# Service difficulty reports: N13124

A list on [N13124](https://openairdocs.org/aircraft/N13124.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 3 · 106 reports

- [SDR JJBA20260220057](https://openairdocs.org/sdr/JJBA20260220057.md): Wire · broken · Feb 18, 2026 · N13124 · Emb EMB145XR · Light System Wiring
  > MCD EXTERNAL EMERG LIGHT INOPERATIVE. FOUND BROKEN WIRE BEFORE SPLICE SP7426 REPAIRED WIRE. R/R MCD EXT EMER LIGHT ASSY OPS CHECK SAT.
- [SDR JJBA20260115025](https://openairdocs.org/sdr/JJBA20260115025.md): Engine · failed · Jan 12, 2026 · N13124 · Emb EMB145XR · Engine (Turbine/Turboprop)
  > ON CLIMBOUT HEARD A BIG BANG FROM NR 1 ENGINE AND NR 1 ENGINE SHUTDOWN. ALL INDICATORS WERE IN THE NORMAL ON TAKE OFF. DID ATTEMPT ANOTHER ENGINE RESTART IN FLIGHT WITH NO SUCCESS. NOISE OCCURRED AT 9000 AND THEY LEVELED OFF AT 11000. PERFORMED BORESCOPE INSPE
- [SDR JJBA20250707001](https://openairdocs.org/sdr/JJBA20250707001.md): Lamp · inoperative · Jul 4, 2025 · N13124 · Emb EMB145XR · Emergency Lighting
  > MCD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MCD EMERGENCY LIGHT LAMP. OPS CHECK SAT.
- [SDR JJBA20250127021](https://openairdocs.org/sdr/JJBA20250127021.md): Lamp · inoperative · Jan 24, 2025 · N13124 · Emb EMB145XR · Emergency Lighting
  > RH OVERWING EMERGENCY LIGHT OUT. REMOVED AND REPLACED BULB. OPS CHECK SAT.
- [SDR JJBA20230317024](https://openairdocs.org/sdr/JJBA20230317024.md): Unknown · unknown · Mar 14, 2023 · N13124 · Emb EMB145XR · Standard Practices/Structures
  > RH WING BOTTOM LATERAL FAIRING ANGLE BRACKETS CRACKED AT FR46, FR48, FR48.5, FR50 (BOTH BRACKETS). COMPLETED THE REPAIR OF THE RH WING BOTTOM LATERAL FAIRING ANGLE BRACKETS.
- [SDR JJBA20230313017](https://openairdocs.org/sdr/JJBA20230313017.md): Unknown · unknown · Mar 9, 2023 · N13124 · Emb EMB145XR · Standard Practices/Structures
  > CORROSION ON FLOOR BRACKET AT FS 21 AT SERVICE DOOR. REMOVED AND REPLACED FLOOR BRACKET AT FS 21 AT SERVICE DOOR.
- [SDR JJBA20220919022](https://openairdocs.org/sdr/JJBA20220919022.md): Lamp · inoperative · Sep 16, 2022 · N13124 · Emb EMB145XR · Emergency Lighting
  > SEAT 18C&D OVER WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED SEAT 18CD OVER WING EMERGENCY LIGHT LAMP. OPS CHECK GOOD
- [SDR JJBA20220808001](https://openairdocs.org/sdr/JJBA20220808001.md): Battery Pack · inoperative · Aug 3, 2022 · N13124 · Emb EMB145XR · Emergency Lighting
  > RH EMERGENCY EXIT LOWER LIGHT INOPERATIVE. REMOVED AND REPLACED RH EMERGENCY EXIT LOWER LIGHT. OPS CHECK FAILED. REMOVED AND REPLACED EMERGENCY BATTERY #3. OPS CHECK SAT
- [SDR JJBA20220410013](https://openairdocs.org/sdr/JJBA20220410013.md): Battery Pack · inoperative · Apr 10, 2022 · N13124 · Emb EMB145XR · Emergency Lighting
  > EMERGENCY LIGHT NEAR MAIN DOOR INOPERATIVE. REMOVED AND REPLACED #1 EMERGENCY BATTERY. OPS CHECK SAT AT THIS TIME
- [SDR JJBA202201186020](https://openairdocs.org/sdr/JJBA202201186020.md): B-Nut · loose · Jan 16, 2022 · N13124 · Emb EMB145XR · Hydraulic System, Main
  > HYD SYS 1 FAIL ON EICAS. LH NLG DOOR ACTUATOR HOSE B NUT LOOSE AND LEAKING - RESECURED. REPLENISHED #1 HYD SYSTEM. LEAK AND OPS CHECK SAT.
