N522QS
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
MAIN EXIT SIGN/LIGHT: MAIN CABIN EXIT LIGHT ON THE BOTTOM LEFT REAR SIDE IS INOP. CORRECTIVE ACTION: REMOVED THE MAIN CABIN DOOR EXIT LIGHT AND FOUND IT NOT CONNECTED. COULD NOT LOCATE THE AIRFRAME CONNECTOR THROUGH THE MOUNTING HOLE IN THE INTERIOR. REMOVED THE LEATHER COVERING FROM THE AFT SIDE OF THE CABIN DOOR DIVIDER WALL. LOCATED THE AIRFRAME WIRING. ROUTED AS NEEDED. CONNECTED EXIT LIGHT. OPS CHECK GOOD. INSTALLED THE EXIT LIGHT. IAW CE680A MM 33-5CHJ0, CSPM 20-30-20
RIGHT MAIN LANDING DISAGREE INDICATION DISPLAYED UPON SELECTING GEAR DOWN FOR LANDING. QRH PROCEDURE COMPLETED AND GEAR DISAGREE MESSAGE REMAINED. LANDED WITHOUT INCIDENT. CORRECTIVE ACTION: REPLACED MLG UPLOCK SWITCHES IAW AMM 32-32-25
DUTING LANDING EXTENSION ONLY THE MAINS CAME DOWN. GOT TWO GREEN FOR THE MAINS AND A YELLOW CROSS HATCHED FOR THE NOSE + "GEAR DISAGREE N". ABOUT 30SECONDS LATER WHEN PREPARING TO DO THE CHECKLIST THE NOSEGEAR SUDDENLY EXTENDED AND WE HAD THREE GREEN. LANDED NORMALLY. CORRECTIVE ACTION; REMOVED AND REPLACED NOSE GEAR ACTUATOR & UPLOCK ACTUATOR. C/W NOSE GEAR UPLOCK ACTUATOR POST MAINTENANCE CHECKS REF. MM 32-32-15. C/W NOSE GEAR ACTUATOR POST MAINTENANCE CHECKS REF. MM 32-30-05. ALL OPS CHECKS GOOD.
DURING THE EMERGENCY LIGHT TEST, THE EXIT SIGN OVER THE MAIN CABIN DOOR DOES NOT COME ON. ALL OTHER EMER LIGHTS WORK FINE. ARRIVED AT ALE AND REMOVED FAULTY NR 2 EMERGENCY BATTERY DUE TO INTERNAL FAULT AND INSTALLED REPAIRED BATTERY . LET BATTERY CHARGE AS NEEDED. WORK PERFORMED IAW AMM 33-50-06.
MAIN EXIT SIGN/LIGHT: MAIN EXIT LIGHT SIGN WONT ILLUMINATE . REMOVED THE #1 EMERGENCY POWER SUPPLY BATTERY PN: CBS28-1, SN: 5261M DUE TO INTERNAL FAILURE. INSTALLED REPAIRED UNIT PN CBS28-1 SN 008979 IAW CE680A AMM 33-50-06. POWERED UP AIRCRAFT AND CHARGED PACK AS REQUIRED. OPS CHECKS GOOD. CLOSED UP ACCESS AND SECURED AIRCRAFT.
RT MLG OUTSIDE WHEEL WAS SMOKING ON TAXI IN.HYD FLUID PUDDLED UNDER WHEEL. ARRIVED ON SITE TO EVALUATE HYD LEAK. INSPECTED & FOUND AFT UPPER BRAKE PUCK ON #4 BRAKE ASSY. LEAKING. WASHED DOWN #4 BRAKE & WHEEL ASSY. TO REMOVE LEAKED HYD FLUID. CLEANING #4 WHEEL ASSY. JACKED RT MLG AND REMOVED #4 MLG WHEEL ASSY. REMOVED RT O/B BRAKE ASSY. VERIFIED RH OB BRAKE ASSY SHUTTLE VALVE & CAPS WERE LOCATED PROPERLY. INSTALLED OVRHLD RH OB BRAKE ASSY. INSTALLED ORIGINAL #4 MLG WHEEL ASSY. POWERED ON ACFT VERIFIED HYD FLUID QTY ACCEPTABLE. BLED RT O/B BRAKE ASSY. VERIFIED NO LEAKS. DOWN JACKED ACFT AND VERIFIED HYD FLUID QTY GOOD. ALL MAINTENANCE DONE IAW AMM 32-40-05 AND 32-42-05.
