N777QS
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 APPROACH SELECTED FLAPS 10. FLAPS TRACKED ONLY TO 2 DEGREES AND FLAP FAULT AMBER CAS APPEARED. COMPLIED WITH QRH SELECTED FLAPS BACK TO ZERO AND FLAPS FAIL AMBER CAS APPEARED. COMPLIED WITH QRH FOR ZERO FLAP LANDING. LANDED UNEVENTFULLY. B3 CODE #006786 FPU FAULT OR WIRING FAULT. CORRECTIVE ACTION: FLAP CONTROL UNIT REPLACED. OPS CHECK GOOD. IAW CL350 MM 27-52-33
DURING APPROACH, FLAPS 10 WERE SELECTED & THE FLAPS MOVED UNTIL IT INDICATED 2 DEGREES & MOVEMENT STOPPED FOLLOWED BY AMBER CAUTION EICAS MESSAGE FLAPS FAULT & APPROXIMATELY 10 SECONDS LATER, AMBER EICAS MESSAGE FLAPS NORM PRESS LOW ALSO DISPLAYED. QRH GUIDED US TO SELECT FLAPS 0 & FLAPS RETRACTED TO 0. QRH GUIDED US TO SELECT ALTN FLAPS BUT THE FAULTS WERE STILL DISPLAYED & A NO FLAP LANDING PERFORMED. APON LANDING, FLAPS WERE IN THE UP POSITION BUT SEEM TO BE APPROX 1/4 INCH FROM THE FULLY STOWED POSITION. NO CURRENT OR HISTORY FAULTS FOUND IN MDC. ARRIVED AT ACFT & VERIFIED FLAPS WERE NOT IN THE UP POSTION, POWERED ACT & PERFORMED FULL UP RESET PROCEDURE, FLAPS RESET TO 0. PLACED SWITCHES BACK TO NORMAL GROUND RAN BOTH ENGS & PERFORMED SEVERAL OPS CHECKS OF FLAPS, ALL CHECKS SAT. REMOVED FPU DUE TO FLAPS FAULT & FLAP NORM PRESS LOW FAULT. INSPECTED AREAS THAT CANNOT BE ACCESSED AFTER INSTALLATION. NO DEFECTS NOTED. INSTALLED REPAIRED FPU IAW AMM 77-52-33. INSPECTED AREA & ATTACHING HARDWARE & FLUID LINES, NO DEFECTS NOTED, PERFORMED ELECTRICAL RIG CHECK IAW AMM 27-52-00. VERIFIED MECHANICAL RIG TO BE PROPERLY ADJUSTED, NO ACTION REQUIRED, PERFORMED ALL OPS CHECKS & LEAK CHECKS, NO DEFECTS NOTED.
IN LEVEL FLIGHT AT 6000 FT GEAR & FLAPS UP SPEED 250 KTS. WE GOT AN AMBER ALT BOX MESSAGE ON BOTH PFD'S AND AN EFIS MISCOMPARE ICAS MESSAGE. LEFT ALT (6000) RIGHT ALT (5850) STBY ALT (5800) RAN QRH AVNC 02-5 EFIS MISCOMPARE B3 CODE TO FOLLOW B3-007890 NO ADC-2 INPUT ON R-GP-5 CORRECTIVE ACTION: REMOVED AND REPLACED ADC #1 OPS CHECK GOOD IAW CL-350 AMM 34-13-01.
SHORTLY AFTER A SMOOTH TOUCH DOWN (LESS THAN 10 KNOT CROSSWIND) AND SPOILERS DEPLOYED CALL OUT BY FO, THE FO ALERTED ME THAT NWS FAIL AMBER CAS WAS DISPLAYED ON EICAS. THERE WAS NO STEERING IN PEDALS NOR TILLER. USED DIFFERENTIAL BRAKING FOR STEERING. B3 CODE B3-007265 TROUBLESHOT CREW REPORT OF NWS FAIL AMBER CAS MESSAGE DURING LANDING ROLLOUT WITH CORRELATED FAULT CODE B3-007265. PERFORMED RIGGING OF NWS SYSTEM PER CL350SFP. DURING NWS RIGGING FOUND VOLTAGE ON FDBK 2 OUT OF LIMITS AND UNABLE TO BE ADJUSTED. REMOVED AND REPLACED NWS RVT IN REFERENCE TO AMM 32-51-29. OPS CHECK GOOD AT THIS TIME.