- [SDR JJBA20211004003](https://openairdocs.org/sdr/JJBA20211004003.md): None · none · Oct 4, 2021 · N13124 · Emb EMB145XR · Flight Control System
  > SUPPLEMENTAL INFORMATION: IN PREPARATION FOR OCF, PILOT FELT RATCHETING IN AILERON CONTROL. FLIGHT NEVER OCCURRED. DURING TROUBLESHOOTING, MECHANIC CYCLED THE SYSTEM AND HEARD A POP. INVESTIGATED AND FOUND CABLE HAD COME APART. MISROUTING AROUND CABLE GUARD SU
- [SDR JJBA20210922016](https://openairdocs.org/sdr/JJBA20210922016.md): None · none · Sep 22, 2021 · N13124 · Emb EMB145XR · Fuselage Main, Structure
  > CENTER FUSE IV, UNDER FLOOR, FRAME 59 CORRODED BTW STR 21R-21L. FR 59 SEGMENT BTW STR 20R-20L CUT OUT SPLICE REPAIR. FR 59 SEGMENT BTW STR 20R-20L. 2 SPLICE REPAIRS FABRICATED. NO CORROSION FOUND. CF IV, UNDERFLOOR FR 59 BTW STR 20L-20R REPAIRED WIT 2 SPLICES.
- [SDR JJBA20210922034](https://openairdocs.org/sdr/JJBA20210922034.md): None · none · Sep 22, 2021 · N13124 · Emb EMB145XR · Standard Practices/Structures
  > CORROSION FOUND ON CENTER AISLE LH OMEGA BEAM LOCATED BETWEEN FR 23- FR 29. REMOVED AND REPLACED LH OMEGA BEAM, LOCATED BETWEEN FR 23-FR29
- [SDR JJBA2021092200021](https://openairdocs.org/sdr/JJBA2021092200021.md): None · none · Sep 22, 2021 · N13124 · Emb EMB145XR · Fuselage Structure (General)
  > THE PASSENGER FWD CABIN LH FLOOR OMEGA DOUBLER HAS CORROSION ON THE FWD SURFACE BETWEEN FR 14 TO FR 18. REMOVED AND REPLACED DIGITAL PLATE ON PASSENGER FWD CABIN LH FLOOR BETWEEN FR 14 TO FR 18.
- [SDR JJBA20210922020](https://openairdocs.org/sdr/JJBA20210922020.md): None · none · Sep 22, 2021 · N13124 · Emb EMB145XR · Fuselage Structure (General)
  > CORROSION AT MULTIPLE LOCATONS FOUND ON RH CENTER AISLE LONGITUDINAL BEAM LOCATED BETWEEN FR29-FR36 Y.00+8. REMOVED AND REPLACED BEAM ASSEMBLY ON RH CENTER AISLE LOCATED BETWEEN FR29-FR36 Y.00+8.
- [SDR JJBA20210922019](https://openairdocs.org/sdr/JJBA20210922019.md): None · none · Sep 22, 2021 · N13124 · Emb EMB145XR · Cabin Equipment/Furnishings
  > CORROSION NOTED AT ELT ANTENNA MOUNTING SURFACE. EVALUATED CORROSION AT ELT ANTENNA DOUBLER AND FOUND OUT OF LIMITS. REMOVED AND REPLACED ELT ANTENNA DOUBLER.
