N309QS
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
LOWER EMERGENCY EXIT SIGN LIGHT DOES NOT ILLUMINATE TECHS GOT ONISTE AND VERIFIED THAT THE AFT EMER LIGHT WAS INOP. TECHS THEN SWAPPED THE AFT EMER LIGHT TO THE FWD AND FAULT DID NOT FOLLOW. WE THEN PUT EVERYTHING INTO NORMAL CONFIGURATION AND ALL LIGHTS ARE OPERATING NORMALLY. NO DEFECTS NOTED AT THIS TIME. ALL WORK PERFORMED IAW AMM 33-52-15.
MAIN EXIT SIGN/LIGHT: MAIN EXIT DOOR LIGHT INOP. CORRECTIVE ACTION: REMOVED FAULTY EXIT SIGN AND INSTALLED A CUSTOMER SUPPLIED NEW EXIT SIGN IN ACCORDANCE WITH EMBRAER PHENOM 300 AIRCRAFT MAINTENANCE MANUAL 33-52-13 WITH NO DEFECTS NOTED. P/N ON/OFF: 5315-00 NO SERIAL NUMBER
DRAG CONTROL (SPEEDBRAKES & SPOILERS): SPOILER WAS COMMANDED OPEN, BUT THEY SLAMMED CLOSED AND JOLTED THE AIRCRAFT. VISUAL INSPECTION SHOWED THE SPOILERS FLUTTERING WHILE IN FLIGHT. MULTIPLE SPOILER MESSAGES OCCURRED. CORRECTIVE ACTION: VISUALY CHECKED THE SPOILER SYSTEM AND FOUND NO OBVIOUS DEFECTS, LNTEROGATED CMC &SENT FILES TO MCC AND CRC, PER EMBRAER CRC WE PERFORMED FIM TASK 27-66-00-810-805-A AND SERVICE LETTER SL-505-27-0002 REVISION 2. USING DIGITAL PROTRACTO WE NOTED OUTBOARD SPOILERS HAD BACKLASH OF 2 DEGREES. NOTED PLAY WAS FROM THE PRESSED IN BEARINGS ON THE OUTBOARD SPOILER BELLCRANKS. REPLACED LH AND RH BELLCRANKS IAW MM 27-65÷02 AND OPS CHECKS GOOD AT THIS TIME LAW MM 27-00-00.
CABIN EMERG LIGHT: CABIN EMERG LIGHT ON IN FLIGHT WITH THE SWICH ON ARM POSITION CORRECTIVE ACTION: REMOVED AND REPLACED BATTERIES AT POSITIONS #1 AND #2.PERFORMED OPERATIONAL CHECK WITH NO DEFECTS NOTED. WORK PERFORMED IAW: PHENOM 300 AMM 33-52-01. POSITION #1 P/N: 7450LS-00 S/N: 006309. POSITION #2 P/N 7450LS-00 S/N: 007508.
FLAP: ON APPROACH RECEIVED A FLAP FAIL CAS MESSAGE. FLAP INDICATOR DISPLAYED FLAPS BETWEEN 3 AND FULL WHILE HANDLE WAS SELECTED TO FULL. COMPLETED CHECKLISTS INCLUDING CYCLING FLAPS 3 TIMES AND THEY DID NOT MOVE UP OR DOWN.//CORRECTIVE ACTION//DOWNLOADED CMC DATA AND SENT TO CONTACT CENTER FOR ANALYSIS. CONTACT CENTER SENT RECOMMENDATION TO COMPLETE FIM-4885- 27-53-00-810-812-A. AFTER POWER CYCLE OF AIRCRAFT, CHECKED OPERATION OF ?AP SYSTEM. FLAP FAULT HAS CLEARED UPON OPS CHECK OF SYSTEM. CONTACTED MCC AND CONTACT CENTER. NO HISTORY OF ?AP FAULT SHOWN. SINCE FLAP FAULT HAS CLEARED MCC HAS ELECTED TO RTS AIRCRAFT. ALL WORK ACCOMPLISHED WITH REFERENCE TO PHENOM 500 AMM TASK 27-50-00-710-801-A.
