N407QS
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
REPEAT WRITE-UP- FIRST FLIGHT WAS NORMAL. SECOND FLIGHT AFTER TAXING OUT TO THE RUNWAY THE EMER LIGHTS CAME ON IN THE CABIN. THEY DIDN`T EXTINGUISH UNTIL WE TURNED THEM OFF AFTER SHUT DOWN. REMOVED AND REPLACED NR I AND NR 2 EMERGENCY EXIT LIGHTING BATTERY PACKS PERFORMED RECHARGE PROCEDURE AND OPS CHECKS WITH NO DEFECTS NOTED. WORK PERFORED IAW AMM 33-52-0 I.
CABIN EMERGENCY LIGHTS CAME ON BY THEMSELVES WITH SWITCH IN THE ARM POSITION. EXTINGUISHED BY THEMSELVES APPROX 5 MINS LATER DURING CLIMB. AFTER LANDING, WITH THE MAIN SHIP BATTERIES BOTH OFF, THE EMER LIGHTS TURNED ON & OFF NORMALLY WITH THE SWITCH. RECOMMENDED C/W SLSOS-33-0005 REV.OS, REVIEWED SIL & COMPLETED T/S FIM 33-50-00, POWERED NC & VERIFIED WITH MAIN BATTERIES ON, EMERGENCY LIGHTS OPS AS DESIGNED IN ARM & ON/OFF. TURNED MAIN BATTERIES OFF, & CONFIRMED WHEN EMERGENCY LIGHTS IN ARM, LIGHTS ILLUMINATED. CONFIRMED BREAKERS ARE ENGAGED FOR EMERGENCY LIGHTS & HOT BATTERY BUSS CB. CONFIRMED SINCE BOTH BATTERIES ARE ILLUMINATING WHEN COMMANDED/TESTED & NO FLICKERING OF ANY LIGHTS NOTED. BATTERY PACKS CHKD GOOD. CYCLED ON EMERGENCY LIGHTS SEVERAL MORE TIMES TO RESET INERTIA SWITCHES & PERFORMED INERTIA SWITCH REACTIVATION IAW AMM 33-52-17. NO HISTORY FOR EMERGENCY LIGHT ISSUES, OPS CHKD GOOD.
METALLIC SMELL PRESENT IN COCKPIT ON APPROACH. UNABLE TO LOCATE SOURCE, SMELL DISSIPATED ON GROUND. SHORTLY AFTER THE SMELL APPEARED WE NOTICED THE WX RADAR WAS FAILED. CORRECTIVE ACTION: REPLACED WX RADAR R/T IAW EMB PH300 AMM 34-42-01. PREFORMED OPS CHECKS IAW EMB PH300 AMM 34-42-00 OPS CHECK GOOD
BRK FAIL YELLOW CAS: AFTER TAXING OUT THE BRAKES GRABBED AND THE YELLOW BRK FAIL CAS MESSAGE CAME ON AND WE LOST THE FOOT BRAKES. WE HAD TO USE THE EMERGENCY BRAKES TO STOP THE AIRCRAFT. WE RETURNED TO PARKING USING THE EMERGENCY BRAKES TO STOP THE PLANE CORRECTIVE ACTION; REPLACED BRAKE CONTROL MODULE IAW EMB-505 AMM 32-41-07. FUNCTIONAL CHECK SATISFACTORY AT THIS TIME.
ON TAXI OUT, BRK FAIL CAS ILLUMINATED AFTER TAXIING FOR 10 MIN. EMER BRAKE APPLIED. NO FLAT SPOTS ON MAINS. REPLACED BRAKE CONTROL MODULE. OPS CHECK GOOD. IAW P300 AMM 32-41-07.
ON TAXI OUT, BRK FAIL CAS ILLUMINATED AFTER TAXIING FOR 10 MIN. EMER BRAKE APPLIED. NO FLAT SPOTS ON MAINS. REPLACED BRAKE CONTROL MODULE. OPS CHECK GOOD. IAW P300 AMM 32-41-07.
BRK FAIL YELLOW CAS CAME ON DURING TAXI OUT OF RAMP CORRECTIVE ACTION; REMOVED AND REPLACED BRAKE CONTROL MODULE !AW PHENOM 300 AMM 32-41-07. OPS CHECK GOOD. NO DEFECTS NOTED.
MAIN DOOR: CAN NOT CLOSE MAIN ENTRY DOOR. THE DOOR APPEARS SAGGED DOWN OR OUT OF ALIGNMENT. PINS ARE RETRACTED AND THERE IS NOTHING VISIBLY OBSTRUCTING THE DOOR YET DOOR WILL NOT ALIGN AND CLOSE.
