# Service difficulty reports: N12160

A list on [N12160](https://openairdocs.org/aircraft/N12160.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 · 69 reports

- [SDR JJBA20260723014](https://openairdocs.org/sdr/JJBA20260723014.md): Lamp · inoperative · Jul 21, 2026 · N12160 · Emb EMB145XR · Emergency Lighting
  > LEFT FWD FUSELAGE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LT FWD FUSELAGE EMERGENCY LIGHT LAMP. OPS CHECK SAT.
- [SDR JJBA20260501030](https://openairdocs.org/sdr/JJBA20260501030.md): Lamp · inoperative · Apr 27, 2026 · N12160 · Emb EMB145XR · Emergency Lighting
  > LH EXT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB ON LH EXT OVERWING EMERGENCY LIGHT. OPS CHECK SAT.
- [SDR JJBA20260126069](https://openairdocs.org/sdr/JJBA20260126069.md): Battery Pack · inoperative · Jan 26, 2026 · N12160 · Emb EMB145XR · Emergency Lighting
  > LEFT EMERGENCY DOOR EXIT IDENTIFIER LIGHT INOPERATIVE.BOTH LT & RT TOP EMERGENCY DOOR LIGHT SIGNS INOPERATIVE. REMOVED, CLEANED CONNECTIONS, AND REINSTALLED EMERGENCY DOOR EXIT SIGN. OPS CHECK FAIL. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY. OPS CHECK SAT.
- [SDR JJBA20251120002](https://openairdocs.org/sdr/JJBA20251120002.md): Computer · corroded · Oct 23, 2025 · N12160 · Emb EMB145XR · Communications System
  > DURING REMOVAL OF NAVIGATION UNIT FOR FOM, CORROSION WAS FOUND ON DIFFERENT POINTS OF THE COMPUTER. REPLACEMENT WAS PERFORMED. PERFORM VOR/ILS TEST. OPS CHECK SAT.
- [SDR JJBA20251120105](https://openairdocs.org/sdr/JJBA20251120105.md): Stringer Splice · corroded · Oct 16, 2025 · N12160 · Emb EMB145XR · Fuselage Main, Longeron/Stringer
  > PROFILE SPLICE FOUND WITH CORROSION IN BATHROOM UNDER FLOOR AREA LOCATION FR 60-61 (STA X=20793.0) STGR 17L. REMOVED AND REPLACED STGR SPLICE 17L BETWEEN FR 60-61
- [SDR JJBA20250804131](https://openairdocs.org/sdr/JJBA20250804131.md): Light · inoperative · Jul 31, 2025 · N12160 · Emb EMB145XR · Emergency Lighting
  > RH OVERWING EMERGENCY LIGHT INOPERATIVE. FOUND LIGHT ASSEMBLY NUTPLATE TO BE BROKEN. REMOVED AND REPLACED RH OVERWING EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT.
- [SDR JJBA20241223047](https://openairdocs.org/sdr/JJBA20241223047.md): Inverter · inoperative · Dec 19, 2024 · N12160 · Emb EMB145XR · Emergency Lighting
  > RH EMERGENCY EXIT ROW AFT EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EXIT MARKING ASSEMBLY. OPS CHECK FAILED. REINSTALLED ORIGINAL ASSEMBLY AND REMOVED AND REPLACED #5. OPS CHECK SAT.
- [SDR JJBA20230929047](https://openairdocs.org/sdr/JJBA20230929047.md): Lamp · inoperative · Sep 22, 2023 · N12160 · Emb EMB145XR · Emergency Lighting
  > RH WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RH WING EMERGENCY LIGHT. OPS CHECK SAT
- [SDR JJBA20230920021](https://openairdocs.org/sdr/JJBA20230920021.md): Battery Pack · inoperative · Sep 19, 2023 · N12160 · Emb EMB145XR · Emergency Lighting
  > EMERGENCY LIGHT BATTERIES DEAD. REMOVED AND REPLACED #1 AND #2 EMERGENCY BATTERY, RECHARGED #3 AND #4 EMERGENCY BATTERIES WITH 28V ESS DC BUSS AND OPS CHECKED. OPS CHECK SAT. POSITION 1: PN: ABS-2013-1A SN 51991 TSN 4196.26 CSN 3717
- [SDR JJBA20230919017](https://openairdocs.org/sdr/JJBA20230919017.md): Lamp · inoperative · Sep 17, 2023 · N12160 · Emb EMB145XR · Emergency Lighting
  > LH EXTERIOR FWD EMERGENCY LIGHT IS OUT. REMOVED AND REPLACED LH EXTERIOR FWD EMERGENCY LIGHT. OPS CHECK SAT
- [SDR JJBA20230320023](https://openairdocs.org/sdr/JJBA20230320023.md): Pump · inoperative · Mar 16, 2023 · N12160 · Emb EMB145XR · Hydraulic System, Main
  > HYD 1 SYSTEM LOW QUANTITY ON EICAS THEN 10-15 MINUTES LATER HYD 1 SYSTEM FAIL ON EICAS. REMOVED AND REPLACED HYDRAULIC SYSTEM #1 ELECTRIC MOTOR DRIVEN PUMP. BLED AIR FROM HYDRAULIC SYSTEM 1. OPS CHECK SAT. REMOVED AND REPLACED LH ENGINE DRIVEN HYDRAULIC PUMP.
