N427QS
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
DURING FLIGHT EMER LIGHTS FLICKERING IN THE ON AND ARM POSITION. REMOVED EMER BATT #1 AND #2 AND INSTALLED A CUS SUPP REPAIRED #1 AND #2 UNIT PERFORMED A SATISFACTORY OPS TEST OF THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED ALL WORK PERFORMED IAW EMB-505 AMM 33-52-01-000-801-A/400-801-A.
CABIN EMERGENCY LIGHTS FLICKER WITH EMER LT SWITCH IN THE ARM AND ON POSITION CORRECTIVE ACTION: T/S TO FAULTY #2 BATTERY PACK, MCC REQUESTED R&R OF BOTH FWD AND AFT EMERGENCYBATTERIES. GAINED ACCESS TO #2 BATTER: REMOVING AFT WALL, AC CONDENSOR SHROUD, AND OUTFLOW VALVE SHROUDING. R&R AFT EMERGENCY BATTERY W/ REPAIRED UNIT. REINSTALLED ACCONDENSER SHROUD, OUTFLOW VALVE SHROUD, AND AFT WALL TO ORIGINAL CONFIGURATION.TEMPORARILY REMOVED PILOT AND COPILOT SEATS TO GAIN ACCESS TO #1 EMER BATTERY. R&R #1EMERGENCY BATTERY W/ REPAIRED UNIT, REINSTALLED BOTH SEATS AND ACCESS PANEL TOORIGINAL CONFIGURATION, VERIFIED BOTH SEATS OPERATE AS DESIGNED. PERFORMED OPS CHECK OF BOTH EMERGENCY BATTERIES AND OPS CHECK WAS GOOD. C/W EMB 505 AMM 33-52-01. (BAK).
MAIN CABIN DOOR IS STUCK HALFWAY DOWN/UP AND IS EXTREMELY HARD TO OPEN/CLOSE AFTER THE AIRCRAFT GOT PULLED FROM THE HANGAR. BANGING NOISES CAN BE HEARD WHEN TRYING TO CLOSE DOOR. DOOR BANGING GOT WORSE AFTER THE VIDEO WAS TAKEN. CORRECTIVE ACTION: ARRIVED AT ALRCRAFT AND UNLOCKED DOOR HANDLE AND OPENED DOOR, NO DEFECTS NOTED. PERFORMED GENERAL VISUAL INSPECTION OF MAIN CABIN DOOR, NO DEFECTS NOTED. CLEANED DEBRIS FROM TELESCOPIC ROD AND PERFORMED SEVERAL CYDLES, OPENING AND DOSING THE MAIN CABIN DOOR, NO DEFECTS NOTED. IAW PHENOM 300 AMM PART II TASK 52-12-25-820-801-A
AFTER TAXING OUT WE FELT A HEAVY SHUTTERING ON THE RIGHT SIGHT WHEN BRAKE WAS ABPLIED CORRECTIVE ACTION: PERFORMED BRAKE SYSTEM BLEED PER TASK TC-ES0-32-1001. OPS CHECK GOOD.
EMERGENCY LIGHTS ILLUMINATED DURING FLIGHT WITH THE EMER LT SWITCH IN THE ARM POSITION. PICTURES ATTACHED. REMOVED FWD AND AFT EMER LIGHT BATTERIES AND INSTALLED A CUSTOMER SUPPLIED NEW FWD AND AFT EMER LIGHT BATTERIES IAW PHENOM 300 AMM TASK 33-52-01-000-801-A/400-801-A OPERATIONAL TEST SATISFACTORY PERFORMED IAW PHENOM 300 AMM TASK 33-52-00-710-801-A NO DEFECTS NOTED AT THIS TIME.