- [SDR JJBA20210922018](https://openairdocs.org/sdr/JJBA20210922018.md): None · none · Sep 22, 2021 · N13124 · Emb EMB145XR · Doppler System
  > AFTER REMOVAL OF UPPER TCAS ANTENNA, INSPECTED AIRCRAFT SKIN FOUND SEVERAL SCRATCHES AT MATING SURFACE. REMOVED SCRATCHES ON UPPER TCAS ATTENNA DOUBLER BY BLENDING, MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED UPPER TCAS ANTENNA DOUBLER
- [SDR JJBA20210922017](https://openairdocs.org/sdr/JJBA20210922017.md): None · none · Sep 22, 2021 · N13124 · Emb EMB145XR · Cargo/Baggage Doors
  > CARGO DOOR INTERNAL STRUCTURE LOWER WEB HAS MULTIPLE AREAS OF SCREW INDENTION DAMAGE. REMOVED AND REPLACED AFT CARGO DOOR INNER SKIN WEB.
- [SDR JJBA20210922015](https://openairdocs.org/sdr/JJBA20210922015.md): None · none · Sep 22, 2021 · N13124 · Emb EMB145XR · Fuselage Main, Bulkhead
  > MAIN CABIN - RH O/B FLOOR BOARD SUPPORT STRUCTURE HAS CORROSION MULTIPLE LOCATIONS BETWEEN FR 40 TO FR 41 RH. REMOVED AND REPLACED SILL IN MAIN CABIN - RH OB FLOOR BOARD SUPPORT STRUCTURE BETWEEN FR 40 TO FR 41 RH
- [SDR JJBA20210922014](https://openairdocs.org/sdr/JJBA20210922014.md): None · none · Sep 22, 2021 · N13124 · Emb EMB145XR · Fuselage Structure (General)
  > AFT CARGO COMPARTMENT AT DOOR CUT-OUT LOWER FRAME HAS 3 SCREW HOLES SHOWING SIGNS OF CORROSION BETWEEN FRAME 65 - 68. REMOVED AND REPLACED AFT CARGO COMPARTMENT, DOOR CUT-OUT LOWER FRAME BEAM BETWEEN FRAME 65-68
- [SDR JJBA20210922013](https://openairdocs.org/sdr/JJBA20210922013.md): None · none · Sep 22, 2021 · N13124 · Emb EMB145XR · Fuselage Structure (General)
  > THE PASSENGER ENTRY DOOR WAY FWD FRAME LOWER SPLICE TO FLOOR BEAM IS CRACKED. REMOVED AND REPLACED LOWER REINFORCEMENT SPLICE TO FLOOR BEAM PASSENGER ENTRY DOOR WAY FWD FRAME.
- [SDR JJBA202109083012](https://openairdocs.org/sdr/JJBA202109083012.md): Floor Support · corroded · Sep 3, 2021 · N13124 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > THE PASSENGER CABIN RH SIDE OMEGA FLOOR BEAM DOUBLER HAS CORROSION JUST FWD OF FR19 UPPER SURFACE. BLENDED CORROSION ON RH OMEGA BEAM JUST FORWARD OF FRAME 19. FOUND TO HAVE 100% MATERIAL LOSS AND OUT OF ALLOWABLE LIMITS. CUT OUT DAMAGE ON RH OMEGA BEAM JUST F
- [SDR JJBA20210822011](https://openairdocs.org/sdr/JJBA20210822011.md): Frame · cracked · Aug 22, 2021 · N13124 · Emb EMB145XR · Fuselage Main, Frame
  > DIRECTLY UNDER CAPTAINS DV WINDOW CUTOUT FRAME 10 CRACKED. REMOVED CHANNEL UNDER CAPTAINS DV WINDOW CUTOUT AT FR10. LOCATED AND DRILLED NEW CHANNEL UNDER CAPTAINS DV WINDOW CUTOUT AT FR10. TREATED AND PRIMED ALL HOLES. INSTALLED NEW CHANNEL UNDER CAPTAINS DV W
