# Service difficulty reports: N12567, cancelled Oct 20, 2020

A list on [N12567, cancelled Oct 20, 2020](https://openairdocs.org/deregistered/N12567-2020-10-20.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 · 60 reports

- [SDR ASOA201901214003](https://openairdocs.org/sdr/ASOA201901214003.md): Skin · damaged · Jan 21, 2019 · N12567 · Emb EMB145LR · Cargo/Baggage Doors
  > IAH - DURING MAINTENANCE INSPECTION A PREVIOUS REPAIR ON THE CARGO DOOR LOWER FORWARD CORNER WAS FOUND TO HAVE A CREASE ON THE SKIN. MAINTENANCE REMOVED THE DOUBLER, CUT OUT THE AFFECTED SKIN AND INSTALLED A NEW DOUBLER. PRESSURIZATION CHECKS WERE PERFORMED SA
- [SDR ASOA201804167062](https://openairdocs.org/sdr/ASOA201804167062.md): Wire · broken · Apr 16, 2018 · N12567 · Emb EMB145LR · Light System Wiring
  > INSPECTION FOUND A BROKEN WIRE ON THE EMERGENCY LIGHT STRIP. MAINTENANCE REPLACED THE LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD.
- [SDR ASOA201804167061](https://openairdocs.org/sdr/ASOA201804167061.md): Skin · damaged · Apr 16, 2018 · N12567 · Emb EMB145LR · Horizontal Stabilizer, Plate/Skin
  > FOUND THE RT HORIZONTAL STAB LEADING EDGE DAMAGE AT THE LOWER SIDE SCREW HOLES. MAINTENANCE REPAIRED THE LOWER HORIZONTAL STAB LEADING EDGE IAW ETD 2018-145-037750.
- [SDR ASOA201804137060](https://openairdocs.org/sdr/ASOA201804137060.md): Skin · damaged · Apr 11, 2018 · N12567 · Emb EMB145LR · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STAB LEADING EDGE HAS DAMAGE AT THE SCREW HOLES ON LOWER SIDE. CONTOURED THE AREA BY COLD FORMING. INSTALLED DIMPLED WASHER IAW ETD2018-145-037750.
- [SDR ASOA201804057052](https://openairdocs.org/sdr/ASOA201804057052.md): Door Frame · corroded · Apr 4, 2018 · N12567 · Emb EMB145LR · Fuselage Main, Structure
  > DOOR FRAME HAS CORROSION ON AFT LOWEST DOOR STOP ON SERVICE DOOR. REMOVED DAMAGED SECTION OF THE DOOR FRAME 22. DRILLED AND FABRICATED A DOUBLER SECTION OF THE FRAME AND INSTALLED.
- [SDR ASOA201804057051](https://openairdocs.org/sdr/ASOA201804057051.md): Skin · cracked · Apr 4, 2018 · N12567 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > CRACKED SKIN AT FRAME 75. CUT OUT A 2 X 2 INCH SECTION OF THE SKIN AND INSTALLED FILLER AND DOUBLER.
- [SDR ASOA201803247036](https://openairdocs.org/sdr/ASOA201803247036.md): Yoke · cracked · Mar 24, 2018 · N12567 · Emb EMB145LR · Engine Mount Section
  > #1 ENGINE PYLON LOWER FORWARD YOKE CRACKED. REMOVED AND REPLACED FORWARD YOKE. AIRCRAFT STILL IN C CHECK.
