# Service difficulty reports: N12540

A list on [N12540](https://openairdocs.org/aircraft/N12540.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 · 86 reports

- [SDR ASOA201902274011](https://openairdocs.org/sdr/ASOA201902274011.md): Wire · broken · Feb 27, 2019 · N12540 · Emb EMB145LR · Light System Wiring
  > LCH - FLIGHT 4264 THE VERY LAST EMERGENCY PROX LIGHT STRIP WAS FOUND TO BE INOPERATIVE DUE TO A BROKEN WIRE ON THE LIGHT ASSEMBLY. MAINTENANCE PLACED THE ITEM OM MEL 33-50-00-2 AND THE AIRCRAFT WAS APPROVED OF RETURN TO SERVICE. ON 03/09/19 IAH MAINTENANCE REM
- [SDR ASOA201710134054](https://openairdocs.org/sdr/ASOA201710134054.md): Acm · frozen · Oct 13, 2017 · N12540 · Emb EMB145LR · Cabin Cooling System
  > THE CREW REPORTED SMOKE IN THE CABIN AND FLIGHT DECK. THE AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE NR 2 ACM, OPS TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV
- [SDR ASOA201710047018](https://openairdocs.org/sdr/ASOA201710047018.md): Rib · cracked · Oct 4, 2017 · N12540 · Emb EMB145LR · Wing, Rib/Bulkhead
  > LEFT WING RIB 21 CRACKED. CUT OUT THE SECTION AND INSTALLED FILLER AND DOUBLER.
- [SDR ASOA201710047016](https://openairdocs.org/sdr/ASOA201710047016.md): Floor Support · corroded · Oct 4, 2017 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > RIGHT OMEGA BEAM, FRAME 23 CORRODED BEYOND LIMITS AT SCREW HOLES. REMOVED AND REPLACED THE OMEGA BEAM.
- [SDR ASOA201805264030](https://openairdocs.org/sdr/ASOA201805264030.md): Battery Pack · discharged · May 26, 2017 · N12540 · Emb EMB145LR · Emergency Lighting
  > IAH - DURING MAINTENANCE INSPECTION THE UPPER EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE
- [SDR ASOA201702134006](https://openairdocs.org/sdr/ASOA201702134006.md): Light · disconnected · Feb 13, 2017 · N12540 · Emb EMB145LR · Light System Wiring
  > FLIGHT 4045, THE CREW REPORTED AN OVERHEAD EMERGENCY LIGHT TO BE OUT IN THE AISLE NEAR THE GALLEY. MAINTENANCE INSPECTED THE AIRCRAFT AND RECONNECTED THE AFFECTED EMERGECY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN T
- [SDR ASOA201701163003](https://openairdocs.org/sdr/ASOA201701163003.md): Axle · broken · Jan 16, 2017 · N12540 · Emb EMB145LR · Main Landing Gear Strut/Axle/Truck
  > DURING ROUTINE MAINTENANCE, THE RIGHT MAIN LANDING GEAR SHOCK ABSORBER LOWER AXLE WAS FOUND BROKEN. MAINTENANCE REPLACED THE RIGHT SHOCK ABSORBER LOWER AXLE SPECIAL BOLT.
- [SDR ASOA20150727039C](https://openairdocs.org/sdr/ASOA20150727039C.md): Inverter · inoperative · Jul 27, 2015 · N12540 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE GALLEY EMERGENCY LIGHT WOULD NOT TURN ON. MAINTENANCE REPLACED THE NR 2 AND NR 3 EMERGENCY LIGHT INVERTERS. OPS CHECKS WERE GOOD.
- [SDR ASOA20150506109V](https://openairdocs.org/sdr/ASOA20150506109V.md): Beam · corroded · May 5, 2015 · N12540 · Emb EMB145LR · Fuselage Main, Structure
  > 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 SERVICE.
- [SDR ASOA20150506108V](https://openairdocs.org/sdr/ASOA20150506108V.md): Floor Support · corroded · May 5, 2015 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59-61. MAINTENANCE REMOVED THE CORROSION AND PERFORMED DOUBLER REPAIRS IAW EC5320-02037. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150506107](https://openairdocs.org/sdr/ASOA20150506107.md): Frame · corroded · May 5, 2015 · N12540 · Emb EMB145LR · Fuselage Main, Frame
  > DURING C-CHECK, FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 15-17L. MAINTENANCE PERFORMED A FRAME SEGMENT SPLICE REPAIR IAW SRM 53-31-04, FIGURE 212. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150428102](https://openairdocs.org/sdr/ASOA20150428102.md): Shear Tie · corroded · Apr 28, 2015 · N12540 · Emb EMB145LR · Fuselage Internal Mounting Structure
  > DURING C-CHECK SHEAR TIE AT FRAME 68 CARGO DOOR LOWER BEAM HAS CORROSION. REPAIRED SHEAR TIE AT FRAME 68 IAW SRM 53-31-04. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130514315T](https://openairdocs.org/sdr/ASOA20130514315T.md): Floor Support · corroded · May 14, 2013 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CORROSION AT RT OMEGA BEAM AT NUTPLATE HOLES CORRODED BEYOND LIMITS. R & R HAT SECTION ASSY.