IN FLIGHT AT FL400 WE HAD AN FCE 1 FAILURE. REMOVED FCE PN: 462900-1017 SN: 0550 FROM FCE 1 POSITION AND REPLACED WITH FCE ORIGINALLY IN THE FCE 2 POSITION MENTIONED ABOVE DUE TO FCE 1 FAILURE IN FLIGHT AND UNABLE TO DUPLICATE ON THE GROUND FOR CUSTOMER CONVENIENCE. RIGGING AND OPS CHECK GOOD. WORK DONE IAW EMB 505 MM 27-50-00 2 REMOVED FCE PN: 462900-1017 SN: 0402 FROM FCE 2 POSITION AND REPLACED WITH FCE ORIGINALLY IN THE FCE 1 POSITION MENTIONED ABOVE DUE TO FCE 1 FAILURE IN FLIGHT AND UNABLE TO DUPLICATE ON THE GROUND FOR CUSTOMER CONVENIENCE. RIGGING AND OPS CHECK GOOD. WORK DONE IAW EMB 505 MM 27-50-00
BRAKE COMPUTER: DURING TAXI, MAIN BRAKES PULSING THE ANTI SKID SYSTEM CAUSING A SHUTTERING AT ALL SPEEDS. //SIGNOFF// AFTER COMPLETION OF BRAKE & EMERGENCY BRAKE BLEEDIN IAW EMB-505 MM CHAP 32-40-00, AND NJA TC-E50-32-1001, DATED 21SEP2022. REF ITEM# 3.3 OF THIS WO, FOR DETAILS OF TC. COMPLIED WITH TAXI CHEC .. TAXI CHECK SATISFACTORY. NOTIFIED MCC OF WORK PERFORMED. THEY ARE OK SIGNING THE ITEM OFF.
BLEED AIR: ACRID BURNING RUBBER ODOR NOTED ON 2 CONSECUTIVE TAKEOFFS. ODOR IS STRONGEST AS T/O POWER IS APPLIED AND BEGINS TO DISSAPATE ON CLIMBOUT. // SIGNOFF// CHECKED OIL SIGHT GLASSES FOR SIGNS OF OVERSERVICING. R/H ENGINE OIL 1/4 QT LOW. RAN ENGINES AT IDLE. NO SMELL NOTED IN COCKPIT/CABIN. ATTEMPTED TO ISOLATE ECS TO ONE SIDE, STILL NO SIGN OF ABNORMAL SMELL ALERTED MCC THAT ENGINES NEED TO BE DUPLICATED AT T/0 POWER, MCC ADVISED THAT THIS A/CHAS HAD A RECENT BIRD STRIKE EVENT, FOLLOWED BY A COMPRESSOR WASH, AND THE CONTROLLER BELIEVES THAT THE COMPRESSOR WASH FLUID IS THE CAUSE OF THE SMELL. SEVERAL T/0 POWER RUNS MAY BE NEEDED. AWAITING RUN CURFEW LIFT. REF. PHENOM 300 EMM FIM 72·00-01 AND AMM REF. 71·00-01. PERFORMED HIGH POWER RUNS (T/0 88%) WITH BOTH AND INDIVIDUALLY, FIVE CYCLES ATS MINS INTERVALS AND NO ABNORMAL SMELL WAS NOTED. ALSO PERFORMED PNEUMATIC SYSTEM CHECK IAW EMBSOS MM 36·00·00 AND 72·00·01. NO ABNORMAL SMELL NOTED, CONTACTED MCC WITH FINDINGS AND RANDY IS OK FOR RELEASE. RETURNED BACK TO RAMP. CLOSE UP. OK TO CONTINUE.
