# N13990: 2000 Embraer EMB-145LR, registration cancelled 2011-07-15

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 15, 2011
- Exported to: South Africa
- Status when cancelled: Valid registration
- 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: 145277
- Year built: 2000
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 28, 2000
- Certificate issued: July 11, 2011
- Last registry action: July 11, 2011
- Mode S code: A0A04C
- Owner when cancelled: [General Aviation Services LLC](https://openairdocs.org/faa-owner/GENERAL%20AVIATION%20SERVICES%20LLC)
- Location: [Dover, DE](https://openairdocs.org/faa-place/DE/Dover)
- Owner type: Corporation
- Owner's area on the map: 39.1815° N, 75.4736° W: Placed by OpenAirDocs at the center of ZIP code 19901, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N13990
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=13990
- Page: https://openairdocs.org/deregistered/N13990-2011-07-15

From the FAA registry file of October 29, 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 (56, newest 50)

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

- [SDR C2XA11SH034](https://openairdocs.org/sdr/C2XA11SH034), Feb 1, 2011: BEAM. CORRODED. SHV - DURING C-CHECK CARGO DOOR LOWER CUTOUT CORRODED BETWEEN FR 65 & 68. REMOVED AND REPLACED CARGO DOOR LOWER BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPR
- [SDR C2XA11SH033](https://openairdocs.org/sdr/C2XA11SH033), Jan 31, 2011: SKIN. CRACKED. SHV - DURING C-CHECK LT SKIN HAS CRACKS AROUND RIVETS BETWEEN FR 77 & 80. REPAIRED SKIN IAW EC5330-02352. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH032](https://openairdocs.org/sdr/C2XA11SH032), Jan 31, 2011: SKIN. CRACKED. SHV - DURING C-CHECK - RT SKIN HAS CRACKS AROUND RIVETS BETWEEN FR 75 & 80. REPAIRED SKIN IAW EC5330-02352. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10TY122](https://openairdocs.org/sdr/C2XA10TY122), Sep 9, 2010: SENSOR. CONTAMINATED. TYS - A/C WAS DIVERTED TO TYS FROM BNA DUE TO E1 OVERTEMP. TYS MAINTENANCE FOUND A LOOSE B-NUT THAT WAS LEAKING HOT AIR ONTO A TEMP SENSOR. TIGHTEN B-NUT AND OP
- [SDR C2XA10IA024](https://openairdocs.org/sdr/C2XA10IA024), Jan 17, 2010: CONTROL PANEL. INOPERATIVE. IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT ARM. MAINTENANCE REMOVED AND REPLACED THE CABIN / EMERGENCY LIGHT CONTRO
- [SDR C2XA10IA023](https://openairdocs.org/sdr/C2XA10IA023), Jan 17, 2010: BATTERY PACK. DISCHARGED. FLIGHT 2314, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT ARM. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AND NUMBER T
- [SDR C2XA10IA022](https://openairdocs.org/sdr/C2XA10IA022), Jan 17, 2010: BATTERY PACK. DISCHARGED. IAH - FLIGHT 2314, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT ARM. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AND NU
- [SDR C2XA09SH350](https://openairdocs.org/sdr/C2XA09SH350), Oct 20, 2009: DUCT. DIRTY. PACK NR 1 PRODUCES BURNING SMELL WHEN ON. MAINTENANCE PERFORMED EMB-145 FIM TASK 21-20-00-810-801-A. MAINTENANCE ALSO CLEANED NR 1 PACK RAM AIR DUCT. MAINTENANC
- [SDR C2XA09TY241](https://openairdocs.org/sdr/C2XA09TY241), Sep 18, 2009: BULB. BLOWN. TYS - A/C AT GATE IN TYS WHEN CREW COMPLIED WITH FIRE TEST OF THE BAGGAGE COMPARTMENT AND TEST FAIL. MAINTENANCE REMOVED AND REPLACED THE BULBS AND OPS CHECK GO
