N661QS
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
SHORTLY AFTER REACHING CRUISE FLIGHT AT FLIGHT LEVEL 350, WE HAD A DOOR SEAL ANNUNCIATOR ILLUMINATE, AND A FLASHING MASTER CAUTION LIGHT. REMOVED AND REPLACED MED INFLATABLE SEAL WITH REF TO CE-560XLS AMM 52-10-04, OPS AND LEAK CHECKS GOOD. PN ON: 9914195-4 SN: 1119 PN OFF:9914195-4 SN: UNREADABLE
FLOOR EMERG EXIT LIGHT: FORWARD STRIP OF AISLE EMERGENCY LIGHTS ON LEFT SIDE OF AIRCRAFT ARE INOP. ALL OTHER EMERGENCY LIGHTS ARE OPERATING NORMAL. CORRECTIVE ACTION: REMOVED L/H FWD EMERGENCY/ PATH LIGHT STRIP FROM AIRCRAFT P/N: 9919040-9 S/N: 121003902. INSTALLED NEW LIGHT STRIP IN LEFT HAND FORWARD LOCATION P/N: 9919040-26 S/N: 202400000039947. PERFORMED OPERATION CHECK OF PATH LIGHTING AND EMERGENCY LIGHTING SYSTEM OP CHECK GOOD. ALL WORK DONE JAW CESSNA 560 AMM 33-50-00.
MAIN DOOR PRE-CATCH HANDLE SPINS ON THE STEM. CORRECTIVE ACTION; RESECURED PRECATCH RELEASE HANDLE JAMNUT IAW CE-560XL AMM 52-10-01. NO FURTHER DEFECTS NOTED.
MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. REPAIRED INSULATION BY BELLCRANK. OPS CHECK GOOD. IAW CE-560XL MM 52-10-00.
REPAIRED CORRODED AREA LOCATED AT THE RH SIDE OF THE AFT WALL OF THE NOSE LANDING GEAR WHEEL WELL BY BLENDING, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION. FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH AEROSPACE QUALITY RESEARCH AND DEVELOPMENT ENGINEERING REPAIR ORDER.
RT MLG HAD A BLOW OUT HALF WAY THROUGH OUR LANDING ROLL. THE ANTISKID FAIL ANNUNCIATOR ILLUMINATED AROUND THE SAME TIME AS THE AIRCRAFT STARTED TO PULL TO THE RIGHT. AIRCRAFT REMAINED ON RUNWAY, BUT IS DISABLED. REMOVED RH MAIN WHEEL & TIRE ASSY & INSTALLED OVERHAULED UNIT IN RT POSITION. PERFORMED BLEEDING OF ANTI SKID BRAKE SYSTEM IAW 32-44-00, ALSO PERFORMED ANTISKID SYSTEM FUNCTIONAL TEST IAW MM 32-44-00, OPS & LEAK CHECK GOOD. NO DEFECTS NOTED. INSPECTED MG UPPER BARREL-TO-TRUNNION ATTACHMENT, ACTUATOR ATTACHMENTS & SUPPORT STRUCTURE FOR ANY INDICATIONS OF STRUCTURAL DAMAGE. NO INDICATIONS OF STRUCTURAL DAMAGE NOTED AT THIS TIME. PERFORMED UNSCHEDULED HARD/OVERWEIGHT LANDINGS, MX IAW MM 05-50-00.
MAIN HYDRAULICS: DURING A CLIMB GOING THROUGH 11,500 FEET WE HAD A STAB-MIS-COMP ANNUNCIATOR LIGHT COME ON , AFTER ABOUT 30 SECONDS THE AUTO PILOT DISCONNECTED AND THE AIRPLANE PITCHED DOWN AGGRESSIVELY. IT TOOK THE PIC AND SIC TOGETHER TO PULL BACK ON THE YOKE TO STOP THE DESCENT. THE TRIM WHEEL WOULD NOT MOVE FORWARD OR AFT WHEN TRYING TO MOVE IT. AFTER SLOWING DOWN TO 200KTS WE WERE ABLE TO MOVE TRIM WHEEL AND CONTROL THE AIRPLANE. WE RAN THE APPROPRIATE CHECKLIST AND THE STAB-MIS-COMP ANNUNCIATOR LIGHT WENT OUT. HOWEVER, ON FINAL THE STAB-MIS-COMP CAME BACK ON AND STAYED ON UNTIL WE SHUT DOWN THE ENGINES AT FBO // SIGNOFF// APPLIED AIR DATA TEST SET. TESTED STAB SYSTEM SEVERAL TIMES. NOTED THE AIR SPEED SWITCH WORKING INTERMITTENTLY. REMOVED OLD AND INSTALLED NEW SWITCH. LEAK AND OPERATIONAL CHECKS OF SYSTEM GOOD. WORK DONE IAW 560XL MM CH 34-11-01. OLD P/N D45C-24 S/N 2233 NEW P/N D45C-24 S/N 2321
DURING 48 MONTH INSPECTION FOUND CRACK IN BOTTOM AFT SECTION OF RUDDER TRIM TAB. REPAIRED RUDDER TRIM TAB CRACK PER AQRD ERO-106811 REVISION IR TITLED N661QS RUDDER TRIM TAB REPAIR DATED AUG 25 2022, FAA APPROVED ON FORM FORM 8110-3 DATED AUG 25-2022. CHECKED BALANCE OF RUDDER AFTER REPAIR AND PAINT AND FOUND TO BE WITHIN LIMITS IAW CESSNA 560XL SRM 51-60-00, 51-60-03.