BATTERY OVERHEAT & TEMP INDICATION: BATTERY EXCEDENCE EICAS MESSAGE ILLUMINATED IN FLIGHT AT FL410. EMERGENCY CHECKLIST COMPLIED AND ELECTRICAL EMERGENCY BUTTON PUSHED. BOTH #1 BATTERY AND #1 GENERATOR WERE HIGH VOLTAGE. // SIGNOFF// REMOVED AND REPLACED LH GENERATOR IAW EMBRAER EMB-505 AMM 24-3L-02-000-801-A. OPS CHECK GOOD AT THIS TIME.
WITHIN 200' OF LEVELLING AT FL450, BATTERY EXEEDANCE YELLOW CAS. LATER IT EXTINGUISHED. SHORTLY AFTER IT WOULD COME ON & OFF & THEN REMAINED ON, HAD ALREADY BEGUN TO RUN QRH. DIVERTED TO KSTL. BATTERY VOLTAGE ON SCHEMATIC SHOWED 29 V & GEN 1 SHOWED 29.1. HAVE CW FIM 24-36-00-810=802-A & FOUND THE LT GCU WAS CAUSING ISSUE. SWAPPED GCU'S FROM LT AND RT TO VERIFIED LT GCU CAUSING THE ISSUE. SWAPPED BACK TO ORIGINAL POSITION. REMOVED AND AND REPLACED THE LT GCU.
EMERG EXIT SIGN/LIGHT: MAIN DOOR EMERGENCY EXIT SIGN HAS ONE BULB INOP. ALSO, THE FORWARD ATTACH POINT IS LOOSE. THE SIGN STILL WORKS AND IS READABLE. REMOVED AND REPLACED NEW MAIN ENTRY DOOR EMERGENCY EXIT SIGN. OPS CHECK NORMAL. WORK PERFORMED IAW PHENOM AMM 33-52-15.
EMERGENCY LIGHTING: EMERGENCY LIGHTS ARE ILLUMINATED WITH EMER LT SWITCH IN ARM POSITION AND ELECTRICAL POWER APPLIED. LIGHTS APPEAR DIM. // SIGNOFF // POWERED UP AIRCRAFT AND VERIFIED DISCREPANCY, NOTED THAT EXIT SIGN ON MED DOOR AND EMERGENCY DOOR WAS DIM. MCC PLACE BOTH DATIERV PACKS ON ORDER, REMOVED FORWORD EMERGENCY BATTERV PN 6450LS-00 SN 000789 AND LNSTALLLED NEW UNLT PN 7450LSâ¢00 SN 006371, REMOVED AFT EMERGENCY BATTERY PN 6450LS-00 SN 000762 AND INSTALLED NEW UNIT PN 74501-S·OO SN 006503, OPERATIONAL CHECKS OKAY, REF PHENOM 300 AMM 33-52-01,
DURING INITIAL MLG RETRACTION, CREW HEARD A WHINING NOISE FROM REAR OF ACFT & GOT A RED MLG DISAGREE CAS MESSAGE & 3 YELLOW CAS MESSAGES,: HYD PRESS LO, BRK FAIL, & PUSHER FAIL. NOTED ON SYS SYNOPTIC PAGE, HYD PRESS INDICATING 0. RAN MLG DISAGREE QRH & CAS EXTING WHEN MLG LEVER DOWN. RAN APPR QRH CHKLISTS, DIVERTED, USED EMER BRAKING. POST FLT INSP, COULDN`T FIND IND OF HYD LEAK, NEITHER DPI POPPED, & HYD RES SHOWED NORM QTY. AFTER STOPPING, SHUTDOWN ENGS, INSPECT ACFT FOR HOT BRAKES, & DID NOT RETRACT FLAPS. FLAPS STILL IN FULL POSITION. INSPECT LT & RT HYD EDPS IAW EMM 05-50-00-210-822. REMOVED ENGS & FIRE CONTROL PANEL. INSTALLED A REPAIRED ENG & FIRE CONTROL PANEL IAW AMM 26-21-02. OPS CHKD GOOD.
