N564QS
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
WHILE ACCOMPLISHING SL680A-32-11 - LANDING GEAR - MAIN LANDING GEAR TRAILING LINK ENHANCED INSPECTION; SN: 27486606 LH, FOUND EVIDENCE OF CRACKS INSIDE THE LH TRAILING LINK WHICH COULD CONDEMN THE PART ACCORDING TO THE TOLERANCES CALLED OUT PER THE SERVICE LETTER. CORRECTIVE ACTION: REPLACED TRAILING LINK. OPS CHECK GOOD. IAW CE680A MM 32-10-15
NOSE TUNNEL CORROSION.
HI-LOC CLEARANCE AND INTERFERENCE.
CONSISTENT RESONANCE VIBRATION IN YOKE FLIGHT CONTROLS WITH AUTO PILOT ON AND OFF IN FAIRLY STABLE AIR. NOTICEABLE IN MULTIPLE SPEEDS AND PITCH ANGLES. CORRECTIVE ACTION: VISUALLY EXAMINED ALL TRIM TABS AND CONTROL SURFACES AND GEAR DOORS (WELGHT ON WHEELS) FOR DEFECTS COULD NOT NOTE ANY OBVIOUS DEFECTS. WILL NEED TO ACQUIRE TOOLLNG TO EXAMINE GEAR DOORS IN RETRACTED POSITIONS AND FOR ELEVATOR AND ALLERON FREE PLAY CHECKS. (6-30-25 DT) JACKED ALRCRAFT AND RETRACTED GEAR. INSPECTED CLOSED DOORS FOR RIGGING AND FLUSHNESS, AS WELL AS FOR ANY LOOSENESS. NO DEFECTS NOTED. LOWERED GEAR AND CONFIRMED 3 GREEN. LOWERED AIRCRAFT STILL WAITING FOR FREE PLAY TOOLLNG (DT 7-1-25) CW AILERON AND ELEVATOR FREE PLAY CHECKS. NOTED NO DEFECTS. REF AMM 27-10-00 & 27-37-00 MXC CONTACTED CREW AND THEY SUSPECT POSSIBLE RH ENGINE VIBE. REMOVED AND REPLACED RH STARTER GENERATOR. ENGINE RUNS REVEALED NO DEFECTS. REF AMM 80-10-20
EXIT LIGHT ON EXTERIOR LAV WALL, EXIT LIGHT ON LAV KICK PANEL AND FLOOR LIGHT UNDER KICK PANEL DID NOT ILLUMINATE DURING CHECK. EMERGENCY LIGHTS BATTERY PACKS CHARGED FOR 1 HOUR PER AFM AND STILL FAILED CHECK. LIGHTS WILL ILLUMINATE ON SHIPS POWER. CORRECTIVE ACTION; REMOVED #4 BATTERY PACK AND INSTALLED NEW #4 BATTERY PACK IAW RADIANT POWER INSTRUCTIONS SIL-CBS28-1-2024-001 REV A. OPERATIONAL CHECKED GOOD PUT AIRCRAFT BACK TO ORIGINAL CONFIGURATION IAW CE680A AMM CH. 33-50-00.
EMERGENCY LIGHTING: #1 EMERGENCY BATTERY PACK DOESN'T HOLD A CHARGE OVERNIGHT.
LEFT MLG LANDING GEAR RETRACTION: AFTER TAKE OFF WHEN WE RETRACTED THE LANDING GEAR WE GOT A LH MAIN GEAR DISAGREE CAS MSG WITH A X IN THE LH MAIN GEAR BOX. WE ALSO GOT AN ASSOCIATED SSD FAIL CAS MSG CORRECTIVE ACTION: REPLACED DOWN LOCK SWITCH. OPS CHECK GOOD. IAW MODEL 680A MM 32-30-15.
DURING CLIMB OUT AFTER TAKEOFF, WITH 1.2 NOSE DOWN STAB TRIM, EXPERIENCED SIGNIFICANT NOSE UP CONTROL PRESSURE. REQUIRING PILOT NOSE DOWN YOKE PRESSURE. LEVELED OFF AT 10,000 FT & SLOWED ACFT UNTIL NO PITCH CONTROL PRESSURES FELT. PRIMARY TRIM UNRESPONSIVE. COMPLETED JAMMED STAB TRIM SYS CHECKLIST. REMOVED MACH TRIM ACTUATOR LINKAGE AND REPLACED SHEARED RIVETS, REINSTALLED MACH TRIM ACTUATOR. REMOVED AND REPLACED DAMAGED MACH TRIM CONTROL CABLES. RE-ROUTED MACH TRIM ELECTRICAL HARNESS DUE TO BINDING. PERFORMED ELEVATOR CONTROL CABLE TENSION AND ADJUSTMENT. PERFORMED ELEVATOR TRIM TAB CABLE TENSIONS AND RIGGING.