- [SDR C2XA09CL073](https://openairdocs.org/sdr/C2XA09CL073), May 22, 2009: O-RING. DETERIORATED. EWR - FLIGHT 2038 - THE CREW REPORTED A BLEED 1 LEAK IN ROUTE TO MSN. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPL
- [SDR C2XA09IA120](https://openairdocs.org/sdr/C2XA09IA120), May 8, 2009: CLAMP. LEAKING. IAH - FLIGHT 2944, THE CREW REPORTED AN ENGINE ONE BLEED LEAK INDICATION DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANC
- [SDR C2XA09IA119](https://openairdocs.org/sdr/C2XA09IA119), May 8, 2009: O-RING. BLOWN. IAH - FLIGHT 2944, THE CREW REPORTED AN ENGINE ONE BLEED LEAK INDICATION DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANC
- [SDR C2XA09IA072](https://openairdocs.org/sdr/C2XA09IA072), Mar 10, 2009: STRUCTURE. LEAKING. DURING CRUISE A REPORT OF FUEL LEAKING FROM THE LEFT WING WAS MADE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FULLY FU
- [SDR C2XA09SH047](https://openairdocs.org/sdr/C2XA09SH047), Feb 1, 2009: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK, LEFT OMEGA BEAM HAS CORROSION AT SECTION AROUND THE CARBON FIBER CROSS-MEMBER AT FRM 19. MAINTENANCE REPAIRED LT OMEGA BEAM AT SECTION ARO
- [SDR C2XA09SH046](https://openairdocs.org/sdr/C2XA09SH046), Feb 1, 2009: SUPPORT. CORRODED. SHV - DURING C-CHECK, CORROSION ON WASTE VALVE SUPPORT BEHIND SERVICE PANEL. MAINTENANCE INSTALLED NEW WASTE DRAIN DUMP VALVE SUPPORT ASSY IAW EMB 145 SRM 51-40
- [SDR C2XA08IA197](https://openairdocs.org/sdr/C2XA08IA197), Aug 26, 2008: CONNECTOR. LOOSE. IAH DURING A CHECK INSPECTION THE EMERGENCY LIGHT ON THE GALLEY SERVICE DOOR SWING ARM WAS FOUND TO BE INOPERATIVE. MX RECONNECTED A LOOSE PLUG CONNECTED TO THE
- [SDR C2X2008F00020](https://openairdocs.org/sdr/C2X2008F00020), Aug 14, 2008: PUMP. LEAKING. ACFT EN ROUTE FROM EWR TO TYS WHEN THE HYD 1 SYSTEM MESSAGE WAS HYD LOW QUANTITY. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENG DRIVEN HYD PUMP IAW EMB 145AMM 2
- [SDR C2XA08CL075](https://openairdocs.org/sdr/C2XA08CL075), Jun 29, 2008: CONNECTOR. LOOSE. DURING ROUTINE MAINTENANCE THE COCKPIT STEP EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE RESECURED THE ELECTRICAL CONNECTOR ON THE COCKPIT STEP EMERGENCY 
- [SDR C2XA07IA205](https://openairdocs.org/sdr/C2XA07IA205), Sep 15, 2007: CONNECTOR. LOOSE. EWR - FLIGHT 2762 THE CREW REPORTED AN ELECTRICAL SMOKE SMELL IN THE VICINITY SEAT 1A. FOUND LUMINESCENT LIGHT BULB ARCHING AT CONTACT PINS, LIGHT BULB REMOVED;
- [SDR C2XA07RI082](https://openairdocs.org/sdr/C2XA07RI082), Sep 14, 2007: LIGHT. DEFECTIVE. FLT 2754 - YOW - CREW REPORTED ELECTRICAL ODOR FROM SEAT 1A AREA. MX FOUND FLUORESCENT LIGHT ARCING AT CONTACT. MX REMOVED AND REPLACED LIGHT ASSEMBLY AND PERFO
- [SDR C2XA07SH022](https://openairdocs.org/sdr/C2XA07SH022), Apr 15, 2007: FITTING. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND CORROSION ON SHEAR CLIPS AT FRAMES 65 & 68. MAINTENANCE REPAIRED SHEAR CLIPS AT FRAMES 65 & 68 IAW EC 5330-01458. AIRCRAF
- [SDR C2XA07SH021](https://openairdocs.org/sdr/C2XA07SH021), Apr 15, 2007: FIREWALL. CHAFED. SHV - DURING C-CHECK MAINTENANCE APU FIREWALL LOWER SECTION HAS RIVET INDENTATION. MAINTENANCE REPAIRED APU FIREWALL AT FRAME 81 LOWER SECTION IAW EC5310-01359.