- [SDR ASOA20130514314](https://openairdocs.org/sdr/ASOA20130514314.md): Profile · corroded · May 14, 2013 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CORROSION AT "T" PROFILE BEYOND LIMITS. R & R T PROFILE LT SIDE AT OMEGA BEAM.
- [SDR ASOA20130514313](https://openairdocs.org/sdr/ASOA20130514313.md): Gusset · corroded · May 14, 2013 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CORROSION AT GUSSET Y=0.00 CORRODED AROUND SCREW HOLES BEYOND LIMITS. R & R GUSSET
- [SDR ASOA20130514312](https://openairdocs.org/sdr/ASOA20130514312.md): Gusset · corroded · May 14, 2013 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CENTER OMEGA BEAM GUSSET HAS CORROSION BEYOND LIMITS. R & R GUSSET.
- [SDR ASOA20130513311](https://openairdocs.org/sdr/ASOA20130513311.md): Gusset · corroded · May 13, 2013 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CORROSION BEYOND LIMITS ON GUSSET. R & R GUSSET.
- [SDR ASOA20130513310](https://openairdocs.org/sdr/ASOA20130513310.md): Floor Support · corroded · May 13, 2013 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.
- [SDR ASOA20130513309](https://openairdocs.org/sdr/ASOA20130513309.md): Floor Support · corroded · May 13, 2013 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > RT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.
- [SDR ASOA20130513308](https://openairdocs.org/sdr/ASOA20130513308.md): Floor Support · corroded · May 13, 2013 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CORROSION BEYOND LIMITS AT FLOOR SUPPORT. R & R FLOOR SUPPORT.
- [SDR ASOA20130513307](https://openairdocs.org/sdr/ASOA20130513307.md): Floor Support · corroded · May 13, 2013 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > RT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.
- [SDR ASOA20130513306](https://openairdocs.org/sdr/ASOA20130513306.md): Sill · corroded · May 13, 2013 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > RT SILL CORRODED BEYOND LIMITS. R & R SILL.
- [SDR ASOA20130513305](https://openairdocs.org/sdr/ASOA20130513305.md): Sill · corroded · May 13, 2013 · N12540 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > LT SILL CORRODED BEYOND LIMITS. R & R SILL.
- [SDR ASOA20130513304](https://openairdocs.org/sdr/ASOA20130513304.md): Sill · corroded · May 13, 2013 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > LT SILL CORRODED BEYOND LIMITS. R & R SILL.
- [SDR ASOA20130123005C](https://openairdocs.org/sdr/ASOA20130123005C.md): Light · inoperative · Jan 23, 2013 · N12540 · Emb EMB145 · Emergency Lighting
  > DURING ROUTINE MX, THE LT EXTERNAL AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX REPLACED THE LIGHT ASSY AND OPS CHECKED GOOD.
- [SDR ASOA20121126155](https://openairdocs.org/sdr/ASOA20121126155.md): Battery · inoperative · Nov 23, 2012 · N12540 · Emb EMB145LR · Emergency Lighting
  > NR 4 BATTERY FOR EMERGENCY LIGHT IN CEILING IS INOPERATIVE. R & R NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD. ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20121127158](https://openairdocs.org/sdr/ASOA20121127158.md): Skin · damaged · Nov 22, 2012 · N12540 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > THE REAR FUSELAGE RT SKIN WAS DAMAGED DURING GROUND OPERATIONS. THE DAMAGE IS LOCATED BETWEEN FRAMES 62 & 63, STR 15R & 17R. REPAIRED DENT WITH FILLER AND DOUBLER. CUTOUT DAMAGED PORTION OF FRAME. FABRICATED AND INSTALLED FRAME SPLICE. REMOVED DAMAGED SEC
- [SDR ASOA20121010091](https://openairdocs.org/sdr/ASOA20121010091.md): Fmu · faulty · Oct 10, 2012 · N12540 · Emb EMB145LR · Fuel Controlling System
