# Service difficulty reports: N18982, cancelled Aug 16, 2011

A list on [N18982, cancelled Aug 16, 2011](https://openairdocs.org/deregistered/N18982-2011-08-16.md).

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

Page 1 of 2 · 65 reports

- [SDR C2XA11TY082](https://openairdocs.org/sdr/C2XA11TY082.md): Door · lack of lube · Jun 13, 2011 · N18982 · Emb EMB145LR · Doors
  > 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.md): Bracket · worn · Sep 25, 2010 · N18982 · Emb EMB145LR · Ailerons
  > LEFT AILERON PCA BRACKET HAS MIGRATED HAT BUSHING. REMOVED AND REPLACED AILERON BRACKET IAW EC5750-01177.
- [SDR C2XA10TY147](https://openairdocs.org/sdr/C2XA10TY147.md): Skin · corroded · Sep 21, 2010 · N18982 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > 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.md): Skin · corroded · Sep 21, 2010 · N18982 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > TYS - CORROSION ON FUSELAGE LOWER SKIN INSIDE CARGO FROM FRAME 60-62 STRINGER 20R- 21R. REMOVED DAMAGE, FABRICATED DOUBLER, AND INSTALLED REPAIR IAW EC 5330-02244.
- [SDR C2XA10TY141](https://openairdocs.org/sdr/C2XA10TY141.md): Bushing · worn · Sep 16, 2010 · N18982 · Emb EMB145LR · Ailerons
  > 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 IAW EC5740-01152. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR C2XA10TY140](https://openairdocs.org/sdr/C2XA10TY140.md): Bushing · migrated · Sep 16, 2010 · N18982 · Emb EMB145LR · Spoilers
  > 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 BOTH HAT BUSHINGS IAW EC5740-01152. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF
- [SDR C2XA10TY139](https://openairdocs.org/sdr/C2XA10TY139.md): Bushing · worn · Sep 16, 2010 · N18982 · Emb EMB145LR · Wing, Control Surface Attach Fittings
  > 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 EC5740-01152. ALL WORK WAS ACCOKMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR C2XA10TY138](https://openairdocs.org/sdr/C2XA10TY138.md): Bushing · worn · Sep 16, 2010 · N18982 · Emb EMB145 · Wing, Control Surface Attach Fittings
  > 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 IAW EC5740-01152. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR C2XA10TY137](https://openairdocs.org/sdr/C2XA10TY137.md): Bushing · worn · Sep 16, 2010 · N18982 · Emb EMB145LR · Wing, Control Surface Attach Fittings
  > 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 WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR C2XA10TY136](https://openairdocs.org/sdr/C2XA10TY136.md): Bushing · worn · Sep 16, 2010 · N18982 · Emb EMB145LR · Wing, Control Surface Attach Fittings
  > 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 THE HAT BUSHING IAW EC5740-01152. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE C
- [SDR C2XA10TY135](https://openairdocs.org/sdr/C2XA10TY135.md): Bushing · worn · Sep 16, 2010 · N18982 · Emb EMB145LR · Wing, Control Surface Attach Fittings
  > 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 EC5740-01152. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR C2XA10TY134](https://openairdocs.org/sdr/C2XA10TY134.md): Bushing · missing · Sep 16, 2010 · N18982 · Emb EMB145LR · Wing, Control Surface Attach Fittings
  > 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 BUSHING IAW EC5740-01152, A/C WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR C2XA10TY130](https://openairdocs.org/sdr/C2XA10TY130.md): Fitting · worn · Sep 15, 2010 · N18982 · Emb EMB145LR · Ailerons
  > 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.md): Fitting · worn · Sep 15, 2010 · N18982 · Emb EMB145LR · Ailerons
  > 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.md): Panel · damaged · Sep 14, 2010 · N18982 · Emb EMB145LR · Vertical Stabilizer, Plate/Skin
  > PANEL 321CL INSIDE SURFACE HAS COMPOSITE DAMAGE NEAR L/E. REPAIRED PANEL IAW EMB 145 EC5530-01183.
- [SDR C2XA10TY124](https://openairdocs.org/sdr/C2XA10TY124.md): Stringer · chafed · Sep 12, 2010 · N18982 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > 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 STRUCTURE FABRICATED ONE ANGLE AND INSTALLED IAW EMB 135/145 SRM 53-24-02.
- [SDR C2XA09IA295](https://openairdocs.org/sdr/C2XA09IA295.md): O-Ring · blown · Nov 29, 2009 · N18982 · Emb EMB145LR · Pneumatic Distribution System
  > 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 AND REPLACED BLOWN O-RINGS AT JOINT NUMBER 21 LEFT, LEAK CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS
- [SDR C2XA09IA289](https://openairdocs.org/sdr/C2XA09IA289.md): O-Ring · blown · Nov 13, 2009 · N18982 · Emb EMB145LR · Pneumatic Distribution System
  > 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 REPLACED THE O-RINGS AT LOCATIONS 3 AND 1 ON THE BLEED AIR SYSTEM, OPERATIONALLY AND LEAK CHECKED WI