AT 1600 FEET, 200 KNOTS, AFTER SELECTING FLAPS 1, HAD A YELLOW FLAPS FAIL CAS. EXECUTED THE QRH AND THE FLAPS RESET DID NOT CLEAR THE FAULT. FLAP HANDLE WAS IN THE 1 DETENT. CONTINUED THE QRH AND LANDED FLAPS 0 UNEVENTFULLY. //SIGNOFF// REMOVED AND REPLACE FLAP RELAY AND VERIFIED FLAP RIGGING PER 680A AMM 27-50-30. OPS CHECK GOOD AT THIS TIME.
FLOOR EMERG EXIT LIGHT: UNDER SEAT 10 EMER LIGHT WILL NOT GO ON WITH EITHER SWITCH SELECTED TO ARM OR ON. PATH LIGHT UNDER SEAT 10 DOES WORK WHEN SELECTED. COMPLIED WITH TC-FLT-33-001 CESSNA 680A EMERGENCY LIGHTING POWER SUPPLY BATTERY EXERCISE PROCEDURE REV 2 DATED 20OCT2022.
ENG CNTRL FAULT L AMBER CAS: WHILE CONFIGURING FOR LANDING, ENG CNTRL FAULT L AMBER CAS MESSAGE APPEARS, FOLLOWED BY AMBER X'S THROUGH THE AILERON AND RUDDER TRIMS AND L SIDE SPOILERS INDICATION ON THE EICAS PANEL, PLUS LOSS OF OIL TEMP, LOSS OF HYDRAULIC VOLUME INDICATIONS.//CORRECTIVE ACTION//DOWNLOADED ARIES FOR REVIEW AND DATA WAS TRANSMITTED TO TEXTRON, FOUND GEA #2 FAULT IN DATA HISTORY BUT NO CURRENT FAULT, INSPECTED GEA#2 CONNECTORS PT405 FOR PIN SECURITY AND CONNECTOR CONDITION PER TEXTRON RECOMONDATION, AND PERFORMED LEFT ENGINE RUN TO VERIFY NO CURRENT ENG CNTRL FAULT, ALL SYSTEMS OPERATING NORMAL IAW CESSNA 680A MM31-33-0-31-50-00
APU (EXCEPT GENERATOR): APU FILLED CABIN WITH SMOKE AFTER RUNNING APPROXIMATELY 3 MINUTES. // SIGNOFF// REMOVED APU PN:3800785-1 SN:P-729 DUE TO FAULTY AND INSTALLED CUSTOMER SUPPLIED REPAIRED APU P/N 3800785-1 S/N P-799. PERFORM OPS CHECK OF APU AND LEAK CHECKS OF APU OIL AND FUEL SYSTEMS. WITH NO DEFETS NOTED. ALL WORK IAW CE-680A AMM 49-10-00 AND 12-20-20.
APU SMOKE: ON FIRST START OF THE DAY WHEN APU BLEED WAS TURNED ON SMOKE CAME OUT OF THE AIR-CONDITIONING VENTS. CHECKED OIL QUANTITY AND FOUND IT AT MAX PERFORMED BORESCOPE OF APU EXHAUST TURBINE AND FOUND OIL SWIRLS. THIS IS COMMON WITH OVERSERWICING CONDITIONS AND WILL GET SMOKE OR STRONG ODOR UPON SHUTDOWN. DESERVICED APU OIL AND RESERVICED OIL TO APPROPIATE LEVEL. RETURNED APU TO NORMAL CONFIGURATION, STARTED APU AND TURNED BLEED AIR ON. NO SMOKE OR SMELLS NOTED WORK PERFORMED PER CE680 AMM 49-10-15. PERFORMED TC-68A-21-181006M.
APU SMOKE: SHORTLY AFTER TURNING ON THE APU BLEED AIR, THE COCKPIT BEGAN TO FILL UP WITH SMOKE. AFTER TURNING OFF THE APU BLEED AIR THE SMOKE BEGAN TO DISSIPATE. REMOVED CABIN HEPA FILTER P/N 9914836-1 S/N 0538 AND INSTALLED NEW CABIN HEPA FILTER P/N 9914836-1 S/N 0456. FILTER INSTALLED AFTER PERFORMING TASK TC-68A-21-181006M REV 1 DATED 10/16/2018 ENVIROMENTAL CONTROL SYSTEM BLEED AND TRIM AIR DUCT BURN PROCEDURES. NO CABIN OR COCKPIT SMELL OR BURNING OIL OR SMOKE. NO FURTHER ACTION REQUIRED AT THIS TIME. ALL MAINTENANCE PERFORMED IAW CE-680A AMM 21-70-10 HEPA FILTER REPLACED DUE TO REPORTED SMOKE IN COCKPIT.
