N360QS
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
AFTER 1ST NR 2 ENGINE START, PAX DOOR OPEN CAS MSG ILLUMINATED. ATTEMPTED NUMEROUS TRYS OPENING & CLOSING THE DOOR. NO VISIBLE OBSTRUCTIONS. FROM INSIDE, IT APPEARS THE TOP LEFT PIN MAY NOT BE CLOSING ALL THE WAY. ACCOMPLISHED INSPECTIONS & OPS CHKD OF MED AS REQUIRED. ALL CHKD GOOD IAW AMM 52-11-00, SL: 505-52-0001 AND STEPS FOR WORK ACCOMPLISHED .
CABIN EMERGENCY LIGHTS WERE FLASHING IN FLIGHT IN THE ARM POSITION. REMOVED AND REPLACED FWD AND AFT EMERGENCY BATTERIES IAW AMM 33-52-01. OPS TEST CHECKED GOOD AND RECHARGED. NO DEFECTS NOTED.
FUSELAGE DRAIN: BETWEEN 12000 AND 16000, WE EXPERIENCED A SUDDEN ONSET VIBRATION SEEMINGLY ORIGINATING FROM THE FLOOR AREA NEAR THE COCKPIT. WE COULD HEAR A LOUD VIBRATION AS WELL. IT DISSIPATED AS WE CLIMBED ABOVE 16,000. IT MAY NOT BE AUDIBLE IN ATTACHED VIDEO, BUT WE INCLUDED TWO VIDEOS (1ST WITH VIBRATION, 2ND AFTER IT STOPPED.) DISCUSSED IN FLIGHT WITH MAINTENANCE CONTROLLER WHO SUGGESTED POTENTIAL PRESSURIZATION DRAIN ISSUE AND AOG. CORRECTIVE ACTION; REMOVED AND REPLACED 2 EACH FUSELAGE DRAINS, ONE HAD A WEEK SPRING AND OTHER WAS CRACKED UPON REMOVAL ALL WORK ACCOMPLISHED IAW PHENOM 300 AMM 53-05-00
ABOVE FL 180, IN LEVEL FLIGHT, 300KTS OR ABOVE INDICATED, LOUD ACOUSTIC HUM FROM MID CABIN, RIGHT SIDE. ALSO A SLIGHT VIBRATION CAN BE FELT THERE TOO, ABOVE FL 230, A THUD CAN BE FELT IN COCKPIT FLOOR. CORRECTIVE ACTION; UPON INSPECTION OF AIRCRAFT FOUND THE FORWARD WING TO FUSELAGE FAIRING SEAL AFT TRAILING EDGE SEPARATED FROM THE AIRFRAME. COMPLIED WITH WING TO FUSELAGE FAIRING SEAL RTV APPLICATION REF. WC NO. E50-53-0001_1. RESECURED AFT TRAILING OF EDGE SEAL. NO DEFECTS NOTED AT THIS TIME.
