N417QS
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
GEN 1 OFF BUS YELLOW CAS IN FLIGHT WITH ASSOCIATED VIBRATION. RAN CHECKLIST AND EVENTUALLY SHUT DOWN LEFT ENGINE PER QRH. PERFORMED UNEVENTFUL ONE ENGINE INOPERATIVE LANDING AND SHUT DOWN OPERATING ENGINE. CORRECTIVE ACTION: REMOVED STARTER PN: 400SG180Q-6 SN S04367. INSTALLED OVERHAULED STARTER GENERATOR. REPOSITIONED AC ONTO RAMP. PERFORMED STARTER GENERATOR OPERATIONAL CHECKS, ALL CHECKS ARE SATISFACTORY AT THIS TIME AND NO FAULTS WERE NOTED DURING OPERATION. RETURNED AC TO ORIGINAL CONFIGURATION. WORK PERFORMED IAW AMM 24-31-01.
CABIN EMERG LIGHT ALL CABIN EMERGENCY LIGHT REMAIN ILLUMINATED WITH THE SWITCH IN THE ARM POSITION. LIGHTS ALSO FLICKER ON AND OFF WHILE IN THE ARM POSITION. CORRECTIVE ACTION: REPLACED FORWARD EMERGENCY BATTERY. OPS CHECK GOOD. PHENOM 300 AMM 33-52-01-400-801
LEFT MAIN CABIN DOOR TELESCOPING ROD IS SEPARATING FROM THE MAIN CABIN DOOR. COMPLIED WITH REPAIR OF THE MED AND INSTALLED A NEW TELESCOPING ROD FITTING PN 500-09754-011.
LG LEVER DISAG RED CAS: ON FINAL APPROACH, WE RECIEVED A LG LEVER DISAG CASS MESSAGE. WE COMPLIED WITH THE QRH PROCEEDURE (EAP12-3). AFTER CYCLING THE GEAR, A LOUD BANG WAS NOTED COMING FROM THE NOSE GEAR. THE FREE FALL HANDLE WAS THEN PULLED TO GET A THREE GREEN INDICATION. AIRCRAFT LANDED UNEVENTFULLY.
CAPTAIN ALTITUDE/AIRSPEED INDICATION: DURING DECENT WE RECIEVED ALT MISCOMPARE ICON ON BOTH PFDS. JUST AFTER THAT WE RECIEVED A SWPS FAULT YELLOW MESSAGE. WE LEVELED OFF AT 10000FT TO TROUBLE SHOOT AND RUN THE CHECKLIST. THE CAPTAIN SIDE ALTIMETER WAS APPX 300 FT HIGH FROM THE FO AND THE STBY. AFTER SEVERAL MINUTES BOTH MEASAGES DISAPPEARED AND THE ALTITUDES ALL MATCHED UP AGAIN. AFTER RUNNING THE SWPS FAULT CHECKLIST WE LANDED IN A NORMAL CONFIGURATION. // SIGNOFF// COMPLIED WITH EMBRAER RECOMMENDATION OF TASK 34-15-07-210 802-A DETAILED VISUAL INSPECTION OF IASP WITH NO DEFECTS NOTED AT THIS TIME, 8-19-23 HB DG, PERFORMED AIR DATA SYSTEM . FUNCTIONAL CHECK IAW PHENON 300AMN PART 2 34-15-00-72D-801·A NO DEFECT NOTED PER EMBRAER CONTACT CENTER N CASE OF NO FAULTS FOUND, RELEASE THE AIRCRAFT AND KEEP MONITORING THE SYSTEM,
AFTER ENGINE START, EMER LT NOT ARMED CAS ILLUMINATED WITH SWITCH IN THE ARM OR ON POSITION. CABIN EMER LIGHTS REMAIN ON WITH SWITCH IN ON OR ARM POSTITON. CONDITION OCCURS WITH AIRCRAFT POWERED OR UNPOWERED. NO SUCCESS WITH RESET PROCEDURE. REPLACED #1 AND #2 EMERGENCY LIGHT BATTERIES WITH 'MODIFIED" UNITS IAW AMM 33-52-01/400. COMPLETED EMERGENCY LIGHTS OPERATIONAL TEST IAW AMM 33-52-00-710-801-A.
ALL CABIN EMERGENCY LIGHTS STAY ILLUMINATED WHEN THE SWITCH IS IN THE ARM POSITION. ATTEMPTED TO CHARGE BATTERIES, OPS CHECK FAILED. DISCONNECTED CONNECTOR PLUG FROM AFT BATTERY AND LIGHTS WORKED AS THEY SHOULD. REMOVED AND REPLACED AFT BATTERY WITH NEW BATTERY. CHARGED BATTERY FOR ONE HOUR AND OPS CHECKED SYSTEM WITH NO DEFECTS NOTED IAW AMM 33-52-01. ORIG SUBMISSION DATE: 12/27/2022
BRK FAIL YELLOW CAS: BRK FAIL ON LONG APPROACH, COMPLETED THE QRH AND PERFORMED A NORMAL LANDING. "CORRECTIVE ACTION" REMOVED BRAKE CONTROL MODULE, INSTALLED INSPECTED MODULE, REMOVED BRAKE CONTROL MODULE P/N DAP00101-02, S/N 0044RH. INSTALLED INSPECTED MODULE, REF PHENOM 300 AMM 32-41-07-400-801A, JACKED AIRCRAFT. COMMPLIED WITH HYDRAULIC SYSTEM BLEEDING PROCEDURES, LEAK AND OPS CHECKED BRAKE CONTROL MODULE NO DEFECTS NOTED. TRF PHENOM 300 AMM 29-10-00 32-41-00,32-41-00,32-41-07.
BLEED 1 LEAK YELLOW CAS ILLUMINATED - BLEED 1 LEAK AMBER CAS MESSAGE ILLUMINATED IN CRUISE FLIGHT AT 13,000 FEET. THE BLEED 1 AND 2 SWITCHES AND XBLEED KNOB WERE SELECTED OFF IN THE APPROPRIATE SEQUENCE AS DIRECTED BY THE QRH PROCEDURE. THE BLEED 1 LEAK CAS MESSAGE EXTINGUISHED MOMENTARILY TWICE AND THEN REMAINED ILLUMINATED FOR THE DURATION OF THE FLIGHT. A PRECAUTIONARY SHUTDOWN OF THE NUMBER ONE ENGINE WAS CONDUCTED AS DIRECTED BY THE QRH. **SUPPLEMENTAL INFORMATION - REMOVED & REPLACED DEFECTIVE AMS CONTROLLER IAW MM 36-21-01. OPS CHK GOOD.