FLOOR EMERG EXIT LIGHT: UNDER SEAT #5, FORWARD FACING SEAT ON LEFT SIDE, FLOOR EMERGENCY LIGHT IS INOP. // SIGNOFF // GAINED ACCESS TO SEAT 5 EMEERGENCY LIGHT AND FOUND THAT THE WIRES HAD BEEN PULLED OUT OF THE PINS INSIDE OF THE CONNECTOR TO THE AIRCRAFT HARNESS, DISCONNECTED CONNECTOR AND GAINED ACCESS TO ADJACENT SEAT LIGHT ASSY AND CONNECTED TO VERIFY OPERATION RESTORED. ACCESS ITEMS NOT NEEDED FOR REPLACEMENT OF SEAT 5 LIGHT ASSY. AND WAITED ON PARTS AFTER WAITING FOR PARTS TO ARRIVE RECIEVED LIGHT ASSY AND INSTALLED INTO SEAT 5. COMPLETED OPS CHECK GOOD AND RESTORED ALL REMAINING ACCESS ITEMS AS REQUIRED. WORK DONE WITH REFERENCE TO CE680A AMM 33-20-01
CABIN EMERG LIGHT: WITH THE MAIN BATTERIES L&R BATT OFF AND THE EMER LTS SWITCH ON ARM NO CABIN EMERGENCY LIGHT ILLUMINATE.///SIGN-OFF///RESET FWD EMERGENCY LIGHT G-SWITCH IN PEDISTAL, PERFORMED SEVERAL EMER LIGHT CHECKS IN NORM, OFF & ARM POSITIONS. IAW CE-680A MM 33-50-00. OPS CHECK GOOD.
CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. ACCOMPLISHED FIELD REPAIR SR-680A-ATA53-25890 REV- DATED JUNE 1, 2020 AND 8100-9 DATED 6/1/2020; STANDARD REPAIR.
ALL LANDING GEAR RETRACTION DID NOT RETRACT - ON TAKEOFF GEAR WOULD NOT RETRACT. EICASS MESSAGE WOW MISCOMPARE WAS PRESENT. COMPLETED CHECKLIST. WOW EICASS MESSAGE WENT OUT ELECTED TO TRY AND RAISE GEAR. LOUD NOISE AND BANGING HEARD AS GEAR RETRACED AIRCRAFT WAS ROCKING. ELECTED TO LOWER GEAR. THREE GREEN INDICATED. WOW INDICATION STAYED OUT. UNEVENTFUL LANDING AND TAXI IN. REMOVED AND REPLACED NLG SQWAT SWITCH COMPLIED WITH SATIFACTORYRIG AND GEAR SWINGS NO FURTHER DEFECTS NOTED AT THIS TIME IAW MM 32-60-10.
RIGHT WING INBOARD FLAP LOWER SKIN DAMAGE (DENT).
DURING LEVEL FLIGHT AT 10,000 FEET, AND SPEED OF APPROXIMATELY 180 KIAS, THE "CONTROL LOCK ON" CAS MESSAGE ILLUMINATED ON THE PFD'S. THE CONTROL LOCK LEVER WAS CHECKED TO BE IN THE UNLOCKED DETENT . AFTER MOVING THE LEVER SLIGHTLY, AND FIRMLY RETURNING IT TO THE UNLOCKED POSITION, THE CAS MESSAGE EXTINGUISHED. SUB: INSPECTED CONTROL LOCK SYSTEM AND PERFORMED CONTROL LOCK SYSTEM FUNCTIONAL TEST. NO DEFECTS NOTED AT THIS TIME. WORK DONE IN REF TO MODEL 680A MAINTENANCE MANUAL CHAPTER 27-70-00-5
ON APPROACH, RIGHT MAIN GEAR DID NOT INDICATE DOWN. RAN CHECK LIST. STILL DID NOT INDICATE DOWN. REMOVED AND REPLACED THE UPLOCK SWITCH IAW MM 32-32-25. OPS CHECKED GOOD.