# N258JQ: 2003 Embraer EMB-145LR, registration cancelled 2019-09-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 27, 2019
- Exported to: Mexico
- Status when cancelled: Valid registration
- Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212)
- Engine: [Rolls-Royce AE3007 series](https://openairdocs.org/engine/rolls-royce-ae3007-series) (registry code 54582)
- Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs)
- Serial number: 145768
- Year built: 2003
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 12, 2003
- Certificate issued: October 9, 2018
- Last registry action: October 9, 2018
- Mode S code: A2760D
- Owner when cancelled: [Southern Aircraft Consultancy Inc Trustee](https://openairdocs.org/faa-owner/SOUTHERN%20AIRCRAFT%20CONSULTANCY%20INC%20TRUSTEE)
- Location: Bungay Suffolk, United Kingdom
- Owner type: Corporation
- The mark today: https://openairdocs.org/aircraft/N258JQ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=258JQ
- Page: https://openairdocs.org/deregistered/N258JQ-2019-09-27

From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Embraer EMB-145LR: https://openairdocs.org/model/embraer-emb-145lr.md

## Service difficulty reports (45)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR UHLA201509220733](https://openairdocs.org/sdr/UHLA201509220733), Sep 22, 2015: SKIN. DENTED. 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), Nov 2, 2014: ACCESS DOOR. OPEN. 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 B
- [SDR CHQA20141020299](https://openairdocs.org/sdr/CHQA20141020299), Oct 20, 2014: ISIS. FAULTY. RECEIVED A STANDBY ATTITUDE INDICATION FAILURE IN FLIGHT. DIVERTED THE ACFT & LANDED WITHOUT INCIDENT. REPLACED THE ISIS. OPERATIONAL CHECKS WERE GOOD WITH NO F
- [SDR CHQA20140903247](https://openairdocs.org/sdr/CHQA20140903247), Sep 3, 2014: LIGHT. INOPERATIVE. 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 FU
- [SDR CHQA20140815245](https://openairdocs.org/sdr/CHQA20140815245), Aug 15, 2014: FLOOR SUPPORT. CORRODED. 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), Aug 11, 2014: SKIN. CRACKED. 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), Aug 10, 2014: FLOOR SUPPORT. CORRODED. 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), Aug 10, 2014: FLOOR SUPPORT. CRACKED. 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), Apr 25, 2014: LIGHT. INOPERATIVE. DURING INSPECTION, THE EMERGENCY FLOOR PROXIMITY STRIP LIGHT AT ROWS 8 & 9 WAS FOUND TO BE INOPERATIVE. REPLACED THE EMERGENCY FLOOR STRIP LIGHT. OPERATIONAL CH
- [SDR CHQA20140226071](https://openairdocs.org/sdr/CHQA20140226071), Feb 26, 2014: HYDRAULIC SYSTEM. LOW. 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 SERV
- [SDR CHQA20120822298](https://openairdocs.org/sdr/CHQA20120822298), Aug 22, 2012: FRAME. CORRODED. 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 
- [SDR CHQA20120817302](https://openairdocs.org/sdr/CHQA20120817302), Aug 17, 2012: SUPPORT. CRACKED. 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
- [SDR CHQA20120817299](https://openairdocs.org/sdr/CHQA20120817299), Aug 17, 2012: BEAM. CORRODED. 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), Aug 17, 2012: SILL. CORRODED. 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
- [SDR CHQA20120728226](https://openairdocs.org/sdr/CHQA20120728226), Jul 28, 2012: SWITCH. FAULTY. 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 WI
- [SDR CHQA20120725225](https://openairdocs.org/sdr/CHQA20120725225), Jul 25, 2012: UNKNOWN. ODOR. CREW REPORTED A BURNING ODOR DURING FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE ISOLATED THE BURNING ODOR TO COOLING PACK 1. MAINTEN
- [SDR CHQA201100292](https://openairdocs.org/sdr/CHQA201100292), Jul 23, 2011: DUCT. DISCONNECTED. 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 F
- [SDR CHQA201100248](https://openairdocs.org/sdr/CHQA201100248), Jun 25, 2011: AHRS. FAULTY. 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 AIL
- [SDR CHQA201100230](https://openairdocs.org/sdr/CHQA201100230), Jun 22, 2011: RECOVERY UNIT. MALFUNCTIONED. 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 F
- [SDR CHQA201100227](https://openairdocs.org/sdr/CHQA201100227), Jun 19, 2011: ACTUATOR. MALFUNCTIONED. 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 
- [SDR CHQA201100225](https://openairdocs.org/sdr/CHQA201100225), Jun 16, 2011: FEEL UNIT. MALFUNCTIONED. 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 WITH