LEFT MLG BRAKE: WHILE TAXING, JUST BARELY TOUCHING THE BRAKES, THE BRAKES WOULD GRAB AND JERK THE AIRCRAFT! BOTH LEFT AND RIGHT SIDE! ALSO DURING SHARP TURNS, THERE WAS A GRINDING SOUND.// SIGNOFF// RESEARCHED AC SYSTEM SYSTEM DESCRIPTION OPERATION, MM PROCEDURES & AC HISTORY. ARRIVED AT AC. REQUESTED AND WAITED FOR AC REPOSITION INTOHANGAR FOR MX CONVENIENCE, EXTENDED WAIT DUE TO HEAVY INCOMING TRAFFIC. PREPPED FOR EMBRAER RECOMMENDATIONS. ACCOMPLISHED GVI OF BRAKE ASSY, BRAKE WEAR PINS IAW EMB-505 AMM 32-45-21 NO DEFECTS NOTED. CONFIRMED HYD RESERVOIR LEVEL SATISFACTORY IAW 12-13-00 NO DEFECTS NOTED. ACCOMPLISHED BLEEDING OF MAIN HYD SYSTEM IAW EMB-505 AMM 29-10-00 DURING BLEEDING OF RH BRAKE ASSY FOUND SUBSTANTIAL AMOUNTS OF AIR. CHECKED AND SERVICED NLG AND MLG TIRES IAW EMB-505 AMM 12-14-00. ACCOMPLISHED GVI OF MLG WHEELS IAW EMB-505 AMM 32-45-00 NO DEFECTS NOTED. CHECKED MLG SHOCK ABSORBER IAW EMB-505 AMM 12-14-02 WITH NO DEFECTS NOTED. TOWED AC OUT OF HANGAR, PREPPED FOR TAXI CHECK. COORDINATED WITH AIRPORT OPERATIONS FOR TAXI CHECK. AIRPORT EXPERIENCED LARGE AMOUNT OF TRAFFIC DUE TO LOCAL EVENT, WAITED FOR TAXI CLEARANCE FOR 45MINS. PERFORMED TAXI CHECK, BRAKE APPLICATION SMOOTH THROUGH ENTIRE BRAKE TRAVEL. NO ABRUPT BRAKING WHEN SLIGHT BRAKE APPLIED. TAXI CHECK GOOD. WORK DONE IAW EMB-505 AMM 71-00-00. 28JAN2024
MAIN DOOR: MAIN ENTRY DOOR BINDS UPON CLOSURE.. WILL NOT CLOSE FULLY. OPEN MAIN CABIN DOOR, INSPECTED, PINS, SEALS, INSIDE AND OUTSIDE DOOR HANDLE. NO DISCREPANCY NOTED. CHECKED DOOR LOCKS INDICATOR NO DISCREPANCY NOTED. OPEN AND CLOSED MAIN DOOR SEVERAL TIMES FROM INSIDE AND OUTSIDE. NO DISCREPANCY NOTED VERIFIED AIRCRAFT STATUS PAGE INDICATION STATUS. INDICATED WHEN DOOR IS OPEN AND CLOSE. NO CAS MESSAGE RELATED TO THIS ISSUES IAW PHENOM 300 AMM 52-10-00 UNABLE TO DUPLICATED DOOR ISSUE.
AFTER TAKEOFF WE SELECTED GEAR UP. THE LEFT MAIN LANDING GEAR DIDN'T FULLY RETRACT (YELLOW CROSSHATCH ICON) THEN AN LG LEVER DISAG RED-CAS MESSAGE POSTED. WE FOLLOWED THE CHECKLIST AND SELECTED THE GEARLEVER DOWN. ALL WHEELS PROPERLY DEPLOYED AND WE GOT THREE GREEN. WE LANDED WITHOUT ANY PROBLEMS. //SIGNOFF//REMOVED DEFECTIVE UPLOCK BOX ASSEMBLY PN 2617-1000-401 SN 00850, REMOVE THE UPLOCK SENSOR FROM OLD UPLOCK ASSEMBLY AND INSTALLED IT ON THE REPLACEMENT UPLOCK ASSEMBLY, INSTALLED CUSTOMER SUPPLIED REPAIRED UPLOCK ASSEMBLY PN 2617-1000-401 SN 00041, PERFORMED OPS AND LEAK CHECK, OPS AND LEAK CHECK GOOD IAW PHENOM 300 AMM 32-31-05
ENROUTE THE CABIN EMERGENCY LIGHTING BEGAN TO FLASH ON AND OFF. REMOVED AND REPLACED THE #1 AND# 2 EMERGENCY LIGHT POWER UNIT WITH A TESTED UNITS IAW EMB-505AMM 33-52-01-000-801-A AND 33-52-01-400-801-A. SYSTEM OPERATIONAL CHECK GOOD.
