N358QS
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
EMERGENCY LIGHTING: ONE HOUR INTO FLIGHT, OBSERVED ALL CABIN EMERGENCY LIGHTS FLASHING ON AND OFF WITH THE SWITCH IN THE ARMED POSITION. REMOVED AND REPLACED #1 AND #2 EMERGENCY LIGHTING BATTERIES PERFORMED OPS CHECK AND CHARGING OF THE EMERGENCY LIGHTING OPS CHECK GOOD AT THIS TIME REF AMM 33-52-01.
EMERG EXIT SIGN/LIGHT: WHEN EMER LIGHTS IS IN THE ARM POSITION, THE LIGHTS STAY ON CONSTANTLY. AND IN THE SCENT THE LIGHTS WOULD FLICKER. REMOVED FWD EMERGENCY BATTERY IAW AMM 33-52-01-000-801-A INSTALLED REPAIRED EMERGENCY BATTERY IAW AMM 33-52-01 400-801-A PERFORMED SATISCATORY OPS TEST OF EMERGENCY BATTERY IAW AMM 33-52-01-710-A
LEFT ENGINE ENGINE VIBRATION: ON CLIMBOUT THROUGH FL250 WE FELT ENGINE VIBRATIONS AND WE HEARD A MUFFLED BANG. WE THEN RECEIVED CAS MESSAGES ABOUT ENGINE EXCEEDENCE AND NO DISPATCH, THEN ENGINE 1 FAILURE AND WE SMELLED SOMETHING BURNING THAT WENT AWAY AFTER WE SECURED THE ENGINE. WE RAN THE ENGINE FAILURE QRH, THEN DECIDED TO NOT RUN THE ENGINE RESTART QRH BECAUSE N2 WAS INDICATION 0.0%. AS WE DESCENDED INTO WARMER AIR, N2 CLIMBED TO 4.0%. ON POSTFLIGHT, I NOTED THAT THE L ENGINE OIL LEVEL WAS NOT VISIBLE IN THE SIGHT GAUGE. REMOVED LT ENGINE. PERFORMED ALL REQUIRED ENGINE RUN/LEAK CHECKS WITH NO DEFECTS NOTED. ALL MAINTENANCE PERFORMED IAW AMM 71-00-00 & EMM 71-00-00.
EMERGENCY LIGHTING: AFT AISLE LIGHT (JUST BEFORE LAV) IS INOP AND OUT OF ITS SOCKET.
WHILE CLOSING THE MAIN ENTRY DOOR FOUND THE FWD TELESCOPING ROD MOUNTING BRACKET TO THE DOOR DAMAGED. BRACKET IS CRACKED AND BENT PULLING THE RIVET FROM THE DOOR FRAME, DOOR FRAME IS CRACKED AS WELL. I HAVE ATTACHED PICTURES OF THE DAMAGE. /// CORRECTIVE ACTION /// COMPLIED WITH THE ETD2022-P300-04409702 AND INSTALLED NEW TELESCOPIC ROD FITTING. INSTALLED "NEW" SHROUD AFT PAX DOOR PN: 506-45250-4002 SN: NIA ALL WORK PERFORMED IAW EMB PHENOM 300 AMM CH.33-26-50.
EMERGENCY LIGHTS FAILED FUNCTIONAL TEST-LOWER STEP LIGHTS DO NOT ILLUMINATE WITH AFT BATTERY CONNECTED. FOUND BROKEN WIRE W801-00009-22- REPAIRED PER SWPM AND OPEN FUSE F0037- REPLACED WITH NEW AND OPERATIONAL TEST GOOD. THIS REPORT SUBMITTED TO COMPLY WITH PART 135 OPERATOR'S GENERAL MAINTENANCE MANUAL (GMM) REQUIREMENTS.
CABIN EMERG LIGHT: EMERG LIGHTS COME IN FLIGHT. AFTER 5 MINUTES THEY START FLASHING ON AND OFF RAPIDLY. // SIGNOFF// REMOVED FWD EMERGENCY LIGHT BATTERY P/N 7450LS-O0 S/N 005429 AND INSTALLED CUSTOMER SUPPLIED NEW UNIT P/ N 7450LS-00 5/N 005816. REMOVED AFT EMERGENCY UGHT BATTERY P/N 6450LS-O0 5/N 000726 AND INSTALLED CUSTOMER SUPPLIED NEW UNIT P /N 7450LS-O0 5/ N 005829 AND OPS CHECKED GOOD REFERENCE EMB PHENOM 300 AMM 33-52-01.
AT FL410 A BATTERY EXCEEDENCE WAS DISPLAYED ON EICAS. AFTER A FEW SECONDS THE MESSEAGE EXTINGUISHED AND THEN ILLUMINATED AGAIN. AFTER COMPLETING CHECKLIST WE DIVERTED TO NEAREST SUITABLE AIRPORT. PERFORMED FIM TASK 24-36-00-810-802-A BATTERY VOLTAGE EXCEEDED ALL OPERATIONAL CHECKS WAS GOOD AT THIS TIME. ADVISED CONTACT CENTER, COULD NOT DUPLICATE SQUAK OF FINDINGS. THEY EVALUATED INFO AND CMC FILES AND RECOMMENDED TO REPLACED RPDU. REPLACED FAULTY RPDU PN SX7EG21-3 SN 0308 WITH TEST RPDU IAW AMM 24-65-02 ALL OPS CHECK GOOD AT THIS TIME.