ABOUT 15 MINUTES PRIOR TO LANDING ALL THE EMERGENCY LIGHTS IN THE CABIN BEGAN TO FLICKER AND CONTINUED ALL THE WAY THROUGH SHUT DOWN. WE CHECKED AGAIN ON THE GROUND, AND THE CABIN EMERGENCY LIGHTS WERE STILL FLICKERING. REMOVED AND REPLACED #1 FWD POSITION ON AND #2 AFT POSITION EMERGENCY LIGHT BATTERY #1 PN OFF 7450LS-00 S/N 006086 #2 PN OFF 7450LS-00 S/N 007669
DURING TAKEOFF, CREW NOTICED A LOUD SQUEAL COMING FROM THE AREA NEAR THE EMERGENCY OVER WING EXIT. TECHS SET UP FOR ENG RUN. AFTER ENGINES ARE STARTED, WE PRESSUREIZED THE CABIN TO DELTA 0.7 AND HEARD THE SQUEAL FROM EMERGENCY EXIT. REMOVED EMERGENCY EXIT AND COMPLETED GVI OF THE EXIT. FOUND LOTS OF DIRT ON VENT FLAP. CLEANED AND REINSTALLED EMER EXIT. THREE TECHS STARTED ENG AND PRESSURED TO DELTA 1.0 WITH NO SQUEAL NOISE. NO FURTHER DISCREPANCIES NOTED. REF: AMM 52-20-20
CLIMBING THRU 29,000 FT, RECEIVED BLD 1 LEAK CAS IND. FOLLOWED QRH, REDUCE POWER NR 1 ENG & WAITED 3 MINS FOR MESGE TO EXTING. 3 MINS, MESGE EXTINGUISH. RETURNED TO KSAT. BLD 1 LEAK MESGE RETURNED. INTERMIT & FOLLOWED CHKLIST, SHUTDOWN NR 1 ENG. DECLARED AN EMERGENCY & LANDED. MESGE INTERMIT TO GROUND. ILLUM & THEN OUT FOR ABOUT A MIN. RAN ENGS AT 50% N1 & BLD 1 CAS MESGE ILLUM & STAYED ON. ANALYSIS INDICD BLD LP 3 LEAK. PERFED FAULT ISOL IAW FIM 36-21-00-810-805. PERFRD VIS INSP OF BLD LEAK THERMOSTATS. R & R THERMOSTAT S0395, WIRING TOUCHING ACM DUCT & BURN TO INSULATION. PERFRD RESIST CHKS, NO DEFECTS. R & R RESISTOR R0107 IAW SWPM 20-41-20, WD 36-20-50-1. RAN ENGS W/BLD ON & NO DEFECTS & NO GROUND. IT
MAIN DOOR TELESCOPING ROD: TELESCOPING ROD MOUNT BROKEN. COMPLIED WITH THE ETD2022-P300-04650764 AND INSTALLED NEW TELESCOPIC ROD FITTING P/N 500-09754-001 S/N N/A. INSTALLED NEW SHROUD AFT PAX DOOR PN: 506-45250-4002 SN: N/A. ALL WORK PERFORMED IAW EMB PHENOM 300 AMM CHAPTER 52-10-00.
MAIN DOOR HANDLE: TEFLON SLIDER BEHIND MAIN ENTRY HANDLE FALL OFF // SIGNOFF// REMOVED FAULTY MAIN DOOR EXTERNAL HANDLE PN: UKN. INSTALLED NEW MAIN DOOR EXTERIOR HANDLE PN 505-09870-403 WITH A NEW BEARING PN: MS27646-41 AND NEW HARDWARE AS NEEDED. SWAPPED THE KEY LOCK TO THE NEW HANDLE AS IT DOESN'T COME WITH ONE. PERFORMED OPS CHECK OF THE MAIN PASSENGER DOOR AND OPS CHECK WAS SATISFACTORY. RETURNED THE AIRCRAFT TO ITS ORIGINAL CONDITION. WORK WAS PERFORMED IRW PHENOM 300 AMM 52-11-24 AND AMM 52-11-26.
BEFORE ENGINE START, AFTER CLOSING MAIN CABIN DOOR, RED PASSENGER DOOR WARNING REMAINED ILLUMINATED. DOOR LOCK FLAGS (2) ARE NOT VISIBLE ON MAIN CABIN DOOR. FOUND HARNESS FOR MED AIRSTAIR LIGHT NOT PROPERLY ROUTED AND GROMMET NOT IN PLACE. ADJUSTED HARNESS AND RESET GROMMET. INSTALLED MED AIRSTAIR AND LININGS PERFORMED FURTHER OPERATIONAL CHECKS OF MED. ALL OPERATIONAL CHECKS SATISFACTORY MECHANICALLY AND ELECTRICALY. NO FURTHER DEFECTS NOTED AT THIS TIME. IAW AMM 52-14-00-400-801-A
MAIN DOOR VISUAL INDICATOR: LOCK INDICATOR LENS MISSING, WHEN VIEWED WITH DOOR OPEN, LOCATED FORWARD AND MIDWAY ON DOOR. *** CORRECTIVE ACTION *** FOUND DOOR INDICATOR WINDOW WITH MISSING LENS. ACCESS WILL NEED TO BE GAINED TO LOCATE MISSING LENS. GAINED ACCESS TO MAIN DOOR INTERNALS BY GAINING ACCESS REF PHENOM 300 AMM 52-14-00. WAS ABLE TO LOCATE MISSING LENS. REATTACHED LENS IN APPROPRIATE LOCATION AND SECURED WITH ADHESIVE. REINSTALLED ALL ACCESS GAINED. WORK PERFORMED REF PHENOM 300 AMM 52-14-00.
