# Service difficulty reports: N258JQ, cancelled Sep 27, 2019 A list on [N258JQ, cancelled Sep 27, 2019](https://openairdocs.org/deregistered/N258JQ-2019-09-27.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR UHLA201509220733](https://openairdocs.org/sdr/UHLA201509220733.md): Skin · dented · Sep 22, 2015 · N258JQ · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING INSPECTION, A DENT WAS FOUND IN THE FORWARD FUSELAGE AFT OF THE NLG. REPAIRED IAW ETD 2015-145-088747. - [SDR CHQA20141102311](https://openairdocs.org/sdr/CHQA20141102311.md): Access Door · open · Nov 2, 2014 · N258JQ · Emb EMB145LR · Service Doors > A HUMMING NOISE FROM THE LOWER LT NOSE AREA DURING CLIMB. THE CREW ELECTED TO RETURN TO FIELD & LANDED WITHOUT FURTHER INCIDENT. FOUND THE GPU ACCESS PANEL TO BE OPEN. THE DOOR WAS CLOSED & NO FURTHER DEFECTS WERE NOTED. - [SDR CHQA20141020299](https://openairdocs.org/sdr/CHQA20141020299.md): Isis · faulty · Oct 20, 2014 · N258JQ · Emb EMB145LR · Integrated Flight System > RECEIVED A STANDBY ATTITUDE INDICATION FAILURE IN FLIGHT. DIVERTED THE ACFT & LANDED WITHOUT INCIDENT. REPLACED THE ISIS. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20140903247](https://openairdocs.org/sdr/CHQA20140903247.md): Light · inoperative · Sep 3, 2014 · N258JQ · Emb EMB145LR · Emergency Lighting > DURING INSPECTION THE LT OVERWING EXTERIOR EMER LIGHT WAS FOUND TO BE INOPERATIVE. RE-LAMPED THE LT OVERWING EMER LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20140815245](https://openairdocs.org/sdr/CHQA20140815245.md): Floor Support · corroded · Aug 15, 2014 · N258JQ · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION THE CTR OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE CTR OMEGA BEAM FROM FRAMES 16 TO 23 WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140811246](https://openairdocs.org/sdr/CHQA20140811246.md): Skin · cracked · Aug 11, 2014 · N258JQ · Emb EMB145LR · Fuselage Main, Plate/Skin > DURING INSPECTION THE SKIN WAS FOUND TO BE CRACKED BELOW STRINGER 2L AT FRAME 75. THE SKIN WAS REPAIRED IAW ETD 2014-145-067832. - [SDR CHQA20140810244](https://openairdocs.org/sdr/CHQA20140810244.md): Floor Support · corroded · Aug 10, 2014 · N258JQ · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION THE CTR OMEGA BEAM INBD FLANGE WAS FOUND TO BE CORRODED FRAME 23 - 24. THE OMEGA BEAM FLANGE WAS REPAIRED IAW SRM 53-00-10. - [SDR CHQA20140810243](https://openairdocs.org/sdr/CHQA20140810243.md): Floor Support · cracked · Aug 10, 2014 · N258JQ · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION THE RT SIDE OMEGA BEAM SUPPORT AT FRAME 47 & 48 WAS FOUND TO BE CRACKED. THE RT OMEGA BEAM SUPPORT WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140425124](https://openairdocs.org/sdr/CHQA20140425124.md): Light · inoperative · Apr 25, 2014 · N258JQ · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE EMERGENCY FLOOR PROXIMITY STRIP