GEAR POSITION & WARNING: ON CLIMBOUT, AFTER THE GEAR GEAR AND FLAPS WERE SELECTED UP, THE 3 GREEN GEAR INDICATORS EXTINGUISHED AND THE GEAR UNLOCK LIGHT REMAINED ON WITH THE STAB MISCOMPARE AND HYD PRESS ANNUCIATORS ON. THE CHECKLIST WAS COMPLETED AND THE GEAR EXTENDED WITH 3 GREEN AND NO RED AND THE STAB MISCOMPARE AND HYD PRESS EXTINGUISHED. LANDING WAS NORMAL. NO OVERWEIGHT LANDING AND GEAR EMERGENCY BOTTLE WAS NOT USED. "CORRECTIVE ACTION" NLG STRUT WAS REPLACKED WITH NEW SEALS AND SERVICED AS REQUIRED PERFORMED MULTIPLE OPS CHECKS, OPS CHECKS PASSED LANDING GEAR LIGHTS CAME OFF AND ON AS REQUIRED NOT LEAKS FOUND DISCONNECTED MULE THE SERVICED THE HYDRAULIC RESEVOIR AS REQUIRED IN REF. TO CE-560XL AMM 12-12-01 CE-56XL AMM 12-20-32 AND CE-560XL AMM 32-01-00.
RIGHT MLG INDICATOR LIGHT: ON FINAL APPROACH WE SELECTED THE GEAR DOWN AND HAD NO RIGHT MAIN GEAR INDICATOR LIGHT TO ILLUMINATE. WE PERFORMED A GO AROUND, PERFORMED THE QRH, AND BLEW THE GEAR DOWN MANUALLY. WE DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. REMOVED AND REPLACED BULBS IN RH MLG INDICATOR LIGHT. OPS CHECK GOOD. REF CE 560XL MM 33-10-06. PERFORMED MAIN LANDING GEAR HYDRAULIC SYSTEMS-ADJUSTMENT/TEST & VERIFIED THREE GREEN LIGHTS (GEAR DOWN & LOCKED) & NORMAL OPERATION OF GEAR EXTENSION & RETRACTION CYCLE TIME DURING GEAR SWINGS. THEN SERVICED GEAR & BRAKE PNEUMATIC BOTTLE AS REQUIRED. REF CE-560XL MM 32-01-00 & 12-13-01 FOR MX PERFORMED. EMERGENCY RELEASE MECHANISM IS RESTORED TO NORMAL CONFIG.
RIGHT MLG INDICATOR LIGHT: ON FINAL APPROACH WE SELECTED THE GEAR DOWN AND HAD NO RIGHT MAIN GEAR INDICATOR LIGHT TO ILLUMINATE. WE PERFORMED A GO AROUND, PERFORMED THE QRH, AND BLEW THE GEAR DOWN MANUALLY. WE DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. /// CORRECTIVE ACTION /// REMOVED AND REPLACED BULBS IN RH MLG INDICATOR LIGHT. OPS CHECK GOOD. REF CE 560XL MM 33-10-06. PERFORMED MAIN LANDING GEAR HYDRAULIC SYSTEMS-ADJUSTMENT/TEST & VERIFIED THREE GREEN LIGHTS (GEAR DOWN & LOCKED) & NORMAL OPERATION OF GEAR EXTENSION & RETRACTION CYCLE TIME DURING GEAR SWINGS. THEN SERVICED GEAR & BRAKE PNEUMATIC BOTTLE AS REQUIRED. REF CE-560XL MM 32-01-00 & 12-13-01 FOR MX PERFORMED. EMERGENCY RELEASE MECHANISM IS RESTORED TO NORMAL CONFIG. MX VENDOR SUBMITTED SDR #DXTR202204131 FOR SAME EVENT.