  > CREW REPORTED ENGINE NR 2 STARTED SURGING (ERRATIC ACCEL & DECEL) ON DESCENT BETWEEN FL 260& FL250 N1 SPIKE 45-65 ITT SPIKE BETWEEN 400-600. MX R & R ENGINE NR 2 FPMU WITH OPS AND LEAK CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120827114](https://openairdocs.org/sdr/ASOA20120827114.md): Light · malfunctioned · Aug 27, 2012 · N12540 · Emb EMB145LR · Emergency Lighting
  > DURING POSTFLIGHT INSP THE CREW REPORTED THE EMERGENCY LIGHT AT 3BC TO BE INOPERATIVE. THE EMERGENCY LIGHT SYS WAS OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120827113](https://openairdocs.org/sdr/ASOA20120827113.md): Light · malfunctioned · Aug 27, 2012 · N12540 · Emb EMB145LR · Emergency Lighting
  > DURING PREFLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY LIGHT AT 3BC TO BE INOPERATIVE. MX RESET THE EMERGENCY LIGHT SYS, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120519040R](https://openairdocs.org/sdr/ASOA20120519040R.md): Controller · faulty · May 19, 2012 · N12540 · Emb EMB145LR · Cabin Pressure Controller
  > CREW REPORTED LOSS OF CABIN PRESSURIZATION AT FL330. CREW MANUALLY DEPLOYED PAX O2 MASK AT 12,100 FT WITH CABIN ALT SHOWING 20,000 FT IAW ENGINEERING INSTRUCTIONS AND ASSISTANCE MX R & R THE DIGITAL PRESSURIZATION CONTROLLER, CABIN PRESS. AQUISITION MODULE (C
- [SDR ASOA20120121008](https://openairdocs.org/sdr/ASOA20120121008.md): Unknown · odor · Jan 21, 2012 · N12540 · Emb EMB145LR · Air Distribution System
  > THE CREW REPORTED SEVERE TURBULANCE AT FL360. LOST ABOUT 1000FT, AP DISENGAGED AND THEY ALSO REPORTED A BURNING ODOR FOR ABOUT A MINUTE. MX COMPLIED WITH TURBULENCE INSPECTION. NO DEFECTS WERE NOTED. AUTOPILOT OPS CHECKED GOOD. NO DEFECTS FOUND. PERFORME
- [SDR C2XA11RI178](https://openairdocs.org/sdr/C2XA11RI178.md): Flashlight · melted · Nov 9, 2011 · N12540 · Emb EMB145LR · Emergency Lighting
  > FLT 4154 EWR - CREW REPORTED A ELECTRICAL SMELL NEAR MAIN CABIN DOOR WITH OBSERVATION OF F/A FLASHLIGHT MELTED. EWR MX REMOVED AND REPLACED THE FWD F/A FLASHLIGHT AND CRADLE ASSY IAW EMB 145 AMM 33-50-16 WITH OPERATIONAL CHECK SUCCESSFUL. ACFT WAS APPROVED F
- [SDR C2XA11RI176](https://openairdocs.org/sdr/C2XA11RI176.md): Light · malfunctioned · Nov 6, 2011 · N12540 · Emb EMB145LR · Emergency Lighting
  > DURING SCHEDULED MAINTENANCE INSPECTION, ROW 12 CEILING EMERGENCY LIGHT WOULD NOT ILLUMINATE. MX RESET SYSTEM AND OPERATIONALLY CHECKED THE LIGHT SUCCESSFULLY IAW EMB145 AMM 33-50-00-700-801A. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11CL227](https://openairdocs.org/sdr/C2XA11CL227.md): Strut · worn · Oct 10, 2011 · N12540 · Emb EMB145LR · Nose/Tail Landing Gear Strut/Axle
  > CLE FLT 5850 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL, AND A ENGINE 1/2 REV DISAGREE MESSAGE DURING CLIMBOUT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NOSE STRUT DEFLATED. DURING REPACK OF THE NOSE ST
- [SDR C2XA11CL154](https://openairdocs.org/sdr/C2XA11CL154.md): Proximity Switch · faulty · Jun 24, 2011 · N12540 · Emb EMB145LR · Landing Gear Position and Warning
  > AVP - FLT 6089 THE CREW REPORTED A LOUD BANGING NOISE FROM UNDER FIRST OFFICER'S FLOOR. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR UPLOCK PROXIMITY SWITCH AND THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA11TY080](https://openairdocs.org/sdr/C2XA11TY080.md): Structure · corroded · Jun 8, 2011 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > MINOR CORROSION FWD AND AFT OF THE CARGO DOOR SILL. REMOVED CORROSION AND FOUND TO BE SERVICABLE IAW EC5330-01458 ALODINE, PRIMED AND PAINTED IAW EMB 135/145 CPM 51-21-04, 05&06.