LIGHT AT ROWS 8 & 9 WAS FOUND TO BE INOPERATIVE. REPLACED THE EMERGENCY FLOOR STRIP LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA20140226071](https://openairdocs.org/sdr/CHQA20140226071.md): Hydraulic System · low · Feb 26, 2014 · N258JQ · Emb EMB145LR · Hydraulic System, Main > CREW REPORTED AFTER TAKEOFF THEY RECEIVED A HYD SYS 1 LOW QTY MSG. THE CREW DECLARED AN EMERGENCY & RETURNED TO FIELD. THE ACFT LANDED WITHOUT INCIDENT. MX SERVICED THE NR 1 HYD SYS. NO LEAKS WERE NOTED & THE ACFT WAS RETURNED TO SERVICE. - [SDR CHQA20120822298](https://openairdocs.org/sdr/CHQA20120822298.md): Frame · corroded · Aug 22, 2012 · N258JQ · Emb EMB145LR · Fuselage Main, Frame > DURING INSPECTION, CORROSION WAS FOUND ON FRAME 65 AT LATERAL "L" AT THE CARGO DOOR THRESHOLD. FRAME 65 WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-011847 AND SRM 51-40-02. - [SDR CHQA20120817302](https://openairdocs.org/sdr/CHQA20120817302.md): Support · cracked · Aug 17, 2012 · N258JQ · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, THE RIGHT OMEGA BEAM SUPPORT WAS FOUND TO BE CRACKED AT FRAME 47. MAINTENANCE REPLACED THE RIGHT OMEGA BEAM SUPPORT AT FRAME 47 IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20120817299](https://openairdocs.org/sdr/CHQA20120817299.md): Beam · corroded · Aug 17, 2012 · N258JQ · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE BAGGAGE DOOR CUTOUT RIB 15R FRAME 65 THROUGH FRAME 68. THE BEAM WAS REPLACED IN ACCORDANCE WITH SRM 51-10-03. - [SDR CHQA20120817297](https://openairdocs.org/sdr/CHQA20120817297.md): Sill · corroded · Aug 17, 2012 · N258JQ · Emb EMB145LR · Fuselage Miscellaneous Structure > DURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR SILL PLATE AT ALL 3 NUT PLATE LOCATIONS. THE SERVICE DOOR SILL WAS REPLACED IN ACCORDANCE WITH SRM 51-40-08. - [SDR CHQA20120728226](https://openairdocs.org/sdr/CHQA20120728226.md): Switch · faulty · Jul 28, 2012 · N258JQ · Emb EMB145LR · Windshield/Door Rain/Ice Removal > CREW REPORTED THAT ON DESCENT, WITH THE WINDSHIELD HEAT TURNED ON FOR ABOUT 10 MINUTES, A SLIGHT ELECTRICAL ODOR WAS PRESENT. CREW FURTHER REPORTED THAT BOTH WINDSHIELDS WERE NOT HEATING. WINDSHIELD HEAT WAS TURNED OFF AND THE ODOR DISSIPATED. MAINTENANCE R - [SDR CHQA20120725225](https://openairdocs.org/sdr/CHQA20120725225.md): Unknown · odor · Jul 25, 2012 · N258JQ · Emb EMB145LR · Air Distribution System > CREW REPORTED A BURNING ODOR DURING FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE ISOLATED THE BURNING ODOR TO COOLING PACK 1. MAINTENANCE COULD NOT DUPLICATE THE BURNING ODOR AND OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100292](https://openairdocs.org/sdr/CHQA201100292.md): Duct · disconnected · Jul 23, 2011 · N258JQ · Emb EMB145LR · Air Distribution System > CREW REPORTED, RECEIVED AN AILERON MIS-TRIM MESSAGE FOLLOWED BY AN AUTO-PILOT FAIL. THE CREW REPORTED THAT THE AILERONS WERE