N761QS
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
TOP EXIT SIGN LIGHT INOP BOTTOM IS ON. BEGAN TROUBLESHOOTING. POWERED UP AIRCRAFT AND PERFORMED OPS CHECKS OF INTERIOR EMERGENCY LIGHTS. FOUND THE TOP EXIT SIGN LIGHT AT THE EMERGENCY EXIT INOP. GAINED ACCESS TO CONNECTION AND FOUND CONNECTOR AT THE LIGHT ASSEMBLY BROKEN OFF. SENT PICTURES TO MCC AND PLACED PARTS ON ORDER. PART WAS REMOVED AND INSTALLED FOR CONTINUED SERVICE. DUE TO TOP EXIT LIGHT CONNECTOR BROKEN REMOVED. OPS CHECK GOOD, ALL WORK DONE IAW SMM 33-50-01.
ELECTRICAL FAULT CYAN CAS: CYAN ELECTRICAL FAULT EICAS MSG CAME ON DURING THE CLIMB PASSING FL200. THE BUS TIE SWITCH CLOSED. THE LEFT AUX BUS WAS ISOLATED. THE LEFT MAIN BUS WAS FED BY THE LEFT GEN. THE L ESS BUS WAS FED BY THE RIGHT GEN VIA THE BUS TIE. THE L AUX BUS RECONNECTED TO THE L MAIN BUS DESCENDING THROUGH FL200. THE B3 CODE IN THE AIR WHILE THIS WAS GOING ON WAS:B3-007122, LEFT PROTECTION PCB (LPROT) FAILURE. CHECK THE LEFT PROTECTION PCB PCB1 IN THE LDCPC (A35). THE MESSAGE TURNED AMBER UPON LANDING. CORRECTIVE ACTION; SWAPPED LT & RT ENGINE GENERATORS FOR CUSTOMER CONVENIENCE. RAN BOTH ENGINES AND PERFORMED MAIN GENERATOR OPERATIONAL TESTS WITH NO DEFECTS NOTED. REF. CL350 AMM 24-31-05.
DURING TAKEOFF, AS THE ROLL BEGAN PLANE STARTED PULLING RT OF CENTERLINE. ADDED LT RUDDER TO STAY ON CENTERLINE. ON REACHING 50-60 KNTS, PLANE PULLED HARD RT & ABORTED TAKEOFF. ALL ENGINE PARAMETERS APPEARED NORMAL, & NO EICAS MESSAGES DISPLAYED. ON TAXI INTO RAMP AREA, LINEMEN ADVISED LT MAIN BRAKES SMOKING. ON INVESTIGATION, LT MAIN INBD BRAKE APPEARED STUCK IN ON POSITION. R & R NR 2 BRAKE ASSY IAW AMM 32-43-13, OPS & LEAK CHKD GOOD. R & R DEFECTIVE INBD BRAKE CONTROL VALVE IAW AMM 32-43-09 OPS & LEAK CHKD GOOD. TAXIED, AIRCRAFT DID NOT PULL TO RT.
AFTER APU ON SPEED FOR OVER 2 MINUTES, TURNED ON ECS TO APU. BLUISH-GRAY SMOKE BOILED OUT OF THE COCKPIT AIR VENTS, HEAVIER OUT OF THE COPILOTS SIDE. NO SMOKE NOTED IN CABIN. REMOVED APU PN 3800710-1 SN P-187 IAW CMP 490001. INSTALLED ON NEW APU IAW MM 49-10-00. SERVICED APU WITH 254 OIL IAW 36-150 IAW MM CHAPTER 49-20-00. PERFORMED APU OPERATIONAL TEST, ALL TEST PASSED. LEAK CHECKED GOOD. NEW APU CLEARED SMOKE DISCREPANCY. WORK PERFORMED IAW CMP 539701 & 36-150 MM CHAPTER 49-20-00.