CABIN/COCKPIT HAS STRONG ACRID STENCH, SUSPECT ATOMIZED TURBINE OIL FROM AIR CYCLE MACHINE PASSED THE LABYRINTH SEAL. REMOVED APU P/N 3800774-1, S/N P-609 DUE TO SMOKE IN THE COCKPIT. INSTALLED A REPAIRED APU. OPS CHECK GOOD. IAW BOMBARDIER CL350 MM CH 49-11-01.
THE WIRING HARNESS FOR THE OPERATION OF THE MAIN CABIN DOOR IS UNPLUGGED. IT APPEARS THE VENEER HAS SEPARATED FROM THE FRAME OF THE INTERIOR, DISCONNECTING THE CABIN DOOR. THE INTERIOR LIGHTS ON THAT SWITCH ARE ALSO INOP. MAINTENANCE WAS ON THE AIRCRAFT ALL NIGHT. THE OUTDOOR SWITCH FOR THE MAIN CABIN DOOR WORKS NORMALLY AS DOES THE ELECTRIC DRIVEN MOTOR. REMOVED THE LH EQUIPMENT RACK ACCESS INTERIOR PANEL, RECONNECTED MAIN CABIN DOOR SWITCH, REINSTALLED THE EQUIPMENT RACK ACCESS INTERIOR PANEL. MAIN ENTRY DOOR, MAIN ENTRY DOOR LIGHTS, BAGGAGE DOOR LIGHTS OPERATIONAL CHECKS GOOD. WORK ACCOMPLISHED IN REFERENCE WITH BD-100 CL350 SMM 25-24-03
LAV EMERG LIGHT: THE RIGHT READING/EMERGENCY LIGHT ABOVE THE LAV DOES NOT ILLUMINATE WITH EITHER READING BUTTON, OR WITH EMERGENCY LIGHTS ACTIVATED. THE LIGHT IN QUESTION IS THE VERY AFT ROUND LIGHT ABOVE THE SEATED LAV. // SIGNOFF// GAINED ACCESS. REMOVED AND REPLACED LIGHT ASSY PN: RL6998-068G WITH NEW ASSY PN: RL6998-068G. OPS CHECKS GOOD. REF CL 350 SMM 33-26-05
ON TAKEOFF THERE IS A STRONG DIRTY SOCK ODOR WHICH SEEMS TO DISSIPATE IN FLIGHT. THE APU IS OPERATING ON TAKEOFF UNTIL ABOUT 1000 AGL. ON ARRIVAL MAINTENANCE SAID THEY CAN STILL SMELL ODOR. REPLACED APU WITH AN INSPECTED UNIT AND PERFORMED SATISFACTORY OPERATIONAL AND LEAK CHECKS IAW MM 49-11-01. NO DEFECTS NOTED.
WHILE AT 40000 FEET, TURNED MICROWAVE SWITCH ON FROM COCKPIT. FIRST OFFICER THEN WENT BACK TO GALLEY & SMELLED BURNING ELECTRICAL ODOR. ALSO NOTED THAT THE MICROWAVE DID NOT TURN ON EVEN THOUGH COCKPIT MICROWAVE SWITCH WAS ON. IT MAY HAVE COME FROM CB PANEL BEHIND TOUCH SCREEN IN GALLEY. TURNED THE MICROWAVE SWITCH OFF IN THE COCKPIT THE ODOR SEEMED TO DISSIPATE. REMOVED MICROWAVE OVEN, REF CL 350 SMM 25-30-03. INSPECTED ALL WIRING & COMPONENTS OF MICROWAVE OVEN. CHECKED ALL RESISTANCES & VOLTAGE READINGS WITH NO DEFECTS NOTED. CYCLED SWITCH IN COCKPIT & CHECKED FOR PROPER OPERATION OF REMOTE CONTROLLED CB, NO DEFECTS NOTED. REF DWG W1002531123. INSTALLED REPAIRED MICROWAVE OVEN & PERFORMED OPERATION