- [SDR C2XA07SH019](https://openairdocs.org/sdr/C2XA07SH019), Apr 14, 2007: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK MAINTENANCE FOUND CENTER OMEGA BEAM WITH CORROSION AT FRAME 20 AND FRAME 23. MAINTENANCE REPAIRED CENTER OMEGA BEAM AT FRAME 20 TO 23 IAW E
- [SDR C2XA06IA144](https://openairdocs.org/sdr/C2XA06IA144), Sep 5, 2006: ELEVATOR. MALFUNCTIONED. DAL - FLIGHT 2923, THE CREW REPORTED THAT THE ELEVATOR WAS NON-RESPONSIVE UNDER LOAD IN FLIGHT. THE AIRCRAFT LANDED AT DAL WITHOUT INCIDENT. MAINTENANCE INSPECT
- [SDR C2XA06CL060](https://openairdocs.org/sdr/C2XA06CL060), Jun 20, 2006: SMOKE. DETECTED. CLE FLIGHT 2705 THE CREW REPORTED NR 1 PACK NOISE FROM THE ACM WITH SMELL AND SMOKE FROM THE SIDE VENTS. MAINTENANCE INSPECTED AND RELEASED THE AIRCRAFT IAW MEL
- [SDR C2XA06IA051](https://openairdocs.org/sdr/C2XA06IA051), Mar 28, 2006: RETAINER. DAMAGED. IAH - FLIGHT 2971, THE CREW REPORTED LOSS OF ENGINE TWO OIL QUANTITY AND PRESSURE. THE CREW SHUT DOWN THE NUMBER TWO ENGINE, AND RETURNED TO IAH WHERE IT LANDED
- [SDR C2XA04CL106](https://openairdocs.org/sdr/C2XA04CL106), Oct 11, 2004: WIRE. LOOSE. DURING MAINTENANCE THE NR 2 AND 3 AISLE PATH EMERGENCY LIGHTING WERE INOPERATIVE. RESECURED GROUND WIRE AND SYSTEM CHECKED GOOD.