MAIN DOOR: MAIN ENTRY DOOR "HANGS UP" ABOUT THE HALFWAY OPEN POINT. DOOR IS DIFFICULT TO OPEN THE REMAINDER OF THE WAY WITH THE RED HANDLE. STANDING ON THE TOP STEP IS REQUIRED TO OPEN THE DOOR FURTHER. WHEN CLOSING YOU CAN FEEL RESISTANCE AT ABOUT THE SAME POINT.//CORRECTIVE ACTION// TROUBLESHOT THE DISCREPANCY FOUND THE MAIN ENTRY DOOR HINGES AND LOCK PINS DRY OUT. CLEANED AND LUBRICATED MAIN ENTRY DOOR IAW EMBRER PHENOM 300 AMM 52-11-21. COMPLIED MULTIPLE TIEM OPENING AND CLOSING THE MAIN ENTRY DOOR NO DEFECTS NOTED AT THIS TIME.
MAIN DOOR: MAIN CABIN DOOR WILL NOT OPEN OR CLOSE PROPERLY. DOOR GETS STUCK HALFWAY THROUGH ITS TRAVEL GOING UP OR DOWN. // SIGNOFF // REPLACED AFT PASSENGER DOOR TELESCOPING ROD IA W EMBRAER 505 AMM 52-10-00. NO SERIAL NUMBER FOUND ON ASSY.
CABIN EMERGENCY LIGHTS FLASHING IN FLIGHT WITH THE EMER LT SWITCH IN ARM. CORRECTIVE ACTION: REMOVED FWD EMER BATTERY P/N 6450LS-00, S/N 001098 AND AFT EMERGENCY BATTERY P/N 6450LS-00, S/N 000966 AND INSTALLED MODIFIED UNIT. OPERATIONS CHECKS GOOD. THIS SDR IS A CORRECTION TO THE SDR FILED EARLIER TO CORRECT THE UNIQUE CONTROL FROM #DXTA202101310465 TO IT IS A CORRECTION TO DXTA2021013104658.
WHILE COMPLYING WITH EMBRAER SB 505-55-0004 FOUND THE FOLLOWING FLIGHT CONTROL BALANCE WEIGHT TO NOT MEET SB SPECIFICATIONS AND REQUIRING REPLACEMENT: ONE LT ELEVATOR HORN WEIGHT P/N PE915109-L42, TWELVE LT ELEVATOR ADJUSTABLE WEIGHTS P/N PE915109-L33, ONE RT ELEVATOR HORN WEIGHT P/N PE915109-L42, AND FIVE RT ELEVATOR ADJUSTABLE WEIGHTS P/N PE915109-L33.
DURING THE TAIL CONE REMOVAL FOR ELEVATOR CONTROL CABLE INSPECTION FOUND THE LT ROD ASSY FOR THE RUDDER TORQUE TUBE DAMAGED. PN AFFECTED WAS 3836-2.
NOTED A STRONG ODOR FROM PRESSURIZATION SYS WHEN ENGS STARTED & VERY LOUD ROARING SOUND DURING TAKEOFF, CLIMB OUT, DESCENT & LANDING. PERFORMED ENG RUNS & PRESSURIZED ACFT TO 4.2 PSI, AT TAKEOFF POWER SMELLED ODOR WITH NO SMOKE FOR APPROX 5 SECONDS. RETURNED ENGS TO IDLE THEN BACK TO TAKEOFF POWER. ODOR DID NOT RETURN. REPEATED 4 TIMES WITH NO ODOR OR ROARING SOUND IAW AMM 21-31-00 & 71-00-01.
