N432QS
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
DOOR WOULD NOT PROPERLY CLOSE. WE LIFTED AND PUSHED THE DOOR UP, PULLED THE LATCH OUT AND ROTATED THE LATCH UP TO CLOSE. IT GAVE A LOT OF RESISTANCE AND WOULD NOT FULLY LOCK. THE DOOR WAS THEN STUCK CLOSED WITH THE VENT STILL IN. WHEN LATCH WAS PULLED DOWN TO OPEN. THE LATCH WAS LOSE AND WOULD NOT OPEN. WITH A LOT OF TRIES, THE DOOR WAS EVENTUALLY OPENED. CORRECTIVE ACTION: OPENED MAIN CABIN DOOR AND PERFORMED VISUAL INSPECTION OF DOOR SEALS, DOOR PINS, HINGES AND DOOR HANDLE AND FOUND NO EVIDENCE OF BINDING OR DAMAGE TO MECHNICAL DOOR PINS. CLOSED DOOR FROM INSIDE AND DOOR CLOSED WITH NO PROBLEMS. OPENED DOOR AND CLOSED PAX DOOR WITH OUTSIDE HANDLE WITH WITH NO ABNORMAL RESISTANCE OPENED AND CLOSED DOOR 10 TIMES (DOOR VENT OPERATED) WITH NO PROBLEMS AT THIS TIME ALL WORK DONE USING AMM 52-10-00
IN FLIGHT, DURING CRUISE, WITH THE EMERGENCY LIGHT SWITCH IN THE ARM POSITION, THE EMERGENCY LIGHTS IN THE CABIN ILLUMINATED. CYCLED THE SWITCH FROM ARM TO OFF, THEN BACK TO ARM. THE LIGHTS EXTINGUISHED. AFTER LANDING, DURING TAXI IN, WITH THE EMERGENCY LIGHT SWITCH IN THE ARM POSITION, THE EMERGENCY LIGHTS IN THE CABIN ILLUMINATED AGAIN. TRIED CYCLING THE EMERGENCY LIGHT SWITCH TO OFF, THEN BACK TO ARM. EMERGENCY LIGHTS ILLUMINATED AGAIN WHEN THE SWITCH WAS PLACED IN THE ARM POSITION. TRIED CYCLING THE SWITCH TO ON, THEN TO OFF, THEN BACK TO ARM. THE LIGHTS ILLUMINATED AGAIN WHEN SWITCH WAS RETURNED TO THE ARM POSITION. REMOVED AND REPLACED FWD AND AFT EMERGENCY BATTERIES IAW EMB505AMM 33-52-01, CHECKED GOOD. NO DEFECTS NOTED.
EMERGENCY LIGHTS FIRST FLICKERED THEN STEADY ON WHEN EMER LT SWITCH IN ARM POSITION. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY BATTERY PACKS. IAW EMB 505 MM 33-52-01. OPS CHECK GOOD.
DURING DESCENT AT FL220 AND 310KIAS A LOUD VIBRATION/HUM BEGAN ABRUPTLY. IT STOPPED AFTER SLOWING BELOW 295KIAS. DURING THE REST OF THE DESCENT TO 16000 FEET IT WOULD BEGAN AGAIN ANY TIME THE AIRSPEED WENT OVER 300KIAS. FOUND FORWARD, LOWER, WING TO BODY FAIRING SEAL LOOSE FROM FAIRING AND THE L/H AND R/H INBD LEADING EDGE FILLET FAIRING SEALS TO HAVE MINOR DETERIATION. COMPLIED WITH EMBRAER PHENOM 300 FWD WING TO FUSELAGE FAIRING SEA I RTV APPLLCATION WORK CARD# ES0-53-001-1, REV.0 DATED 23 JUN 2022 AND EMBRAER ETD-2014-P300-00137555 REV. H PARAGRAPH C1-C2.
DESCENDING THROUGH FL260. PILOTS HEARD A LOUD HIGH FREQUENCY VIBRATION IN THE COCKPIT. AIRSPEED WAS 305KTS. LEVELED OFF AT FL200, SLOWED & VIBRATION WENT AWAY BELOW 290KTS. SPED UP ABOVE 305KTS, VIBRATION RESUMED. INSPECTED THE LT & RT WING-TO-BODY FORWARD-FAIRING SEALS. NO DISCREPANCIES. INSPECTED WING-TO-BODY FAIRING NACA AIR-INLET POLYURETHANE FILM. NO DISCREPANCIES. INSPECT FUSELAGE DRAINS. NO DISCREPANCIES. R & INSP LT & RT COWLINGS. NO DISCREPANCIES. INSPECTED LT & RT UPPER & LOWER PYLONS. FOUND EROSION TAPE ON THE RT UPPER PYLON DAMAGED. WORK PERFORMED IAW AMM 05-50-27.
