N914JX
Registered owner: DELUX PUBLIC CHARTER LLC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
CREW REPORTED- AFTER TAKE-OFF FROM PBI FOâS AIRSPEED INCREASED WITH ALTITUDE AND AT 4000MSL ACTIVATED THE HIGH SPEED WARNING. THE CA & STANDBY AIRSPEED INDICATED NORMALLY. RETURNED FOR LANDING AT PBI, DURING DESCENT THE FOâS AIRSPEED DECREASED TO ZERO ON FINAL APPROACHED.-CORR ACTION- MX COPILOT'S AIRSEED IRRACTIC ON TAKEOFF - TROUBLESHOT, PERFORMED OPERATIONAL/LEAK CHECK OF THE #2 ADC SYSTEM, VERIFIED DISCREPANCY. REMOVED #2 PITOT LINE AND PURGED LINE OF DEBRI, NOTED #2 PITOT WAS CLOGGED. RESECURED #2 ADC PITOT LINE AND PERFORMED OPERATIOANL CHECKS OF THE #2 ADC WTIH NO DEFECTS NOTED.
PILOT REPORTED- AFTER NORMAL TAKEOFF LG AIR/GND FAIL CAUTION MESSAGE PRESENTED MOMENTS AFTER GEAR FINISHED ITS RETRACT CYCLE. CYCLED GEAR IN AIR TO NO AVAIL. MX, OPS AND CREW ELECTED TO PERFORM AN AIR RETURN. LANDING WAS NORMAL AND SPOILERS, T/R'S DEPLOYED AND OPERATED (BUT STOW HAD A FAILURE, SEE ASSOCIATED SNAG) AND BRAKES WERE ALL NORMAL AND OPERATIVE. MX CORR ACTION- SERVICED NLG STRUT. JACKED AIRCRAFT AND ADJUSTED MLG PROX. SENSORS. PERFORMED JACK AND CYCLE OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME.
CREW REPORTED- AIR RETURN TO BCT DUE TO LG AIR/GRND FAIL. CORR ACTION MX REMOVED NOSE WOW HARNESS W019 (PN:145-21495-403), SN:NA AND INSTALLED A CUSTOMER SUPPLIED âREPAIREDâ HARNESS W019 (PN:145-21495-403), SN:NA REMOVED NOSE WOW SWITCH (PN:80-057-01), SN:42055 AND ISTALLED A CUSTOMER SUPPLIED âTESTEDâ SWITCH (PN:80-057-01), SN:24868. GAINED ACCESS TO LEFT AND RIGHT MLG WOW WIRING HARNESS. REMOVED L/H W510 PROXIMITY SWITCH P/N80-057-01 S/N 1711 AND INSTALLED CUSTOMER SUPPLIED 'TESTED" PROXIMITY SWITCH P/N80-057-01 S/N 1329 . REMOVED R/H W510 PROXIMITY SWITCH P/N80-057-01 S/N NA AND INSTALLED CUSTOMER SUPPLIED 'NEW" PROXIMITY SWITCH P/N80-057-01 S/N 1714 REMOVED RH W510 (PN:145-21586-406 SN:N/A) AND INSTALLED A CUSTOMER SUPPLIED "NEW" HARNESS (PN:145-21586-405 SN:JSX24-109). REMOVED RH W509 (PN:145-21585-405 SN:N/A) AND INSTALLED A CUSTOMER SUPPLIED "NEW" HARNESS (PN:145-21585-405 SN:N/A). REMOVED LH W510 (PN:145-21586-405 SN:N/A) AND INSTALLED A CUSTOMER SUPPLIED "REPAIRED" HARNESS (PN:145-21586-405 SN:N/A). REMOVED LH W509 (PN:145-21585-405 SN:N/A) AND INSTALLED A CUSTOMER SUPPLIED "REPAIRED" HARNESS (PN:145-21585-405 SN:N/A). PERFORMED VARIOUS SATISFACTORY OPS CHECKS.RESTORED AIRCRAFT TO ORIGINAL CONFIGURATION. NOSE PROXIMITY SWITCH P/N80-057-01, OFF S/N 42055 ; ON: 24868 NOSE HARNESS PN:145-21495-403#1 W510 PN:145-21586-405, NSN#1 W509 PN:145-21585-405, NSN#1 PROX SENSOR PN:80-057-01, OFF SN:1711; ON SN:1329#2 W510 PN:145-21586-405, NSN#2 W509 PN:145-21585-405, NSN#2 PROX SENSOR PN:80-057-01, OFF SN: NA; ON SN:1714. CHECKED CONTINUITY FOR RELATED RELAYS. VISUALLY INSPECTED HARNESS FOR WOW PROX SWITCHES ON BOTH MAINS AND NOSE. TESTED ALL WOW PROX SWITCHES. #1 ON THE RIGHT MAIN AND #2 ON THE LEFT MAIN FAILED REMOVED AND REPLACED WITH NEW WOW PROX SWITCHES P/N 80-527-01. PERFORMED AIR/GROUND SYSTEM OPS CHECK. CHECKED GOOD. NO DEFECTS AT THIS TIME.