- [SDR JJBA20221129027](https://openairdocs.org/sdr/JJBA20221129027.md): Duct · leaking · Nov 29, 2022 · N12160 · Emb EMB145XR · Pneumatic Distribution System
  > BLEED 1 LEAK IN FLIGHT. INSPECTED AND FOUND BLEED LEAK AT DUCT BETWEEN PRECOOLER AND BLEED VALVE, R/R DUCT AND Y DUCT L/H PYLON. PERFORMED HIGH POWER RUNS FOR ENG LEAK CHECKS, NO BLD 1 LEAK CHECK NOTED, OPS CHECK SAT LEAK CHECK SAT
- [SDR JJBA20220512040](https://openairdocs.org/sdr/JJBA20220512040.md): None · none · May 12, 2022 · N12160 · Emb EMB145XR · Fuselage Structure (General)
  > UPPER AFT FUSELAGE EXTERIOR - FUSELAGE SKIN CRACKED STARTING AT 2 EA FASTENER HOELS ON FR75 STGR 2R. REPAIRED CRACK UPPER AFT FUSELAGE EXTERIOR SKIN AT FR75 BETWEEN STGR 2R.
- [SDR JJBA20220504041](https://openairdocs.org/sdr/JJBA20220504041.md): None · none · May 4, 2022 · N12160 · Emb EMB145XR · Fuselage Structure (General)
  > MAIN CABIN AFT WET AREA CENTER OMEGA BEAM HAS CORROSION AROUND NUTPLATE HOLE AT FR59-FR60 Y=0. REPAIRED CORROSION AROUND 2 EACH NUTPLATE HOLES BY CUTOUT AND INSTALL OF 2 EA DOUBLERS AT DAMAGED AREA CENTER OMEGA BEAM AT FR59-FR60 AT Y=0
- [SDR JJBA20220418042](https://openairdocs.org/sdr/JJBA20220418042.md): None · none · Apr 18, 2022 · N12160 · Emb EMB145XR · Fuselage Structure (General)
  > CORROSION ON RH GUSSET BETWEEN FR22-FR23 Y.00. REMOVED AND REPLACED RH GUSSET BETWEEN FR 19 - FR23 Y.00
- [SDR JJBA20211201003](https://openairdocs.org/sdr/JJBA20211201003.md): Pump · inoperative · Dec 1, 2021 · N12160 · Emb EMB145XR · Hydraulic Pump (Electric/Engine), Main
  > E1 HYD PUMP FAIL ON EICAS AFTER ROTATION. REMOVED AND REPLACED E1 HYD PUMP. DURING BLEED FOUND BAD O-RING ON HYD PRESSURE LINE FROM SYS 1 ELE HYD PUMP. REMOVED AND REPLACED O-RING. NO LEAKS NOTED. OPS AND LEAK CHECK SAT.
- [SDR JJBA20210927038](https://openairdocs.org/sdr/JJBA20210927038.md): Battery Pack · inoperative · Sep 27, 2021 · N12160 · Emb EMB145XR · Emergency Lighting
  > INTERIOR EMERGENCY EXIT LIGHTS OVER BOTH WINGS INOPERATIVE. REMOVED AND REPLACED #3 BATT POWER SUPPLY. OPS CHECK SAT.
- [SDR JJBA20210416029](https://openairdocs.org/sdr/JJBA20210416029.md): Handle · loose · Apr 16, 2021 · N12160 · Emb EMB145XR · Emergency Exits
  > ROW 18A EXIT PANEL OVER TOP HANDLE LOOSE. RESECURED OVER WING EXIT DOOR OPEN AND CLOSE HANDLE ACCESS PANEL APPLIED NEW VELCRO. NO FURTHER DEFECTS NOTED.