THE CONNECTION ON CAPTAINS O2 MASK, BETWEEN THE MASK HOSE & THE HOSE COMING OFF THE FLOW INDICATOR BROKE. O2 WAS TURNED OFF & THERE IS 900 PSI IN O2 BOTTLE. REMOVED OLD O2 MASK BOX PN 1186F6-23, SN 1431. INSTALLED A REPAIRED O2 MASK STORAGE BOX PN 1186F6-23, SN 00391 IAW AMM 35-11-01 & SERVICED IAW AMM 12-16-00. OPERATIONS CHECKED GOOD AT THIS TIME.
RT SEAT BRAKE PEDALS REQUIRE EXCESSIVE TRAVEL BEFORE BRAKING ACTION OCCURS. BRAKING ACTION APPEARS NORMAL AND BRAKES HOLD ACFT STATIONARY AT HIGH POWER SETTINGS. VERIFIED DISCREPANCY. INSPECTED MASTER CYLINDERS AND CHECKED TIGHTNESS OF FITTINGS. NO DEFECTS NOTED. BLED BRAKE SYSTEM AND SERVICED RESERVOIR PER CESSNA 560 M/M 32-42-00. OPS AND LEAK CHECK GOOD.
DURING THE CONTROL AND SPEED BRAKE CHECK, THE RT ENGINE SHUTDOWN AFTER BRINGING THE THROTTLE TO IDLE. RAN BOTH ENGINES AND ACCOMPLISHED RAPID DECELERATION CHECKS ON BOTH (10 TIMES) EACH. NO DISCREPANCIES NOTED. TAXIED TO RUN-UP AREA AND EXTENDED SPEED BRAKES. RAN ENGINES ABOVE 85 PERCENT N1 AND SPEED BRAKES STOWED. RAPIDLY DECELERATED BOTH ENGINES, NO FAULTS. CHECKED IDLE INDEX ON FUEL CONTROL UNIT. CHECKED GOOD. DONE IN REF TO MM.
IN FLT, RT FUEL FILTER BYPASS CAME ON. LT FUEL FILTER BYPASS CAME ON APPROX 2 MIN`S LATER. INTERMITTENT UNTIL FL300, STAYED ON UNTIL PARKING & SHUTDOWN. LT BOOST PUMP ANNUNCIATED SHORT FINAL. (M2B) - TOOK FUEL SENDER FROM LT & RT WING SUMP & FUEL FILTER DRAIN FOR ANALYSIS. DRAINED & SUMPED ALL FUEL FROM BOTH TANKS & REPLACED BOTH AIRFRAME FUEL FILTERS & BOTH ENG FILTERS IAW MM 28-00-02, 28-21-05 & PWA MM 73-10-02. INSPECTED INSIDE BOTH FUEL TANKS & FOUND NO DEBRIS OR ON FUEL FILTERS. PUMPED FRESH FUEL INTO TANKS. GROUND RAN BOTH ENG`S, NO DEFECTS IN FUEL SYS OR LEAKS AT FILTERS OR FUEL TANK ACCESS PANELS IAW MM 28-10-00. ALSO VISUALLY VERFIIED PROPER PLACARDS TO BE INSTALLED AT A/C FUELING POINTS.
UPON APPLYING BRAKES FROM A NORMAL TAXI SPEED, THERE IS INITIALLY NO BRAKING RESPONSE, FOLLOWING BY A HARD, GRABING BRAKE, FEELS AS THROUGH THE ANTI SKID IS NOT ALLOWING THE BRAKES TO FUNCTION, THEN GRABS. BLED BRAKE SYSTEM. PERFORMED FUNCTIONAL CHECK OF BRAKE SYSTEM. SYSTEM CHECK NORMAL. FOUND LOOSE CONNECTOR IN LT WHEEL WELL. TIGHTENED CONNECTOR. PERFORMED TRANSDUCER CHECK AND TAXI CHECK. BOTH CHECKS NORMAL. ALL WORK DONE IAW CITATION 560 MM 32-42-00.
LT ENGINE OIL PRESSURE REACHED 100 PSI PRIOR TO REACHING COMPUTED TAKE OFF POWER SETTING. REPLACED LT ENGINE OIL PRESSURE TRANSDUCER, ADJUSTED LT ENGINE OIL PRESSURE REGULATOR .5 TURN COUNTERCLOCKWISE OIL PRESSURE AT GROUND IDLE LOW 65 PSI AT TAKE OFF POWER 90 PSI PRESSURE WITHIN LIMITS. OPS AND LEAK CHECK OF TRANSDUCER GOOD, CHECK IAW MM CHAPTER 77-31-01, MM CHAPTER 79-20-01 AND 71-00-00.
ON LANDING AT LAS POWER BRAKE ACCUMULATOR AND ANTI-SKID ANUNCIATORS ILLUMINATED, BRAKES WERE INOP ON LANDING. AIRCRAFT CAME TO REST WITHOUT INCIDENT. SERVICED BRAKE ACCUMULATOR IAW CESSNA CITATION 560 MM CHAPTER 12-12-02, BLED BRAKES IAW CHAPTER 32-42-00, OPERATIONAL CHECK OF BRAKE AND ANTI-SKID SYSTEM SATISFACTORY ON TAXI CHECK.