N379QS
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
RED "DOOR PAX OPEN" CAS MSG CAME ON 41 MINUTES INTO THE FLIGHT. CRUISE ALTITUDE WAS 41,000 FEET AND OUTSIDE AIR TEMP -26C. ALL PRESSURIZATION INDICATIONS WERE NORMAL, DOOR LATCHES CHECKED GOOD ON PRE/POST FLIGHT. CORRECTIVE ACTION: REMOVED SUSPECTED DAMAGE PAX DOOR HARNESS P/N 505-24447-401 5/N F038683319 AND INSTALLED NEW CUSTOMER SUPPLIED PAX DOOR HARNESS P/N 507-26093-401 S/N F043927034. PERFORMED OP CHECKS WITH NO DEFECTS NOTED. INSTALLED PAX DOOR AIRSTAIRS AND CLOSED ALL GAINED ACCESS. REF EMB505 AMM 52-14-00, WSM 52-70-50
IN FLIGHT, NOTICED EMERGENCY LIGHTS CAME ON WITH SWITCH IN ARM POSITION. AFTER LANDING, TURNED SWITCH TO OFF AND BACK TO ARM AND LIGHTS STILL REMAINED ON. DURING TROUBLESHOOTING FOUND EMERGENCY LIGHT CIRCUIT BREAKER TRIPPED, AFTER RESET, SELECTED EMERGENCY LIGHT SWITCH TO ARM & EMERGENCY LIGHTS WENT OFF. FOUND EXIT MARKER LIGHT AT MAIN ENTRY DOOR HALFWAY ON. REMOVED ENTRY DOOR EXIT MARKER SIGN IAW AMM 33-52-15-00A 801-A. LIGHT DEFECTIVE, INSTALLED NEW EXIT MARKER SIGN IAW AMM 33-52-15-400-801A. NO DEFECTS NOTED, PERFORMED OPS TEST IAW AMM 31-33-52-00-710-801A. NO DEFECTS NOTED.
STANDBY EMERGENCY POWER: AFTER MOVING THE CABIN EMERGENCY LIGHT SWITCH FROM THE OFF POSITION TO ARM, A "EMER LIGHT NOT ARMED" CAS MESSAGE APPEARED. AFTER NUMEROUS TIMES OF RECYCLING THE SWITCH THE CAS MESSAGE DISAPPEARED. HOWEVER, WHILE IN ROUTE, WE NOTICED THAT THE EMERGENCY LIGHTS IN THE CABIN WERE ILLUMINATED. WE WERE UNABLE TO EXTINGUISH THEM WITH ANY LIGHT SWITCH POSITION OTHER THAN OFF. THEY ARE NORMALLY EXTINGUISHED IN THE ARMED POSITION AS WELL. CORRECTIVE ACTION; REPLACED BOTH EMERGENCY BATTERY PACKS IAW PHENOM 300 AMM 33-52-01. OPS CHECK GOOD.
LAV SERVICE DOOR: LAV CAP CAME OFF IN FLIGHT AND BENT/WARPED LAV DOOR. CORRECTIVE ACTION; ONCE DOOR OPENED PANEL CORRECTED .PERFORMED A GVI OF THE DOOR AND FOUND NO DEFECTS NOTED. RESECURED THE LAV CAP WITH NO DEFECTS NOTED. WORK PERFORMED IAW EMB505 AMM 05-00-00.
REPAIR LH WING TRAILING EDGE. IAW ETD2024-P300-04893827-REV A. REPAIRED LH WING TRAILING EDGE USING PERMANENT REPAIR IAW ETD2024-P300-04893827-REV A. LH WING SKIN CORROSION. SEE TASK AND INSPECTIONS FOR DETAILS. THIS REPAIR IS CONSIDERED A MINOR REPAIR.