- [SDR C2XA09RI057](https://openairdocs.org/sdr/C2XA09RI057.md): Cooling Fan · malfunctioned · Apr 13, 2009 · N18982 · Emb EMB145LR · Air Distribution Fan
  > 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 CHECK SUCCESSFULLY. NO SMOKE/ NO BURNING SMELL NOTED. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09RI013](https://openairdocs.org/sdr/C2XA09RI013.md): Module · defective · Jan 13, 2009 · N18982 · Emb EMB145LR · Cabin Pressure Control System
  > FLIGHT 2675 - EWR - FLIGHT CREW REPORTED PRESSURIZATION SYSTEM SPIKING UNCOMMANDED. EWR MX R&R CPAM AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA08IA215](https://openairdocs.org/sdr/C2XA08IA215.md): Proximity Switch · faulty · Sep 24, 2008 · N18982 · Emb EMB145LR · Landing Gear Retraction/Extension System
  > 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 CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE PROXIMITY SWITCH ON
- [SDR C2XA08IA210](https://openairdocs.org/sdr/C2XA08IA210.md): Indicator · inoperative · Sep 18, 2008 · N18982 · Emb EMB145LR · Fuel Indicating System
  > 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 ACFT AND PLACED THE FUEL SYSTEM ON MEL 28-40-00/1 CAT B CTL NR 154609 AND THE ACFT WAS APPROVED
- [SDR C2XA08TY105](https://openairdocs.org/sdr/C2XA08TY105.md): Bulb · inoperative · Sep 11, 2008 · N18982 · Emb EMB145LR · Emergency Lighting
  > 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. WORK WAS ACCOMPLISHED IAW AMM 33-50-10. (K)
- [SDR C2XA08TY103](https://openairdocs.org/sdr/C2XA08TY103.md): Lamp · burned out · Sep 9, 2008 · N18982 · Emb EMB145LR · Emergency Lighting
  > 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.md): Structure · eroded · Sep 7, 2008 · N18982 · Emb EMB145LR · Horizontal Stabilizer Structure
  > 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.md): Firewall · dented · Sep 4, 2008 · N18982 · Emb EMB145LR · APU Cowling/Containment
  > 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 EC5310-01359. AC WILL BE RELEASED AT THE END OF THE CHECK. (K)
- [SDR C2X2008F00027](https://openairdocs.org/sdr/C2X2008F00027.md): Inlet · corroded · Sep 4, 2008 · N18982 · Emb EMB145LR · Engine Air Intake System
  > 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 EC542001146/ AC WO; BE RELEASED AT THE END OF THE CHECK. (K)
- [SDR C2X2008F00026](https://openairdocs.org/sdr/C2X2008F00026.md): Inlet · corroded · Sep 4, 2008 · N18982 · Emb EMB145LR · Engine Air Intake System
  > 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 EC5420-01145. AC WILL BE RELEASED AT THE END OF THE CHECK. (K)
- [SDR C2X2008F00007](https://openairdocs.org/sdr/C2X2008F00007.md): O-Ring · failed · Jul 20, 2008 · N18982 · Emb EMB145LR · Engine Bleed Air System
  > IAH - FLIGHT 2944 - DURING PREFLIGHT THE CREW REPORTED A BURNING ODOR AND BLEED LEAK NR 2 INDICATION. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED A BLOWN O-RING IN THE CARGO COMPARTMENT, LEAK AND OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE
- [SDR C2XA08IA133](https://openairdocs.org/sdr/C2XA08IA133.md): Coffeemaker · odor · May 25, 2008 · N18982 · Emb EMB145LR · Buffet/Galleys
  > 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 CAT D CONTROL NR 146579", AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDE
- [SDR C2XA08RI051](https://openairdocs.org/sdr/C2XA08RI051.md): Inverter · inoperative · Mar 30, 2008 · N18982 · Emb EMB145LR · Emergency Lighting
  > FLIGHT 3132 - EWR - THE FLIGHT CREW REPORTED AFT GALLEY WALL EMERGENCY LIGHT NOT ILLUMINATING. EWR MX REMOVED AND REPLACED AFT GALLEY WALL EMERGENCY LIGHT INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA08CL035](https://openairdocs.org/sdr/C2XA08CL035.md): Sign · inoperative · Mar 23, 2008 · N18982 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT SIGN IN FRONT OF ROW 3 BC WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY EXIT SIGN. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA07IA198](https://openairdocs.org/sdr/C2XA07IA198.md): Switch · shorted · Sep 5, 2007 · N18982 · Emb EMB145LR · Communications System
  > IAH - DURING MAINTENANCE INSPECTION THE CAPTAINS GLARESHIELD PUSH TO TALK SWITCH SHOCKED AND SMOKED WHEN DEPRESSED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC
- [SDR C2XA07RI036](https://openairdocs.org/sdr/C2XA07RI036.md): Smoke Detector · malfunctioned · May 24, 2007 · N18982 · Emb EMB145LR · Smoke Detection
