# N13969: 1999 Embraer EMB-145LR, registration cancelled 2021-07-31 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 31, 2021 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212) - Engine: [Allison AE-3007A](https://openairdocs.org/engine/allison-ae-3007a) (registry code 03030) - Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs) - Serial number: 145141 - Year built: 1999 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 25, 1999 - Certificate issued: April 4, 2018 - Last registry action: April 4, 2018 - Mode S code: A09FEC - Owner when cancelled: [Flight Lease Holdings LLC](https://openairdocs.org/faa-owner/FLIGHT%20LEASE%20HOLDINGS%20LLC) - Location: [West Palm Beach, FL](https://openairdocs.org/faa-place/FL/West%20Palm%20Beach) - Owner type: LLC - Owner's area on the map: 26.7158° N, 80.0668° W: Placed by OpenAirDocs at the center of ZIP code 33401, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N13969 - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=13969 - Page: https://openairdocs.org/deregistered/N13969-2021-07-31 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 (105, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ASOA20141030122](https://openairdocs.org/sdr/ASOA20141030122), Oct 30, 2014: LIGHT. DAMAGED. DURING MX INSPECTION, THE MAIN CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. R & R THE EMERGENCY LIGHT ASSY AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO - [SDR ASOA20140806253](https://openairdocs.org/sdr/ASOA20140806253), Aug 6, 2014: BEAM. CORRODED. DURING C-CHECK, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERV - [SDR ASOA20140806252](https://openairdocs.org/sdr/ASOA20140806252), Aug 6, 2014: STRINGER. CRACKED. DURING C-CHECK, STRINGER 6R WAS FOUND TO BE CRACKED AT FRAME 13. MAINTENANCE R & R THE STRINGER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20140805250](https://openairdocs.org/sdr/ASOA20140805250), Aug 5, 2014: HINGE FITTING. WORN. DURING C-CHECK THE LT ELEVATOR INBD HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE HINGE FITTING IAW SRM 51-40- - [SDR ASOA20140805249V](https://openairdocs.org/sdr/ASOA20140805249V), Aug 5, 2014: FITTING. CRACKED. DURING C-CHECK, THE RT OTBD FLAP INBD ROOT FITTING WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MAINTENANCE R & R THE FITTING IAW EC5750-01628. THE A - [SDR ASOA20140805248V](https://openairdocs.org/sdr/ASOA20140805248V), Aug 5, 2014: YOKE. WORN. DURING C-CHECK THE RT ENGINE FWD UPPER YOKE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE PERFORMED A REAMING REPAIR AND INSTA - [SDR ASOA20140725234](https://openairdocs.org/sdr/ASOA20140725234), Jul 25, 2014: YOKE. CRACKED. DURING C-CHECK, THE RT ENGINE FORWARD LOWER MOUNT YOKE WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE YOKE IAW EC5450-01094. THE ACFT WAS APPROVED FOR RETURN TO - [SDR ASOA20140724233](https://openairdocs.org/sdr/ASOA20140724233), Jul 24, 2014: SKIN. CRACKED. DURING C-CHECK, THE FORWARD FUSELAGE SKIN WAS FOUND TO BE CRACKED AT THE TOP OF THE WINDSHIELD AND LT DV WINDOW LATERAL POST. MAINTENANCE PERFORMED A DOUBLER RE - [SDR ASOA20140314043](https://openairdocs.org/sdr/ASOA20140314043), Mar 14, 2014: FLAPPER BEARING. LEAKING. DURING TAKEOFF ROLL, A FUEL LEAK WAS REPORTED COMING FROM THE LT