N439QS
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
ON TAXI OUT AT FIRST BRAKE APPLICATION NOTICED SIGNIFICANT BRAKE SHUDDER USING BOTH PEDALS. ADDITIONAL BRAKE APPLICATIONS ON THE TAXI OUT REVEALED SHUDDER COMING FROM BOTH PEDALS HOWEVER THE RIGHT PEDAL PRODUCED A MUCH MORE SIGNIFICANT SHUDDER. SERVICED HYDRAULIC RESERVOIR. OPS CHECK GOOD. IAW AMM 32-40-00-870-801A
CAPTAIN ALTITUDE/AIRSPEED INDICATION: AFTER ROTATION, THE LEFT SIDE INDICATED AIR SPEED BECAME UNRELIABLE. THE SYSTEM ANNOUNCED A STALL. FOR THE REMAINDER OF THE FLIGHT, THE LEFT SIDE PFD SHOWED AMBER IAS WITH ZERO INDICATED AIRSPEED. THE RIGHT SIDE PFD SHOWED AMBER IAS BUT RELIABLE AIRSPEED, WHEN COMPARED TO THE STANDBY AS. OTHER AMBER EICAS WERE AP FAIL, SWPS FAULT, YD FAIL. WHITE MESSAGES WERE - VENTRAL RUD FAIL ENG NO DISPATCH CORRECTIVE ACTION; REPLACED L/H IASP. OPS CHECKS GOOD WITH NO DISCREPANCIES NOTED. PERFORMED ADS FUNCTIONAL TEST, TEST GOOD WITH NO FURTHER DISCREPANCIES NOTED. ALL WORK PERFORMED IAW EMBRAER PHENOM 300 AMM 34-15-07 AND EMBRAER PHENOM 300 AMM 24-15-00
CAPTAIN ALTITUDE/AIRSPEED INDICATION: AFTER ROTATION, THE LEFT SIDE INDICATED AIR SPEED BECAME UNRELIABLE. THE SYSTEM ANNOUNCED A STALL. FOR THE REMAINDER OF THE FLIGHT, THE LEFT SIDE PFD SHOWED AMBER IAS WITH ZERO INDICATED AIRSPEED. THE RIGHT SIDE PFD SHOWED AMBER IAS BUT RELIABLE AIRSPEED, WHEN COMPARED TO THE STANDBY AS. OTHER AMBER EICAS WERE AP FAIL, SWPS FAULT, YD FAIL. WHITE MESSAGES WERE - VENTRAL RUD FAIL ENG NO DISPATCH CORRECTIVE ACTION; REPLACED L/H IASP. OPS CHECKS GOOD WITH NO DISCREPANCIES NOTED. PERFORMED ADS FUNCTIONAL TEST, TEST GOOD WITH NO FURTHER DISCREPANCIES NOTED. ALL WORK PERFORMED IAW EMBRAER PHENOM 300 AMM 34-15-07 AND EMBRAER PHENOM 300 AMM 24-15-00
JUST AFTER WHEELS TOUCHED DOWN, SMALL BIRD MADE CONTACT WITH LEFT SIDE OF AIRCRAFT. DURING POST FLIGHT, FOUND FEATHERS AND BIRD REMAINS (BLOOD) IN L #2 ENGINE. PERFORMED BORESCOPE INSPECTION. NO EVIDENCE OF DAMAGE. PERFORMED ENGINE RUNS WITH NO DEFECTS NOTED. IAW PW535E EMM 05-50-00 AND EMB PH300 AMM 71-00-00.
ON DEPARTURE ENG NO TO DATA ILLUM AFTER TAKEOFF & GEAR RETRACT. FOLLOWED BY A YELLOW X OVER NR 2 ENG OIL PRESSURE. SMOKE IN CABIN & DONED O2 MASKS. CLIMBED THROUGH 2000FT E2 OIL LO PRESS RED CAS APPEARED. PERFORMED ENG SHUTDOWN & RETURNED TO FIELD. OIL DRIPPING FROM NR 2 ENG & OIL IND EMPTY. PERFORMED A GVI, FOUND OIL POOLING IN EXHAUST CONE, & INLET, SERVICED THE 1\10.2 ENGINE WITH 4 QTS OF OIL. PERFORMED A BORESCOPE OF 2ND STAGE HIGH COMPRESSOR ROTOR IAW EMM 72-00÷00÷2BOÃâ¬Â¢B05. FOUND OIL ON ROTORS, DETERMINED CARBON SEAL ON NR 2 BEARING FAILED. R & R NR 2 ENG IAW AMM 71-00-00-000÷B01-A, SERVICED RT ENG WITH 6.5 QTS OF OIL IAW AMM 12-12-00, PERFORMED 5-POINT RUNS IAW EMM 71-00-00. NO DEFECTS NOTED.
EMERGENCY LIGHTS FLICKERING ON DESCENT//CORRECTIVE ACTION//FOLLOWED EMBRAER RECOMMENDED SL 505-33-0005 AND FIM 33-50-00-810-801-A AND FOUND NO 2 EMERGENCY LIGHTS BATTERY PACK INOP. REMOVED AND REPLACED NO 2 EMERGENCY LIGHTS BATTERY PACK WITH A CUSTOMER SUPPLIED REPAIRED PART. PERFORMED SATISFACTORY OPERATIONAL TEST OF EMERGENCY BATTERY PACKS AND EMERGENCY LIGHTS I/A/W AMM 33-52-01.
CABIN EMERG LIGHT: IN THE ARM POSITION THE CABIN EMERGENCY LIGHTS STAY ILLUMINATED. HALF WAY THROUGH OUR FLIGHT THEY STARTED PULSATING.////SIGN-OFF////REMOVED AND REPLACE EMERGENCY BATTERY PACKS. IAW EMB-505 AMM 33-52-01-01-010. OPS CHECK GOOD.
MAIN DOOR HANDLE: PUSH BUTTON SPRING MECHANISM IS NOT RETURNING THE PUSH BUTTON FLUSH WITH MAIN CABIN DOOR. IT IS JUST HANGING OPEN. REMOVED MAIN DOOR EXTERNAL HANDLE IAW P300 AMM 52-11-24 AND INSTALLED A SERVICABLE HANDLE IAW P300 AMM 52-11-24 PART WAS REMOVED SERVICEABLE FROM A/C S/N 50500328 AC TAIL N390QS FOR CONTINUED SERVICE ON A/C S/N 50500542 N439QS OPS CHECK GOOD