  > 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 CHECK - NO MSG ON EICAS. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA06SH113](https://openairdocs.org/sdr/C2XA06SH113.md): Floor Support · corroded · Oct 18, 2006 · N18982 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > 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 IAW EMB 145 SRM 53-00-10, FIG 202 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06SH112](https://openairdocs.org/sdr/C2XA06SH112.md): Floor Support · corroded · Oct 18, 2006 · N18982 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > 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 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06SH114](https://openairdocs.org/sdr/C2XA06SH114.md): Floor Support · corroded · Oct 17, 2006 · N18982 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > 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 REPAIR IAW EMB 145 SRM 53-00-10, FIG 203 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA05BT076](https://openairdocs.org/sdr/C2XA05BT076.md): Light · faulty · Oct 29, 2005 · N18982 · Emb EMB145LR · Emergency Lighting
  > DURING SERVICE AND ROUTINE CHECK, MAINTENANCE CLEARED MEL CONTROL 061756, CENTER PORTION OF NR 6 FLOOR EMERGENCY PROXIMITY LIGHT STRIP WILL NOT ILLUMINATE. AIRCRAFT RELEASED IAW MEL 33-50-00/2 CATEGORY -C- CONTROL 061756. REMOVED AND REPLACED NR 6 FLOOR PROX
- [SDR C2XA04IA150](https://openairdocs.org/sdr/C2XA04IA150.md): Control Module · faulty · Nov 25, 2004 · N18982 · Emb EMB145LR · Emergency Lighting
  > IAH- FLIGHT 2463, DURING CREW INSPECTION, IT WAS DISCOVERED THAT THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE LIGHT CONTROL MODULE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04RI013](https://openairdocs.org/sdr/C2XA04RI013.md): Battery · inoperative · Nov 6, 2004 · N18982 · Emb EMB145LR · Emergency Lighting
  > IAH - MX, DURING ROUTINE INSPECTION, MAINTENANCE FOUND EMERGENCY LIGHT STRIP INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK POSITION 3. OPERATIONAL TESTS WERE PERFORMED SUCCESSFULLY. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04SH518](https://openairdocs.org/sdr/C2XA04SH518.md): Floor Support · corroded · Oct 14, 2004 · N18982 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > 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. AIRCRAFT RETURNED TO SERVICE.
- [SDR C2XA04SH515](https://openairdocs.org/sdr/C2XA04SH515.md): Floor Support · corroded · Oct 10, 2004 · N18982 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > 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.md): Floor Support · corroded · Oct 10, 2004 · N18982 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > 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.md): Lever · faulty · Jul 8, 2003 · N18982 · Emb EMB145LR · Landing Gear Selector
  > 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.md): Stringer · chafed · Jan 18, 2003 · N18982 · Emb EMB145LR · Fuselage Main, Longeron/Stringer
  > DURING A SCHEDULED INSPECTION A STRINGER WAS FOUND CHAFED ON THE INBOARD SIDE OF 19L. MAINTENANCE REMOVED CHAFED AREA, FABRICATED SHIMS AND DOUBLERS, REINSTALLED, RESTORED FINISH IAW-EMB-135/145-SRM-53-24-02, CMP-51-21-04/05/06. THE REPAIR WAS SATISFACTORY A
- [SDR C2XA03TY005](https://openairdocs.org/sdr/C2XA03TY005.md): Angle · corroded · Jan 18, 2003 · N18982 · Emb EMB145LR · Fuselage Main, Attach Fittings
  > 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, alodined, primed and painted. I/A/W-EMB-135/145-SRM-51-40-02. The repair was satisfactory and the
- [SDR C2XA03TY009](https://openairdocs.org/sdr/C2XA03TY009.md): Doubler · corroded · Jan 18, 2003 · N18982 · Emb EMB145LR · Fuselage Main, Attach Fittings
  > 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 forward sill, alodined, primed and painted. I/A/W-EMB-135/145-GST-1927/02A, CMP-51-21-04/05/06. The
- [SDR C2XA03TY008](https://openairdocs.org/sdr/C2XA03TY008.md): Doubler · corroded · Jan 18, 2003 · N18982 · Emb EMB145LR · Fuselage Main, Attach Fittings
  > 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 within limits and removed and replaced the doubler for omega beam at FR22, alodined, primed and painte
- [SDR C2XA03TY007](https://openairdocs.org/sdr/C2XA03TY007.md): Sill · corroded · Jan 18, 2003 · N18982 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > 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. IAW-EMB-135/145-SRM-51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON CO
- [SDR C2XA03TY006](https://openairdocs.org/sdr/C2XA03TY006.md): Antenna · corroded · Jan 18, 2003 · N18982 · Emb EMB145LR · Doppler System
  > 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, operational checked good. The aircraft will be released upon complection of the inspection.

Next page: https://openairdocs.org/deregistered/N18982-2011-08-16/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N18982' AND deregistration_id = 'N18982-2011-08-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N18982-2011-08-16/reports

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