CREW REPORTED- AFTER ROTATION ON TAKEOFF, THE MASTER CAUTION SOUNDED WITH AN ASSOCIATED LIGHT LG AIR/GND FAIL. CREW HAD NOT EVEN ATTEMPTED TO RAISE THE GEAR YET. WHILE CONTINUING THE CLIMB TO OUR INITIAL ALTITUDE OF 4000 FEET, THE MASTER WARNING AUDIO WAS CONTINUALLY SOUNDING OFF WITH, TRIM AND FLAPS AUDIO. CREW RAN THE QRH. AUDIO CONTINUED EVEN AFTER FLAPS WERE RETRACTED. AUDIO SUBSIDED ONCE LEVEL OFF AT 4000 FEET. CREW RETURNED TO WEST PALM BEACH AND DURING LANDING THE THRUST REVERSERS WOULD NOT DEPLOY, THE GROUND SPOILERS DID NOT ACTIVATE AND THERE WAS BRAKE DEGRADATION. STEERING STILL WORKED. WHEN FLIGHT ATTENDANT OPENED THE MAIN CABIN DOOR, THE AIRCRAFT FELT AS IF IT WAS STILL PRESSURIZED AT ALTITUDE. THE MASTER WARNING AUDIO SOUNDED AND CREW RECEIVED AN MAIN DOOR OPN WARNING LIGHT. CORR ACTION- MX TROUBLESHOT BY VIA DOWNLOADED CMC/ FADEC FILES AND FORWARDED TO OPERATOR REMOVED LEGU AND INSTALLED A CUSTOMER SUPPLIED REPAIRED LEGU PERFORMED OPS CHECK - OPS CHECKED NORMAL.
CREW REPORTED- ON T/O AT AROUND 200 FT RECEIVED LG A/G FAIL, RAN QRH AND OVERRODE DOWN LOCK BUTTON, AFTER SELECTING GEAR UP RECEIVED EICAS WARNING LG LEVER DISAGREE WHICH DISAPPEARED FROM EICAS SHORTLY AFTER GEAR RETRACTION . GEAR RETRACTED NORMALLY AND WE CLEANED THE AIRCRAFT UP. DURING CLIMB WE WERE RECEIVING AURAL WARNINGS ABOUT TAKEOFF FLAPS WHICH OCCURRED AT ACCELERATION ALTITUDE. CORR ACTION MX R&R'D LGEU OPS TEST GOOD.
CREW REPORTED- LG AIR/GND FAIL UPON DEPARTURE. LANDING GEAR LOCKED DOWN. RAN QRH AND RETURNED TO DAL. CORR ACTION- MX R&R'D LGEU OPS TEST GOOD
CREW REPORTED-LG AIR GND FAIL EICAS MESSAGE AFTER TAKEOFF. USED DN LOCK REL TO RAISE GEAR. MULTIPLE AURAL WARNINGS. TRIPLE CHIME, FLAPS, LANDING GEAR, TRIM. AURAL WARNINGS CONTINUED. RAN QRH. DETERMINED SAFEST OPTION TO RETURN TO DAL. HAD NORMAL BRAKING AND STEERING. IDLE STOP FAIL. PRESSURIZATION THINKS STILL IN THE AIR. GOT STICK SHAKER AT TAXI STOP. MX TROUBLESHOT TO BAD NLG DOWNLOCK PROX SWITCH
CREW REPORTED- E1 OIL PRESS DECREASED TO AMBER RANGE AT APPROX PASSING 15000FT. OIL QTY WAS ALSO DECREASING. SHOWN 3 ON QTY. QRH PROCEDURE RAN FOR E1 LOW OIL PRESSURE. SHUTDOWN ENG PREEMPTIVELY & RETURNED TO DAL. MX OPENED THE ENG 1 COWLING AND FOUND STATOR ALTERNATOR DISCONNECTED & HANGING FROM ENG. FOUND CLAMP BOLT HAD SHEARED & FAILED CAUSING ALTERNATOR TO DISCONNECT FROM AGB CAUSING MASSIVE OIL LEAK. R & R THE STATOR ALTERNATOR. TORQUED & SAFETIED NEW CLAMP. ENG SERVICED WITH OIL. LT STATOR ALTERNATOR OPS CHKD GOOD. INSPECTED MAGNETIC CHIP DETECTOR, DRAINED OIL & PUT NEW OIL, INSPECTED ALTERNATOR STATOR, R & R V-CLAMP & HIGH-POWER ENGINE RUN, OPS CHECK GOOD, NO DEFECTS NOTED.