BINDING AND THEY HAD TO BE FORCED FREE. THE AIRCRAFT LANDED IN KDCA WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO KCMH FOR FURTHER T - [SDR CHQA201100248](https://openairdocs.org/sdr/CHQA201100248.md): Ahrs · faulty · Jun 25, 2011 · N258JQ · Emb EMB145LR · Integrated Flight System > CREW REPORTED THAT DURING FLIGHT RECEIVED AND AILERON MISTRIM MESSAGE AND THAT THE AILERONS WERE BINDING WHILE ATTEMPTING TO TURN RIGHT. THE CREW FORCED THE AILERONS FREE AND THE AIRCRAFT FLEW NORMALLY THE REST OF THE FLIGHT. THE AIRCRAFT LANDED WITHOUT INCI - [SDR CHQA201100230](https://openairdocs.org/sdr/CHQA201100230.md): Recovery Unit · malfunctioned · Jun 22, 2011 · N258JQ · Emb EMB145LR · Aileron Control System > WHILE DESCENDING INTO KCAE ON AUTO PILOT, CREW RECEIVED AND AP MISS TRIM MESSAGE ON EICAS. WHEN THE QUICK DISCONNECT WAS PUSHED INITIALLY THE ROLL CONTROL WAS FROZEN. THE CREW THEN MANUALLY FORCED THE AILERONS OVER TO FREE THEM AND THE AIRCRAFT LANDED WITHOU - [SDR CHQA201100227](https://openairdocs.org/sdr/CHQA201100227.md): Actuator · malfunctioned · Jun 19, 2011 · N258JQ · Emb EMB145LR · Aileron Control System > DURING FLIGHT, THE FLIGHT CREW REPORTED THAT THE AILERONS LOCKED IN STRAIGHT AND LEVEL FLIGHT, FOLLOWED BY AILERON MIS-TRIM. THE CREW HAD TO FORCE THE AILERONS TO GET AUTO PILOT TO DISENGAGE. DURING APPROACH, THE AILERONS LOCKED AGAIN BUT THE CREW WAS ABLE T - [SDR CHQA201100225](https://openairdocs.org/sdr/CHQA201100225.md): Feel Unit · malfunctioned · Jun 16, 2011 · N258JQ · Emb EMB145LR · Aileron Control System > DURING THE FLIGHT TO KSDF WITH THE AUTO PILOT ON MEL, THE FLIGHT CREW REPORTED THAT THE AILERONS LOCKED UP SEVERAL TIMES DURING FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT IN KSDF. MAINTENANCE INSPECTED THE AILERON CABLES AND FOUND NO DEFECTS. THE AILERON - [SDR CHQA201100224](https://openairdocs.org/sdr/CHQA201100224.md): Computer · malfunctioned · Jun 16, 2011 · N258JQ · Emb EMB145LR · Aileron Control System > WHILE DESCENDING THROUGH 5,000FT INTO KDCA THE CREW REPORTED AN AILERON MIS TRIM MESSAGE ON EICAS. THE AUTO PILOT WAS THEN TURNED OFF AND REPORTED THAT THE AILERONS WERE LOCKED. THE CREW WAS ABLE TO FREE THE AILERONS BY FORCING THE AILERONS TO MOVE. THE AIR - [SDR CHQA201100222](https://openairdocs.org/sdr/CHQA201100222.md): Autopilot Sys · malfunctioned · Jun 12, 2011 · N258JQ · Emb EMB145LR · Autopilot System > CREW REPORTED THAT DURING CLIMB AT 22,000 FEET, RECEIVED AN AUTO-PILOT AILERON MISTRIM MESSAGE. THEN AT 27,000 FEET RECEIVED AN AUTO-PILOT FAIL MESSAGE. THE PILOT DISENGAGED THE AUTO-PILOT SYSTEM AND REPORTED HE COULD NOT MOVE THE AILERONS AND THAT THE AUTO- - [SDR CHQA201100221](https://openairdocs.org/sdr/CHQA201100221.md): Servo · inoperative · Jun 10, 2011 · N258JQ · Emb EMB145LR · Aileron Control System > CREW REPORTED THAT DURING CLIMB, AT 22,000 FEET, LOST AILERON CONTROL AND THE CONTROL WAS LOCKED. WITH