# N18982: 2000 Embraer EMB-145LR, registration cancelled 2011-08-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 16, 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: 145223
- Year built: 2000
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 11, 2000
- Certificate issued: August 12, 2011
- Last registry action: August 12, 2011
- Mode S code: A165A6
- 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/N18982
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=18982
- Page: https://openairdocs.org/deregistered/N18982-2011-08-16

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 (65, newest 50)

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

- [SDR C2XA11TY082](https://openairdocs.org/sdr/C2XA11TY082), Jun 13, 2011: DOOR. LACK OF LUBE. TYS - A/C IN CLT WAS FOUND WITH THE MCD WAS STUCK CLOSED. MAINTENANCE IN CLT MAINTENANCE LUBE THE MCD, OPS CHECK GOOD. LOGPAGE (2808755) A/C RELEASED TO SERVICE
- [SDR C2XA10TY152](https://openairdocs.org/sdr/C2XA10TY152), Sep 25, 2010: BRACKET. WORN. LEFT AILERON PCA BRACKET HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED AILERON BRACKET IAW EC5750-01177.
- [SDR C2XA10TY147](https://openairdocs.org/sdr/C2XA10TY147), Sep 21, 2010: SKIN. CORRODED. TYS - CORRODED FASTENERS AND SKIN FR 59-60 STR 21L-20R. REMOVED DAMAGED AREA, FABRICATED DOUBLER, AND INSTALLED DOUBLER IAW EC 5330-02244.
- [SDR C2XA10TY146](https://openairdocs.org/sdr/C2XA10TY146), Sep 21, 2010: SKIN. CORRODED. TYS - CORROSION ON FUSELAGE LOWER SKIN INSIDE CARGO FROM FRAME 60-62 STRINGER 20R- 21R. REMOVED DAMAGE, FABRICATED DOUBLER, AND INSTALLED REPAIR IAW EC 5330-022
- [SDR C2XA10TY141](https://openairdocs.org/sdr/C2XA10TY141), Sep 16, 2010: BUSHING. WORN. TYS - A/C IN A C-CHECK STATUS, INSPECTION FOUND THE RT AILERON PCA BRACKET 3RD LUG WITH A MIGRATED HAT BUSHING. MAINTENANCE REMOVED AND REPLACED THE HAT BUSHING
- [SDR C2XA10TY140](https://openairdocs.org/sdr/C2XA10TY140), Sep 16, 2010: BUSHING. MIGRATED. TYS - A/C CURRENTLY IN A C-CHECK STATUS. INSPECTION FOUND BOTH HAT BUSHINGS FOR THE CENTER HINGE BRACKET, RT SPOILER MIGRATED. MAINTENANCE REMOVED AND REPLACED 
- [SDR C2XA10TY139](https://openairdocs.org/sdr/C2XA10TY139), Sep 16, 2010: BUSHING. WORN. TYS A/C CURRENTLY IN C-CHECK. INSPECTION FOUND THE INBD HINGE BRACKET FOR THE RH SPOILER WITH A MIGRATED HAT BUSHION. MAINTENANCE R & R THE HAT BUSHION IAW EC57
- [SDR C2XA10TY138](https://openairdocs.org/sdr/C2XA10TY138), Sep 16, 2010: BUSHING. WORN. TYS - A/C CURRENTLY IN C-CHECK. INSPECTION FOUND THE RT SPOILER ACTUATOR BRACKET WITH A MIGRATED HAT BUSHING. MAINTENANCE REMOVED AND REPLACED THE HAT BUSHING I
- [SDR C2XA10TY137](https://openairdocs.org/sdr/C2XA10TY137), Sep 16, 2010: BUSHING. WORN. ACFT CURRENTLY IN C-CHECK. INSPECTION FOUND THE RT SPOILER ACTUATOR HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED THE HAT BUSHING IAW EC5740-01152. ALL
- [SDR C2XA10TY136](https://openairdocs.org/sdr/C2XA10TY136), Sep 16, 2010: BUSHING. WORN. TYS - A/A CURRENTLY IN C-CHECK. INSPECTION FOUND THE LT SPEED BRAKE WITH A MIGRATED HAT BUSHING AT THE ACTUATOR ATTACHMENT LUG. MAINTENANCE REMOVED AND REPLACED
- [SDR C2XA10TY135](https://openairdocs.org/sdr/C2XA10TY135), Sep 16, 2010: BUSHING. WORN. ACFT CURRENTLY IN C-CHECK, INSPECTION FOUND THE LT GROUND SPOILER, O/B HINGE WITH A MIGRATED HAT BUSHING. MAINTENANCE REMOVED AND REPLACED THE HAT BUSHING IAW E
