# N13970: 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: 145146
- Year built: 1999
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 26, 1999
- Certificate issued: April 4, 2018
- Last registry action: April 4, 2018
- Mode S code: A0A006
- 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/N13970
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=13970
- Page: https://openairdocs.org/deregistered/N13970-2021-07-31

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 (94, newest 50)

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

- [SDR ASOA20140625153](https://openairdocs.org/sdr/ASOA20140625153), Jun 25, 2014: SKIN. CORRODED. DURING C-CHECK, CORROSION WAS FOUND ON SKIN AROUND SCREW HOLES AND CORRODED NUTPLATES AT THE ADF ANTENNA LOCATION. MAINTENANCE REMOVED CORROSION ON SKIN AT THE 
- [SDR ASOA20140625152](https://openairdocs.org/sdr/ASOA20140625152), Jun 25, 2014: STRIP. CRACKED. DURING C-CHECK, RT WING/FUSELAGE FILLET HAS CRACKS AT RIVET FRAME 48, 10MM AFT AND 6MM FWD, REQUIRES FINAL REPAIR IAW EC5320-01707. MAINTENANCE REPAIRED RT WING
- [SDR ASOA20140625151](https://openairdocs.org/sdr/ASOA20140625151), Jun 25, 2014: BULKHEAD. CRACKED. DURING C-CHECK, RT AFT WHEEL WELL WEB CRACKED OTBD SIDE. MAINTENANCE STOP DRILLED UPPER CRACK, CUT-OUT LOWER DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER AND 
- [SDR ASOA20140625150V](https://openairdocs.org/sdr/ASOA20140625150V), Jun 25, 2014: SHEAR TIE. CRACKED. DURING C-CHECK, SHEAR TIE AT FRAME 24 STRINGER 15R IS CRACKED. R & R SHEAR TIE IAW SRM 51-20-01. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140625149V](https://openairdocs.org/sdr/ASOA20140625149V), Jun 25, 2014: SHEAR TIE. CRACKED. DURING C-CHECK, SHEAR TIE AT FRAME 24 STRINGER 16R IS CRACKED. MAINTENANCE R & R SHEAR TIE IAW SRM 51-20-01 AND SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN T
- [SDR ASOA20140625148V](https://openairdocs.org/sdr/ASOA20140625148V), Jun 25, 2014: SHEAR TIE. CRACKED. DURING C-CHECK, SHEAR TIE FRAME 27, STRINGER 15R IS CRACKED. MAINTENANCE R & R SHEAR TIE IAW SRM 51-20-01 AND SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO 
- [SDR ASOA20140625147V](https://openairdocs.org/sdr/ASOA20140625147V), Jun 25, 2014: SHEAR TIE. CRACKED. DURING C-CHECK SHEAR TIE FRAME 26, STRINGER 15R IS CRACKED. MAINTENANCE R & R SHEAR TIE IAW SRM 51-20-01 AND SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO S
- [SDR ASOA20140625146](https://openairdocs.org/sdr/ASOA20140625146), Jun 25, 2014: SHEAR TIE. CRACKED. SHEAR TIE AT FRAME 80 IS CRACKED BETWEEN STRINGER 3-5R JUST FWD OF APU FIREWALL. MAINTENANCE R & R SHEAR TIE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN 
- [SDR ASOA20140625145](https://openairdocs.org/sdr/ASOA20140625145), Jun 25, 2014: PLATE. CORRODED. DURING C-CHECK, MULTIPLE AREAS OF CORROSION FOUND AROUND LOWER CARGO DOOR STRIKER PLATE AT FRAME 65. MAINTENANCE BLENDED CORROSION, MATERIAL LOSS IS .032" OUT O
- [SDR ASOA20140613127](https://openairdocs.org/sdr/ASOA20140613127), Jun 12, 2014: FRAME. CORRODED. DURING C-CHECK THE CHANNEL ON FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 16-17L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW S
- [SDR ASOA20140608124](https://openairdocs.org/sdr/ASOA20140608124), Jun 8, 2014: DOOR FRAME. CORRODED. DURING C-CHECK, CORROSION FOUND AROUND AFT TWO NUTPLATES ON INSIDE OF MAIN DOOR BOTTOM FRAME. REMOVED CORRODED LOWER AFT DOOR FRAME. LOCATED, DRILLED AND INSTAL