EXCESSIVE FORCE, THE CREW FREED THE AILERON CONTROL. THE CREW RETURNED TO KSDF AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AILERON SERVO MOTOR. - [SDR CHQA201100140](https://openairdocs.org/sdr/CHQA201100140.md): Switch · intermittent · Apr 17, 2011 · N258JQ · Emb EMB145LR · Door Warning System > CREW REPORTED THAT THE FUEL DOOR WAS INDICATING OPEN DURING FLIGHT. THE CREW RETURNED TO KPHL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND TWO LATCHES OPEN ON THE FUELING DOOR AND AN INTERMITTENT SWITCH. MAINTENANCE SECURED THE LATCHES SHUT AND PLACED THE - [SDR CHQA201100063](https://openairdocs.org/sdr/CHQA201100063.md): Seal · loose · Mar 16, 2011 · N258JQ · Emb EMB145LR · Flight Compartment Windows > SHORTLY AFTER TAKEOFF, THE FLIGHT CREW REPORTED A NOISE COMING FROM JUST AFT OF THE CAPTAIN'S DV WINDOW. THEY COULD SEE SOMETHING SLAPPING THE FUSELAGE BUT COULD NOT IDENTIFY WHAT IT WAS SO THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENA - [SDR CHQA201100027](https://openairdocs.org/sdr/CHQA201100027.md): Wire · broken · Jan 26, 2011 · N258JQ · Emb EMB145LR · Light System Wiring > DURING INSPECTION, THE NR 4 EMERGENCY FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO HAVE A BROKEN WIRE AT THE SOCKET END. MAINTENANCE REPLACED THE NR 4 EMERGENCY FLOOR PROXIMITY LIGHT STRIP WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201000217](https://openairdocs.org/sdr/CHQA201000217.md): Light · inoperative · Nov 30, 2010 · N258JQ · Emb EMB145LR · Emergency Lighting > DURING INSPECTION THE EMERGENCY LIGHT FOR THE COCKPIT STEP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE COCKPIT STEP EMERGENCY LIGHT WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201000214](https://openairdocs.org/sdr/CHQA201000214.md): Bulb · burned out · Nov 24, 2010 · N258JQ · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE EMERGENCY LIGHT ON THE MAIN ENTRY DOOR WAS FOUND TO BE INOP. MX FOUND THE BULB FOR THE MAIN ENTRY DOOR EMERGENCY LIGHT MISSING. THE BULB WAS REPLACED WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201000119](https://openairdocs.org/sdr/CHQA201000119.md): Flap · malfunctioned · Jun 11, 2010 · N258JQ · Emb EMB145LR · Trailing Edge Flap Control System > WHILE ON DESCENT INTO DCA WHEN THE CREW ATTEMPTED DEPLOY THE FLAPS TO 9 DEGREE POSITION, A FLAP LOW RATE MESSAGE WAS DISPLAYED FOLLOWED BY A FLAP FAIL MESSAGE AND THE FLAPS CONTINUED TO INDICATE ZERO. THE QRH WAS FOLLOWED AND THE AIRCRAFT DIVERTED TO IAD, LAN - [SDR CHQA201000051](https://openairdocs.org/sdr/CHQA201000051.md): Unknown · malfunctioned · Mar 2, 2010 · N258JQ · Emb EMB145LR · Independent Instruments > CREW RECEIVED ATT: CAGE MESSAGE ON ISIS IN FLIGHT. IN STABLE FLIGHT THE CREW TRIED TO RESET PER QRH AND FAILED TO GET ATT 10'S FLAG AND RETURNED TO FIELD. MAINTENANCE TROUBLESHOT THE FAULT PER FIM 34-01-00-810-809-A AND FOUND IT TO BE A TRANSITORY CONDITION - [SDR CHQA201000044](https://openairdocs.org/sdr/CHQA201000044.md): Battery Pack · discharged · Feb 21, 2010 · N258JQ · Emb EMB145LR · Emergency Lighting > DURING INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT AND THE OVERHEAD EMERGENCY LIGHT ABOVE OVERHEAD BIN 1 WERE INOP. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY PACK WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA200900247](https://openairdocs.org/sdr/CHQA200900247.md): Heat Exchanger · contaminated · Nov 21, 2009 · N258JQ · Emb EMB145LR · Cabin Cooling System > DURING CLIMB, CREW REPORTED A LAVATORY SMOKE WARNING AND A MILD ODOR WITH NO VISIBLE SMOKE. ACFT RETURNED TO FIELD & LANDED WITHOUT INCIDENT. MX TROUBLESHOT FAULT TO THE NR 2 BLEED SYSTEM. BOTH PRECOOLERS HAD BEEN CHANGED THE NIGHT BEFORE FOR SCHEDULED MX & - [SDR CHQA200900245](https://openairdocs.org/sdr/CHQA200900245.md): Smoke Detector · false activation · Nov 15, 2009 · N258JQ · Emb EMB145LR · Smoke Detection > DURING CRUISE THE CREW RECEIVED A BAGGAGE SMOKE MESSAGE AND THE BAGGAGE LIGHT CAME ON. THE CREW DISCHARGED THE BAGGAGE FIRE EXTINGUISHERS PER THE QRH. THE FLIGHT DIVERTED TO IAD AND THE MESSAGE AND LIGHT CLEARED PRIOR TO TOUCHDOWN. THE MESSAGE AND LIGHT APP - [SDR CHQA200900241](https://openairdocs.org/sdr/CHQA200900241.md): Relay · faulty · Nov 8, 2009 · N258JQ · Emb EMB145LR · Smoke Detection > DURING CRUISE THE FLIGHT CREW REPORTED THAT THE BAGGAGE SMOKE LIGHT CAME ON AND THE BAGG SMOKE EICAS MESSAGE FLASHED ON AND OFF. THE CREW REPORTED NO INDICATIONS OF HEAT, SMOKE OR FIRE THROUGH THE BAGGAGE COMPARTMENT VIEWER IN THE LAV. THE AIRCRAFT CONTINUED - [SDR CHQA200900240](https://openairdocs.org/sdr/CHQA200900240.md): Smoke Warning · false activation · Nov 8, 2009 · N258JQ · Emb EMB145LR · Smoke Detection > DURING CRUISE THE FLIGHT CREW REPORTED THAT THE BAGGAGE SMOKE LIGHT CAME ON ALONG WITH A BAGG SMOKE MESSAGE ON EICAS. AFTER A FEW SECONDS THE EICAS MESSAGE CLEARED BUT THE BAGGAGE SMOKE LIGHT REMAINED ON. THE CREW VERIFIED THAT THERE WERE NO INDICATIONS OF S - [SDR CHQA200900143](https://openairdocs.org/sdr/CHQA200900143.md): Tire · blown · Jun 14, 2009 · N258JQ · Emb EMB145LR · Tire > ON TAKE OFF THE RT IB MAIN LANDING GEAR TIRE BLEW. THE FLIGHT CONTINUED NORMALLY UNTIL REACHING DCA WHERE IT WAS NOT ALLOWED TO LAND. THE FLIGHT THEN DIVERTED TO IAD WHERE IT LANDED WITHOUT INCIDENT. UPON INSPECTION AFTER THE FLIGHT THE FWD WOW HARNESS WAS - [SDR CHQA200900137](https://openairdocs.org/sdr/CHQA200900137.md): Wire Harness · damaged · Jun 8, 2009 · N258JQ · Emb EMB145LR · Landing Gear System Wiring > FLIGHT 3048, RDU TO LGA - CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE UPON ROTATION. THE LANDING GEAR LEVER COULD NOT BE MOVED TO THE UP POSITION. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS INSPECTED AND FOUND SAFE - [SDR CHQA200900132](https://openairdocs.org/sdr/CHQA200900132.md): Landing Gear · malfunctioned · May 22, 2009 · N258JQ · Emb EMB145LR · Main Landing Gear > THE FLIGHT CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE IMMEDIATELY AFTER TAKEOFF, AND THE GEAR WOULD NOT RETRACT. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. THE ACFT WAS FERRIED WITH THE GEAR EXTENDED FOR FURTHER TROUBLESHOOTING. A - [SDR CHQA200900128](https://openairdocs.org/sdr/CHQA200900128.md): Electronic Unit · malfunctioned · May 21, 2009 · N258JQ · Emb EMB145LR · Landing Gear Position and Warning > THE CREW RETURNED TO FIELD FOR A LANDING GEAR AIR/GROUND FAIL MESSAGE AND ALSO REPORTED A FAINT ELECTRICAL ODOR ON TAKEOFF. THE CMC WAS DOWNLOADED AND NO FAULT MESSAGES WERE PRESENT. AL RELAY PANELS WERE INSPECTED WITH NO DAMAGE NOTED. THE LGEU WAS REPLACED - [SDR CHQA200900124](https://openairdocs.org/sdr/CHQA200900124.md): Relay · faulty · May 8, 2009 · N258JQ · Emb EMB145LR · Landing Gear Position and Warning > FLIGHT 3043, LGA TO IND, AFTER TAKEOFF WHEN THE LANDING GEAR WAS SELECTED UP, THE CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS AND THE GEAR WOULD NOT RETRACT. THE GEAR INDICATED DOWN AND LOCKED THE ENTIRE FLIGHT. THE AIRCRAFT RETURNED TO LGA - [SDR CHQA200900102](https://openairdocs.org/sdr/CHQA200900102.md): Proximity Switch · faulty · Apr 6, 2009 · N258JQ · Emb EMB145LR · Landing Gear Position and Warning > FLIGHT 3054, BUF TO BOS - THE FLIGHT CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON TAKEOFF. THE AIRCRAFT RETURNED TO BUF AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CMC MESSAGES FOR LGEU FAIL AND PROX SWITCH FAIL. AN AIR/GROUND TEST WAS PERFORM - [SDR CHQA200500145](https://openairdocs.org/sdr/CHQA200500145.md): Smoke · detected · Aug 19, 2005 · N258JQ · Emb EMB145LR · Air Distribution System > AFTER AN HOUR ON THE GROUND, LAV SMOKE IND DURING INITIAL CLIMB AT ABOUT 600 FT. F/A REPORTED SMOKE IN REAR OF CABIN. NO EMERGENCY DECLARED; REQUESTED TO RETURN TO THE FIELD. PRIOR TO PUTTING ON O2 MASKS, SMELLED A PUNGENT SMELL. CLEARED TO LAND AND ATC WA - [SDR CHQA200500031](https://openairdocs.org/sdr/CHQA200500031.md): Engine · contaminated · Feb 13, 2005 · N258JQ · Emb EMB145LR · Air Distribution System > CLIMBING AT 10,000 FT A BURNING SMELL WAS NOTED IN THE COCKPIT. WITHIN A FEW SECONDS, THE SMELL GOT REALLY STRONG AND THE PILOT'S NOSE AND EYES BEGAN TO BURN. THE FLIGHT ATTENDANT AND PASSENGERS ALSO NOTICED THE SMELL. THE CREW CALLED ATC AND ATC DECLARED A - [SDR CHQA200500057](https://openairdocs.org/sdr/CHQA200500057.md): Bulb · burned out · Jan 1, 2005 · N258JQ · Emb EMB145LR · Emergency Lighting > LEFT AFT OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 145 AMM 3-50-10. OPS CHECK GOOD. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N258JQ' AND deregistration_id = 'N258JQ-2019-09-27' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N258JQ-2019-09-27/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.