LH ELEVATOR TORQUE TUBE IS CORRODED. REMOVED CORRODED INBOARD TORQUE TUBE DUE TO LEVEL 2 CORROSION FROM L/H ELEVATOR P/N 6634200-809LH S/N 0000210. INSTALLED NEW CUSTOMER SUPPLIED TORQUE TUBE P/N 6634002-15 PER CESSNA 560XL SRM 51-40-03, 51-40-06, AND 55-20-02.
ALL LANDING GEAR RETRACTION DID NOT RETRACT - UPON RETRACTION RED UNLOCK LIGHT ILLUMINATED PREFORMED CHECKLIST. // SIGNOFF// JACKED AIRCRAFT TO PERFORM GEAR SWINGS. INSTALLED HYD. ROBO MULE. PERFORMED GEAR SWING FAULT WAS DUPLICATED INSPECTED ALL GEAR FOR PROPER STRUT LENGTH ANY OBVIOUS DEFECT PREVENTING GEAR FROM RED UPLOCK LIGHT FROM EXTINGUISH FOUND GEAR UPLOCK SWITCH SQUAT SWITCH OUT OF RIG. ADJUSTED GEAR UPLOCK SWITCH PERFORMED 6 GEAR SWINGS OPS CHECK GOOD IAW CESSNA C560XM MM32-30-05
EVIDENCE OF A RIGHT AC ALTERNATOR FIRE WAS SEEN. THE ENGINE NACELLE PAINT WAS BURNT AFT OF ALTERNATOR VENT AND MOLTEN COPPER COMING OUT OF THE VENT. TROUBLESHOT TO A FAULTY AC GENERATOR. REMOVED AND REPLACED THE AC GENERATOR AND AC GENERATOR PCU. COMPLIED WTIH ERO-900139. RT ENGINE LOWER COWLING TEMPORARY REPAIR. APPLIED ALUMINIUM TAPE FOR REPAIR. COMPLIED WITH OPERATIONAL CHECK OF THE RT AC GENERATOR AT ALL POWER SETTING WITH NO FAULTS. WORK DONE IAW AMM 29-20-01.
DURING CLIMB OUT THRU 6500 FEET, RIGHT FIRE LIGHT CAME ON WITH RIGHT FIRE FAULT DET SYSTEM. RAN APPROPRIATE CHECKLIST AND DETERMINED IT WAS A FIRE DETECTION SYSTEM, DECLARED AN EMERGENCY AND RETURNED FOR LANDING. TROUBLESHOT THE RT FIRE DETECTOR SYSTEM, REMOVED & REPLACED THE RT FIRE DETECTOR CONTROL BOX. SYSTEM OPS CHECKED GOOD IAW MM 26-11-02.
ACM PRODUCED A SOCK ODOR. REMOVED & REPLACED DIRTY WATER SEPARATOR CONDENSER CLOTH IAW MM 12-19-02. OPS & LEAK CHECKS WERE GOOD.
DURING A BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINER COOLING RING SEGMENT SELF LOCKING NUTS, IAW MFG SPECIAL INSTRUCTION 35-2013. LINER COOLING RING SELF LOCKING NUT ON NR 1 ENGINE HAD MISSING HARDWARE. ENGINE WAS DISASSEMBLED TO GAIN ACCESS TO CC LINER. ENGINE WAS INSPECTED, MISSING HARDWARE WAS LOCATED. NEW HARDWARE WAS INSTALLED. WORK WAS ACCOMPLISHED IN REF TO MM 30J2242 R13.
DURING A SCHEDULED INSPECTION, THE ELEVATOR TRIM CABLE WAS FOUND TO BE FRAYED BEYOND LIMITS. THIS CABLE ASSY IS LOCATED WHERE THE CABLE TRANSITIONS FROM A VERTICAL RUN TO THE HORIZONTAL AT A PULLEY LOCATED IN THE HORIZONTAL STABILIZER.
DURING A SCHEDULED INSPECTION, FOUND RT ELEVATOR INBD HINGE CRACKED, VERIFIED WITH NDT, R & R HINGE ASSY.
JUST PRIOR TO DECENT, TRANSFERRED FUEL FROM LT TANK TO RT. AFTER WHICH NOTICED ODOR OF FUEL. OPENED OVERHEAD FRESH AIR VENTS & DID NOT SMELL ANYTHING. ON POST FLT DID NOT SMELL FUEL IN THE HOLE OR THE CARGO BAY, ONLY IN THE CABIN & AFT CLOSET. SUSPECT CREW TRACKED SUBSTANCE INTO CABIN. REMOVED CARPET AND SPOT CLEANED AREA, REINSTALLED CARPET. PERFORMED FUEL CROSS FEED TEST, ALL OPS CHECK GOOD, LEAK CHECK GOOD. NO DEFECTS NOTED.
