHTS TEST FAILS. EVEN WHEN EMER LIGHTS SWITCH IS ON, SEAT 10 LIGHTS, MAIN ENTRY DOOR LIGHTS DO NOT ILLUMINATE. G SWITCH VERIFIED RESET AT THE BEGINNING OF CHARGING CYCLE1. PERFORMED T HE OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM PER AMM 35-50-00 AND T HE EMERGENCY LIGHTS OPERATED NORMALLY WITH NO DISCREPANCIES NOTED. AFTER SPEAKING WITH TEAM 700 THEY ADVISED THE EMERGENCY LIGHTS SHOULD NOT COME ON WITH THE BATTERIES DISCONNECTED AND EMERGENCY LIGHT SWITCH PLACED INTO THE ARM POSIT ION. PER TEAM 700'S RECOMMENDATION WE PERFORMED THE OPERATIONAL CHECK ONCE WITH BATTERIES ONLY, AND AGAIN WITH EXTERNAL DC POWER ONLY, BOTH CHECKS YIELDED THE SAME CORRECT RESULTS PER THE AMM, NO DISCREPANCIES ARE NOTED AT THIS TIME.
EMERGENCY LIGHTING: EMER LTS DO NOT ILLUMINATE AT ALL IN THE CABIN WHEN SWITCH IS PLACED IN THE ARM POSITION.
MAIN HYDRAULICS: HYD PRESS LOW RIGHT AMBER CASS. COMPLIED WITH QRH CHECKLIST. ON INITIAL DESCENT TO DESTINATION HYD VOLUME LOW CASS ILLUMINATED. RAN QRH CHECKLIST. LANDED FLAPS TWO BLEW DOWN GEAR AND USED EMERGENCY BRAKE AND STEERING. CORRECTIVE ACTION: REPLACED HYDRAULIC RESERVOIR. OPS CHECK GOOD. IAW CESSNA 680A AMM 29-10-05
MAIN DOOR: BOTTOM STEP ON MED DETACHED. CORRECTIVE ACTION; INSPECTED MAIN ENTRY DOOR FOUND BOTTOM STEP MOUNTING SCREWS INSERTS OETA01EO FROM STEP ASSY. REMOVED AND REPL.ACED MAIN ENTRY DOOR BOTTOM STEP ASS'Y WITH A OJSTOMER SUPPUEO NEW PART.OPS CHECK OF MAIN ENTRY DOOR STEP LIGHTS OK I/A/W CE-680A IMM 25-20-10.
PRIMARY TRIM: AT 300 KNOTS AMBER CASS "RETRIM NOSE DOWN" ILLUMINATED. WHEN SLOWING BELOW 300 KNOTS, CASS MESSAGE EXTINGUISHED AND STAB TRIM MOVEMENT WAS OBSERVED. IT APPEARS THAT AT 300 KNOTS, THE AIRPLANE IS RUNNING OUT OF TRIM AND REACHING ITS MAX NOSE DOWN TRIM LIMIT. CORRECTIVE ACTION; REMOVED AND REPLACED PRIMARY TRIM ACTUATOR. PERFORMED STABILIZER TRIM POINTER RIGGING WITH REF TO CE680A MM 27-40-00. OPS CHECK GOOD. RESECURED ALL PANELS.