CABIN EMERG LIGHT: CABIN EMERGENCY LIGHTS CAME ON DURING CRUISE FLIGHT IN THE ARM POSITION. CYCLED SWITCH TO OFF AND BACK TO ARM, LIGHTS REMAINED ON. REMOVED ACCESS PANEL 223CLF TO GAINE ACCESS TO FRONT EMERGENCY BATTERY. REMOVED FRONT EMERGENCY BATTERY DUE BEING BAD. INSTALLED CUSTOMER SUPPLIED TESTED EMERGENCY BATTERY IAW AMM 33-52-01. REMOVED ACCESS PANEL 242AZ TO GAIN ACCESS TO REAR EMGERGENCY BATTERY. REMOVED REAR EMERGENCY BATTERY DUE TO BEING BAD. INSTALLED CUSTOMER SUPPLIED NEW EMGERGENCY BATTERY IAW AMM 33-52-01. PERFORMED FUCNTIONAL AND OPERATIONAL CHECKS IN REF TO AMM 33-52-01-710/720, OPS CHECK GOOD. REINSTALLED ACCESS PANELS 223CLF AND 242AZ IN REF TO AMM 06-46-00.
EMERG EXIT SIGN/LIGHT: MAIN CABIN DOOR LOWER EXIT SIGN LIGHT INOPERATIVE. (PRE-FLIGHT) // SIGNOFF// VERIFIED DISCREPANCY, GAINED ACCESS TO THE ELECTRICAL CONNECTOR OF THE LOWER MED EMER EXIT UGHT AND FOUND THE CONNECTOR DISCONNECTED AND WAS CAUGHT IN THE DOOR GEARING. RECONNECTED CONNECTOR AND VERIFIED OPERATION AND PROPER ROUTING OF THE WIRES. RESTORED ACCESS GAINED. WORK DONE IAW PHENOM 300 AMM CH. 33-52-U. OPS CHECKS GOOD.
EMERGENCY LIGHTING: WHEN EMER LT IS PLACED IN ARM POSITION CABIN LIGHTS, AISL LIGHTS AND EXIT LIGHTS ILLUMINATE AND FLASH ON AND OFF. SUSPECT WEAK EMER LIGHT BATTERY//CORRECTIVE ACTION// COMPLIED WITH CHARGING/ OPERATIONAL CHECK OF THE EMERGENCY POWER SUPPLY IAW TC-FLT-33-1001 REV 0 DATED 15DEC2021. OPS CHECK RESULTS PASS. NO FURTHER ACTION REQUIRED
EXTERNAL POWER: APPROX. 5 MIN AFTER AIRCRAFT WAS CONNECTED TO/POWERED BY GPU, SMOKE WAS NOTED IN CABIN, BAGGAGE COMPARTMENT AND OUTSIDE THE TAIL SECTION. BAG SMK WARNING CAS DISPLAYED ON EICAS. AIRCRAFT WAS IMMEDIATELY SHUT DOWN AND DISCONNECTED FROM GPU. UPON FURTHER INSPECTION BY MAINTENANCE, CDM WAS NOTED TO HAVE BURN MARKS. // SIGNOFF// REPLACE CDM MOTOR DUE TO FAILURE AND BURNING, REMOVED AND REPLACED THE COM MOTOR JAW PHENOM 300 AMM CH.21-52-01 .UPON FINAL OPERATIONAL CHECKS FOUND THE COMPRESSOR MOTOR STOPPING CAUSING THE MOTOR TO SUDDENLY STOP AND THE COMPRESSOR LEAKED OIL.SPOKE WITH MCC AND THEY ELECT TO REPLACED THE CDM ASSEMBLY AND THE UNIT LS PLACED ON ORDER. REMOVED AND REPLACED COM WITH INSPECTION UNIT AND REMOVED RECEIVER, INSTILLED NEW RECEIVER SERVLCED VCS IAW PHENOM 300 AMM 21-52-07. PERFORM ALL OPS CHECKS WITH NO DEFECTS NOTED. ALL WORK DONE IAW L'-300 AMM CH 21-52·01.
