N404QS
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 SELECTING THE LANDING GEAR LEVER TO THE DOWN POSITION. WE RECEIVED 2 MAIN GEAR INDICATORS IN THE DOWN AND LOCKED POSITION (GREEN) AND THE NOSE INDICATOR WAS A RED HATCHED BOX. WENT AROUND, PER THE QRH WE CYCLED THE GEAR, RECEIVED 3 GREEN INDICATORS AND DIVERTED TO IAD. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NOSE LANDING GEAR UPLOCK BOX IAW EMB-505 AMM 32-31-05. BLEED UPLOCK ACTUATOR IAW EMB-505 AMM 32-31-05-870-801. PERFORMED OPERATIONAL CHECK OF EMERGENCY EXTENSION SYSTEM IAW EMB-505 AMM 32-35-00-710-801. PERFORMED FUNCTIONAL CHECK OF EXTENSIONAL AND RETRACTION SYSTEM IAW EMB-505 AMM 32-31-00-720-801. OPS CHECK SAT.
LINE SERVICE AGENT FOUND EMERGENCY LIGHTS FLASHING ON RT SIDE OF ACFT. RECHARGED EMERGENCY LIGHTS. OPS CHECKED IAW AMM 33-52-00.
DEPARTED MMUN, HEADING TO KAPF ABOUT 8 MINUTES OUT FROM LANDING ATC ADVISED US THAT THE CONTROLLERS FROM MEXICO SAID THAT A PART OF OUR AIRCRAFT FELL OFF THE PLANE AFTER DEPARTURE. DIVERTED TO RSW, DID A LOW FLY-BY, WAS TOLD ALL LANDING GEAR AND TIRES APPEARED NORMAL. LANDED, HAD CRASH FIRE RESCUE INSPECT THE PLANE AND PROCEEDED TO PARK THERE AFTER. A POST FLIGHT INSPECTION BY BOTH PILOTS REVEALED NOTHING OUT OF THE ORDINARY. INSPECTED LT & RT WING FOR ANY DAMAGE OR MISSING PANELS COULD NOT SEE ANYTHING. INSPECTED LT & RT MLG AND NOSE GEAR FOR ANY MISSING ALSO DID NOT NOTICE ANY DAMAGE OR PANELS MISSING. INSPECTED BOTH ENGINES FOR ANY DAMAGE, REMOVING TOP & BOTTOM COWLING TO INSPECT THE ENGINES, DID NOT NOTICE ANY DAMAGE OR ANYTHING THAT WAS WRONG. NEXT THE FUSELAGE WAS INSPECTED THE BELLY AND ROOF OF AC ALL ANTENNAS WERE IN TACK AND IN PLACE. INSPECTED THE RUDDER AND THE TAIL OF AC FOR ANY DAMAGE OR MISSING PANELS AND DID NOT SEE ANYTHING MISSING OR OUT OF PLACES ALL WORK WAS DONE IAW AMM 32-00-00, 53-00-20; 57-03-00; 72-00-00
FLAP FAILED BETWEEN 1 AND 2. REVIEWED PREVIOUS STEPS AND PROCEEDED WITH THE FOLLOWING: SWAPPED FCE 1 & 2. PERFORMED RIGGING OF FLAP SYSTEM FOR FCE 1 AND PERFORMED OPS CHECKS OF FLAP SYSTEM S TIMES IAW AMM. WORK DONE IAW EMB-505 AMM 27-50-00. PERFORMED RIGGING OF MULTIFUCNTION SPOILER SYS & OPS CHECKS OF SPOILER SYSTEM 5 TIMES AS REQUIRED BY AMM. WORK DONE IAW EMB-505 AMM 27-60-00. PERFORMED OPS CHECKS OF OPS CHECKS OF PITCH TRIM 5 TIMES AS REQUIRED BY AMM. WORK DONE IAW EMB-505 AMM 27-40-00. PERFORMED OPS CHECKS OF THE PRESSURIZATION SYSTEM AS REQUIRED BY AMM IAW AMM 21-31-00. ALL OPS & RIGGING GOOD. RETURNED TO AIRCRAFT TO ORIGNAL CONFIGURATION.