AFTER NORMAL START WITHOUT GPU, WE STARTED TAXIING AND DID THE NORMAL BRAKE CHECK. AFTER MOVING ABOUT 60' ONTO A TAXIWAY I GENTLY APPLIED THE BRAKES AND GOT A YELLOW CAS BRAKE FAIL. THE BRAKES PEDALS THEN FELT AS IF THERE WAS NO PRESSURE. I USED THE PARKING BRAKE TO STOP. TOUBLESHOT TO FAULTY BRAKE CONTROL MODULE, REMOVED AND REPLACED BRAKE CONTROL MODULE IN ACCORDANCE WITH PHENOM 300MM 32-41-07, COMPLIED WITH HYDRALIC SYSTEM OPS CHECK IN ACCORDANCE WITH PHENOM 300MM 29-10-00 NO DEFECTS NOTED. COMPUED WITH BRAKE SYSTEM FUNCTIONAL CHECK IAW MM 32-41-00, NO DEFECTS NOTED, LEAK CHECK PERFORMED NO DEFECTS NOTED,
CABIN EMERGENCY LIGHTS FLASHING IN FLIGHT. EMOVED EMERGENCY POWER UNIT PN:7450LS-00 SN:005344. INSTALLED TESTED UNIT PN 7450LS-00 SN:005655. OPS CHECK GOOD NO DEFECTS NOTED. ALL WORK PER PHENOM 300 EMB 505S AMM 33-52-01.
EMERG LIGHT SWITCH: EMER LIGHTS STAY ILLUMINATED WITH SWITCH IN ARM POSITION. REMOVED FAILED #I & #2 EMERGENCY BATTERIES AND INSTALLED SERVICEABLE #I & #2 EMERGENCY BATTERIES IA W EMS PHENOM 300 AMM 33-52--0 I. OPS CHECKS GOOD.
LEFT MLG BRAKE: LEFT BRAKE WAS VERY ON FIRST LANDING (LEFT SEAT). THE SECOND LANDING WAS OK (RIGHT SEAT). ON TAXI OUT, LEFT BRAKE IS EXTREMELY GRABBY AND JERKS OUT AROUND WITH SHUDDER FROM LEFT SEAT ONLY. WE ALSO FELT A VIBRATION. DURING TAXI BACK TO RAMP, BRAKE FELT NORMAL ON FROM BOTH SEATS. // SIGNOFF// REMOVED AND REPLACE BRAKE CONTROL MODULE IAW EMB505 AMM 32-41-07, JACKED UP AIRCRAFT COMPLIED WITH GEAR SWINGS AND CYCLED FLIGHT CONTROLS. DOWN JACKED AIRCRAFT, BLEED BRAKES. WHEN PUMPING BRAKES NO MORE SQUEAL OR SHUDDERING. OPERATIONAL TEST AND LEAK CHECKED GOOD. NO DEFECTS NOTED REF. P-300 29-10-00. SERVICED HYD RESERVIOR TO PROPER LEVEL AS REQUIRED REF. P-300 MM. 12-13-00
COCKPIT EMERG LIGHT: EMERGENCY LIGHTS FLASHING DURING DECENT CYCLED SWITCH ON AND OFF. PUT SWITCHES IN ARM POSITION THEY STAYED ON DURING THE REST OF FLIGHT. // SIGNOFF // CHECKED E LIGHTS AND FOUND ALL LIGHT CAME ON WITH SWITCH IN ON POSITION. GAINED ACCESS TO FWD. & AFT BATTERIES AND CHECKED BATTERIES IA MB 300 SQL AND FILM WHEN FWD BATTERY WAS DISCONNECTED NO LIGHTS CAME ON. WITH AFT BATTERY DISCONNECTED ALL LIGHTS CAME ON. PUT AFT BATTERY IN FWD POSITION NO LIGHTS CAME ON #2 BATTERY IS DEAD AND WONT CHARGE. PARTS ON ORDER. 10-23-21. REMOVED FAULTY # 2 E- BATTERY PIN 6450LS-OO SIN 001495 AND INSTALLED NEW BATTERY PIN 7450LS-OO SIN 005781 CHARGED AND OPS CHECK GOOD IA MB300 AMM CHAPTER 33-52-01 REINSTALLED ACCESS PANELS.CHARGED E- BATTERIES IAW EMB 300 AMM CHAPTER 33-52-01
MAIN DOOR: RED HANDLE ON MAIN DOOR BROKE OFF. NORMAL FORCE WAS USED TO OPEN DOOR. REMOVED AND REPLACED MCD EXTERNAL HANDLE DUE TO HANDLE BROKEN, OPS CHECKS GOOD, ALL WORK DONE IAW AMM 52-10-00.