WHEN PRIME APPEARANCE WAS FINISHED WITH THERE SERVICE HUB EVENT THEY ATTEMPTED TO CLOSE THE MAIN ENTRY DOOR AND THE HANDLE BROKE OFF IN THEIR HAND. PRIME APPEARANCE CONTACTED ME AND I ADVISED GAMA. AIRCRAFT WAS QUICKLY REPOSITIONED INTO THE HANGAR AND GAMA TECHNICIANS VISUALLY INSPECTED AND NO ADDITIONAL DAMAGE WAS FOUND. REMOVED MAIN DOOR EXTERNAL HANDEL P/N 505-09870-403 S/N NSN DUE TO HANDLE BROKEN OFF AND INSTALLED NEW CUSTOMER SUPPLIED EXTERNAL HANDLE, IAW EMB 505-52-11-24. OPERATIONS CHECK NORMAL, NO DEFECTS NOTED.
DURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (9 EACH BELOW MINIMUM OF 84G); HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH BELOW MINIMUM OF 1095G); MASS WEIGHT INBOARD PART NUMBER PE915109-L40 (1 EACH BELOW MINIMUM OF 2809G); MASS WEIGHT OUTBOARD PART NUMBER PE915109-L41 (1 EACH BELOW MINIMUM OF 2049G). 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 505-11094-615, AS PER SERVICE BULLETIN INSTRUCTIONS. WE ALSO NOTED THE FOLLOWING RIGHT ELEVATOR MASS BALANCE WEIGHTS BELOW TOLERANCE: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (6 EACH BELOW MINIMUM OF 84G); HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH BELOW MINIMUM OF 1095G); MASS WEIGHT INBOARD PART NUMBER PE915109-L40 (1 EACH BELOW MINIMUM OF 2809G); MASS WEIGHT OUTBOARD PART NUMBER PE915109-L41 (1 EACH BELOW MINIMUM OF 2049G). 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 505-11094-616, AS PER SERVICE BULLETIN INSTRUCTIONS. THIS REPORT COMPLIES WITH FAA 14 CFR PART 135 OPERATORâS GMM REQUIREMENTS.
RT ENGINE IDLE SPEED AT 10,000 FEET AND 150KTS WAS 52.9 PERCENT. COMPLIED WITH ADJUSTMENT OF MINIMUM FLOW OF THE RT ENGINE FCU IN REF TO THE MM CH 71-00-00. ALL FINAL OPS CHECKS SATISFACTORY.
AT TAKEOFF BOTH AIRSPEED INDICATORS SHOWED A YELLOW "IAS". THE CO-PILOT AIRSPEED SHOWED 40KTS SLOWER THAN THE LT SIDE AIRSPEED INDICATOR.
DURING INITIAL TAKEOFF ROLL, AIRSPEED INDICATIONS APPEARED NORMAL. AT 70KTS INDICATED F/O NOTED IAS CAPT SIDE + CAPT A/S JUMPED APPROX 30KTS TO APPROX 100KTS. WE CALLED ABORT - ABORT ON THE RUNWAY W/NO ISSUES.
FOUL ODOR COMING FROM OVERHEAD VENTS ESPECIALLY DURING DECENT. IT HAD A FAINT ODOR OF OIL. REMOVED RIGHT ENGINE ASSEMBLY. INSTALLED SERVICEABLE ENGINE ASSEMBLY IN ACCORDANCE WITH MM 71-01-02. ALL OPERATIONAL AND LEAK CHECKS GOOD.
TURNED ON AVIONICS - FMS HAD NO SCREEN (SCREEN BLACK) AND DETECTED SMOKE, KTEB. (S)
TURNED ON AVIONICS, FMS HAD NO SCREEN (SCREEN BLACK) AND DETECTED SMOKE, LIKE INSULATION BURNING ON WIRES. MET WITH CREW. FMS SMELLS BURNED. FMS CDU BAD ONBOARD AIRCRAFT. REMOVED FMS CDU AND INSTALLED REPAIRED UNIT. OPS CHECK WAS GOOD, UPDATED THE NAV DATABASE TO EFFECTIVE PERIOD ENDING AUG 28/08, ALL WORK DONE IAW CE-560 MM CHAP 34-62-00.