UPON LANDING, DEPRESSED BRAKES AND POWER BRAKE LOW PRESS LIGHT CAME ON AND ANTI SKID INOP LIGHT CAME ON. BRAKES WENT TO THE FLOOR. HAD TO USE THE EMERGENCY RED BRAKE HANDLE. FOUND LT BRAKE FLEX LINE AT STRUT LEAKING. REMOVED DEFECTIVE LINE. INSTALLED NEW LINE. BLED BRAKES, LEAK AND OP'S CHECKED GOOD. SERVICED BRAKE RESERVIOR AND EMERGENCY AIR BOTTLE. ALL WORK DONE IAW MM SECTION 32-40-00.
DURING POSTFLIGHT, DISCOVERED DENT IN LT ENGINE PYLON. EVALUATED DAMAGE. REMOVED PYLON LEADING EDGE. INSTALLED NEW LEADING EDGE WITH SEALANT AND RIVETS. PRIMED & PAINTED LEADING EDGE. PER MM 20-33-00. REINSTALLED THE FIRE SEAL REATINERS. IAW SRM 51-30-03.
DURING TAKEOFF ROLL AT 50 KIAS, RED "HDG" FLAGS APPEARED ON CAPTAIN PFD, MFD, AND SIMULTANEOUSLY ON STBY HSI. AFTER 15 SECONDS RED FLAGS DISAPPEARED AND HEADING DATA WAS ONCE AGAIN AVAILABLE ON SAID INSTRUMENTS REMOVED AND REPLACE NR 1 DG IAW MM 34-21-05. OPS CHECKS GOOD.
DURING TAKEOFF ROLL AT 50 KIAS, RED "HDG" FLAGS APPEARED ON CAPTAIN PFD, MFD, AND SIMULTANEOUSLY ON STBY HSI.
AT FL 280 AND 275 KTS RECEIVED AMBER ANNUNCIATOR (AP PITCH MIS-TRIM) AND (TRIM DN), MANUALLY DISCONNECTED AUTOPILOT AND ATTEMPTED TO TRIM DOWN MANUALLY AND ELECTRICALLY, BUT AIRCRAFT WAS FULLY TRIMMED NOSE DOWN TO THE STOP. IN THIS CONDITION AIRCRAFT STILL PITCHED UP. FOUND THE ELEVATOR TRIM CONTROL SYSTEM OUT OF RIG. RIGGED THE TRIM SYSTEM IAW MM. CHAPTER 27-31-00 SYSTEM OPS CHECKS GOOD AT THIS TIME
PILOT'S LEFT BRAKE HAS TENDENCY TO GRAB WHILE TAXING WITH MINIMAL PEDAL PRESSURE. CO-PILOT BRAKES MUST BE DEPRESSED 2 - 3 INCHES BEFORE ANY PRESSURE IS FELT. BLEED BRAKES IAW C560MM CHAPTER 32-42-00, OPS CHECK GOOD.
AFTER RAISING GEAR RED GEAR UNLOCKED LIGHT AND AMBER HYDRAULIC PRESS ON REMAINED ILLUMINATED. PERFORMED RESISTANCE CHECKS ON LT AND RT UPLOCK SWITCHES. BOTH CHECKED GOOD. PERFORMED RESISTANCE CHECK OF NOSE UPLOCK SWITCH. CKD GOOD. DURING LANDING GEAR FUNCTIONAL TEST, FOUND LT MLG UPLOCK HOOK NOT RETRACKING TO THE (CATCH) POSITION. REMOVED HOOK THRU BOLT. CLEANED AND LUBED AND REINSTALLED. LANDING GEAR SYS. OPS CHECKED GOOD IAW MM CHAP. AFTER RAISING GEAR RED GEAR UNLOCKED LIGHT AND AMBER HYDRAULIC PRESS ON REMAINED ILLUMINATED.
REPEAT WRITE UP. ON DESCENT INTO TEB, RUDDER PEDALS WOULD JERK RIGHT AND LEFT. SEEMS TO BE HAPPENING WHEN AFIS SENDS AND RECEIVES.