- [SDR C2XA10TY134](https://openairdocs.org/sdr/C2XA10TY134), Sep 16, 2010: BUSHING. MISSING. TYS - A/C CURRENTLY IN C-CHECK AND INSPECTION FOUND THE CENTER HINGE BRACKET FOR THE LT GROUND SPOILER MISSING A HAT BUSHING. MAINTENANCE REPLACED THE HAT BUSHI
- [SDR C2XA10TY130](https://openairdocs.org/sdr/C2XA10TY130), Sep 15, 2010: FITTING. WORN. LT AILERON O/B FITTING I/B LUG MIGRATED HAT BUSHING. REMOVED, MEASURED AND REPLACED HAT BUSHING IAW EC5740-01152.
- [SDR C2XA10TY129](https://openairdocs.org/sdr/C2XA10TY129), Sep 15, 2010: FITTING. WORN. RT AILERON 3RD FITTING O/B LUG AND O/B FITTING O/B LUG HAD MIGRATED HAT BUSHINGS. REMOVED, MEASURED AND REPLACED HAT BUSHINGS IAW EMB 145 EC5740-01152.
- [SDR C2XA10TY128](https://openairdocs.org/sdr/C2XA10TY128), Sep 14, 2010: PANEL. DAMAGED. PANEL 321CL INSIDE SURFACE HAS COMPOSITE DAMAGE NEAR L/E. REPAIRED PANEL IAW EMB 145 EC5530-01183.
- [SDR C2XA10TY124](https://openairdocs.org/sdr/C2XA10TY124), Sep 12, 2010: STRINGER. CHAFED. AIRCRAFT IN C CHECK STRINGER 19R HAS CHAFE DAMAGE BETWEEN FRAMES 52-53 OUTSIDE OF AIRCRAFT FWD OF HYD MANIFOLD. BLENDED OUT DAMAGED AREA REMOVED 20 PERCENT OF S
- [SDR C2XA09IA295](https://openairdocs.org/sdr/C2XA09IA295), Nov 29, 2009: O-RING. BLOWN. IAH - FLIGHT 3033, DURING CLIMB THE CREW REPORTED A NUMBER ONE BLEED LEAK. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AN
- [SDR C2XA09IA289](https://openairdocs.org/sdr/C2XA09IA289), Nov 13, 2009: O-RING. BLOWN. IAH, FLIGHT 2012, THE CREW REPORTED A BLEED ONE LEAK MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND RE
- [SDR C2XA09RI057](https://openairdocs.org/sdr/C2XA09RI057), Apr 13, 2009: COOLING FAN. MALFUNCTIONED. FLIGHT 3009 - EWR - FLIGHT CREW REPORTED BURNING SMELL AND SMOKE IN THE COCKPIT. EWR MX REMOVED AND REPLACED NR 2 RECIRCULATING FAN AND PERFORMED OPERATIONAL CH
- [SDR C2XA09RI013](https://openairdocs.org/sdr/C2XA09RI013), Jan 13, 2009: MODULE. DEFECTIVE. FLIGHT 2675 - EWR - FLIGHT CREW REPORTED PRESSURIZATION SYSTEM SPIKING UNCOMMANDED. EWR MX R&R CPAM AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT APPROVED FOR RETU
- [SDR C2XA08IA215](https://openairdocs.org/sdr/C2XA08IA215), Sep 24, 2008: PROXIMITY SWITCH. FAULTY. IAH - FLT 2400, THE CREW REPORTED THAT NOSE GEAR DOOR DID NOT CLOSE AFTER T/O, AND THAT IT FINALLY CLOSED AFTER CIRCLING THE FIELD FOR 10 MINUTES. THE AIRCRAFT 
- [SDR C2XA08IA210](https://openairdocs.org/sdr/C2XA08IA210), Sep 18, 2008: INDICATOR. INOPERATIVE. SAV FLIGHT 2517. THE CREW REPORTED A FUEL 1 TO LEVEL WARNING CLIMBING THROUGH 12000. THE ACFT RETURNED TO SAV WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE
- [SDR C2XA08TY105](https://openairdocs.org/sdr/C2XA08TY105), Sep 11, 2008: BULB. INOPERATIVE. ACFT WAS FOUND WITH THE LT SIDE EMERGENCY LIGHT INOPERATIVE. MAINT REMOVED AND REPLACED THE EMERGENCY LIGHT BULB. OPS CHECK GOOD AND WAS RELEASED TO SERVICE. WO
- [SDR C2XA08TY103](https://openairdocs.org/sdr/C2XA08TY103), Sep 9, 2008: LAMP. BURNED OUT. LT EXTERNAL, JUST FWD OF L/E, EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10. OPS CHECK GOOD. ACFT STILL IN C-CHECK. (K)
- [SDR C2X2008F00039](https://openairdocs.org/sdr/C2X2008F00039), Sep 7, 2008: STRUCTURE. ERODED. RT HORZ STAB L/E ERODED. POLISHED L/E AND REIDENTIFIED L/E IAW EC 5530-01116. AC STILL IN C-CHECK. (K)