CABIN EMERG LIGHT: EMERGENCY LIGHTING CAME ON, THEN EVENTUALLY STARTED FLICKERING ON AND OFF. REMOVED EMERGENCY BATTERY PACK #2 DUE TO NOT CHARGING AND INSTALLED NEW CUSTOMER SUPPLIED #2 EMERGENCY BATTERY PACK. OPS CKD NORMAL IAW AMM·33-52-01.
CABIN EMERG LIGHT: OVERHEAD CABIN LIGHTS FLASHING WHILE INFLIGHT WITH EMERG LIGHTS ARMED.//CORRECTIVE ACTION// REMOVED AND REPLACED REAR MAIN BATTERY PN 7638-48P SN G030133027 AND INSTALLED NEW CUSTOMER SUPPLIED REAR MAIN BATTERY PN PN 7638-48P SN G03139823 OPS CHECK GOOD. REF PHENOM 300 MM 24-36-01
EMERG BRAKE: EMERGENCY BRAKE PRESSURE DROPPED TO ABOUT 1600 PSI IN FLIGHT, AND THEN RETURN BACK TO NORMAL 3000 PSI UPON LANDING. // SIGNOFF// FOLLOWED EMB-505 FIM TASK 32-43-00-810-802-A REMOVED AND REPLACED EMERGENCY BRAKE VALVE WITH SERVICEABLE UNIT IAW EMB 505 AMM 32-43-02-400-801-A REMOVED AND REPLACED EMERGENCY BRAKE THERMAL RELIEF VALVE WITH SERVICABLE UNIT IAW EMB 505 AMM 32-43-08-400-801-A BLED BRAKES IAW EMB 505 AMM 32-43-00-820-801-A/500 OPS CHECK GOOD OPERATED SYSTEM SERVERAL TIMES USING HYDRAULIC POWER CART
EMERG EXIT SIGN/LIGHT: UPPER MAIN CABIN EMERGENCY EXIT SIGN NOT ILLUMINATING WHEN THE EMERGENCY LIGHT SWITCH IS IN THE ON POSITION. // SIGNOFF// POWER UP EMERGENCY LIGHTS AND NOTED UPPER EMERGENCY EXIT SIGN ABOVE MAIN CABIN DOOR NOT ILLUMINATING, GAINED ACCESS TO EMERGENCY LIGHT ASSY AND FOUND LIGHT ELECTRICAL PLUG INSTALLED INCORRECTLY. RECONNECTED EMERGENGY LIGHT ELECTRICAL PLUG. PERFORMED SATISFACTORY OPERAATIONAL CHECKS OF EMERGENCY LIGHT SYSTEM I/A/W EMB PHENOM 300 AMM 33-52-00.
MAIN DOOR: MAIN ENTRANCE DOOR HANDLE GETS STUCK HALFWAY WHILE OPENNING THE DOOR. HAVE TO FORCE THE HANDLE TO GET THE DOOR OPEN. // SIGNOFF // PERFORMED NUMEROUS ADJUSTMENTS OF THE MAIN CABIN DOOR ECCENTRIC BUSHINGS IAW EMB 505 AMM 52-10-00 OPS CHECK GOOD, DOOR NOW CLOSES AND OPENS NORMALLY. NO FURTHER DEFECTS NOTED.
EMERGENCY LIGHTS ARE CONTINUOUSLY FLASHING ON AND OFF. REMOVED AND REPLACED AFT EMERGENCY LIGHTING BATTERY. WORK PERFORMED, IAW EMBRAER PHENOM 300 AMM 33-52-01/400. SEE TASK/INSPECTIONS FOR DETAIL. ALL CHECKS GOOD AT THIS TIME.
DUE TO CORROSION ON ELEVATOR BALANCE WEIGHTS REMOVED AND INSTALLED 3 NEW RT ELEVATOR ADJUSTABLE BALANCE WEIGHTS, P/N PE915109-L33. INSTALLED 2 NEW LT ELEVATOR ADJUSTABLE BALANCE WEIGHTS, P/N PE915109-L33.
FLAP FAIL YELLOW CAS ILLUMINATED - AT FL410 WE RECEIVED A SWPS FAULT, FLAP FAIL, PTRIM BKP FAIL, SPOILER FAULT CAS MESSAGES. A YELLOW X APPEARED ON BOTH THE FLAPS AND PITCH TRIM INDICATORS. WHEN A FLIGHT DIRECTOR VERTICAL MODE OTHER THAN ALT WAS SELECTED THE MAXSPEED WARNING APPEARED ABOVE THE SPEED TAPE AND THE FLIGHT DIRECTOR SHOWED A PITCH CHANGE INDICATING A REACTION TO THE MAXSPEED. PRIMARY TRIM WORKED NORMALLY. GROUND SPOILERS DID DEPLOY ON LANDING. PERFORMED FLAPS FAIL QRH. LANDED NORMALLY. *** CORRECTIVE ACTION *** TROUBLESHOT FAULT AND REPLACED #1 FCE WITH MODIFIED UNIT. RIGGED FLAPS SYSTEM, PERFORMED ALL REQUIRED SYSTEM OPS CHECKS W/ SATISFACTORY RESULTS.