- [SDR ASOA20140608123](https://openairdocs.org/sdr/ASOA20140608123), Jun 8, 2014: SHEAR TIE. CORRODED. DURING C-CHECK, CORROSION FOUND ON SHEAR TIE AT FRAME 65. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-31-04. REMOVED AND REPLACED SHEAR TIE IAW SRM 53-
- [SDR ASOA20140608122](https://openairdocs.org/sdr/ASOA20140608122), Jun 8, 2014: FLOOR SUPPORT. CRACKED. DURING C-CHECK LT OMEGA BEAM LOWER FLANGE IS CRACKED AT FRAMES 47-48. R & R FLOOR SUPPORT IAW SRM 51-20-03, AND 53-23-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140608121](https://openairdocs.org/sdr/ASOA20140608121), Jun 8, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK, FLOOR SUPPORT FWD OF SERVICE DOOR FRAME CORRODED AROUND NUTPLATES. R & R FLOOR SUPPORT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140608120](https://openairdocs.org/sdr/ASOA20140608120), Jun 8, 2014: FLOOR SUPPORT. CORRODED. DURING C-CHECK, CORROSION FOUND ON FLOOR SUPPOT AT Y=0.0 FRAME 61. R & R FLOOR SUPPORT IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140608119](https://openairdocs.org/sdr/ASOA20140608119), Jun 8, 2014: CROSSBEAM. CORRODED. DURING C-CHECK, CROSSBEAM AT FRAME 61 CORRODED BETWEEN RT OMEGA BEAM AND RT OTBD FLOOR SUPPORT 100 PERCENT MATERIAL LOSS. R & R CROSSBEAM IAW SRM 51-40-02. ACFT
- [SDR ASOA20140608118](https://openairdocs.org/sdr/ASOA20140608118), Jun 8, 2014: GUSSET. CORRODED. DURING C-CHECK, CORROSION FOUND AROUND POTABLE WATER LINES UNDER JAMB NUTS ON RT OMEGA BEAM GUSSETT FRAME 61. R & R GUSSET IAW SRM 51-40-02. ACFT APPROVED FOR R
- [SDR ASOA20140604102V](https://openairdocs.org/sdr/ASOA20140604102V), Jun 4, 2014: FLOOR SUPPORT. CRACKED. DURING C-CHECK, RT OMEGA BEAM INBD LOWER FLANGE WAS FOUND TO BE CRACKED BETWEEN FRAMES 47-48. MAINTENANCE R & R THE BEAM FLANG IAW SRM 51-40-02. THE ACFT WAS AP
- [SDR ASOA20140604101](https://openairdocs.org/sdr/ASOA20140604101), Jun 4, 2014: FLOOR SUPPORT. CRACKED. DURING C-CHECK, RT OMEGA BEAM OUTBOARD LOWER FLANGE WAS FOUND TO BE CRACKED BETWEEN FRAMES 47-48. MAINTENANCE REMOVED AND REPLACED THE BEAM FLANGE IAW EMB 145 S
- [SDR ASOA20140604100](https://openairdocs.org/sdr/ASOA20140604100), Jun 4, 2014: STIFFENER. CORRODED. DURING C-CHECK, FRAME 65 STIFFENER BETWEEN STRINGERS 15-16L WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE STIFFENER IAW SRM 51-40-02. THE ACFT WAS APPROVED FO
- [SDR ASOA20140604099](https://openairdocs.org/sdr/ASOA20140604099), Jun 4, 2014: DOOR SILL. CORRODED. DURING C-CHECK, THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140122012](https://openairdocs.org/sdr/ASOA20140122012), Jan 22, 2014: SKIN. CRACKED. FOUND CRACK IN SKIN BETWEEN THE PILOTS WINDSHIELD AND THE DV WINDOW CUTOUTS IN THE SUPPORT FRAME. MAINTENANCE PERFORMED A TEMPORARY REPAIR IAW EC 5310-01758. AL
- [SDR ASOA20131003393](https://openairdocs.org/sdr/ASOA20131003393), Oct 3, 2013: A/C PACK. ODOR. CREW NOTICED SMOKE IN THE COCKPIT AND RETURN TO DEPARTURE. MX TROUBLESHOTING FOR SMOKE IN COCKPIT IAW FIM 21-20-00-816-801-A. SMOKE AND HAZE APPEARS WHEN THE NR
- [SDR ASOA20120722048](https://openairdocs.org/sdr/ASOA20120722048), Jul 22, 2012: STRINGER. CORRODED. DURING C-CHECK. STRINGER 21R CORRODED BETWEEN FR 10-11. R & R STRINGER IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11IA234](https://openairdocs.org/sdr/C2XA11IA234), Oct 9, 2011: DISPLAY. SHORTED. IAH - FLIGHT 4229 WAS DELAYED DUE TO CREW REPORT OF CAPTAINS MFD BLANKING OUT FOLLOWED BY STRONG ELECTRICAL SMELL. MAINTENANCE REMOVED AND REPLACED THE AFFECTED