EMERGENCY LIGHTS STARTED FLICKERING DURING CRUISE. SWITCHED LIGHT TO OFF POSITION FOR 1 MIN, BACK TO ARM, & LIGHTS STARTED FLICKERING AGAIN AFTER 30 SECS. ACCESSED FWD & AFT BATTERY. DURING ACCESS & BEFORE MAINT PERFORMED, FOUND THE EMER LIGHT CLL ON, RESET THE CS. PERFORMED FJM IAW TASK 33-50-00-810-802-A. & THE BATTERY OPS TEST FAILED IAW MM 33-00-710-801-A. LIGHTS ARE FLICKERING WITHIN 1 MIN ON BOTH FWD & AFT BATTERIES CONNECTED. HAVE SAME RESULT WITH EITHER BATTERY DISCONNECTED & 1 BATTERY CONNECTED AT A TIME, EMER LIGHTS FLICKER WITHIN A MIN ON BOTH BATTERIES. BATTERIES ARE CURRENTLY CHARGING. THE.FORWARD BATTERY REPLACED OR HAD A CAP CHECK-FUNCTIONAL TEST ON 8-2-2025 WRITTEN ON THE STICKER ON TOP OF FWD BATTERY, MCC HAS REQUESTED THAT AFTER THE BATTERY CHARGE PROCESS THEY WOULD TAKE FOR ME TO PERFORM THE FLM/ OPS TEST OF THE EMER BATTERY MULTIPLE TIMES AND REPORT FINDINGS. THE BATTERY CHARGED FOR 30 MIN IN THE ARM POSITION, TURNED EMER LIGHTS ON & THEY STAYED ON FOR OVER AN HOUR. DISCONNECTED BOTH BATTERIES ONE AT A TIME & LIGHTS REMAINED ON. CHARGED THE BATTERIES AGAIN FOR 90 MINS. DURING CHARGING PROCESS, FOUND NUT PLATE IN THE AFT LAV FLOOR MOUNT FOR THE DLVIDER TO BE MISSING. REMOVED THE FLOOR PANEI & FOUND NUT PLATE .UNDER FLOOR. REQUESTED NUT PLATE & RIVETS TO REPAIR THE BAD NUTPLATE.
DURING FLIGHT, EMER LIGHTS FLICKERED A FEW TIMES & THEN STAYED ON CONTINUOUSLY FOR THE REST OF FLIGHT WITH THE SWITCH IN THE ARM POSITION. PERFORMED EMERGENCY LIGHTS BATTERY TOP CHARGE, PUT EMERGENCY LIGHTS SWITCH TO ON, LEFT ON FOR 30 MINS, PUT SWITCH IN ARM TO CHARGE BATTERIES AFTER ABOUT 25 MINS. THEY BEGAN FLASHING. REMOVED EMERGENCY BATTERY NR 1 & REPLACED WITH SUPPLIED REPAIRED BATTERY. REMOVED FAULTY EMERGENCY BATTERY NR 2 WITH SUPPLIED REPAIRED BATTERY. OPS CHECK GOOD WITH NO DEFECTS NOTED. WORK DONE IAW TC TC-505-33-200403, AND AMM 33-52-01.
IN CRUISE, FL430, AN AIR NOISE HEARD, FEELING A PRESSURE BUMP, & NOTED CABIN ALTITUDE FLUCTUATING BETWEEN -600FPM AND +400FPM. LASTED APPROX 4 MINS & LEVELED OFF AT 0. AFTER 10 MINS FLUCTUATIONS AGAIN, NOT EXCEEDING -300FPM TO +150FPM. LASTED ABOUT 3 MINS, RETURNING TO NORMAL. HAPPENED 3 TIMES, NEVER GETTING WORSE THAN ORIG CYCLE. DURING FLUCTUATIONS, PRESS MODE SELECTOR, SELECTED TO MANUAL, NO THRUST OR ALTITUDE CHANGES, FLUCTUATION STOPPED FOR 2.5 MINS. CREW RECEIVED A CABIN CLIMB RATE EXCEEDING 2500 FPM, & RAPID FLUCTUATIONS ONCE PRESS SELECTOR KNOB TO AUTO. R & R OUTFLOW VALVE ECMU CONTROLLER IAW AMM 21-31-01-000-801-A. R & R PRESSURE, A/CON CONTROL PANEL IAW AMM, 21-01-01-400-801-A. OP CHECKS GOOD.