CABIN EMERG LIGHT: WAITED ON TAXI WAY FOR APPROXIMATELY AN HOUR WITH THE ENGINES RUNNING WAITING RO DEICE. WENT IN THE CABIN AFTER DEICE TO INSPECT THE WINGS AND NOTICED THE INTERIOR EMERGENCY LIGHTS FLICKERING ON/OFF RAPIDLY. RECYCLED THE SWITCH IN THE CABIN AND THE LIGHTS REMAINED ILLUMINATED IN THE ARM POSITION. SEVERAL MINUTES LATER STARTED FLICKERING ON/OFF AGAIN.//CORRECTIVE ACTION// REMOVED BOTH FWD AND AFT EMERGENCY BATTS AND INSTALLED 2 TESTED BATTERIES IAW EMB-505 AMM 33-52-01 ALL OPS CHECK GOOD. PN OFF:6450LS-00 SN OFF: 001671 PN ON:6450LS-00
MAIN DOOR HANDLE: MAIN DOOR EXTERIOR HANDLE IS BROKEN OFF OF THE AIRPLANE. REMOVED DAMAGED MAIN CABIN DOOR EXTERIOR HANDLE P/N PE25060-4C-25 AND INSTALLED CUSTOMER SUPPLIED NEW PART P/N PE25060-4C-25 AND OPS CHECKED GOOD WITH REFERENCE TO PHENOM 300 AMM 52-11-243.
AIRCRAFT CREW REPORTED "EMER LT NOT ARM YELLOW CAS: DURING ENGINE START WITH GPU, EMER LT NOT ARM CAS MESSAGE WOULD DISPLAY MOMENTARILY AND EXTINGUISH ON ITS OWN WITHOUT PILOT ACTION. CORRECTIVE ACTION: PERFORMED TROUBLESHOOTING BASED ON THE EMBRAER PHENOM 300 FIM TASK CHAPTER 33-50-00 AND FOUND NR 1 EMERGENCY BATTERY LIGHTS (COCKPIT) FAULTY. PERFORMED REPLACEMENT NR 1 (COCKPIT) EMERGENCY LIGHT BATTERY IN ACCORDANCE WITH PHENOM 300 AMM CHAPTER 33-52-01. PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHT BATTERY IN ACCORDANCE WITH PHENOM 300 AMM CHAPTER 33-52-00. NO DEFECTS NOTED. THIS REPORT COMPLIES WITH FAA 14 CFR PART 135 OPERATOR'S GMM REQUIREMENTS.
GND SPLR FAIL YELLOW CAS: ON APPROACH WE ATTEMPTED TO DEPLOY SPEEDBRAKES, BUT IMMEDIATELY GOT A FAIL MESSAGE AND A SWITCH DISAGREE MESSAGE. A MOMENT LATER, THAT WAS FOLLOWED BY A GND SPLR FAIL MESSAGE. THE FIRST TWO EXTINGUISHED WHEN THE SWITCH WAS PLACED IN THE CLOSED POSITION, BUT THE GND SPLR FAIL PERSISTED. PERFORMED FIM TASK 27-66-00-810-805. INSPECTED LVDT'S IAW AMM 27-66-02-210. NO DEFECTS NOTED. PERFORMED MULTIPLE FUNCTIONAL CHECKS IAW AMM 27-60-00-720-801 WITH NO DEFECTS AT THIS TIME.
WHEN EMERGENCY LT IS IN THE ARM POSITION, THE EMERGENCY LIGHTS IN THE CABIN FLICKER. CORRECTIVE ACTION: REMOVED AND REPLACED BOTH FWD AND AFT EMERGENCY LIGHT POWER UNITS, IAW EMBRAER PHENOM 300 AMM 33-52-01. OPERATIONS CHECK GOOD. FWD REMOVED P/N 6450LS-00 S/N 001201; FWD INSTALLED P/N6450LS-00 S/N 002172; AFT REMOVED P/N 6450LS-00 S/N 001214; AFT INSTALLED P/N 6450LS-00 S/N 000620.