LEFT MLG LANDING GEAR RETRACTION: AFTER TAKEOFF, THE LANDING GEAR HANDLE COULD NOT BE MOVED TO THE UP POSITION WHICH DID NOT ALLOW ALL 3 GEAR TO BE RETRACTED. AMBER WOW MISCOMPARE CAS MESSAGE DISPLAYED. RETURNED TO DEPARTURE AIRPORT. PERFORMED MLG OPS CHECK IAW CE-680A MM 32-00-00. OPS CHECKS GOOD. AT THIS TIME. NO OTHER DEFECTS NOTED.
EMERGENCY EXIT SIGN ON DIVIDING WALL BEHIND SEAT NUMBER 7 IS INOPERATIVE DURING EMER LTS CHECK. POWERED UP AC AND VERIFIED THAT THE EXIT SIDN IN THE LH AFT BULKHEAD DID NOT WORK PROPERLY REMOVED DEFECTIVE EXIT SIGN FROM THE LH AFT BULKHEAD PT#9919054-1 SN 17C324 AND INSTALLED A NEW UNIT PT#9919054-1 SN 19G289 IAW CE-680AS M
CABIN EMERG LIGHT: DURING PREFLIGHT THE EMERGENCY LIGHTS SWITCH WAS SELECTED TO THE ARM POSITION: THE RELEVANT LIGHTS ILLUMINATED FOR A FEW SECONDS AND THEN WENT OFF. AFTER RUNNING THE APU FOR 1 HOUR THE TEST WAS REPEATED RESORTING IN THE SAME OUTCOME // SIGNOFF// ACCOMPLISHED TC-FLT-33-1001 (CESSNA 680 / 680A / 700 / EMBRAER EMERGENCY LIGHTING POWER SUPPLY BATTERY EXERCISE PROCEDURE IAW THE LATEST REVISION POSTED ON COMPLY 365. NO FAULTS FOUND. PERFORMED OPS-CHECK AND OPS-CHECK GOOD. CONTACTED MCC AND VERIFIED NORMAL OPERATION. MCC IS OK WITH SIGNOFF. WORK PERFORMED IRW CE-680A AMM 33-50-00. 21MAY2022.
OIL PRESSURE LOW L RED CAS: DURING CRUISE NOTICED THE LEFT ENGINE OIL PRESSURE FLUCTUATING BETWEEN 45 AND 50 PSI. THEN WENT BELOW 36 PSI SO WE DISENGAGE THE AUTO THROTTLE AND SET THE N2 BELOW 88%. ON OUR DESCENT TO LAND WE HAD THE OIL PRESSURE LOW LEFT RED CAS MESSAGE AS THE PRESSURE WENT BELOW 20 PSI. WE THEN RAN THE CHECKLIST AND SECURED THE ENGINE. POSITIVE OIL PRESSURE ON THE WINDMILLING ENGINE REMAINED UNTIL JUST PRIOR TO LANDING PROBABLY MAY BE ONE MINUTE // SIGNOFF// GAINED ACCESS AND DISPLACED THE HYD PUMP WITH NO SPILLAGE OF OIL UPON REMOVAL, BUT NOTED THE HYD PUMP TO HAVE EVIDENCE OF WHAT APPEARS TO BE HYD FLUID IN THE PUMP CAVITY. CURRENTLY THERE IS NO EVIDENCE OF OIL AT THE HYD AGB SEAL. COMPLETED A LH ENGINE DOWNLOAD AND SUBMITTED FOR EVALUATION. ACCOMPLISHED AN INSPECTION OF THE BREATHER TUBE WITH NO EXCESSIVE OIL NOTED. PERFORMED A VISUAL INSPECTION OF OIL SYSTEM CONNECTORS WITH NO DEFECTS NOTED. FOLLOWING STARTER LIMITS PERFORMED 2 EA DRY MOTORS AND SERVICED THE OIL TO MIN WITH 4. 75 QTS OF 2380, ACCOMPLISHED AN ADDITIONAL DRY MOTOR AND COMPLETED THE SERVICING WITH A TOTAL OF 5 QTS TO THE MIDDLE OF MIN AND MAX. SPOKE WITH PWC AND NOTED THAT DUE TO POSITIVE OIL PRESSURE, ENGINE IS STILL CONSIDERED SERVICEABLE PENDING ADDITIONAL INSPECTION FINDINGS. REINSTALLED COMPONENTS REMOVED FOR INSPECTION AS REQUIRED. ACCOMPLISHED A LEFT HAND ENGINE RUN AT IDLE AS REQUESTED FOR 15MIN AND NOTED NO FLUCTUATIONS OF THE OIL PRESSURE AT THIS TIME. FOUND THE HYD AGB SEAL TO BE LEAKING BEYOND THE 2CC/HR LIMIT. NOTED A FEW DROPS COMING FROM THE HYD PUMP DRAIN (HYD FLUID). NO OTHER LEAKS NOTED AT IDLE. POST ENGINE RUNS NO ADDITIONAL OIL SERVICING REQUIRED. GAINED ACCESS AND ACCOMPLISHED THE REMOVAL OF THE HYD AGB SEAL AS REQUIRED AND NOTED THE SEAL TO BE MISSING THE OUTER SEAL ST6202-030. ACCOMPLISHED THE REPLACEMENT WITH NEW SERVICEABLE LEFT HAND ENGINE HYD AGB SEAL (P/N: 30B6462-01) WITH ASSOCIATED PACKING AS REQUIRED. REINSTALLED ACCESS GAINED AS REQUIRED. COMPLIED
PASSENGER / CREW DOORS: MAIN DOOR MOTOR ARM DISCONNECTED FROM THE DOOR. // SIGNOFF// MAIN DOOR MOTOR ARM RING WAS MISSING WHICH ALLOWED THE ARM TO DISCONNECT. OREDERED NEW WASHER PIN AND RING AND REPLACED THEM WITH CUSTOMER SUPPLIED PARTS. ALL WORK DONE IAW CE 680A MM 52-15-15 OPS CHECK GOOD
REPAIR OF LEFT AND RIGHT MAIN LANDING GEAR SIDE BRACE ACTUATOR INBOARD FITTING(S) CHAFE DAMAGE PER TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ31258M1 DATED: 08/27/2021.