TURNED ON AVIONICS - FMS HAD NO SCREEN (SCREEN BLACK) AND DETECTED SMOKE, LIKE INSULATION BURNING ON WIRES. REP MET WITH CREW. FMS SMELLS BURNED. FMS CDU P/N 18355-0101-0101, S/N 41266 BAD ONBOARD ACFT. REMOVED FMS CDU PN 18355-0101-0101, SN 41266 AND INSTALLED REPAIRED UNIT P/N SAME, S/N U1187. OPS CHECK WAS GOOD- UPDATED THE NAV DATABASE TO EFFECTIVE PERIOD ENDING AUG 28/08, ALL WORK DONE IAW MM CHAP 34-62-00.
WHEN FLAP HANDLE IS MOVED OUT OF (ZERO) POSITION, AIRCRAFT WILL ROLL RT. MANUALLY STOPPED THE ROLL AT 30 DEGREE BANK. AUTOPILOT WAS (OFF). [SUP 05-03-07] ADJUSTED RIGHT FLAP ACTUATOR ROD END OUT 1/2 TURN TO MATCH LEFT FLAP. IAW CE560 M/M CH 27-51-00 M/M CH 27-51-00, OPS CHECKED AND TRAVEL CHECKED GOOD.
RT ENGINE SHUT DOWN WHEN ASSOCIATED THROTTLE BROUGHT TO IDLE AFTER ENGINE START. GOOD AMOUNT OF FUEL THEN FOUND UNDER ENGINE ON GROUND. TROUBLESHOT, BY REMOVING COWLING, ON NR 2 ENGINE, MOVED CONTROL LEVER. FOUND NO OUT OF RIG PROBLEM. STARTED NR 1 AND NR 2 ENGINES. MOVED CONTROL LEVERS FAST THEN SLOW SEVERAL TIMES TO 65 - 70 PERCENT N2. BOTH ENGINES OPS CHECKED NORMAL IAW CESSNA 560 ULTRA M/M 71-01-03.
DURING THE T/O ROLL AT APPROX 40 TO 60 KNOTS CAPT A/S INDICATOR REMAINED BLANK AND A/S COMPARISON MONITOR ILLUMINATED. T/O WAS ABORTED. VERIFIED DISCREPANCY. NOTED DIRT DEBRIS IN LT PITOT. PURGED PITOT LINE & TUBE WITH AIR. LEAK TEST CHECKS GOOD. AIRSPEED OPERATIONAL CHECKS GOOD. MAINTENANCE DONE IAW 560 MAINTENANCE MANUAL CH 34-11-05.
DURING INSPECTION, LOOKED INTO DORSAL NACA SCOOPS,MATERIAL MISSING FROM AIR VANES PN 6512072-11, 6512072-12 LOCATED IN TRANS DUCT MISSING MATERIAL LOCATION WAS A CONCERN BECAUSE ITS ONLY ROUTE WAS TO END UP IN VENT J-BOX (AIR MIXING BOX) WHERE IT WOULD HAVE PASSED CABIN PRESS, FRESH AIR CHECK VALVE (POSSIBLY WEDGING VALVE OPEN) THIS WOULD HAVE NOT ALLOWED A/C TO HOLD PRESS. 1ST PIECE WAS FOUND WEDGED IN CHECKVALVE (VALVE COULD NOT SEAL) 2ND PIECE WAS FOUND PAST OVERHEAD BLOWER WEDGED IN DUCT WORK (NO DAMAGE TO BLOWER CAGE). LOCATED BROKEN PARTS REMOVED, REPLACED BROKEN PARTS WITH NEW. CLOSED UP CABIN INTERIOR AND DUCT WORK. REASSEMBLED TAILCONE DUCTING. CHECKVALVE WAS SERVICEABLE REINSTALLED.
WITH THE AUTOPILOT ON, THE ELEVATOR TRIM WORKED NORMAL. WHEN THE AUTOPILOT WAS TURNED OFF, THE ELEVATOR TRIM LOCKED INTO POSITION AND WOULD NOT MOVE. WHEN THE AUTOPILOT WS TURNED BACK ON, THE TRIM WORKED NORMAL. (X)