EMERGENCY LIGHTING: IN FLIGHT THE EMERGENCY LIGHTS WERE BLINKING ON AND OFF WITH SWITCH IN ARM POSITION. AFTER CYCLING THE EMER LIGHT SWITCH THE EMER LIGHTS REMAINED ON WITH SWITCH IN ARM POSITION. //SIGNOFF// GAINED ACCESS TO AND REMOVED AND REPLACED THE FWD AND AFT EMERGENCY LIGHT BATTERY PACKS WITH NEW PACKS, COMPLETED RESET OF G SWITCH, AND COMPLETED OPERATIONAL CHECKS WITH NO FAULTS. WORK DONE WITH REFERENCE TO EMB505 AMM 33-52-01
RIGHT MLG BRAKE: ON TAXI OUT RT MAIN BRAKE STARTED TO MAKE SHUTTER/GRINDING SOUND WHEN APPLYING ANY AMOUNT OF BRAKE PRESSURE. FELT LIKE THERE WAS NO BRAKE ON RIGHT SIDE. WAS NOT FELT WHILE MOVING WHEN BRAKES NOT APPLIED. NOISE AND SENSATION CAN BE HEARD AND FELT WHILE TAXING. RT MAIN BRAKE APPEARS TO BE VISUALLY OK SEEMS LIKE SOMETHING WITH BCU OR ANTISKID SYSTEM. // SIGNOFF // COMPLIED WITH GVI OF MLG BRAKES. NO VISUAL DEFECTS NOTED AT THIS TIMIE COMPLIED WITH MLG BRAKE BLEEDING PROCEDURE. COMPLIED WITH TAXI CHECK. OP'S CHECK GOOD IAW PHENOM 300AMM TASK 32-40-00-870-801·A. NO SHUTTER/ GRINDING OR NOISES NOTICE AT THIS TIME,
RIGHT MLG BRAKE: DURING TAXI OUT, THE RIGHT, MAIN BRAKE INTERMITTENTLY FAILED. APPLYING THE BRAKES RESULTED IN A GRINDING SOUND AND IT FAILED TO ENGAGE FULLY. THE AIRCRAFT HAD TO BE STOPPED WITH THE LEFT BRAKE ONLY. //SIGN OFF // VERIFIED SEVERAL WHEEL SPEED TRANSDUCES FAILS ( RH SIDE) IN CMC HISTORY. REPLACED WITH A REPAIRED UNIT THE RH WHEEL SPEED TRANSDUCER OPERATIONAL TEST CHECKED GOOD IAW PHENON AMM 32-41-06 PERFORMKED SATISFACTORY OPERATIONAL TEST OF BRAKING SYSTEM VIA ENGINE RUN & TAXI IAW PHENON AFM NO DEFECTS NOTED
DURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHT BELOW TOLERANCE AT LEFT ELEVATOR: HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH BELOW MINIMUM OF 1095G). WEIGHT HAS BEEN REPLACED WITH A NEW MASS WEIGHT AND THE ELEVATOR BALANCING WAS PERFORMED WITH NO FURTHER DEFECTS NOTED.THE ELEVATOR WAS RE-IDENTIFIED TO PART NUMBER 505-11082-603 AS PER SERVICE BULLETIN INSTRUCTIONS. WE ALSO NOTED THE FOLLOWING RIGHT ELEVATOR MASS BALANCE WEIGHT BELOW TOLERANCE: HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH BELOW MINIMUM OF 1095G). WEIGHTS HAS BEEN REPLACED WITH A NEW MASS WEIGHT AND THE ELEVATOR BALANCING WAS PERFORMED WITH NO FURTHER DEFECTS NOTED.THE ELEVATOR WAS RE-IDENTIFIED TO PART NUMBER 505-11082-604 AS PER SERVICE BULLETIN INSTRUCTIONS. THIS REPORT COMPLIES WITH FAA 14 CFR PART 135 OPERATORâS GMM REQUIREMENTS
MAIN DOOR HANDLE - MAIN CABIN DOOR EXTERIOR HANDLE KEEPS BINDING UP REQUIRING ABNORMALLY HIGH FORCE TO OPEN THE DOOR FROM THE OUTSIDE. THE INTERIOR HANDLE OPENS THE CABIN DOOR WITH NORMAL PRESSURE. ///SIGN-OFF///LUBED MAIN DOOR LATCH PINS JAW EMB 505 AMM 52·11-21. OPERATIONAL CHECKS NORMAL.