- [SDR JJBA20210319002](https://openairdocs.org/sdr/JJBA20210319002.md): Armrest · cracked · Mar 19, 2021 · N12160 · Emb EMB145XR · Passenger Compartment Equipment
  > CRACK FOUND ON PAX SEAT ARMREST AT 3A, 5A, 8A, 9A AND 21A. REMOVED AND REPLACED SEAT 3A, 5A, 8A, 9A, AND 21A
- [SDR JJBA20210115040](https://openairdocs.org/sdr/JJBA20210115040.md): Light · inoperative · Jan 15, 2021 · N12160 · Emb EMB145XR · Emergency Lighting
  > RT FWD WING TO FUSELAGE EMERGENCY LIGHT INOPERATIVE. R &R RT FWD WING TO FUSELAGE EMERGENCY LIGHT. OPERATIONS CHECK SATISFACTORY.
- [SDR JJBA20201031042](https://openairdocs.org/sdr/JJBA20201031042.md): Light · inoperative · Oct 31, 2020 · N12160 · Emb EMB145XR · Emergency Lighting
  > EXTERNAL LEFT HAND FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT HAND FWD EMERGENCY LIGHT. OPERATIONS CHECK SATISFACTORY.
- [SDR JJBA202009086002](https://openairdocs.org/sdr/JJBA202009086002.md): Cover · dislodged · Sep 6, 2020 · N12160 · Emb EMB145XR · Emergency Exits
  > EMERGENCY EXIT COVER HANDLE AT 18A HANGING DOWN. RE-SECURED VELCRO FOR EMERGENCY EXIT COVER HANDLE.
- [SDR JJBA202009084001](https://openairdocs.org/sdr/JJBA202009084001.md): Trim Panel · unsecure · Sep 4, 2020 · N12160 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > EXIT ROW 18A WINDOW TRIM NOT SECURE. RE-SECURED TRIM ON THE LT OVER WING ESCAPE HATCH, NO DEFECTS NOTED.
- [SDR JJBA20190630020](https://openairdocs.org/sdr/JJBA20190630020.md): Controller · inoperative · Jun 30, 2019 · N12160 · Emb EMB145XR · Cabin Pressure Controller
  > PRESSURIZATION FAILED IN AUTO MODE DURING CLIMB OUT, PRESS MANUAL MODE WORKED FINE. R&R PNEUMATIC OUTFLOW VALVE. OPS CHECK FAILED (PN 2099L011100 SN 02211)R&R ELECTROPNEUMATIC OUTFLOW VALE (PN 2097K011100 SN 00407). OPS CHECK FAILED. R&R DIGITAL AUTO CONTROLLE
- [SDR JJBA201904121009](https://openairdocs.org/sdr/JJBA201904121009.md): Sleeve · disconnected · Apr 11, 2019 · N12160 · Emb EMB145XR · Air Distribution System
  > CABIN PRESSURIZATION LEAK IN FLIGHT - AIRCRAFT DEPRESSURIZED. FOUND PACK 2 ACM DUCT SLEEVE DISCONNECTED & TORN, R&R SLEEVE. PERFORMED OPS/LEAK CHECK OF COOLING PACK SYSTEM & PRESSURIZATION CONTROL SYSTEM. OPS AND LEAK CHECK SAT.
- [SDR JJBA20190119033](https://openairdocs.org/sdr/JJBA20190119033.md): Door · cracked · Jan 19, 2019 · N12160 · Emb EMB145XR · Engine Thrust Reverser
  > LT UPPER THRUST REVERSER DOOR FORWARD FLANGE CRACKED. REPAIRED LT UPPER THRUST REVERSER DOOR FORWARD FLANGE.
- [SDR JJBA20190119032](https://openairdocs.org/sdr/JJBA20190119032.md): Angle · cracked · Jan 19, 2019 · N12160 · Emb EMB145XR · Landing Gear System
  > NLG UP-LOCK LEFT AND RIGHT ANGLE CORNERS CRACKED. REMOVED AND REPLACED NLG UP-LOCK LEFT AND RIGHT ANGLES.
- [SDR JJBA20190117034](https://openairdocs.org/sdr/JJBA20190117034.md): Skin · dented · Jan 17, 2019 · N12160 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT REPAIR OF DENT AFTER 5,000 FLIGHT CYCLES AT AREA BETWEEN FR 19 AND 20 AND STR 11L AND 12L. PERFORMED PERMANENT REPAIR OF THE 2 EA DENTS ON THE LT EXTERNAL SKIN AT FRAME 19-20 STR 11L-12L
- [SDR JJBA20190117031](https://openairdocs.org/sdr/JJBA20190117031.md): Crossbeam · cracked · Jan 17, 2019 · N12160 · Emb EMB145XR · Landing Gear Retraction/Extension System
  > NLG UP-LOCK CROSSBEAM CRACKED. REMOVED AND INSTALLED NEW NLG UP-LOCK CROSSBEAM.