- [SDR C2XA04BT078](https://openairdocs.org/sdr/C2XA04BT078), Jul 15, 2004: LIGHT. INOPERATIVE. CREW REPORTED, (STRIP OF EMERGENCY AISLE PATH LIGHTS NOT WORKING.) MAINTENANCE RELEASED THE AIRCRAFT IAW MEL NR 33-50-00/02 CATEGORY C-PLACARD NR 044167 AND RET
- [SDR C2XA03BT114](https://openairdocs.org/sdr/C2XA03BT114), Nov 28, 2003: PROXIMITY SENSOR. FAULTY. CREW REPORTED, AFTER GEAR RETRACTION, LANDING GEAR INDICATED UP. OBVIOUS WIND NOISE SUSPECTED GEAR DOORS DID NOT RETRACT. AIRCRAFT REPORTEDLY HAD EXCESSIVE DRAG
- [SDR C2XA03BT077](https://openairdocs.org/sdr/C2XA03BT077), Aug 5, 2003: PANEL. FAULTY. EWR CO2879, CREW REPORTED, LAV SMOKE WARNING DURING FLIGHT WITH ASSOCIATED SMOKE ALARM. PERFORMED QRH. NO VISIBLE SIGN OF SMOKE OR FIRE. FLIGHT CONTINUED UNEVEN
- [SDR C2XA03TY098](https://openairdocs.org/sdr/C2XA03TY098), Jul 27, 2003: FLOOR SUPPORT. CORRODED. DURING A SCHEDULED 2C INSPECTION THE LT LAV SIDEWALL FLOOR SUPPORT HAD CORRODED NUT PLATED AND RIVETS FWD AND AFT. MAINTENANCE REMOVED AND REPLACED THE LT LAV F
- [SDR C2XA03TY097](https://openairdocs.org/sdr/C2XA03TY097), Jul 27, 2003: FLOORBEAM. CORRODED. TYS- DURING A SCHEDULED 2C INSPECTION THE LT AND RT AISLE OMEGA BEAM AT THE SECOND CARBON CROSS BAR WAS FOUND CORRODED. MAINTENANCE CUT OUT DAMAGED SECTIONS ON 
- [SDR C2XA03TY095](https://openairdocs.org/sdr/C2XA03TY095), Jul 23, 2003: SILL. CORRODED. TYS, DURING A SCHEDULED INSPECTION THE SERVICE DOOR AFT. SILL WAS FOUND CORRODED. MAINTENANCE BLENDED THE DAMAGED AREA, ALODINED, PRIMED AND FILLED WITH HYSOL 9
- [SDR C2XA03TY094](https://openairdocs.org/sdr/C2XA03TY094), Jul 23, 2003: SILL. CORRODED. DURING A SCHEDULED INSPECTION THE SERVICE DOOR FORWARD SILL WAS FOUND CORRODED. MAINTENANCE BLENDED THE DAMAGED AREA, ALODINED, PRIMED AND FILLED WITH HYSOL 939
- [SDR C2XA03TY093](https://openairdocs.org/sdr/C2XA03TY093), Jul 23, 2003: SEAT TRACK. CORRODED. DURING A SCHEDULED INSPECTION THE LW1, CABIN SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-145-AMM-53-01-06.
- [SDR C2XA03TY092](https://openairdocs.org/sdr/C2XA03TY092), Jul 23, 2003: SEAT TRACK. CORRODED. DURING A SCHEDULED INSPECTION THE ROW 2, CABIN SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-145-AMM-53-01-06.
- [SDR C2XA03IA021](https://openairdocs.org/sdr/C2XA03IA021), Feb 14, 2003: BATTERY PACK. DISCHARGED. DURING MAINTENANCE THE MECHANIC NOTED THAT THE EMERGENCY FLOOR LIGHTING FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE BATTERY PACK, PE
- [SDR C2XA03IA020](https://openairdocs.org/sdr/C2XA03IA020), Feb 14, 2003: BATTERY PACK. DISCHARGED. DURING MAINTENANCE THE MECHANIC NOTED THAT THE EMERGENCY FLOOR LIGHTING FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT B
- [SDR C2XA02CL173](https://openairdocs.org/sdr/C2XA02CL173), Aug 16, 2002: PROXIMITY SENSOR. FAILED. CLE FLIGHT#3222 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF.A EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT
- [SDR C2XA02CL130](https://openairdocs.org/sdr/C2XA02CL130), Jun 8, 2002: INVERTER. FAULTY. DURING ROUTINE MAINTENANCE THE FLOOR PROXIMITY STRIP LIGHTS FROM ROW 12 TO LAST ROW WILL NOT ILLUMINATE.MAINTENANCE REPLACED THE #6 EMERGENCY LIGHT AC/DC INVERT