CABIN EMERG LIGHT: EMER LIGHTS STAY ON IN ARMED POSITION. REMOVED AND REPLACED BAD FWD EMERGENCY BATTERY WITH CUSTOMER SUPPLIED NEW ONE OPS CHECK GOOD JAW EMB 300 33-52â¢01 OFF PN 74SDLS-00 SN 006677 ON PN 74SOLS·OO SN 007122. REMOVED AND REPLACED BAD AFT EMERGENCY BATTERY WITH CUSTOMER SUPPLIED NEW ONE OPS CHECK GOOD JAW EMB 300 33-52-01
FLAP FAIL YELLOW CAS: DURING DESCENT THROUGH FL220 WE EXPERIENCED THE INDICATIONS OF AN FCE1 FAILURE. ALL MESSAGES DISPLAYED SIMULTANEOUSLY. SWPS FAULT (YELLOW) FLAP FAIL (YELLOW) PTRIM BKP FAIL (YELLOW) SPOILER FAULT (WHITE) NO CONFIGURATIONS CHANGES WERE BEING COMMANDED AT THE TIME OF THE FAILURE.//CORECTIVE ACTION// CND FAULT, PERFORMED 3 SATISFACOTRY OPERATIONAL CHECKS OF THE FLAP SYSTEM. ALL WORK DONE IN REF TO PHENOM 300 AMM -27-50-00.
DURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01, ONE AILERON MASS BALANCE WEIGHT WAS FOUND TO BE BELOW MINIMUM WEIGHT. REPLACED WEIGHT WITH NEW, PART NUMBER PE915109-L31 PER SERVICE BULLETIN INSTRUCTIONS. THIS REPORT SUBMITTED TO COMPLY WITH PART 135 OPERATOR'S GENERAL MAINTENANCE MANUAL (GMM) REQUIREMENTS.
MAIN DOOR: LOWER LOCK INDICATOR ON MED IS NOT READABLE. VISOR IS IN PLACE BUT FLAG CANNOT BE SEEN. REMOVED MAIN ENTRY DOOR STEPS AND MOVED INTERIOR DOOR TAPE OUT OF THE WAY WHICH WAS OBSTRUCTING THE DOOR FLAG INDICATION ON MED LOWER WINDOW. REINSTALLED MAIN ENTRY DOOR STEPS AND SIDE TRIM. SYSTEM OPS CHECK GOOD, NO DISCREPANCIES NOTED AT THIS TIME. ALL MAINTENANCE ACCOMPLISHED IAW EMBRAER PHENOM 300 AMM 52-14-00.
AIRCRAFT CREW REPORTED AN EMERGENCY LIGHT IN ARM POSITION WILL NOT GO OUT. PERFORMED TROUBLESHOOTING BASED ON THE AMM CHAPTER 33-52-01 AND FOUND NR 2 EMERGENCY BATTERY LIGHT (AFT)FAULTY. PERFORMED REPLACEMENT #2(AFT) EMERGENCY LIGHT BATTERY WITH A TESTED BATTERY IN ACCORDANCE WITH AMM CHAPTER 33-52-01. PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHT BATTERY IN ACCORDANCE WITH AMM CHAPTER #33-52-00 WITH NO DEFECTS NOTED.
EMERGENCY LIGHTING: EMER LIGHT IN ARM POSITION WILL NOT GO OUT. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW EMB AMM 33-50-11.