- [SDR JJBA20190115030](https://openairdocs.org/sdr/JJBA20190115030.md): Crossbeam · cracked · Jan 15, 2019 · N12160 · Emb EMB145XR · Landing Gear Retraction/Extension System
  > NLG UP-LOCK AFT CROSSBEAM CRACKED. REMOVED AND REPLACED NLG UP-LOCK AFT CROSSBEAM.
- [SDR JJBA20190114029](https://openairdocs.org/sdr/JJBA20190114029.md): Beam · corroded · Jan 14, 2019 · N12160 · Emb EMB145XR · Fuselage Main, Structure
  > SERVICE DOOR THRESHOLD BEAM CORRODED AS MARKED. INSTALLED NEW SERVICE DOOR THRESHOLD BEAM.
- [SDR JJBA20190111028](https://openairdocs.org/sdr/JJBA20190111028.md): Structure · cracked · Jan 11, 2019 · N12160 · Emb EMB145XR · Wing Miscellaneous Structure
  > NR 1 LT LEADING EDGE ATTACH FLANGE IS CRACKED. MARKED. TRIMMED AND REMOVED DAMAGE ON NR 1 LEADING EDGE ATTACH FLANGE. PERFORMED HFEC INSPECTION ON NR 1 LT LEADING EDGE ATTACH FLANGE BLENDED AREA. NO DEFECTS FOUND. TREATED AND PRIMED BLENDED AREA ON NR 1 LT LEA
- [SDR JJBA20190108026](https://openairdocs.org/sdr/JJBA20190108026.md): Door Sill · corroded · Jan 8, 2019 · N12160 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > RT FLOOR SILL AFTER 48 TO FR 52 CORRODED AS MARKED. INSTALLED RT FLOOR SILL AT FR 48 TO FR 52.
- [SDR JJBA20190108023](https://openairdocs.org/sdr/JJBA20190108023.md): Fitting · cracked · Jan 8, 2019 · N12160 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > FR 62 STR 6-7 SHEAR CLIP IS CRACKED. INSTALLED NEW SHEAR CLIP ON FR 62 STR 6-7R.
- [SDR JJBA20190107022](https://openairdocs.org/sdr/JJBA20190107022.md): Rib · cracked · Jan 7, 2019 · N12160 · Emb EMB145XR · Fuselage Main, Structure
  > LT GEAR WALL AFT LOWER RIB CRACKED. REMOVED AND REPLACED LT GEAR WALL AFT LOWER RIB.
- [SDR JJBA20190107021](https://openairdocs.org/sdr/JJBA20190107021.md): Bracket · cracked · Jan 7, 2019 · N12160 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > FR 60 STRG 4-5 R TORSION BAR BRACKET IS CRACKED. REMOVED AND REPLACED TORSION BAR BRACKET FROM FR 60 BETWEEN STR4R - STR5R.
- [SDR JJBA201812107005](https://openairdocs.org/sdr/JJBA201812107005.md): Actuator · inoperative · Dec 7, 2018 · N12160 · Emb EMB145XR · Elevator Control System
  > MAIN PITCH TRIM INOPERATIVE. R&R HORIZONTAL STAB ACTUATOR. OPS CHECK SAT. INSTALLED AND SEALED PANELS 324EL, 321EL, 325LR, 321DR, 321CL, 333DC, 321AL. NO DEFECTS NOTED AT THIS TIME.