- [SDR C2XA11IA198](https://openairdocs.org/sdr/C2XA11IA198), Sep 5, 2011: FLAPPER VALVE. LEAKING. IAH - FLIGHT 2816, THE CREW REPORTED FUEL LEAKING FROM THE LEFT WING ON TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMO
- [SDR C2XA11SH112](https://openairdocs.org/sdr/C2XA11SH112), Aug 2, 2011: AHRS. MALFUNCTIONED. FLIGHT 2391 A/C N13970 AIR RETURN FROM EWR-"ON THE CLIMBOUT LOST TWICE ATT AND HDG ON CPT SIDE. MAINTENANCE REMOVED AND REPLACED NR 1 AHRS COMPUTER 800 SERIES A
- [SDR C2XA11IA172](https://openairdocs.org/sdr/C2XA11IA172), Jul 31, 2011: COMPUTER. INOPERATIVE. FLT 2391, CREW REPORTED TAHT THE CAPTAIN LOST ATT AND HDG TWICE DURING CLIMB. THE AIRCRAFT RETURNED TO EWR WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLAC
- [SDR C2XA11RI120](https://openairdocs.org/sdr/C2XA11RI120), Jul 3, 2011: PROXIMITY SWITCH. DEFECTIVE. FLIGHT 2666 - EWR - FLIGHT CREW REPORTED SPOILER FAIL INDICATION AND SPOILER OPEN INDICATION ON EICAS DURING CLIMBING. CREW PERFORMED AIR RETURN AND LANDED UNEV
- [SDR C2XA11TY077](https://openairdocs.org/sdr/C2XA11TY077), Jun 6, 2011: CONTACTOR. DEFECTIVE. TYS - A/C WAS EN ROUTE FROM CLE TO GSP WHEN CREW GOT A CAUTION LIGHT OF THE BACKUP BATTERY OFF BUS. A/C DIVERTED INTO TYS WHERE MAINTENANCE REMOVED AND REPLACED
- [SDR C2XA11IA071](https://openairdocs.org/sdr/C2XA11IA071), Apr 11, 2011: SIGNAL COND UNIT. INOPERATIVE. FLIGHT 2769, THE CREW REPORTED A FUEL 1 - 2 LOW LEVEL INDICATION ON EICAS. THE AIRCRAFT RETURNED WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIR
- [SDR C2XA11IA021](https://openairdocs.org/sdr/C2XA11IA021), Jan 20, 2011: PROXIMITY SWITCH. INOPERATIVE. IAH - FLIGHT 2689, DURING CRUISE THE CREW REPORTED "SPOILER OPEN" AND "SPOILER FAIL" MESSAGES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MA
- [SDR C2XA10TY114](https://openairdocs.org/sdr/C2XA10TY114), Aug 12, 2010: SKIN. CRACKED. LEFT AND RIGHT AFT FUSELAGE SKIN HAS CRACKS AT FASTENERS LOCATED AT FRAMES 77 THRU 79. REAMED HOLES TO REMOVE CRACKS INSTALLED BUSHING AND RIVETS IAW EC5330-022
- [SDR C2XA10TY112](https://openairdocs.org/sdr/C2XA10TY112), Aug 3, 2010: FRAME. CORRODED. BOTTOM AFT CORNER OF SERVICE DOOR FRAME HAS CORROSION. REPAIRED FRAME 22 IAW EC5310-01373.
- [SDR C2XA10TY108](https://openairdocs.org/sdr/C2XA10TY108), Aug 2, 2010: SILL. CORRODED. CARGO DOOR SILL CORRODED. REMOVED AND REPLACED DOOR SILL IAW EMB 135/145 SRM 51-40-02.
- [SDR C2XA10TY053](https://openairdocs.org/sdr/C2XA10TY053), Apr 8, 2010: INVERTER. INOPERATIVE. EMERGENCY EXITS LIGHTS AT WING INOP. REMOVED AND REPLACED INVERTER NR 5 IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD.
- [SDR C2XA10CL036](https://openairdocs.org/sdr/C2XA10CL036), Feb 26, 2010: BATTERY. DISCHARGED. DURING ROUTINE MAINTENANCE THE CABIN AISLE PATH LIGHT STRIP AND EMERGENCY EXIT DOOR SIGNS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHT 
- [SDR C2XA10IA072](https://openairdocs.org/sdr/C2XA10IA072), Feb 15, 2010: INVERTER. INOPERATIVE. IAH - DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT SIGN OVER THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO I
- [SDR C2XA10IA067](https://openairdocs.org/sdr/C2XA10IA067), Feb 15, 2010: INVERTER. INOPERATIVE. LCH - DURING MAINTENANCE INSPECTION, THE NUMBER FIVE AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE INVERT