WING WHERE THE OTBD FLAP MEETS THE AILERON. THE ACFT RETURNED, WHERE IT LANDED WITHOUT INCIDENT - [SDR ASOA20131221141](https://openairdocs.org/sdr/ASOA20131221141), Dec 21, 2013: CHARGER. INOPERATIVE. DURING MAINTENANCE INSPECTION, THE RT OVERWING EMERGENCY LIGHT WAS DISCOVERED INOPERATIVE. MX R & R NR 4 EMERGENCY LIGHT BATTERY CHARGER OPS CHECKED SUCCESSFUL. - [SDR ASOA20131003075](https://openairdocs.org/sdr/ASOA20131003075), Oct 3, 2013: SEAL. FAULTY. CREW REPORTED A SLOW CABIN PRESSURE LOSS AT FL 310. CABIN ALTITUDE WENT UP TO 14,600 FT IN EMERGENCY DESCENT. MX REPLACED THE CARGO DOOR TRIM SEAL. CABIN OXYGEN - [SDR ASOA20130510046](https://openairdocs.org/sdr/ASOA20130510046), May 10, 2013: WINDOW FRAME. CRACKED. DURING POST FLIGHT WALKAROUND, CREW REPORTED FINDING A FUSELAGE SKIN CRACK ON THE LT DV WINDOW UPPER FRAME AREA. MX PERFORMED REPAIR ON UPPER BEAM ATTACHED TO D - [SDR ASOA20130324020C](https://openairdocs.org/sdr/ASOA20130324020C), Mar 24, 2013: CONTROLLER. FAULTY. THE CREW REPORTED A BURNING ELECTRICAL ODOR ON DESCENT IN COCKPIT/CABIN ASSOCIATED WITH WINDSHIELD HEAT NOT WORKING. MX INSPECTED AND REPLACED THE NR 2 WINDSHIE - [SDR ASOA20121004089](https://openairdocs.org/sdr/ASOA20121004089), Oct 4, 2012: CONTROL UNIT. FAULTY. ON TAXI, BRAKES REQUIRED 50-60 PERCENT ACTUATION ON PEDALS TO ENGAGE FOLLOWED BY BRAKE DEGRADED MESSAGE WHICH CLEARED. ON GATE RETURN, BRAKES COMPLETELY FAILED - [SDR ASOA20120822075](https://openairdocs.org/sdr/ASOA20120822075), Aug 22, 2012: STRINGER. CORRODED. STRINGER 21L CORRODED FR. 10-14. R & R STRINGER IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20120822074](https://openairdocs.org/sdr/ASOA20120822074), Aug 22, 2012: STRINGER. CORRODED. STRINGER 21R CORRODED FR 10-14. R & R STRINGER IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20120822073](https://openairdocs.org/sdr/ASOA20120822073), Aug 22, 2012: SUPPORT. CORRODED. LOWER CARGO DOOR CUT OUT SUPPORT CORRODED. R & R CARGO DOOR LOWER CUT OUT SUPPORT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20120822072](https://openairdocs.org/sdr/ASOA20120822072), Aug 22, 2012: SUPPORT. CORRODED. LT EMERGENCY EXIT LOWER SUPPORT CORRODED. REPAIRED LT EMERGENCY EXIT IAW EC5220-01041. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20120822071](https://openairdocs.org/sdr/ASOA20120822071), Aug 22, 2012: SKIN. CORRODED. SERVICE DOOR CUT OUT HAS CORROSION AT FR 22. REPAIRED IAW EC5310-01373. ACFT WAS APPROVED FOR RETURN TO SERVICE. - [SDR ASOA20120117006](https://openairdocs.org/sdr/ASOA20120117006), Jan 17, 2012: BATTERY PACK. INOPERATIVE. CREW REPORTED ROW 1-7 EMERGENCY LIGHT STRIP INOPERATIVE. REMOVED, CHARGED, AND RE-INSTALLED NR 2 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-50-04 WITH OPS CHECK SU - [SDR C2XA11IA206](https://openairdocs.org/sdr/C2XA11IA206), Sep 10, 2011: LIGHT. MALFUNCTIONED. IAH - FLIGHT 2127, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE ROW 123 A & C SIDE PANEL EXIT LIGHTS TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAF - [SDR C2XA11RI140](https://openairdocs.org/sdr/C2XA11RI140), Aug 22, 2011: TRACK. OBSTRUCTED. FLIGHT 6029 - IAD - FLIGHT CREW REPORTED FO DV WINDOW NOT CLOSED IN FLIGHT. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. IAD MX FOUND DEBRIS ON THE DV WIN - [SDR C2XA11RI138](https://openairdocs.org/sdr/C2XA11RI138), Aug 15, 2011: ANTI-ICE VALVE. INOPERATIVE. FLIGHT 2169 - EWR - FLIGHT CREW REPORTED WING ANTI ICE FAIL DURING CLIMB. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED WING 1 - [SDR C2XA11TY047](https://openairdocs.org/sdr/C2XA11TY047), Apr 20, 2011: RELAY. INOPERATIVE. RUDDER HARD OVER PROTECTION MESSAGE ON EICAS. R & R RELAY K0774. OPS CHECK GOOD. CLOSED - [SDR C2XA10IA333](https://openairdocs.org/sdr/C2XA10IA333), Dec 10, 2010: LIGHT. INOPERATIVE. MCI - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHT STRIP AT ROW 8 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, - [SDR C2XA10RI154](https://openairdocs.org/sdr/C2XA10RI154), Dec 7, 2010: BRACKET. BROKEN. FLIGHT 3134 - EWR - FLIGHT CREW REPORTED AFT EMERGENCY LIGHT BRACKET BROKEN. EWR MX REMOVED AND REPLACED BRACKET AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. A - [SDR C2XA10SH243](https://openairdocs.org/sdr/C2XA10SH243), Jul 20, 2010: SKIN. CRACKED. SHV - DURING C-CHECK THE LT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 77-79 AND STRINGERS 2L-8L. MAINTENANCE REMOVED THE CRACKS AND PERFO - [SDR C2XA10SH242](https://openairdocs.org/sdr/C2XA10SH242), Jul 20, 2010: SKIN. CRACKED. SHV - DURING C-CHECK THE RT AFT SKIN WAS FOUND TO HAVE CRACKS AT FASTENERS BETWEEN FRAMES 77-79 AND STRINGERS 2R-7R. MAINTENANCE REMOVED THE CRACKS AND PERFORME - [SDR C2XA10SH241](https://openairdocs.org/sdr/C2XA10SH241), Jul 20, 2010: FITTING. WORN. SHV - DURING C-CHECK THE VERTICAL STABILIZER FITTING AT FRAME 75 AT 12:00 POSITION WAS FOUND TO HAVE ELONGATED BOLT HOLES AND CAUSING FRETTING WITH ADJACENT SKI - [SDR C2XA10SH240](https://openairdocs.org/sdr/C2XA10SH240), Jul 20, 2010: SKIN. CORRODED. SHV - DURING C-CHECK THE CARGO DOOR LOWER INNER SKIN WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5230-01208. THE AIRCRAFT WAS APPROVE - [SDR C2XA10SH239](https://openairdocs.org/sdr/C2XA10SH239), Jul 20, 2010: STRINGER. CORRODED. SHV - DURING C-CHECK STRINGER 21R WAS FOUND TO BE CORRODED BETWEEN FRAMES 12 AND 13. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5310-01522. THE AIRCRAFT WAS A - [SDR C2XA10SH238](https://openairdocs.org/sdr/C2XA10SH238), Jul 15, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 29. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT W - [SDR C2XA10SH237](https://openairdocs.org/sdr/C2XA10SH237), Jul 15, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT W - [SDR C2XA10SH236](https://openairdocs.org/sdr/C2XA10SH236), Jul 15, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT W - [SDR C2XA10SH235](https://openairdocs.org/sdr/C2XA10SH235), Jul 15, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 44. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT W - [SDR C2XA10SH234](https://openairdocs.org/sdr/C2XA10SH234), Jul 15, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 49.5. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE AIRCRAFT WAS APP - [SDR C2XA10SH233](https://openairdocs.org/sdr/C2XA10SH233), Jul 15, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 29. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS A - [SDR C2XA10SH232](https://openairdocs.org/sdr/C2XA10SH232), Jul 15, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS A - [SDR C2XA10SH231](https://openairdocs.org/sdr/C2XA10SH231), Jul 15, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS A - [SDR C2XA10SH230](https://openairdocs.org/sdr/C2XA10SH230), Jul 15, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 44. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE AIRCRAFT WAS APPROVED - [SDR C2XA10SH229](https://openairdocs.org/sdr/C2XA10SH229), Jul 15, 2010: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 49.5. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE AIRCRAFT WAS APPROVE - [SDR C2XA10RI084](https://openairdocs.org/sdr/C2XA10RI084), Jun 22, 2010: UNKNOWN. ODOR. FLIGHT 3063 - EWR - FLIGHT CREW REPORTED BURNING PLASTIC SMELL DURING FLIGHT. EWR MX PERFORMED FIM TASK FOR ABNORMAL SMELL IN COCKPIT AND COULD NOT DUPLICATE AN - [SDR C2XA10IA114](https://openairdocs.org/sdr/C2XA10IA114), Apr 7, 2010: UNKNOWN. MALFUNCTIONED. ATL - FLIGHT 2432, THE CREW REPORTED A BAGG SMOKE MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIR - [SDR C2XA10CL012](https://openairdocs.org/sdr/C2XA10CL012), Jan 26, 2010: CONNECTOR. CORRODED. DAY FLT 2234 THE CREW REPORTED A NR 2 T/R DISAGREE ON TAKEOFF ROLL. THE AIRCRAFT ABORTED AND TAXIED BACK TO THE GATE. MAINTENANCE PLACED THE T/R SYSTEM ON MEL A - [SDR C2XA09RI088](https://openairdocs.org/sdr/C2XA09RI088), May 2, 2009: POTENTIOMETER. DEFECTIVE. FLIGHT 2447 - STL - FLIGHT CREW REPORTED THAT UPON LANDING, ACFT EXPERIENCED AN ABRUPT UNCOMMANDED TURN TO THE RIGHT SIDE. IMMEDIATELY CREW PRESSED STEERING DIS - [SDR C2XA09RI087](https://openairdocs.org/sdr/C2XA09RI087), May 2, 2009: MANIFOLD. DEFECTIVE. FLIGHT 2447 - STL - FLIGHT CREW REPORTED THAT UPON LANDING, ACFT EXPERIENCED AN ABRUPT UNCOMMANDED TURN TO THE RIGHT SIDE. IMMEDIATELY CREW PRESSED STEERING DIS - [SDR C2XA09RI049](https://openairdocs.org/sdr/C2XA09RI049), Apr 3, 2009: UNKNOWN. ODOR. FLIGHT 4932 - EWR - FLIGHT CREW REPORTED STRONG ODOR OF SMOKE IN THE COCKPIT SHORTLY AFTER INITIAL DESCENT. EWR MX RAN PACKS, PRESSURIZED AIRCRAFT, TURNED W/S H - [SDR C2XA09RI050](https://openairdocs.org/sdr/C2XA09RI050), Apr 2, 2009: UNKNOWN. ODOR. FLIGHT - 2554 - EWR-JAX - FLIGHT CREW DIVERTED TO SAV DUE TO LIGHTNING STRIKE ACCOMPANIED WITH STRONG BURNING SMELL IN COCKPIT. MX INSPECTED AIRCRAFT AND FOUND - [SDR C2XA08TY104](https://openairdocs.org/sdr/C2XA08TY104), Sep 10, 2008: LIGHT. INOPERATIVE. ACFT WAS IN FOR A SERVICE/ ROUTINE CHECK AND THE EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED LIGHT IAW AMM 33-50-09. OPS CHECK GO - [SDR C2XA08RI138](https://openairdocs.org/sdr/C2XA08RI138), Sep 8, 2008: LIGHT. INOPERATIVE. RIC MX DURING ROUTINE INSPECTION RIC MX FOUND EMERGENCY LIGHT FLOOR STRIP INOPERATIVE. RIC MX R&R EMERGENCY LIGHT STRIP AND PERFORMED OPS CHECK SUCCESSFULLY. AC All 105: https://openairdocs.org/deregistered/N13969-2021-07-31/reports.md ## 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 20010731019949I](https://openairdocs.org/incident/20010731019949I), Jul 31, 2001: Emb EMB145 (N13969), Houston, TX, Substantial damage. (-23) 07/31/01: This office received a call from an officer from the Houston police department (hpd) regarding a ground incident (hpd #103010301-K) involving a… --- 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.