BRK FAIL YELLOW CAS: ON TAXI OUT AT KASG WE HAD A BRAKE FAIL CAS MESSAGE ILLUMINATE. I ATTEMPTED TO USE THE MAIN BRAKES TOO SLOW THE AIRCRAFT TO A STOP AND GOT NO INDICATION OF BRAKING ACTION. AT THAT POINT THE EMER/PARKING BRAKE WAS ENGAGED TO STOP THE AIRCRAFT. THE FBO TOWED US BACK TO THE RAMP. // SIGNOFF// COMPLIED WITH CMC DOWNLOAD AND SENT TO THE CONTACT CENTER I.A.W EMB-505S AMM 45-45-00 COMPLIED WITH FIM 32-41-00-810-813-A RAN-UP #1 AND #2 ENGINES AND OPERATIONAL CHECKED BRAKES WITH NO CAS FAULTS NOTED I.A.W EMB-505S AFM OPENED UP LAV AREA TO GAIN ACCESS TO BCU TO REMOVE FOR TROUBLESHOOTING OPEN BELLY PANEL 194EL TO ACCESS BCM REOVED ALL CONNECTORS FOR TROUBLESHOOTING C/W BLOCK DIAGRAM 1,6,7 REMOVED BCM UNIT WITH FAULT P/N DAP00101-02 S/N 64JN INSTALLED A INSPECTED/TESTED UNIT P/N DAP00101-02 S/N 21KA TSO: 1614 CSO: 1009 LEAK CHECKED AND OPERATIONAL CHECKED/TAXI CHECK WITH NO FAULTS NOTED I.A.W EMB-505S AMM 32-41-07
BRK FAIL YELLOW CAS: AFTER BLOCK OUT AND TAXIING 150 YARDS YELLOW CAS MESSAGE APPEARED. BRAKES FAILED ON BOTH SIDES . // SIGNOFF// -PERFORMED OPS CHECK OF THE HYDRAULIC SYSTEM AND FUNCTIONAL CHECK OF THE BRAKE SYSTEM. ALL SYSTEMS CHECK ARE SATISFACTORY. NO DEFECTS NOTED 'PERFORMED FINAL SERVICING OF THE HYDRAULIC RESERVOIR. ALL WORK WAS ACCOMPLISHED LAW EMB 505 AMM 12-13-00, 29-10-00 AND 32-41-00.PERFORMED CMC DOWNLOADS AND SENT TO EMBRAER. ATTEMPTED TO DUPLICATE THE SQUAWK BY RUNNING ENGINES. PERFORMED MULTIPLE APPLICATIONS OF THE BRAKES AND RECEIVED NO FAILURES. INTERROGATED THE CMC AND FOUND FAULT CODE 32421300. LOOKED UP THE FAULT CODE IN THE FIM AND IT POINTED TO FIM TASKN32-41-00-810-813-A. EMBRAER ALSO ADVISED US TO PERFORM THE SAME TASK. ACCOMPLISHED FIM TASK AND FOUND NO DEFECTS. ATTEMPTED SEVERAL MORE TIMES TO GET THE BRAKES TO FAIL BUT THE FAILURE NEVER RETURNED. PER EMBRAER RECOMMENDATION , THE BRAKE CONTROL MODULE WILL NEED TO BE REPLACED. REMOVED THE BCM AND INSTALLED AN INSPECTED/TESTED UNIT IAW EMB 505 AMM 32-41-07. SERVICED RESERVOIR AND PERFORMED HYDRAULIC SYSTEM BLEEDING.
WHILE COMPLYING WITH EMBRAER SB 505-55-0004 FOUND THE FOLLOWING FLIGHT CONTROL BALANCE WEIGHTS NOT ACCEPTABLE PER SB AND REPLACED WITH NEW PARTS. ONE LT ELEVATOR HORN WEIGHT P/N PE915109-L42, ONE LT ELEVATOR OB INTERNAL WEIGH P/N PE915109-L41, FOUR LT ELEVATOR ADJUSTABLE WEIGHTS P/N PE915109-L33, ONE RT ELEVATOR HORN WEIGHT P/N PE915109-L42, AND FOUR RT ELEVATOR ADJUSTABLE WEIGHTS P/N PE915109-L33.
BOTH FLAP EXTENSION FAIL, FCE FAULT. DURING CLIMB, AUTOPILOT DISENGAGED AND SWPS FAULT AND SPOILER FAULT CAS MESSAGES DISPLAYED. PERFORMED A FLAP SYSTEM OPERATIONAL CHECK IAW MM 27-50-00. OPS CHECKED GOOD, NO ACTIVE FAULT MESSAGES DISPLAYED. CONSIDERED TRANSITORY CONDITION.