- [SDR C2X2008F00028](https://openairdocs.org/sdr/C2X2008F00028), Sep 4, 2008: FIREWALL. DENTED. AC IS CURRENTLY IN C-CHECK AND THE APU FIREWALL WAS FOUND CHAFED AT THE LOWER BEND (STR 21L/ 21R) EXTERIOR SURFACE. MAINTENANCE REPAIRED THE DAMAGE AREA IAW EC5
- [SDR C2X2008F00027](https://openairdocs.org/sdr/C2X2008F00027), Sep 4, 2008: INLET. CORRODED. AC IS CURRENTLY IN C-CHECK AND CORROSION WAS FOUND ON THE NR 2 ENGINE INLET ATTACH FLANGE MOUNTING HOLES. MAINTENANCE REPAIRED THE NR 2 ENGINE INLET IAW EC54200
- [SDR C2X2008F00026](https://openairdocs.org/sdr/C2X2008F00026), Sep 4, 2008: INLET. CORRODED. AC IS CURRENTLY IN C-CHECK AND CORROSION WAS FOUND ON THE NR 1 ENGINE INLET ATTACH FLANGE MOUNTING HOLES. MAINTENANCE REPAIRED THE NR 1 ENGINE INLET IAW EC5420-
- [SDR C2X2008F00007](https://openairdocs.org/sdr/C2X2008F00007), Jul 20, 2008: O-RING. FAILED. IAH - FLIGHT 2944 - DURING PREFLIGHT THE CREW REPORTED A BURNING ODOR AND BLEED LEAK NR 2 INDICATION. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACE
- [SDR C2XA08IA133](https://openairdocs.org/sdr/C2XA08IA133), May 25, 2008: COFFEEMAKER. ODOR. JAN - FLIGHT 2461 DURING TAXI THE CREW REPORTED AN ELECTRIC SMELL IN GALLEY AREA. CONTRACT MAINTENANCE, "FOUND COFFEE MAKER NR 1 MAKING SMELL PLACED ON NEF-6L01
- [SDR C2XA08RI051](https://openairdocs.org/sdr/C2XA08RI051), Mar 30, 2008: INVERTER. INOPERATIVE. FLIGHT 3132 - EWR - THE FLIGHT CREW REPORTED AFT GALLEY WALL EMERGENCY LIGHT NOT ILLUMINATING. EWR MX REMOVED AND REPLACED AFT GALLEY WALL EMERGENCY LIGHT INVER
- [SDR C2XA08CL035](https://openairdocs.org/sdr/C2XA08CL035), Mar 23, 2008: SIGN. INOPERATIVE. DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT SIGN IN FRONT OF ROW 3 BC WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY EXIT SIGN. OPERATIONAL
- [SDR C2XA07IA198](https://openairdocs.org/sdr/C2XA07IA198), Sep 5, 2007: SWITCH. SHORTED. IAH - DURING MAINTENANCE INSPECTION THE CAPTAINS GLARESHIELD PUSH TO TALK SWITCH SHOCKED AND SMOKED WHEN DEPRESSED. MAINTENANCE REMOVED AND REPLACED THE AFFECTE
- [SDR C2XA07RI036](https://openairdocs.org/sdr/C2XA07RI036), May 24, 2007: SMOKE DETECTOR. MALFUNCTIONED. FLT 2754 - EWR - CREW REPORTED LAV SMOKE MSG ON EICAS, NO SMOKE NOTICED. EWR MX RESET LAV SMOKE DETECTOR IAW EMB 145 AMM 26-14-00. MX PERFORMED OPERATIONAL CHEC
- [SDR C2XA06SH113](https://openairdocs.org/sdr/C2XA06SH113), Oct 18, 2006: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAMES 29 AND 33. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR I
- [SDR C2XA06SH112](https://openairdocs.org/sdr/C2XA06SH112), Oct 18, 2006: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 1
- [SDR C2XA06SH114](https://openairdocs.org/sdr/C2XA06SH114), Oct 17, 2006: FLOOR SUPPORT. CORRODED. SHV - DURING C-CHECK THE CENTER OMEGA BEAM FLANGE WAS FOUND TO BE CORRODED AT FRAMES 33 AND 34. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED SHIM FILLER R
- [SDR C2XA05BT076](https://openairdocs.org/sdr/C2XA05BT076), Oct 29, 2005: LIGHT. FAULTY. DURING SERVICE AND ROUTINE CHECK, MAINTENANCE CLEARED MEL CONTROL 061756, CENTER PORTION OF NR 6 FLOOR EMERGENCY PROXIMITY LIGHT STRIP WILL NOT ILLUMINATE. AIRC
- [SDR C2XA04IA150](https://openairdocs.org/sdr/C2XA04IA150), Nov 25, 2004: CONTROL MODULE. FAULTY. IAH- FLIGHT 2463, DURING CREW INSPECTION, IT WAS DISCOVERED THAT THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE LIGHT CONTROL MOD