DURING ACCOMPLISHMENT OF EMBRAER SB 505-55-0004 REV 01 PART I,II,III (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE: LEFT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (11 EACH BELOW MINIMUM OF 84G); HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH BELOW MINIMUM OF 1095G). RIGHT ELEVATOR MASS BALANCE WEIGHTS BELOW TOLERANCE: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (11 EACH BELOW MINIMUM OF 84G); HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH BELOW MINIMUM OF 1095G), ALL WEIGHTS HAVE BEEN REPLACED WITH A NEW MASS WEIGHTS AND THE ELEVATOR BALANCING WAS PERFORMED WITH NO FURTHER DEFECTS NOTED. THE LEFT ELEVATOR WAS RE-IDENTIFIED TO PART NUMBER 505-11082-601 AND THE RIGHT TO PART NUMBER 505-11082-602, AS PER SB INSTRUCTIONS. AT THE RUDDER WE NOTED THE ADJUSTABLE WEIGHTS PART NUMBER PE915109-L27 (4 EACH BELOW MINIMUM OF 455G), ALL WEIGHTS HAVE BEEN REPLACED WITH A NEW MASS WEIGHTS AND THE RUDDER BALANCING WAS PERFORMED WITH NO FURTHER DEFECTS NOTED. THE RUDDER WAS RE-IDENTIFIED TO PART NUMBER 505-39061-619, AS PER SERVICE BULLETIN INSTRUCTIONS. AT THE AILERON MASS WEIGHTS PART NUMBER PE915109-L31(1 EACH BELOW MINIMUM OF 1787G), ALL WEIGHTS HAS BEEN REPLACED WITH A NEW MASS WEIGHTS AND THE AILERON BALANCING WAS PERFORMED WITH NO FURTHER DEFECTS NOTED. THE AILERON WAS RE-IDENTIFIED TO PART NUMBER 505-14735-643, AS PER SERVICE BULLETIN INSTRUCTIONS. THIS REPORT COMPLIES WITH FAA 14 CFR PART 135 OPERATORâS GMM REQUIREMENTS.
AFTER TAKEOFF, NOTED LOW FREQUENCY RUMBLE ASSOCIATED WITH RIGHT THROTTLE MOVEMENT. THEN GOT GEN 2 OFF BUS CAS MESSAGE. RIGHT ENGINE SHUT DOWN IAW QRH. SIGNIFICANT CARBON VISIBLE ON BOTTOM OF RIGHT ENGINE ON POST FLIGHT. SIGN OFF. PERFORMED GVI OF RT ENGINE COWLS AND STARTER GENERATOR INTAKE AND EXHAUST, INTACT NO DEFECTS NOTED. EXHAUST NOTED CARBON BUILDUP ON COWL, POWERED AIRCRAFT UP WITH GPU, ATTEMPTED MULTIPLE DOWNLOAD OF FILE ALL WERE UNREADABLE, REMOVED STARTER GENERATOR AND FOUND PIECE OF METAL FELL OUT OF INTERNAL SECTION. INSTALLED OVERHAULED STARTER GENERATOR ON RT ENGINE, IAW EMBRAER AMM 24-31-01. REQUIRES OPS CHECK, DUE TO DCU UNAVAILIBLE FOR DOWNLOAD, PRATT AND WHITNEY. PERFORMED HIGH POWER ENGINE RUNS AND NO VIBRATION NOTED. OPERATIONAL CHECKS OF GENERATOR WAS GOOD, NO OTHER DEFECTS NOTED.