- [SDR C2XA10RI066](https://openairdocs.org/sdr/C2XA10RI066.md): Switch · defective · May 18, 2010 · N12540 · Emb EMB145LR · Pneumatic Distribution System
  > FLIGHT 2183 - EWR - FLIGHT CREW REPORTED BLEED NR 2 LOW TEMP ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED BLEED NR PUSH BUTTON SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN
- [SDR C2XA10TY027](https://openairdocs.org/sdr/C2XA10TY027.md): Line · leaking · Feb 12, 2010 · N12540 · Emb EMB145LR · Airfoil Anti/De-ice System
  > TYS - A/C WAS EN ROUTE TO ATL FROM EWR WHEN A STAB ANTI ICE FAIL MESSAGE SHOWED. CREW DIVERTED TO TYS AND CHANGE PLANES AND CONTINUED. MAINTENANCE FOUND A LINE LEAKING GOING TO A PRESSURE SWITCH.
- [SDR C2XA10IA026](https://openairdocs.org/sdr/C2XA10IA026.md): Connector · defective · Jan 18, 2010 · N12540 · Emb EMB145LR · Light System Wiring
  > IAH - DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE OUTSIDE OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LEFT EMERGENCY EXIT LIGHT CONNECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS A
- [SDR C2XA10RI001](https://openairdocs.org/sdr/C2XA10RI001.md): Unknown · odor · Jan 5, 2010 · N12540 · Emb EMB145LR · Air Distribution System
  > FLIGHT 2603 - EWR - FLIGHT CREW REPORTED FUEL SMELL IN COCKPIT AFTER APU START. EWR MX PROCEEDED WITH APU OPERATIONAL CHECK BUT COULD NOT DUPLICATE ANY TYPE OF SMELL. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09IA204](https://openairdocs.org/sdr/C2XA09IA204.md): Light · inoperative · Aug 12, 2009 · N12540 · Emb EMB145LR · Passenger Compartment Lighting
  > GSP - FLIGHT 2675 - THE FLIGHT ATTENDANT REPORTED THE PASSENGER READING LIGHT AT 18C STARTED SMOKING MIDWAY THROUGH THE FLIGHT AND WOULD NOT TURN OFF. THE FLIGHT ATTENDANT USED THE RESET SWITCH BUTTON, AND THE LIGHT EXTINGUISHED AND SMOKE STOPPED. THE AIRCRA
- [SDR C2XA09SH241](https://openairdocs.org/sdr/C2XA09SH241.md): Sill · corroded · Aug 1, 2009 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CARGO DOOR CUTOUT LOWER SILL HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH238](https://openairdocs.org/sdr/C2XA09SH238.md): Floor Support · corroded · Aug 1, 2009 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CENTER OMEGA BEAM FRAME 20 CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED AND COMPLETED REPAIR AT CENTER OMEGA BEAM FRAME 20 IAW EMB-145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH237](https://openairdocs.org/sdr/C2XA09SH237.md): Floor Support · cracked · Aug 1, 2009 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON LT OMEGA BEAM FACE AND FLANGE BETWEEN FRAMES 20-23 AND CRACKED AT FRAME 22. MAINTENANCE REMOVED AND REPLACED AND COMPLETED REPAIR OF LT OMEGA BEAM BETWEEN FRAME 20-22 BY INSTALLING A BEAM SPLICE AT FRAME 19.5
- [SDR C2XA09SH183](https://openairdocs.org/sdr/C2XA09SH183.md): Floor Support · corroded · Jun 29, 2009 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CK, CENTER OMEGA BEAM HAS CORROSION AT FR 20. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-21-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH182](https://openairdocs.org/sdr/C2XA09SH182.md): Floor Support · corroded · Jun 29, 2009 · N12540 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CK, LT OMEGA BEAM HAS CORROSION BETWEEN FR 20 AND 23. REPAIRED OMEGA BEAM IAW EC 5320-01229. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH181](https://openairdocs.org/sdr/C2XA09SH181.md): Beam · corroded · Jun 29, 2009 · N12540 · Emb EMB145LR · Fuselage Main, Structure
  > SHV - DURING C-CK, CARGO DOOR LOWER CUTOUT HAS CORROSION. REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH180](https://openairdocs.org/sdr/C2XA09SH180.md): Bracket · damaged · Jun 29, 2009 · N12540 · Emb EMB145LR · Wing, Attach Fittings
  > SHV - DURING C-CK, LT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHINGS. REMOVED AND REPLACED LT AILERON PCA ATTACHMENT BRACKET IAW EC 5750-01177. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09SH179](https://openairdocs.org/sdr/C2XA09SH179.md): Bracket · damaged · Jun 29, 2009 · N12540 · Emb EMB145LR · Wing, Attach Fittings
  > SHV - DURING C-CK, RT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHINGS. REMOVED AND REPLACED RT AILERON PCA ATTACHMENT BRACKET IAW EC 5750-01177. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Next page: https://openairdocs.org/aircraft/N12540/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 = 'N12540' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N12540/reports

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