- [SDR ASOA201706055083](https://openairdocs.org/sdr/ASOA201706055083.md): Control Unit · faulty · Jun 5, 2017 · N12567 · Emb EMB145LR · Landing Gear Brake System
  > PILOT REPORTED RIGHT BRAKE PEDAL WHEN COMMANDED RESULTS IN ALMOST NO BRAKING ACTION. ADDITIONALLY THE RIGHT IB BRAKE TEMP ALWAYS STAYED AT ZERO DESPITE THE RIGHT OB BRAKE TEMP GOING INTO THE AMBER INDICATION AFTER MODERATE BRAKING. MX REMOVED AND REPLACED BRAK
- [SDR ASOA201612225092](https://openairdocs.org/sdr/ASOA201612225092.md): Light · inoperative · Dec 22, 2016 · N12567 · Emb EMB145LR · Emergency Lighting
  > CREW REPORTED MOST AFT CABIN EMERGENCY LIGHTS ARE INOPERATIVE. MX REMOVED AND REPLACED THE LIGHT AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160611028](https://openairdocs.org/sdr/ASOA20160611028.md): Control Module · odor · Jun 11, 2016 · N12567 · Emb EMB145LR · Passenger Compartment Lighting
  > HEAVY ELECTRICAL SMOKE ODOR REPORTED FROM MAIN CABIN DOOR AREA SPREAD TO THE GALLEY. R & R CABIN LIGHT CONTROL MODULE WITH OPS CHECK GOOD. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150626033](https://openairdocs.org/sdr/ASOA20150626033.md): Charger · inoperative · Jun 26, 2015 · N12567 · Emb EMB145LR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, THE LT FWD FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE R & R NR 4 EMERGENCY LIGHT BATTERY CHARGER AND REPAIRED WIRE NR W192-8593-20 WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150520029](https://openairdocs.org/sdr/ASOA20150520029.md): Charger · faulty · May 20, 2015 · N12567 · Emb EMB145LR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE LT FWD EXTERNAL EMERGENCY LIGHT AND AISLE CEILING LIGHT WOULD NOT TEST. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECKS WERE GOOD.
- [SDR ASOA20150304023](https://openairdocs.org/sdr/ASOA20150304023.md): Charger · inoperative · Mar 4, 2015 · N12567 · Emb EMB145LR · Emergency Lighting
  > DURING A-CK INSPECTION, THE LT WING FWD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 1 BATTERY CHARGER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130806350T](https://openairdocs.org/sdr/ASOA20130806350T.md): Bearing · worn · Aug 6, 2013 · N12567 · Emb EMB145LR · Horizontal Stabilizer Structure
  > ACFT LT AND RT HORIZONTAL STABILIZER SPHERICAL BEARINGS HAD PLAY IN THE HOUSING. MX REAMED BOTH HOUSINGS AND REPAIRED AND INSTALLED SPHERICAL BEARINGS IAW SRM 55-30-02. COMPLIED WITH BACKLASHES IAW AMM 27-40-00; ALL WORK ACCOMPLISHED AND WAS RELEASED TO SER
- [SDR ASOA20130702069](https://openairdocs.org/sdr/ASOA20130702069.md): Transducer · faulty · Jul 2, 2013 · N12567 · Emb EMB145LR · Landing Gear Brake System
  > PILOT REPORTED DURING BRAKE APPLICATION (RT ONLY) CLUNKING NOISE COMES FROM FWD OF COCKPIT UNTIL HARD BRAKE APPLICATION. BRAKING ACTION REDUCED UNTIL HARD APPLICATION. MX R & R NR 3 WHEEL SPEED TRANDUCER AND HARNESS WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROV
- [SDR ASOA20130412035](https://openairdocs.org/sdr/ASOA20130412035.md): Light · inoperative · Apr 12, 2013 · N12567 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION THE EMERGENCY LIGHT PROXIMITY STRIP BETWEEN ROW 4 AND 7 WAS FOUND INOPERATIVE. MX RESET SYS AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121010081](https://openairdocs.org/sdr/ASOA20121010081.md): Duct · disconnected · Oct 10, 2012 · N12567 · Emb EMB145LR · Air Distribution System
  > THE CREW REPORTED ODOR OF SMOKE AT SEATS 6-7. MX INSPECTED AND FOUND DUCT AT NR 2 RECIRCULATION FAN OFF UNDER FLOOR. MX REINSTALLED DUCT AT NR 2 RECIRCULATION FAN AND OPS CHECKED GOOD.
- [SDR ASOA20120812109](https://openairdocs.org/sdr/ASOA20120812109.md): Battery Pack · discharged · Aug 12, 2012 · N12567 · Emb EMB145LR · Emergency Lighting
  > DURING PREFLIGHT INSP THE CREW REPORTED TAHT THE FIRST 3 AISLE PATH EMERGENCY LIGHTS WOULD ONLY STAY ILLUMINATED FOR 15 SECONDS AND THEN GO IFF, AND THAT THE EMERGENCY EXIT SIGN IN THE GALLEY WOULD ALSO NOT STAY ILLUMINATED. MX R & R THE NR 1 AND NR 2 EMERGEN
- [SDR ASOA20120812108](https://openairdocs.org/sdr/ASOA20120812108.md): Battery Pack · discharged · Aug 12, 2012 · N12567 · Emb EMB145LR · Emergency Lighting
  > DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST 3 AISLE PATH EMERGENCY LIGHTS WOULD ONLY STAY ILLUMINATED FOR 15 SECONDS AND THEN GO OFF, AND THAT THE EMERGENCY EXIT SIGN IN THE GALLEY WOULD ALSO NOT STAY ILLUMINATED. MX R & R THE NR 1 AND NR 2
- [SDR ASOA20120525108](https://openairdocs.org/sdr/ASOA20120525108.md): Sill · corroded · May 24, 2012 · N12567 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CORROSION ON REPAIR DOUBLER RT SILL FRAME 20. BLENDED CORROSION, WITHIN LIMITS. TREATED, PRIMED, PAINTED.