- [SDR JJBA20210822010](https://openairdocs.org/sdr/JJBA20210822010.md): Support · corroded · Aug 22, 2021 · N13124 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CARGO DOOR CUTOUT INTERNAL SUPPORT STRUCTURE CORRODED AT FWD LOWER EDGE. REMOVED LOWER PART OF SHEAR CLIP. LOCTED AND DRILLED NEW LOWER END OF SHEAR CLIP. INSTALLED LOWER PART OF SHEAR CLIP. INSTALLED DOOR CLIP. INSTALLED NEW T PROFILE. TOPCOATED FASTENERS ON
- [SDR JJBA20210822009](https://openairdocs.org/sdr/JJBA20210822009.md): Support Beam · cracked · Aug 22, 2021 · N13124 · Emb EMB145XR · Passenger/Crew Doors
  > PASSENGER DOOR UPPER AFT REINFORCING SUPPORT BEAM CRACKED AT FR19 AND STGR 3L. REMOVED BEAM AT FR19, LEFT STRINGER 3. LOCATED, DRILLED, DEBURRED NEW SUPPORT BEAM. TREATED AND PRIMED FASTENER HOLES. INSTALLED PASSENGER DOOR UPPER AFT REINFORCING SUPPORT BEAM. R
- [SDR JJBA20210822008](https://openairdocs.org/sdr/JJBA20210822008.md): Doubler · damaged · Aug 22, 2021 · N13124 · Emb EMB145XR · Fuselage Main, Bulkhead
  > LH - FR 14 BETWEEN STGR LH7 AND STGR LH8 - LH BULKHEAD - SUPPORT DOUBLER - HOLE ELONGATED. REMOVED EXISTING DOUBLER. FABRICATED REPAIR DOUBLER. CLEANED, TREATED AND APPLIED PRIMER TO REPAIR AREA AND DOUBLER. INSTALLED REPAIR DOUBLER. RESTORED FINISH.
- [SDR JJBA2021090822007](https://openairdocs.org/sdr/JJBA2021090822007.md): Skin · cracked · Aug 22, 2021 · N13124 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > EXTERNAL SKIN CRACKED AT FO'S DV WINDOW CUTOUT AFT UPPER CORNER. CUTOUT DAMAGED AREA AND REMOVED ALL EXISTING FASTENERS IN REPAIR AREA. TREATED AND PRIMED FUSELAGE SKIN. FABRICATED, LOCATED AND DRILLED REPAIR FOR FUSELAGE SKIN ABOVE FO'S DV WINDOW. TREATED AND
- [SDR JJBA2021090822006](https://openairdocs.org/sdr/JJBA2021090822006.md): Frame · cracked · Aug 22, 2021 · N13124 · Emb EMB145XR · Fuselage Main, Frame
  > DIRECTLY UNDER FO'S DV WINDOW CUTOUT FRAME 10 CRACKED. REMOVED CHANNEL UNDER FO'S DV WINDOW CUTOUT AT FR10. LOCATED AND DRILLED NEW CHANNEL UNDER FO'S DV WINDOW CUTOUT AT FR10. TREATED AND PRIMED ALL HOLES. INSTALLED NEW CHANNEL UNDER FO'S DV WINDOW CUTOUT AT
- [SDR JJBA2021090885005](https://openairdocs.org/sdr/JJBA2021090885005.md): Attach Fitting · corroded · Aug 5, 2021 · N13124 · Emb EMB145XR · Wing, Control Surface Attach Fittings
  > LEFT WING AILERON ATTACHMENT LUGS "4" EACH HAVE LIGHT SURFACE CORROSION EXPOSED AND BARE METAL. BLENDED CORROSION 4 EACH LUGS.
- [SDR JJBA20210729004](https://openairdocs.org/sdr/JJBA20210729004.md): Attach Fitting · corroded · Jul 29, 2021 · N13124 · Emb EMB145XR · Wing, Control Surface Attach Fittings
  > RIGHT WING AILERON ATTACHMENT LUGS "4" EACH HAVE LIGHT SURFACE CORROSION EXPOSED AND BARE METAL. BLENDED CORROSION 4 EACH AREAS ON RIGHT AILERON LUGS UPPER SURFACE.