- [SDR CHQA201100224](https://openairdocs.org/sdr/CHQA201100224), Jun 16, 2011: COMPUTER. MALFUNCTIONED. 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 AILE
- [SDR CHQA201100222](https://openairdocs.org/sdr/CHQA201100222), Jun 12, 2011: AUTOPILOT SYS. MALFUNCTIONED. 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 PIL
- [SDR CHQA201100221](https://openairdocs.org/sdr/CHQA201100221), Jun 10, 2011: SERVO. INOPERATIVE. 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 
- [SDR CHQA201100140](https://openairdocs.org/sdr/CHQA201100140), Apr 17, 2011: SWITCH. INTERMITTENT. 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
- [SDR CHQA201100063](https://openairdocs.org/sdr/CHQA201100063), Mar 16, 2011: SEAL. LOOSE. 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 COUL
- [SDR CHQA201100027](https://openairdocs.org/sdr/CHQA201100027), Jan 26, 2011: WIRE. BROKEN. 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 FLO
- [SDR CHQA201000217](https://openairdocs.org/sdr/CHQA201000217), Nov 30, 2010: LIGHT. INOPERATIVE. DURING INSPECTION THE EMERGENCY LIGHT FOR THE COCKPIT STEP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE COCKPIT STEP EMERGENCY LIGHT WITH NO FURTHER DE
- [SDR CHQA201000214](https://openairdocs.org/sdr/CHQA201000214), Nov 24, 2010: BULB. BURNED OUT. 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 
- [SDR CHQA201000119](https://openairdocs.org/sdr/CHQA201000119), Jun 11, 2010: FLAP. MALFUNCTIONED. 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 A
- [SDR CHQA201000051](https://openairdocs.org/sdr/CHQA201000051), Mar 2, 2010: UNKNOWN. MALFUNCTIONED. 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. MAINT
- [SDR CHQA201000044](https://openairdocs.org/sdr/CHQA201000044), Feb 21, 2010: BATTERY PACK. DISCHARGED. DURING INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT AND THE OVERHEAD EMERGENCY LIGHT ABOVE OVERHEAD BIN 1 WERE INOP. MAINTENANCE REPLACED THE NR 1 EMERGENCY LI
- [SDR CHQA200900247](https://openairdocs.org/sdr/CHQA200900247), Nov 21, 2009: HEAT EXCHANGER. CONTAMINATED. 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 FAU
- [SDR CHQA200900245](https://openairdocs.org/sdr/CHQA200900245), Nov 15, 2009: SMOKE DETECTOR. FALSE ACTIVATION. 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 FLIGH
- [SDR CHQA200900241](https://openairdocs.org/sdr/CHQA200900241), Nov 8, 2009: RELAY. FAULTY. 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 INDICATION
- [SDR CHQA200900240](https://openairdocs.org/sdr/CHQA200900240), Nov 8, 2009: SMOKE WARNING. FALSE ACTIVATION. 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 CLEA
- [SDR CHQA200900143](https://openairdocs.org/sdr/CHQA200900143), Jun 14, 2009: TIRE. BLOWN. 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 T
- [SDR CHQA200900137](https://openairdocs.org/sdr/CHQA200900137), Jun 8, 2009: WIRE HARNESS. DAMAGED. 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 
- [SDR CHQA200900132](https://openairdocs.org/sdr/CHQA200900132), May 22, 2009: LANDING GEAR. MALFUNCTIONED. 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 LA
- [SDR CHQA200900128](https://openairdocs.org/sdr/CHQA200900128), May 21, 2009: ELECTRONIC UNIT. MALFUNCTIONED. 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 
- [SDR CHQA200900124](https://openairdocs.org/sdr/CHQA200900124), May 8, 2009: RELAY. FAULTY. 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 WOU
- [SDR CHQA200900102](https://openairdocs.org/sdr/CHQA200900102), Apr 6, 2009: PROXIMITY SWITCH. FAULTY. 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. 
- [SDR CHQA200500145](https://openairdocs.org/sdr/CHQA200500145), Aug 19, 2005: SMOKE. DETECTED. 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
- [SDR CHQA200500031](https://openairdocs.org/sdr/CHQA200500031), Feb 13, 2005: ENGINE. CONTAMINATED. 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. T
- [SDR CHQA200500057](https://openairdocs.org/sdr/CHQA200500057), Jan 1, 2005: BULB. BURNED OUT. LEFT AFT OVERWING EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED LIGHT BULB IAW EMB 145 AMM 3-50-10. OPS CHECK GOOD.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20091115051149I](https://openairdocs.org/incident/20091115051149I), Nov 15, 2009: Embraer EMB-145LR (N258JQ), Dulles, VA, No damage. Chatauqua airlines flight 3055, an EMB145LR, N258JQ, diverted and landed on runway 1L after reporting a cargo fire indication while enroute from…

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