- [SDR ASOA20120519106T](https://openairdocs.org/sdr/ASOA20120519106T.md): Shear Tie · cracked · May 19, 2012 · N12567 · Emb EMB145LR · Fuselage Internal Mounting Structure
  > SHEAR CLIP FOUND CRACKED AT FRAME 61 BETWEEN STR 6L AND 7L. MX R & R THE SHEAR CLIP IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR ASOA20120519105](https://openairdocs.org/sdr/ASOA20120519105.md): Shear Tie · cracked · May 19, 2012 · N12567 · Emb EMB145LR · Fuselage Internal Mounting Structure
  > SHEAR CLIP CRACKED AT FRAME 80 AT THE APU FIRE BOTTLE. MX R & R THE SHEAR CLIP IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR ASOA20120519104](https://openairdocs.org/sdr/ASOA20120519104.md): Crossbeam · corroded · May 19, 2012 · N12567 · Emb EMB145LR · Fuselage Main, Structure
  > CORROSION WAS FOUND IN THE ISLE AT FRAME 20 CROSS-MEMBER THAT WAS BLENDED OUT OF LIMITS. MX R & R THE CROSS-MEMBER IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR ASOA20120519103](https://openairdocs.org/sdr/ASOA20120519103.md): Floor Support · cracked · May 19, 2012 · N12567 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > THE RT OTBD OMEGA BEAM SUPPORT WAS FOUND CRACKED AT FRAME 47 TO 48. MX R & R THE SUPPORT IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR ASOA20120519102](https://openairdocs.org/sdr/ASOA20120519102.md): Skin · canning · May 19, 2012 · N12567 · Emb EMB145LR · Cargo/Baggage Doors
  > DENT ON THE CARGO DOOR. MX RECONTOURED DENT, SKIN HAD A OIL CAN, SO THEY CUT OUT DAMAGE, FABRICATED A FILLER AND DOUBLER, THEN INSTALL FILLER AND DOUBLER IAW SRM 53-20-01 AND ETD 2011-145-102644. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE C
- [SDR ASOA20120519101](https://openairdocs.org/sdr/ASOA20120519101.md): Seat Track · corroded · May 19, 2012 · N12567 · Emb EMB145LR · Fuselage, Seat/Cargo Attach Fittings
  > THE LEFT OTBD SEAT TRACK WAS FOUND CORRODED BEYOND LIMITS AT FRAME 50. MX R & R THE SUPPORT AT FRAME 50 IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR ASOA20120525110](https://openairdocs.org/sdr/ASOA20120525110.md): Floor Support · corroded · May 12, 2012 · N12567 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CORROSION IN GUSSET CENTER OMEGA BEAM FRAME 20. BLENDED CORROSION, WITHIN LIMITS. TREATED, PRIMED AND PAINTED.
- [SDR ASOA20120525109](https://openairdocs.org/sdr/ASOA20120525109.md): Bracket · corroded · May 12, 2012 · N12567 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > CORROSION ON BRACKET AT PAX DOOR ENTRANCE BELOW FLOOR. BLENDED CORROSION, WITHIN LIMITS. TREATED, PRIMED AND PAINTED.