WHILE ATTEMPTING TO SET T/O POWER, NR 1 THROTTLE WOULD NOT REMAIN IN T/O DETENT. TAKEOFF ABORTED, NR 2 ENG SHUTDOWN NORMALLY. IN THROTTLE CUTOFF, NR 1 ENG ACCELERATED TO APPROX 72 % N1. WITH EECS SELECTED TO MANUAL, NR 2 ENG NORMAL. PRIOR TO SELECTING EECS MANUAL, BOTH ENGINES SET AT 66% N1. UPON SELECTING MANUAL, UNABLE TO CONTROL NR 1 ENG WITH THROTTLE LEVER & IT ACCELERATES TO 72% N1, UPON ATTEMPTING ENG SHUTDOWN, NR 2 ENG SHUTDOWN NORMALLY, UNABLE TO SHUTDOWN NR 1 ENG WITH EEC IN AUTO. UTILIZED NR 1 ENG FIRE SWITCH TO SHUT DOWN ENG. OPERATED NR 1 , 2 THROTTLES THROUGH ENTIRE OPERATIONS, FOUND THAT NR 2 THROTTLE IS MUCH SMOOTHER THROUGH OPS THAN NR 1. NR 1 IS GRITTY FEELING & WILL NOT STAY AT FULL POWER. PUT NR 1 AT CUFF OFF, DISCONNECTED CABLE FROM FUEL CONT. RAN THROUGH OPS, FELT SAME, LINKAGE NOT MOVING. DISASSEMBLED CENTER PEDISTAL & PILOTS FLOOR & SEAT IN ORDER TO CHECK FOR MOVEMENT OF PUSH RODS, TORQUE TUBE & FWD LINKAGE, ALL OPS NORMAL OTHER THAN GRITTY FEEL & NOT HAVING FULL MOTION. STARTED DIS-ASSEMBLY OF AFT CABIN AND DISCONNECTED FWD CABLE FROM AFT CABLE TO CHECK FOR MOVEMENT AT CONNECTIONS MORE REMOVAL OF FURNISHING AND CABLE CLAMPS REQ IN ORDER TO GET CABLES SEPERATED. IAW 560XL M/M 76-11-03. SEPERATED CABIN BELOW AFT CABIN AREA. FWD CABLE IS SMOOTH. DISCONNECTED AFT CABLE FROM MID CABLE IN AFT BAGGAGE SIDE WALL OVER DOOR. MID CABLE CHECKS GOOD. FOUND AFT CABLE BINDING. DISCONNECTED CLEVIS AT THROTTLE BELLCRANK. REMOVED CABLE RIBBON FROM CABLE SHROUD- CABLE BROKEN. REPLACED CABLE IAW 560XL MM CHAPT 76-11-03. GROUND RUNS & OPS CHECKS GOOD AFTER RECONNECTING CABLES & RIGGING CABLES. ORIGINAL SUBMISSION: 9/23/2009
22-1 AUTO PILOT DISENGAGED 5 SECONDS AFTER SELECTING FLAPS TO 15 DEGREES. AUTO PILOT FAIL AMBER LIGHT SHOWED ON PFD'S. SEEMED LIKE AUTO PILOT TRIM COULD NOT KEEP UP. LUBRICATED ELEVATOR TRIM ACTUATORS AND COMPLIED WITH A SATISFACTORY OPS CHECK OF THE ELEVATOR TRIM SYS AND AUTO PILOT SYS IAW CH'S 22-11-01. AND 27-32-04 OF THE MM.
AUTO PILOT DISENGAGED 5 SECONDS AFTER SELECTING FLAPS TO 15 DEGREES. AUTO PILOT FAIL AMBER LIGHT SHOWED ON PFD'S. SEEMED LIKE AUTO PILOT TRIM COULD NOT KEEP UP. LUBRICATED ELEVATOR TRIM ACTUATORS AND COMPLIED WITH A SATISFACTORY OPS CHECK OF THE ELEVATOR TRIM SYS AND AUTO PILOT SYS IAW MM 22-11-01 & 27-32-04.
AUTO PILOT DISENGAGED 5 SECONDS AFTER SELECTING FLAPS TO 15 DEGREES. AUTO PILOT FAIL AMBER LIGHT SHOWED ON PFD'S.