CREW REPORTED- AFTER DEPARTURE, CREW RECEIVED A PTRIM MAIN INOP MASTER WARNING CAUTION. CREW RAN THE QRH AND DISCONNECTED THE MAIN SYS CUTOUT SWITCH AND DISCONNECTED THE AUTOPILOT. PER MAINTENANCE CONTROL AND MISSION CONTROL CREW RETURNED TO DALLAS WITHOUT FURTHER INCIDENT. CORR ACTION MX TROUBLESHOT TO BAD FO SIDE AP TRIM SWITCH. R&R'D SWITCH OPS TEST GOOD
ISSUE CREW REPORTED STRONG ELECTRICAL ODOR FROM THE COCKPIT AFTER TAKE OFF. SEEMED TO GO AWAY AFTER 1 MINUTE POSSIBLE LIGHT SMOKE NEAR OUR FEET. TURNED BACK TO AIRPORT BJC AND LANDED. CORR ACTION MX- GAINED ACCESS TO AIRCRAFT. POWERED ON ALL ELECTRICAL SYSTEMS WITH GPU. WHILE SYSTEMS RUNNING INSPECTED UNDER THE COCKPIT FLOOR AND THE UNDERFLOOR ELECTRICAL BAY. WHILE IN THE ELECTRICAL BAY FOUND MULTIPLE DUST BUNNY'S INSIDE #2 DU COOLING FAN AND, IN THE LH DTC LRU. CLEANED CLOGGED COOLING FANS. INSPECTED FOR ANY FOWL ODER OR BURNING. NO FAULTS FOUND GAINED ACCESS TO THE BATTERY COMPARTMENT. INSPECTED FOR ANY FOWL ODER OR BURNING. NO FAULTS FOUND GAINED ACCESS TO THE PACK 1 AND PACK 2 DUCTING AFT OF REAR BULKHEAD. INSPECTED FOR ANY FOWL ODER OR BURNING. NO FAULTS FOUND POWERED UP APU, ENGAGED PACK 1 AND PACK 2. RAN FOR 30 MIN. INSPECTED FOR ANY FOWL ODER OR BURNING. NO FAULTS FOUND POWERED UP ENG 1 AND ENG 2 ENGAGED PACK 1 AND PACK 2. LET ENGINE RUN FOR 10 MIN. INSPECTED FOR ANY FOWL ODER OR BURNING. NO FAULTS FOUND.
CREW REPORTED RUDDER OSCILLATIONS AFTER AUTOPILOT ENGAGED TO 14000 FEET THEN STOPPED, ALMOST AS THOUGH THE AIRCRAFT WAS OVER CORRECTING RUDDER INPUT. OSCILLATED TO THE EXTENT OF CAUSING THE AIRCRAFT TO NOT ROLL INTO TURN SMOOTHLY BUT RATHER ROLLED SO FAR AND STOPPED AND THEN BEGAN TO ROLL AGAIN. HAND FLEW OUT OF ORANGE COUNTY ON DEPARTURE AND STILL WAS NOTICEABLE WITH YD ENGAGED BUT TO A MUCH LESSER DEGREE. MX DID AN OPERATIONAL TEST OF THE AUTO PILOT SYSTEM OPS CHECK GOOD, ALL COMMANDS WERE FOLLOWED WITH NO DISCREPANCIES. DID A FULL DEFLECTION OPERATIONAL TEST OF THE RUDDER WITH HYDRAULIC EMDP'S. OPS CHECK GOOD. TROUBLESHOT THE YAW TRIM SETTING AND FOUND THE RUDDER NOT CENTERED CORRECTLY EVEN WHEN THE EICAS INDICATION SHOWS IT BEING CENTERED. BLED HYDRAULIC SYSTEM #1 AND #2 AND DID RUDDER PCU TEST. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.
ISSUE-CREW REPORTED SHORTLY AFTER TAKEOFF RUDDER OVERBOOST WAS PRESENTED ON THE EICAS, AFTER RUNNING THE QRH PUSHED OUT SYSTEM 2. MESSAGE DID NOT PERSIST. BELOW 135 PUSHED IN SYSTEM 2 MESSAGE DID PERSIST. CORR ACTION- MX TROUBLESHOT TO BAD RUDDER PRESSURE SWITCH. R&R'D PRESSURE SWITCH OPS TEST GOOD.