- [SDR C2XA10IA066](https://openairdocs.org/sdr/C2XA10IA066), Feb 15, 2010: INVERTER. INOPERATIVE. LCH - DURING MAINTENANCE INSPECTION THE NUMBER TWO AND THREE AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER T
- [SDR C2XA10RI023](https://openairdocs.org/sdr/C2XA10RI023), Jan 22, 2010: LIGHT. INOPERATIVE. FLIGHT 2218 - RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND EMERGENCY LIGHT BULBS ABOVE SEATS AT ROW 12 INOPERATIVE. MX REMOVED AND REPLACED LIGHT BULBS AND PE
- [SDR C2XA10RI022](https://openairdocs.org/sdr/C2XA10RI022), Jan 22, 2010: BULB. BURNED OUT. FLIGHT 2218 - RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND EMERGENCY LIGHT BULBS ABOVE SEATS AT ROW 12 INOPERATIVE. MX REMOVED AND REPLACED LIGHT BULBS AND PE
- [SDR C2XA09CL023](https://openairdocs.org/sdr/C2XA09CL023), Mar 5, 2009: PROXIMITY SWITCH. FAULTY. CLE FLIGHT 2351 - THE CREW REPORTED A SPOILER FAIL MESSAGE IN FLIGHT. SPOILER OPEN MESSAGE ON THE EICAS. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDEN
- [SDR C2XA09CL002](https://openairdocs.org/sdr/C2XA09CL002), Jan 4, 2009: BATTERY. DISCHARGED. DURING ROUTINE MX THE EMERGENCY FLOOR LIGHT CTR STRIP WAS FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR3 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.
- [SDR C2XA08CL121](https://openairdocs.org/sdr/C2XA08CL121), Nov 17, 2008: HYDRAULIC SYSTEM. CONTAMINATED. MKE - FLIGHT 2948 - THE CREW REPORTED THE NR 1 HYDRAULIC SYSTEM FLUID SHOWED 1/4 LEVEL AFTER 43 MINUTES IN FLIGHT. THE SYSTEM WAS SERVICED PRIOR TO DEPARTURE FR
- [SDR C2XA08RI167](https://openairdocs.org/sdr/C2XA08RI167), Nov 14, 2008: LANDING GEAR. MALFUNCTIONED. FLIGHT 2361 - EWR - FLIGHT CREW REPORTED NLG WOULD NOT RETRACT NORMALLY, CREW HAD TO USE DOWNLOCK RELEASE TO RETRACT GEAR, THEN GEAR EXTENDED NORMALLY. EWR MX P
- [SDR C2XA08CL108](https://openairdocs.org/sdr/C2XA08CL108), Sep 24, 2008: BATTERY. INOPERATIVE. DURING ROUTINE MX THE RT WING FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY. OPS CHECKS WERE GOOD.
- [SDR C2XA08CL109](https://openairdocs.org/sdr/C2XA08CL109), Sep 24, 2008: LIGHT. INOPERATIVE. DURING ROUTINE MX THE LT WING AFT EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE LIGHT ASSEMBLY. OPS CHECKS WERE GOOD.
- [SDR C2XA08RI081](https://openairdocs.org/sdr/C2XA08RI081), Jun 2, 2008: UNKNOWN. ODOR. FLIGHT 2251 - IND - FLIGHT CREW REPORTED ELECTRICAL SMELL IN COCKPIT. SYSTEM RESET WAS PERFORMED AND NO DEFECTS WAS NOTED. ACFT WAS APPROVED TO RETURN TO SERVIC
- [SDR C2XA08TY050](https://openairdocs.org/sdr/C2XA08TY050), May 13, 2008: BRACKET. DAMAGED. TYS - DURING A CURRENT C-CHECK INSPECTION THE LT AILERON I/B PCA ACTUATOR ROD ATTACHMENT FITTING WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE PCA BRA

All 94: https://openairdocs.org/deregistered/N13970-2021-07-31/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 20041123031569I](https://openairdocs.org/incident/20041123031569I), Nov 23, 2004: Emb EMB145 (N13970), Cleveland, OH. (-23) Passenger refused to comply with crewmember instructors to stow bag prior to taxi, both from flight attendant and pilot. Passenger made sarcastic…

## Other aircraft with N13970

- [Cancelled 1971-01-28](https://openairdocs.org/deregistered/N13970-1971-01-28): Piper PA-23-250, S/N 27-4585. Exported to United Kingdom. Owner: [Aviation Services International Inc](https://openairdocs.org/faa-owner/AVIATION%20SERVICES%20INTERNATIONAL%20INC), [Lockhaven, PA](https://openairdocs.org/faa-place/PA/Lockhaven)

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