- [SDR JJBA2018091817011](https://openairdocs.org/sdr/JJBA2018091817011.md): Trim Panel · out of adjust · Sep 17, 2018 · N12160 · Emb EMB145XR · Passenger Compartment Equipment
  > CAPTAIN SIDE OVER WING EMERGENACY EXIT APPEARS UNSEATED. ADJUSTED SIDE WALL TRIM. NO DEFECTS NOTED AT THIS TIME. CAPT EMERGENCY WINDOW SECURED
- [SDR ASOA20160421036](https://openairdocs.org/sdr/ASOA20160421036.md): Battery Pack · discharged · Apr 21, 2016 · N12160 · Emb EMB145XR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION THE COCKPIT EMERGENCY LIGHT AND FWD EMERGENCY LIGHT MARKER WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 1 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO
- [SDR ASOA20140315025](https://openairdocs.org/sdr/ASOA20140315025.md): Check Valve · leaking · Mar 15, 2014 · N12160 · Emb EMB145XR · Aircraft Fuel Distribution System
  > THE CREW REPORTED FUEL LEAK IN RT WING FUEL VENT. LONG VAPOR TRAILS SPOTTED BY TOWER AND PASSENGER WHILE THE ACFT WAS IN CLIMB ATTITUDE. MAINTENANCE INSPECTED AND REPLACED THE RT WING FUEL CHECK VALVE. LEAK CHECKED GOOD. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR ASOA20131105195](https://openairdocs.org/sdr/ASOA20131105195.md): Skin · cracked · Nov 5, 2013 · N12160 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING A-CHECK INSPECTION, THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED FRAME 77 JUST ABOVE STRINGER 6L. MX REMOVED THE DAMAGE AND INSTALLED AN OVERSIZED RIVET, AND ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130910167H](https://openairdocs.org/sdr/ASOA20130910167H.md): Skin · cracked · Sep 10, 2013 · N12160 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING 2A INSPECTION, AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED IN 2 PLACES AT A RIVET ON FR 78 BELOW STR06L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR IAW APPROVED TECH DISPOSITION ETD2013-145-038298, AND THE ACFT WAS APPROVED FOR RETURN TO SERVI
- [SDR ASOA20130910166](https://openairdocs.org/sdr/ASOA20130910166.md): Skin · cracked · Sep 10, 2013 · N12160 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING 2A INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FR78 BELOW STR 6R. MX REMOVED THE DAMAGE, AND PERFORMED A BUSHING REPAIR IAW APPROVED TECHNICAL DISPOSITION ETD2013-145-038298, AND THE ACFT WAS APPROVED FOR RETURN TO SERVI
- [SDR ASOA20130910165](https://openairdocs.org/sdr/ASOA20130910165.md): Skin · cracked · Sep 10, 2013 · N12160 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING 2A INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FR 77, BELOW STR 3R. MX WAS ABLE TO REMOVE THE CRACK AND INSTALL AN OVERSIZED RIVET, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130327032](https://openairdocs.org/sdr/ASOA20130327032.md): Connector · loose · Mar 27, 2013 · N12160 · Emb EMB145XR · Light System Wiring
  > DURING MX INSPECTION THE AFT SIDE OF EMERGENCY LIGHT AT ROW 12 WAS FOUND INOPERATIVE. MX FOUND AND REPAIRED LOOSE CONNECTION WITH OPS CHECKS SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120518076](https://openairdocs.org/sdr/ASOA20120518076.md): Inverter · inoperative · May 18, 2012 · N12160 · Emb EMB145XR · Emergency Lighting
  > DURING MX INSPECTION THE AFT EXIT ROW CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX R & R THE AFFECTED EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11RI173](https://openairdocs.org/sdr/C2XA11RI173.md): Unknown · smoke · Oct 30, 2011 · N12160 · Emb EMB145XR · Air Distribution System
  > FLT 4379 EWR CREW REPORTED SMOKE IN COCKPIT DURING TAXI ASSOCIATED WITH ADVANCEMENT OF THRUST ON ENGINE NR 2 AND PERFORMED GATE RETURN. EWR MX PERFORMED ENGINE RUNS WITH PACKS OPERATING AND NO SMOKE OR SMELL NOTED. EWR MX SUSPECTS DE-ICE FLUID MAY HAVE CAUSE
- [SDR C2XA11TY153](https://openairdocs.org/sdr/C2XA11TY153.md): Metering Unit · inoperative · Oct 5, 2011 · N12160 · Emb EMB145XR · Fuel Controlling System
  > ACFT HAD ENGINE NR 1 UNCOMMANDED SHUTDOWN ON APPROACH. MAINTENANCE REMOVED AND REPLACED NR 1 FPMU. OPS AND LEAK CHECKED GOOD AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA11IA230](https://openairdocs.org/sdr/C2XA11IA230.md): Fmu · malfunctioned · Oct 5, 2011 · N12160 · Emb EMB145XR · Fuel Controlling System
  > RAP - FLIGHT 6158, ON APPROACH TO RAP FROM DEN THE CREW REPORTED A NUMBER ONE ENGINE UNCOMMANDED SHUTDOWN. THE AIRCRAFT LANDED AT RAP WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE FPMU, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND
- [SDR C2XA11CL140](https://openairdocs.org/sdr/C2XA11CL140.md): Inverter · inoperative · Jun 3, 2011 · N12160 · Emb EMB145XR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE LOWER FORWARD EMERGENCY EXIT LIGHT AT SEAT 12A WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 5 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Next page: https://openairdocs.org/aircraft/N12160/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 = 'N12160' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N12160/reports

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