- [SDR C2XA02CL119](https://openairdocs.org/sdr/C2XA02CL119), May 31, 2002: ODOR. DETECTED. CLE FLIGHT 3248 THE CREW REPORTED THE APU CAUSES A SMELL IN THE CABIN. MAINTENANCE INSPECTED AND PERFORMED A OPERATIONAL CHECK OF THE APU AND NO DEFECTS WERE FO
- [SDR C2XA01CL237](https://openairdocs.org/sdr/C2XA01CL237), Dec 4, 2001: CONNECTOR. CORRODED. CLE FLIGHT#3308 THE CREW REPORTED A BURNING SMELL COMING FROM THE #2 HOT JUG.MAINTENANCE RELEASED AIRCRAFT I/A/W MEL 25-60-02/3.MAINTENANCE CLEARED THE MEL BY R
- [SDR C2XA01TY115](https://openairdocs.org/sdr/C2XA01TY115), Sep 13, 2001: STRINGER. CHAFED. TYS During a scheduled inspection, Stringer 19R was found chafed at frame 53, Maintenance blended chafed area, performed dye-penetrant inspection, alodined, pri
- [SDR C2XA01TY114](https://openairdocs.org/sdr/C2XA01TY114), Sep 13, 2001: STRINGER. CHAFED. TYS During a scheduled inspection, Stringer 19L was found chafed at frame 53. Maintenance blended chafed area, performed dye-penetrant inspection, alodined, pri
- [SDR C2XA01TY113](https://openairdocs.org/sdr/C2XA01TY113), Sep 13, 2001: BATTERY. DISCHARGED. TYS DURING A SCHEDULED INSPECTION, THE EMERGENCY AISLE LIGHTING SYSTEM BATTERY SUPPLY NUMBER 4 WAS FOUND DEAD. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY L
- [SDR C2XA01TY112](https://openairdocs.org/sdr/C2XA01TY112), Sep 13, 2001: BEAM. CORRODED. TYS During a scheduled inspection, The left omega beam was found corroded at frame 20. Maintenance removed damaged area, fabricated repair filler, shims & exter
- [SDR C2XA01TY111](https://openairdocs.org/sdr/C2XA01TY111), Sep 13, 2001: ATTACH FITTING. GOUGED. TYS DURING A SCHEDULED INSPECTION, THE LEFT AILERON CENTER INBOARD ATTACH FITTING WAS FOUND GOUGED. MAINTENANCE BLENDED OUT THE DAMAGED AREA, PERFORMED DYE-PENE
- [SDR C2XA01TY110](https://openairdocs.org/sdr/C2XA01TY110), Sep 13, 2001: TUBE. BENT. TYS During a scheduled inspection. The left engine fire extingisher line was found bent. Maintenance removed and replaced the fire extingisher line I.A.W.-EMB-1
- [SDR C2XA01TY109](https://openairdocs.org/sdr/C2XA01TY109), Sep 13, 2001: SKIN. CHAFED. TYS DURING A SCHEDULED INSPECTION, THE CARGO DOOR SKIN AROUND THE EXTERIOR HANDLE WAS FOUND CHAFED. MAINTENANCE REMOVED THE DAMAGED AREA, PERFORMED DYE-PENETREN
- [SDR C2XA01TY108](https://openairdocs.org/sdr/C2XA01TY108), Sep 6, 2001: STEP. CORRODED. TYS DURING A SCHEDULED INSPECTION THE FLOOR GUSSET LOCATED AFT OF THE COCKPIT ENTRANCE STEP WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION AROUND THE RIVETS. MAIN

All 56: https://openairdocs.org/deregistered/N13990-2011-07-15/reports.md

## Other aircraft with N13990

- [Cancelled 1973-05-10](https://openairdocs.org/deregistered/N13990-1973-05-10): Piper PA-23-250, S/N 27-4608. Owner: [Wiggins Airways](https://openairdocs.org/faa-owner/WIGGINS%20AIRWAYS), [Norwood, MA](https://openairdocs.org/faa-place/MA/Norwood)

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