- [SDR C2XA11CL064](https://openairdocs.org/sdr/C2XA11CL064.md): Smoke Warning · false activation · Mar 3, 2011 · N12567 · Emb EMB145LR · Smoke Detection
  > ICT FLT 6056 THE CREW REPORTED A LAV SMOKE EICAS MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND PERFORMED LAV SMOKE SYSTEM OPERATIONAL CHECKS. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR C2XA10SH248](https://openairdocs.org/sdr/C2XA10SH248.md): Skin · cracked · Jul 21, 2010 · N12567 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK THE LT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 77-79 AND STRINGERS 2-10L. MAINTENANCE REMOVED THE CRACKS AND PERFORMED BUSHING REPAIRS IAW EC5330-02080 AND EC5330-02188. THE AIRCRAFT WAS APPROVED FOR RETURN TO SE
- [SDR C2XA10SH247](https://openairdocs.org/sdr/C2XA10SH247.md): Skin · cracked · Jul 21, 2010 · N12567 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 78-79 AND STRINGERS 2-10R. MAINTENANCE REMOVED THE CRACKS AND PERFORMED BUSHING REPAIRS IAW EC 5330-02080 AND EC5330-02188. THE AIRCRAFT WAS APPROVED FOR RETURN TO S
- [SDR C2XA10SH246](https://openairdocs.org/sdr/C2XA10SH246.md): Frame · cracked · Jul 21, 2010 · N12567 · Emb EMB145LR · Fuselage Main, Frame
  > SHV - DURING C-CHECK FRAME 10 AT STRINGER 10L (RIGHT BELOW THE LT DV WINDOW) WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED FRAME SEGMENT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10SH245](https://openairdocs.org/sdr/C2XA10SH245.md): Frame · cracked · Jul 21, 2010 · N12567 · Emb EMB145LR · Fuselage Main, Frame
  > SHV - DURING C-CHECK FRAME 10 AT STRINGER 10R (RIGHT BELOW THE RT DV WINDOW) WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED FRAME SEGMENT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10TY022](https://openairdocs.org/sdr/C2XA10TY022.md): Fuse · blown · Feb 5, 2010 · N12567 · Emb EMB145LR · Emergency Lighting
  > TYS - A/C IN FOR A 3A CHECK WHEN INSPECTION FOUND THE LT FWD OVERWING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE FUSE IN BATTERY TRAY 1. OPS CHECK GOOD IAW EMB 135/145 VCMM 33-21-20 AND EMB 145 AMM 33-50-00. RELEASED TO SERVICE.
- [SDR C2XA10IA003](https://openairdocs.org/sdr/C2XA10IA003.md): Light · inoperative · Jan 3, 2010 · N12567 · Emb EMB145LR · Emergency Lighting
  > IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE LEFT FORWARD EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA09IA332](https://openairdocs.org/sdr/C2XA09IA332.md): Line · contaminated · Dec 30, 2009 · N12567 · Emb EMB145LR · Pitot/Static System
  > IAH - FLIGHT 2263, THE CREW REPORTED AN ALTITUDE AND IAS ERROR WITH A BURNING SMELL. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE DRAINED THE WATER FROM THE PITOT STATIC SYSTEM. INSPECTED THE COCKPIT, CURRENT RELAY SENSORS WITH NO DEFECTS NO
- [SDR C2XA09IA069](https://openairdocs.org/sdr/C2XA09IA069.md): Charger · inoperative · Feb 28, 2009 · N12567 · Emb EMB145LR · Emergency Lighting
  > LCH - DURING MAINTENANCE INSPECTION THE COCKPIT CEILING AND NR 1 AISLE PATH, CEILING, AND WING TO FUSELAGE FRONT FAIRING LEFT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY CHARGER, OPERA
- [SDR C2XA09TY035](https://openairdocs.org/sdr/C2XA09TY035.md): Skin · dented · Feb 24, 2009 · N12567 · Emb EMB145 · Fuselage Main, Plate/Skin
  > AIRCRAFT HAD TWO DENTS BETWEEN FRM 20/21 AND STR14L/16L. REPAIRED DENTED AREA BY FABRICATING L-ANGLE IAW IC2009-145/01434A. RE-CONTOURED SKIN, PERFORMED NDT, INSTALLED L-ANGLE AND RESTORED ORIGINAL FINISH IAW IC 2009-145/01434A. AIRCRAFT RELEASED AND RETURN
- [SDR C2XA09TY024](https://openairdocs.org/sdr/C2XA09TY024.md): Battery Pack · failed · Jan 27, 2009 · N12567 · Emb EMB145LR · Emergency Lighting
  > ACFT WAS FOUND WITH THE AFT CEILING EMERGENCY LIGHT INOP. MX R&R THE NR 4 EMERGENCY LIGHT POWER SUPPLY IAW AMM 145 33-50-04. OPS CHECK GOOD AND WAS RELEASED TO SERVICE.