DURING FLIGHT, CREW FELT UNCHARACTERISTICALLY FATIGUED, AND HAD HEADACHES AND TUNNEL VISION. SELECTED DIFFERENT ECS POSITIONS FROM LT TO RT ENGINE AND DISCOVERED THAT RT ENGINE ECS WAS ALLOWING FUMES INTO CABIN AND COCKPIT. CLEARED CABIN AND COCKPIT OF FUMES. NOTICED A DIFFERENCE IN AIR QUALITY WHEN RT ENGINE ECS WAS DISABLED. COCKPIT AND CABIN AIR SEEMED TO BE MORE CONTROLLABLE ON LT ENGINE FOR TEMP CONTROL AS WELL. INSPECTED FOR PROPPER OIL LEVELS ON LT & RT ENGINES, APU AND TAIL PIPES FOR TRACES OF OIL. NONE NOTED. RAN BOTH ENGINES AT MAX CRUISE & CYCLED ECS CONTROL FROM LT ENGINE TO RT ENGINE TO BOTH ENGINES TO EMERGENCY CONTROL AND BACK FOR APPROX 20 MINUTES. NO ODOR OR SIGNS OF FUMES OR OIL IN CABIN OR COCKPIT. PERFORMED VISUAL INSPECTION OF INSIDE OF DUCTS, TUBING & DRAIN LINES. NO SIGNS OF FOD OR OIL INSIDE DUCTS. INSPECTED REFRIDGERATION UNIT & PERFORMED TEMP CONTROL & ENVIRONMENTAL CONTROL CHECKS. ALL WORK DONE IAW MM 21-00-00, 21-50-05, 21-60-00 & 21-50-00. ALL OPS CHECKS GOOD. NO DEFECTS NOTED.
WHEN STARTING DESCENT OUT OF 23,000, RED GEAR UNSAFE INDICATION ON LT MAIN LANDING GEAR CAME ON AND AIRSPEED WENT RED. SLOWED BELOW 195 MAX GEAR SPEED, AIRSPEED WENT BACK GREEN, GEAR INDICATION STILL UNSAFE. GEAR EXTENDED NORMALLY WITH 3 GREEN. REMOVED LT MLG AFT UPLOCK PROXIMITY SWITCH AND INSTALLED INSPECTED LT MLG AFT UPLOCK PROXIMITY SWITCH IAW MM 32-10-11. COMPLIED WITH OPS CK AND FUNCTIONAL CHECKS.
ON TAKEOFF, GEAR RETRACTION, RT MAIN GEAR STAYED YELLOW 2-3 SECONDS LONGER THAT LT OR NOSE; ON GEAR EXTENSION FOR LANDING, RT MAIN GEAR INDICATED RED. REMOVED RIGHT MLG ACTUATOR, INSTALLED REPAIRED ACTUATOR. OPS CHECK GOOD. WORK PERFORMED REFERENCING CMP 321004.
AFTER TAKEOFF GEAR HANDLE SELECTED UP RT MAIN GEAR INDICATED RED, GEAR UNSAFE. GEAR SELECTED DOWN AND BACK UP IAW CHECK LIST THEN OPERATED PROPERLY. T/S AND FOUND RT FWD UPLOCK PROXIMITY SWITCH ON HIGH END OF TOLERANCE. ADJUSTED PROX SWITCH AS REQ SWUNG GEARS, OPS CHECK GOOD. NO DEFECTS NOTED. ALL WORK PERFORMED IAW MM CHAPTER 32-10-11 (12).
AFTER TAKEOFF, GEAR HANDLE SELECTED UP RT MAIN GEAR INDICATED RED, GEAR UNSAFE.
ON TAKEOFF ANTI-SKID LITE ILLUMINATED THEN WENT OUT. ON LANDING ANTI-SKID LITE AGAIN ILLUMINATED AND RT BRAKE WENT COMPLETELY TO THE FLOOR WITHOUT ANY AFFECT. LT BRAKE IS OK. BELOW 10KTS BOTH BRAKES WORKED FINE. THIS HAPPENED TWICE. FOUND AUTOSKID TRANSDUCER DAMAGED. REMOVED AND REPLACED RT OTBD WHEEL SPEED TRANSDUCER PERFORMED ANTI SKID FUNCTIONAL CK. OP'S CK GOOD AT THIS TIME, REF MM 32-40-35 AND 32-40-00.