- [SDR C2XA04RI013](https://openairdocs.org/sdr/C2XA04RI013), Nov 6, 2004: BATTERY. INOPERATIVE. IAH - MX, DURING ROUTINE INSPECTION, MAINTENANCE FOUND EMERGENCY LIGHT STRIP INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK POSITION 3. OPE
- [SDR C2XA04SH518](https://openairdocs.org/sdr/C2XA04SH518), Oct 14, 2004: FLOOR SUPPORT. CORRODED. DURING C-CHECK THE LEFT OMEGA SHAPE WAS FOUND CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB SRM 53-21-10, FIGURE 201. AI
- [SDR C2XA04SH515](https://openairdocs.org/sdr/C2XA04SH515), Oct 10, 2004: FLOOR SUPPORT. CORRODED. DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND CORRODED BETWEEN FRAMES 23 AND 25. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW SRM 53-22-10.
- [SDR C2XA04SH516](https://openairdocs.org/sdr/C2XA04SH516), Oct 10, 2004: FLOOR SUPPORT. CORRODED. DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLE REPAIR IAW SRM 53-21-10.
- [SDR C2XA03CL122](https://openairdocs.org/sdr/C2XA03CL122), Jul 8, 2003: LEVER. FAULTY. CREW REPORTED THAT LANDING GEAR LEVER WILL NOT GO UP WITHOUT OVERRIDE BUTTON. MAINTENANCE REMOVED AND REPLACED LANDING GEAR LEVER. OPERATIONAL CHECKS GOOD.
- [SDR C2XA03TY010](https://openairdocs.org/sdr/C2XA03TY010), Jan 18, 2003: STRINGER. CHAFED. DURING A SCHEDULED INSPECTION A STRINGER WAS FOUND CHAFED ON THE INBOARD SIDE OF 19L. MAINTENANCE REMOVED CHAFED AREA, FABRICATED SHIMS AND DOUBLERS, REINSTALLE
- [SDR C2XA03TY005](https://openairdocs.org/sdr/C2XA03TY005), Jan 18, 2003: ANGLE. CORRODED. TYS, During a scheduled inspection corrosion was found on the center ramp angle between frames 19 and 20. Maintenance removed and replaced the center ramp angle
- [SDR C2XA03TY009](https://openairdocs.org/sdr/C2XA03TY009), Jan 18, 2003: DOUBLER. CORRODED. TYS, During a scheduled inspection corrosion was found on the galley spar joint caps by the sevice door. Maintenance removed and replaced the doubler on galley 
- [SDR C2XA03TY008](https://openairdocs.org/sdr/C2XA03TY008), Jan 18, 2003: DOUBLER. CORRODED. TYS, During a scheduled inspection corrosion was found on doubler of right omega beam at frame 20 and 22. Maintenance cleaned doubler at FR20 and found to be wi
- [SDR C2XA03TY007](https://openairdocs.org/sdr/C2XA03TY007), Jan 18, 2003: SILL. CORRODED. TYS, DURING A SCHEDULED INSPECTION FLOOR PANEL SUPPORT AT STRINGER 15L AT FRAME 18L AND 21L WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL.
- [SDR C2XA03TY006](https://openairdocs.org/sdr/C2XA03TY006), Jan 18, 2003: ANTENNA. CORRODED. Tys, During a scheduled inspection the lower TCAS antenna base was found corroded. Maintenance removed and replaced the antenna. I/A/W-EMB-145-34-43-02, operati

All 65: https://openairdocs.org/deregistered/N18982-2011-08-16/reports.md

## Other aircraft with N18982

- [Cancelled 1941-04-28](https://openairdocs.org/deregistered/N18982-1941-04-28): Aero Industries Technical Inst G-1GLIDER, S/N 1, built 1938. Owner: [Susca Peter](https://openairdocs.org/faa-owner/SUSCA%20PETER), [Glendale, CA](https://openairdocs.org/faa-place/CA/Glendale)
- [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N18982-undated): Beech B19, S/N MB871. Triennial form not returned

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