- [SDR C2XA08RI065](https://openairdocs.org/sdr/C2XA08RI065.md): Light · inoperative · May 9, 2008 · N12567 · Emb EMB145LR · Smoke Detection
  > FLIGHT 2648 - EWR - FLIGHT CREW REPORTED BAG SMOKE DETECT WOULD NOT ILLUMINATED ON TEST. EWR MX RESET THE SYSTEM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA08RI017](https://openairdocs.org/sdr/C2XA08RI017.md): Proximity Switch · intermittent · Feb 11, 2008 · N12567 · Emb EMB145LR · Landing Gear Position and Warning
  > FLIGHT 2761 - EWR - CREW REPORTED THAT AFTER ROTATION, LDG/AIR GRD FAIL MESSAGE AND REV DISAGREE MESSAGE APPEARED ON EICAS. MESSAGES CLEARED UPON GEAR EXTENSION NEAR EWR. EWR MX REMOVED AND REPLACED NLG AIR/GRD PROXIMITY SWITCH AND PERFORMED OPERATIONAL CHEC
- [SDR C2XA07RI100](https://openairdocs.org/sdr/C2XA07RI100.md): Control Lever · defective · Nov 25, 2007 · N12567 · Emb EMB145LR · Landing Gear Selector
  > FLT 2490 - EWR - CREW REPORTED THAT LANDING GEAR WILL NOT RETRACT AFTER TAKEOFF. CREW PROCEEDED WITH AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED LANDING GEAR CONTROL LEVER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED T
- [SDR C2XA07IA075](https://openairdocs.org/sdr/C2XA07IA075.md): Inverter · inoperative · Mar 24, 2007 · N12567 · Emb EMB145LR · Emergency Lighting
  > MCI - DURING MAINTENANCE INSPECTION AISLE PATH LIGHTS 6, 7 & 8 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06BT056](https://openairdocs.org/sdr/C2XA06BT056.md): Socket · loose · Dec 10, 2006 · N12567 · Emb EMB145LR · Emergency Lighting
  > BTV 2A CHECK FOUND RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP BASE IAW EMB145 AMM 33-50-10. OPS CHECK GOOD.
- [SDR C2XA06IA110](https://openairdocs.org/sdr/C2XA06IA110.md): Battery · discharged · Jul 15, 2006 · N12567 · Emb EMB145LR · Emergency Lighting
  > IAH - FLIGHT 3225, DURING PREFLIGHT INSPECTION, THE CREW REPORTED EMERGENCY AISLE PATH LIGHT WAS INOPERATIVE. MAINTENANCE RECHARGED THE AISLE PATH LIGHTING, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06IA101](https://openairdocs.org/sdr/C2XA06IA101.md): Inverter · inoperative · Jun 18, 2006 · N12567 · Emb EMB145LR · Emergency Lighting
  > STL - DURING MAINTENANCE INSPECTION, THE FORWARD EMERGENCY FLOOR LIGHT STRIPS 2 & 3 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FO
- [SDR C2XA06SH047](https://openairdocs.org/sdr/C2XA06SH047.md): Door Frame · corroded · Apr 19, 2006 · N12567 · Emb EMB145LR · Fuselage Main, Structure
  > SHV - DURING C-CHECK THE AFT LOWER SERVICE DOOR CUTOUT FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC5310-01373. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA06SH046](https://openairdocs.org/sdr/C2XA06SH046.md): Skin · gouged · Apr 19, 2006 · N12567 · Emb EMB145LR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK THE FUSELAGE SKIN AT FRAME 7 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A PATCH REPAIR IAW EMB 145 SRM 53-11-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA04CL119](https://openairdocs.org/sdr/C2XA04CL119.md): Contactor · failed · Nov 20, 2004 · N12567 · Emb EMB145LR · Electrical Power System Wiring
  > CREW REPORTED A BURNING ODOR AND CRACKING SOUND BEHIND THE CAPTAINS SEAT AFTER THE APU FAILED. REPLACED THE APU LINE CONTACTOR. AIRCRAFT RETURNED TO SERVICE.
- [SDR C2XA04TY085](https://openairdocs.org/sdr/C2XA04TY085.md): Sill · corroded · May 23, 2004 · N12567 · Emb EMB145LR · Fuselage Miscellaneous Structure
  > DURING A SCHEDULED 1C INSPECTION THE SERVICE DOOR SILL WAS FOUND CORRODED. MAINT. REMOVED THE REPLACED THE SERVICE DOOR SILL IAW EMB 135/145 SRM 51-40-02 AND IC-2004145/2152. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Next page: https://openairdocs.org/deregistered/N12567-2020-10-20/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 = 'N12567' AND deregistration_id = 'N12567-2020-10-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N12567-2020-10-20/reports

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