FORWARD (LEFT) TAILCONE SKIN DAMAGE (GOUGE/BAR MARK). REF ENGINEERING MEMO DQ29509M1
FLAPS FAIL AMBER CAS ILLUMINATED - ON APPROACH FLAPS WERE SELECTED TO 2. FLAPS DID NOT MOVE AND HAD A FLAPS FAIL EICAS MESSAGE. DID THE FLAPS FAIL APPROACH CHECKLIST. FLAPS FAIL MESSAGE STAYED ILLUMINATED. COMPLETED FLAP FAIL APPROACH AND LANDING CHECKLIST.// SIGNOFF // INSPECTED FLAPS FOR BINDING AND POSITION OF FLAPS, FOUND ALL FLAP PANELS TO BE IN THE FULL UP POSITION AND NO DISCREPANCIES NOTED.GAINED ACCESS TO FLAP CONTROLLER, POWERED AIRCRAFT AND INSPECTED FOR BIT CODES, DURING POWER UP FOUND BIT CODE 2 LATCHED WITH NO FLAP FAIL MESSAGES PRESENT IN COCKPIT. MOVED FLAPS TO FIRST DETENT, FLAPS DID NOT MOVE AND ON FLAP CONTROLLER NOTED BIT CODE 5 AND 2, WITH FLAPS FAIL MESSAGE. IAW CESSNA 680A MM 27-50-00. PERFORMED FLAPS RESET PROCEDURES, ON FLAP CONTROLLER ALL BIT CODES EXTINGUISHED, MOVED FLAPS THROUGH ALL FLAP POSITIONS WITH NO FAULTS. WHILE PERFORMING FLAP MOMENT PROCEDURES SIMULATED WING LOAD TO EACH FLAP PANEL DURING MOVEMENT,ALSO WHILE MONITORING FLAP POSITIONS SENSORS ON CDMS WITH FAULTS NOTED. CONTACTED MCC WITH FINDINGS AND TO REVIEW DOWNLOADS OF THE ARES, MCC NOTICED WHEN FLAPS WERE SELECTED TO FLAPS 1 NO MOVEMENT OCCURRED UNTIL FLAPS 2 WAS SELECTED AND DETERMINED FLAP SELECTOR HANDLE TO BE INTERMITTENTLY NOT SENDING SIGNAL TO FLAP CONTROLLER AT FLAP 1 POSITION TO MOVE FLAPS. FLAP HANDLE WILL NEED TO BE REPLACED AT THIS TIME. CLEANED AND INSPECTED ALL FLAP ACTUATORS AND ROLLERS, NO DISCREPANCIES NOTED, CLEANED AND LUBED ALL FLAP ACTUATORS. IAW CESSNA 680A MM 27-20-05. GAINED ALL ACCESS FOR REMOVAL OF FLAP HANDLE. REMOVED FAULTY FLAP HANDLE DUE TO INTERMITTENTLY LOSING SIGNAL FROM FLAP FULL UP TO FLAPS 1 SELECTION P/N 6765760-1, S/N FHA-259 IAW CESSNA 680A MM 27-50-15. INSTALLED REPAIRED FLAP HANDLE P/N 6765760-1, S/N FHA 243. REPAIRED BY TEXTRON AVIATION INC. CERT # CNQR918C, TRACKING # 303351808, W/O # 19248692, DATED 21/OCT/2019. IAW CESSNA 680A MM 27-50-15. PERFORMED FLAP MOVEMENT FUNCTIONAL TEST IAW CESSNA 680A MM AND FUNCTION TEST GOOD NO FAU
CABIN DOOR TOP STEP THREADED HOLE DAMAGE. REFERENCE TEXTRON AVIATION ENGINEERING MEMO REF: DQ24022M1 DATED DEC. 4, 2019.