DURING ACCOMPLISHMENT OF SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING: LEFT ELEVATOR ADJUSTABLE MASS BALANCE WEIGHTS BELOW TOLERANCE. PART NUMBER PE915109-L33 (13 EACH) AS FOLLOWS 5=82G,8=83G (MINIMUM 84G) AND HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH) 1=1091G (MINIMUM 1095G). ALL WEIGHTS HAS BEEN REPLACED WITH A NEW MASS WEIGHTS AND THE ELEVATOR BALANCING, WAS PERFORMED WITH NO FURTHER DEFECTS NOTED. THE ELEVATOR WAS RE-IDENTIFIED TO PART NUMBER 505-11082-601, AS PER SERVICE BULLETIN INSTRUCTIONS. WE ALSO NOTED THE FOLLOWING RIGHT ELEVATOR ADJUSTABLE MASS BALANCE WEIGHTS BELOW TOLERANCE: PART NUMBER PE915109-L33 (10 EACH) AS FOLLOWS 3=83G,6=82G,1=81G (MINIMUM 84G) AND HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH) 1=1082G (MINIMUM 1095G). ALL WEIGHTS HAVE BEEN REPLACED WITH A NEW MASS WEIGHTS, AND THE ELEVATOR BALANCING WAS PERFORMED WITH NO FURTHER DEFECTS NOTED. THE ELEVATOR WAS RE-IDENTIFIED TO PART NUMBER 505-11082-602, AS PER SERVICE BULLETIN INSTRUCTIONS. THIS REPORT COMPLIES WITH FAA 14 CFR PART 135 OPERATORâS GMM REQUIREMENTS.
RIGHT ENGINE - UPON DECENT A E2 OIL LO PRESS ILLUMINATED, WITH ASSOCIATED ENGINE PRESSURE INDICATION SHOWING 28 AND FALLING. THUS DIRECTING US TOWARD THE NAP 1-16 ENGINE SHUTDOWN PROCEDURE WHICH WE ACCOMPLISHED AND LANDED IN MSP. ///SIGN-OFF/// EVALUATED AND FOUND THAT THE RH ENGINE HYDRAULIC PUMP GARLOCK SEAL WAS LEAKING EXCESSIVELY, ALSO FOUND THAT THE RH ENGINE SG MAG SEAL IS SEEPING DUE TO SEAL BEING PINCHED, REMOVED HYDRAULIC PUMP GARLOCK SEAL AND INSTALLED NEW SEAL, REMOVED SG MAG SEAL AND INSTALLED NEW SEAL ALL WORK IAW PWC 535E MM CH 72-0-01 LK AND OPS CK GOOD.
WHILE FLYING AT FL410, RECEIVED A CAUTION WITH SWPS FAULT, FLAP FAIL, PTRIM BKP FAIL AND GND SPLR FAIL ANNUNCIATIONS. GROUND SPOILER ANNUNCIATION SWITCHED TO SPOILER FAULT. SSEC ALSO DISPLAYED ON THE BACKUP ATTITUDE INDICATOR. AIRCRAFT WOULD NOT DESCEND WITH AUTOPILOT VS. WERE EASILY ABLE TO HAND FLY AN ILS APPROACH AND FLEW AT FLAP 0 SETTING. 2 YELLOW X IN THE FLAPS DEPICTION AND TWO YELLOW X IN THE PITCH DEPICTION DISPLAYED. TRIED TO MOVE THE FLAPS ON FINAL WITH NO SUCCESS. MANUAL TRIP WORKED FINE. LANDING WAS NON-EVENTFUL. THE FLIGHT DIRECTOR LOCKED IN LEVEL FLIGHT INDICATION. CLICKED IT OFF FOR EASIER FLIGHT CONTROL INPUTS. REPALCED THE NR 1 FCE WITH MODIFIED UNIT IAW AMM 27-03-01-400-801-A. RIGGED FLAPS SYSTEM IAW AMM CH 27-50-00-820-801-A. PERFORMED FLAPS SYSTEM OPS CHECK IAW AMM 27-40-00, AND PERFORMED HS PITCH TRIM SYSTEM IAW AMM 27-40-00. PERFORMED PRESSURIZATION SYSTEM OPS CHECKS IAW AMM 21-31-00. SATISFACTORY.
MOST CADMIUM PLATED HARDWARE INSTALLED IN WING INTERGRAL FUEL TANKS HAVE DEVELOPED CORROSION. HARDWARE REQUIRES REPLACEMENT. MULTIPLE PART NUMBERS AFFECTED.
NOSE STEERING WAS NOT RESPONDING CORRECTLY DURING TAXI AND WAS JERKY. MAINTENANCE FOUND SEALS LEAKING.
NOSE WHEEL STEERING PULLING TO LT ON TAXI.