ALL LANDING GEAR RETRACTION DID NOT RETRACT - AFTER TAKEOFF THE GEAR LEVER WOULD NOT MOVE UP TO THE RETRACT POSITION. ABOUT 60 SECONDS LATER WE GOT A WOW MISCOMPARE MESSAGE. WE RAN THE EMER/ABNORMAL CHECKLIST, DECLARED AN EMERGENCY AND LANDED NORMALLY. // SIGNOFF // REMOVED WORN OUT NOSE LANDING GEAR SQUAT SWITCH CAM BRACKET AND FOUND THAT THERE WAS NOT A CAM BEARING SPACER INSTALLED IN THE SQUAT SWITCH CAM BRACKET. INSTALLED NEW CUSTOMER SUPPLIED CAM SPACER BEARING, WASHERS AND NUT ON THE NOSE LANDING GEAR SQUAT SWITCH CAM BRACKET LAW CE 680 CMM 32-20-01. JACKED AIRCRAFT AND PERFORMED A NLG SQUAT SWITCH ADJUSTMENT CHECK IAW CE 680 MM 32-60-00. PERFORMED THE OPERATIONAL TEST OF THE LANDING GEAR CONTROL SYSTEM IAW CE 680 MM 32-00-00 WITH NO FURTHER DEFECTS NOTED AT THIS TIME.
ON PUTTING THE LANDING GEAR DOWN ON APPROACH RECEIVED A CAUTION EMERGENY BRAKE LOW PRESSURE WITH EMERGENCY BRAKE PRESSURE SHOWING 0 ACCUMULATOR PRESSURE. RAN QRH AND DIVERTED. REMOVED AND REPLACED EMERGENCY PARKING-BRAKE THERMAL RELIEF VALVE AS REQUIRED. PERFORMED ALL REQUIRED BLEEDLNG TASKS, AND OPS CHECKS. COMPLIED WITH NUMEROUS SATISFACTORY GEAR SWINGS COMPLIED WITH FINAL SERVICING OF HYRDAULLC RESEVIOR IAW MM 12-13-00. NO FURTHER DEFECTS NOTED AT THIS TIME. REF. MM 32-43-08.
THE SMELL OF JET A WAS DETECTED IN THE CABIN DURING DESCENT. COMPLIED WITH FIM 21-20-00-810-801 WITH NO DEFECTS NOTED AT THIS TIME.
"ANTISKID" AND "PWR BRAKE" ANNUNCIATORS ILLUMINATED. EMERGENCY CHECKLIST PROCEDURES PERFORMED INCL SKID CONTROL BREAKER RESET, TO NO AVAIL. NO BRAKES UPON LANDING. TROUBLESHOT AND REPLACED RUPTURED BRAKE LINE ON RT GEAR BRAKE ASSY WITH A NEW BRAKE LINE ASSY IAW MM 32-42-01. BLED BOTH SIDES BRAKES IAW MM 31-41-00. BOTH LINE CLEARANCE CHECKED GOOD IAW MM 32-30-00. DURING GEAR EXTENSION/RETRACTION SLOW CYCLE, SERVICED BRAKE RESERVOIR TO FULL IAW MM 12-12-01 AND SERVICED EMERG BRAKE/GEAR BOTTLE IAW MM 12-13-01. LINE LEAK CHECKED GOOD.
COPILOT SIDE LT BRAKE PEDAL IS MUSHY AND GRABS AFTER APPROXIMATELY ONE-HALF PEDAL DEPRESSION. BLED BRAKES IAW MM 32-42-00 (REV 25). OPS AND LEAK CHECK ON RUN. TAXI CHECK GOOD ON PILOTS AND COPILOTS SIDE. CLOSED BRAKE RESERVOIR ACCESS PANEL. OK TO CLOSE BRAKE RESERVOIR ACCESS PANEL.
POWER BRAKES WILL NOT FUCTION "POWER BRAKE LOW PRESS" AND "ANTI SKID INOP" LIGHTS STAY ON. PUMP RAN CONTINUOUSLY BUT PRESSURE WAS BUILDING UP. UPON FURTHER INVESTIGATION FOUND PRESSURE RELIEF VALVE STUCK IN PUSHED POSITION. RELEASED PUSH BUTTON & BRAKE SYSTEM OPS CHECKED GOOD. FOUND RELIEF VALVE STICKS EVERY TIME IT IS PUSHED IN. REMOVED AND REPLACED BRAKE PRESSURE BLEED VALVE. OPS CHECK AND LEAK CHECK GOOD. NO DISC NOTED IAW MM 32-42-06
MAIN ENTRY DOOR UNLOCK LIGHT ILLUMINATED AFTER DEPARTURE AT ABOUT 200FT AGL. FOUND DOOR LOCK SWITCH PLUNGER NOT TO HAVE ENOUGH TRAVEL. ADJUSTED PLUNGER TRAVEL IAW MM 52-10-02. OPS CHECK GOOD.