EMERG EXIT SIGN/LIGHT: EMER EXIT LIGHT OVER MAIN CABIN DOOR AND BOTH EXIT LIGHTS AT TOP OF STAIRS ILLUMINATED ALL THE TIME. EXIT LIGHTS IN AFT CABIN NOT ILLUMINATED. // SIGNOFF// LIGHTS ARE STA YING ON WITH THE SWITCH IN THE OFF POSTION AND MAIN BATTERIES DISCONNECTED, AFTER SPEAKING WITH TEAM 680 THE SUSPECTED FAILURE IS THE #1 INERTIA SWITCH, RESET THE INERTIA SWITCH AND OPS CHECK AGAIN. AFTER RESETTING THE INERTIA SWITCH THE UGHTS DID GO OUT. UPON REINSTALUNG FLOORBOARDS THE LIGHT CAME BACK ON, WE RESET IT AGAIN AND STARTED FLICKING TAPPING THE SWITCH AND THE LIGHTS STARTED FLICKERING REF CE-680A AMM 33-50-11. MM A CT 22JULY2023. GAINED ACCESS TO #1 EMERGENCY LIGHTS INERTIA SWITCH. REMOVED AND REPLACED #1 EMERGENCY LIGHTING INERTIA SWITCH, PERFORMED EMERGENCY LIGHTING INERTIA SWITCH OPERATIONAL CHECK, OPS CHECK GOOD. PERFORMED EMERGENCY UGHTING OPERA110NAL CHECK, OPS CHECK GOOD. RESTORED ACCESS TO INERTIA SWITCH, NO FURTHER ACTION REQUIRED. WORK PERFORMED IAW CESSNA 680A MM 33-50-00 AND 33-50-11
MAIN EXIT SIGN/LIGHT: THE EXIT SIGN OVER THE MAIN CABIN DOOR AND THE LIGHT UNDER THE SEAT ADJACENT TO THE DOOR REMAIN ON AFTER THE AIRCRAFT HAS BEEN POWERED OFF " CORRECTIVE ACTION" RESET THE INERTIA SWITCH FOR THE EMERGENCY BATTERY #1. THE LIGHTS TURNED OFF. TURNED ON AND OFF THE EMERGENCY LIGHTS AND ALL LIGHTS OPS CHECK GOOD.
COCKPIT ODOR: JUST AFTER LEVEL OFF AT FL 380 A FAINT BUT DISTINCT ODOR WAS NOTICED. IT WAS INTERMITTENT WHILE IN CRUISE BUT BECAME STRONGER DURING THE DESCENT. NO SIGN OF SMOKE AND ALL AIRCRAFT SYSTEMS WERE NORMAL. // SIGNOFF// PERFORMED ENGINE RUNS TO OPERATE ECM. CYCLED COCKPIT AND CABIN TRIM AIR VALVES MULTIPLE TIMES. COMPLETED NETJETS TASK CARD IAW TC-68A-21-181006MR2 REVISION DATE 02-16-2022. REMOVED HEPA FILTER P/N 9914836-1 S/N 0895 AND INSTALLED NEW HEPA FILTER P/N 9914836-1, S/N 0847 IAW CE-680A-21-70-10. NO DEFECTS FOUND
TR FLANGE REPLACEMENT DRILL START. ACCOMPLISHED NORDAM FIELD ENGINEERING DISPOSITION NTRSD-22TP-238; TR FLANGE REPLACEMENT DRILL START REPAIR.
EMERG EXIT SIGN/LIGHT: RIGHT AFT EMERGENCE EXIT LIGHT SIGN, LAV OVER HEAD LIGHT , LAV EMERGENCE FLOOR STRIP LIGHTING AND RIGHT ICE/ WING INSPECTION LIGHT NOT WORKING. //SIGNOFF// RECHARGED BATTERIES AS NEEDED IA W TGFL T-33-1001 (CESSNA 680 I 680A / 700 / EMBRAER EMERGENCY LIGHTING POWER SUPPLY BATTERY EXERCISE PROCEDURE) OP'S CK BAD. REMOVED # 1 EMERGENCY BATTERY PN CBS28-1 SN 006407 INSTALLED "REPAIRED" EMERGENCY BATTERY PN CBS28-1 SN 006030. REMOVED #2 EMERGENCY BATTERY PN CBS28-1 SN 5397M INSTALLED "REPAIRED" EMERGENCY BATTERY PN CBS28-1 SN 006013. REMOVED #3 EMERGENCY BATTERY PN CBS28-1 SN 007740 INSTALLED "REPAIRED" EMERGENCY BATTERY PN CBS28- L SN 005299. REMOVED #4 EMERGENCY BATTERY PN CBS28- L SN 008008 INSTALLED "REPAIRED" EMERGENCY BATTERY PN CBS28-L SN 006110. REF CE-680A MM 33-50-06 OPS CHECK GOOD.
CABIN EMERG LIGHT: DURING THE CABIN EMER LIGHTS TEST PRIOR TO START, THE ISLE LIGHTS UNDER SEATS 5 AND 8 WOULD NOT ILLUMINATE. ALL OTHER LIGHTS FUNCTIONAL. WITH APU POWER ON, ALL ISLE LIGHTS ILLUMINATED (BULBS FUNCTIONAL). // SIGNOFF// REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT UNDER CABIN SEAT #8 WITH A CUSTOMER SUPPLIED REPAIRED PART. PERFORMED SATISFACTORY OPERATIONAL CHECKS OF EMERG. LIGHTING SYSTEM 1/A/W CE-680A AMM 33-50-06.
CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. 7413133-10, -15, -16, 7413133-59. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR SR-680A-ATA53-25890 REV- DATED JUNE 1, 2020 AND 8100-9 DATED 6/1/2020; STANDARD REPAIR - CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75.
ENGINE AGB AFT COVER CORROSION. ACCOMPLISHED PRATT & WHITNEY DAA2021-357-PW306D1-CN0251 DATED APRIL 29, 2021; DEVIATION LETTER - ENGINE MODEL PW306D1 SERIAL NUMBER CN0251 (TTSN 3138.1 HOURS CYCLES: 2053) - ACCESSORY GEAR BOX TOUCH UP REPAIR.
ENGINE AGB AFT COVER. ACCOMPLISHED PRATT & WHITNEY DAA2021-356-PW306D1-CN0250 DATED APRIL 29, 2021; DEVIATION LETTER - ENGINE MODEL PW306D1 SERIAL NUMBER CN0250 (TTSN 3138.1 HOURS CYCLES: 2053) - ACCESSORY GEAR BOX TOUCH UP REPAIR.
STRONG ODOR OF HOT ELECTRICAL COMING FROM COCKPIT AREA. NO SMOKE WAS SEEN. APPLIED POWER & TURNED ON ALL COCKPIT, CABIN LIGHTS, AND OUTLETS. VERIFIED ALL AC OUTLETS & USB PLUGS OPERATE IN CABIN AND COCKPIT VERIFIED COOLING FANS ON GLAIRSHEILD OPERATE OK. NOTED LT LED PANEL IN FLIGHT COMPARTMENT F1016 WAS INOPERATIVE. PULLED AND RESET CB PANEL LED LIGHTS AND LED CAME ON. PERFORMED OPS CHECK OF NC103 AND CHECK IN CMDS WITH NO DEFECTS. PERFORMED GROUND RUNS WITH LT ENGINE. RT ENGINE AND LT & RT, APU CONFIGURATIONS CHECKED PITOT STATIC HEAT, WS HEAT, DC/AC GENERATORS & TRU SYSTEM, OPENED LT PCB ENCLOSURE AND NOTED A ELECTRICAL ODOR FROM PCB NC103. REPLACED NC103 AND FOUND LED F1016 INOPERATIVE AGAIN. TS WIRES FURTHER AND FOUND PIN A AT P1007 NOT LOCKED IN CONNECTOR WITH CONNECTION TO 22RD. LOCKED IN AND FOUND LT TILT PANEL LED BACKLIGHTING TO FUNCTION NORMALLY NO DEFECTS OR ELECTRICAL SMELL NOTED IN FLIGHT COMPARTMENT. ALL WORK IAW LATITUDE 680 AMM 21-25-00, 33-10-00, 24-20-00 24-30-00, 24-30-10,30-40-00 , 30-30-00 AND WDM 33-11-01
WHEN OPENING MAIN CABIN DOOR TO EXIT PLANE, BOLT FROM HAND RAIL SEPARATED FROM ROD THAT ATTACHES TO DOOR. FLOATING ROD INHIBITS DOOR OPENING AND CLOSING PROPERLY. CORRECTIVE ACTION: INSTALLED NEW HARDWARE ON UPPER HANDRAIL SUPPORT STRUT. OPERATIONS CHECKS GOOD, REF CE-680A AMM 52-10-40.
RIGHT ENGINE LOWER FAIRING LEADING EDGE IS MISSING. MISSING PIECE HAD DEPARTED AIRCRAFT AND COULD NOT BE FOUND. DISASSEMBLED R/H ENGINE TO EXTENT NECESSARY TO GAIN ACCESS TO THE BYPASS DUCT LOWER FAIRINGS TO REMOVE REMAINING PIECE OF FAIRING AND ADJOINING CRACK FAIRING PART NUMBER 30B7127-01 AND REPLACED BOTH I/A/W PW306D EMM 72-70-01