COPILOT LT BRAKE PEDAL ONLY (SPONGY) DEPRESSES ALMOST ALL THE WAY TO FLOOR. CAN BE PUMPED UP TO ACHIEVE EFFECTIVENESS BUT PRESSURE IS RAPIDLY LOST IN PEDAL FOLLOWING PUMP UP. LT PILOT SIDE IS OK. PERFORMED BRAKE BLEEDING PROCEDURES ON ALL 4 BRAKE PEDALS. PERFORMED OPS CHECK , OPS CHECK GOOD. ALL WORK WAS PERFORMED IAW MM CH. 32-42-00.
BRAKING IS NOT NORMAL, HAVE TO APPLY MORE THAN NORMAL PRESSURE ON BRAKES, ALMOST STANDING ON THEM. BRAKES HAVE PRESSURE BUT FEEL SPONGY. BLED BRAKE SYSTEM. SERVICED RESERVOIR WITH 1 QT OF 500B-4. TAXIED AIRCRAFT. BRAKE OPERATION NORMAL. ALL WORK DONE IAW CITATION 560MM 32-42-00 AND 12-12-02.
UPON GEAR RETRACTION, GEAR RETRACTED NORMALLY. AFTER HYD PRESS ON LIGHT EXTINGUISHED, RIGHT MAIN GEAR LOWER WITHOUT COMMAND. CLEANED & INSPECTED RT MAIN GEAR UPLOCK ACTUATOR ASSY & MICROSWITCH FOUND DEBRIS ON ACTUATOR & MICROSWITCH FOUND ROLLER ON GEAR STICKING. CLEANED & LUBED ROLLER. LUBED UPLOCK ACTUATOR & MICROSWITCH. PERFORMED MULTIPLE GEAR SWINGS, OPS CHECK GOOD, NO OTHER DEFECTS NOTED AT THIS TIME. ALL WORK DONE IAW CESSNA 560 ULTRA MM 32-30-00.
AFTER LANDING AT SLC, DURING SHUTDOWN COCKPIT FILLED WITH THICK HEAVY SMOKE. FOUND AIR CYCLE MACHINE TO BE AT FAULT, REMOVED DEFECTIVE ACM AND INSTALLED OVERHAULED UNIT IAW HAMILTON STANDARD AND CESSNA 560 MM CHAPTER 21-50-03 PG 201 & 202, OPS CHECKS GOOD.
DURING ROUTINE INSPECTION, LOOKED INTO NACA SCOOPS AND SAW THE UPPER VANE PN 651207211 AND LOWER VANE PN 651207212 MISSING 1 INCH X 1 INCH AND A 1 INCH X 2 INCH PART OF VANE. BOTH CRACKS STARTED AT (V CUT). PARTS WERE FOUND DOWN STREAM PAST THE FRESH AIR CHECK VALVE AND THE OVERHEAD BLOWER WEDGED IN DUCT WORK. REPLACED BROKEN VANES WITH NEW AND SECURED IN PLACE WITH EA9309 IAW MM. BEFORE REINSTALLATION, WE DRILLED A RELIEF HOLE AT THE BOTTOM OF (V). AS WITH OTHER SCR`S, CONCERNED WITH THE BROKEN PARTS BECOMING WEDGED IN THE FRESH AIR CHECK VALVE (WHICH WOULD NOT ALLOW CABIN TO HOLD PRESSURE) AND OR THE OVERHEAD BLOWER FAN.