- [SDR JJBA20210303001](https://openairdocs.org/sdr/JJBA20210303001.md): Controller · inoperative · Mar 3, 2021 · N13124 · Emb EMB145XR · Autopilot Computer
  > AUTOPILOT AND YAW DAMP WOULD NOT ENGAGE AFTER TAKE OFF, NO VERTICAL MODE AVAILABLE. NO LATERAL MODE AVAILABLE. PERFORMED AP FUNCTIONAL CHECK. OPS CHECK SAT. NO DEFECTS NOTED. R&R FLIGHT GUIDANCE CONTROLLER (GC-550). OPS CHECK SAT.
- [SDR JJBA20201230032](https://openairdocs.org/sdr/JJBA20201230032.md): Switch · failed · Dec 30, 2020 · N13124 · Emb EMB145XR · Elevator Tab Control System
  > PITCH TRIM MAIN INOPERATIVE IN FLIGHT. REMOVED AND REPLACED FO YOKE PITCH TRIM SWITCH. OPERATIONS CHECK GOOD.
- [SDR JJBA20201124022](https://openairdocs.org/sdr/JJBA20201124022.md): Skin · cracked · Nov 24, 2020 · N13124 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > CRACK ON REAR FUSE 1 LOWER SKIN, AT DRAIN MAST BETWEEN FR 75 JUNCTION 07 AND BETWEEN STR 21L-21R. REAR FUSELAGE 1 BETWEEN FR 75 & JUNCTION 07 BETWEEN STR 21L &21R OUTER SKIN, CUT OUT PERFORMED TO REMOVE DAMAGE FOR ENGINEERING REVIEW. REAR FUSELAGE 1 BETWEEN
- [SDR JJBA20201124021](https://openairdocs.org/sdr/JJBA20201124021.md): Shear Tie · cracked · Nov 24, 2020 · N13124 · Emb EMB145XR · Fuselage Internal Mounting Structure
  > REAR FUSELAGE 1, FRAME 75A LOWER LEG CRACKED. REAR FUSELAGE 1 FRAME 75A LOWER SECTION LOWER LEG REPAIRED.
- [SDR JJBA20201121020](https://openairdocs.org/sdr/JJBA20201121020.md): Skin · dented · Nov 21, 2020 · N13124 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DENT ON LT CENTER FUSE 1, BETWEEN FR 20-21 AND BETWEEN STR 13L-14L. LT CENTER FUSE 1, BETWEEN FR 20-21 AND BETWEEN STR 13L-14L, SKIN REPAIRED.
- [SDR JJBA20201116019](https://openairdocs.org/sdr/JJBA20201116019.md): Skin · deformed · Nov 16, 2020 · N13124 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > FWD FUSELAGE LT SIDE, THE SKIN IS DEFORMED AROUND THE TAT PROBE. ON FWD FUSELAGE LT SIDE SKIN, AROUND TAT PROBE, PAINT STRIPPED FOR INVESTIGATION. TAT PROBE INNER BASE REMOVED FOR INVESTIGATION. AFTER INVESTIGATION, THE TAT PROBE INNER BASE FOUND WITH DEFOR
- [SDR RAIA201903220003](https://openairdocs.org/sdr/RAIA201903220003.md): Shear Tie · cracked · Mar 22, 2019 · N13124 · Emb EMB145XR · Fuselage Internal Mounting Structure
  > RT AT FLOOR LEVEL SHEAR CLIP AT FRAME 25 IS CRACKED. REMOVED AND REPLACED SHEAR CLIP AT FRAME 25 RT.
- [SDR RAIA201903180002](https://openairdocs.org/sdr/RAIA201903180002.md): Gusset · corroded · Mar 18, 2019 · N13124 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LAV RT GUSSET HAS CORROSION. REMOVED AND REPLACED LAV RT GUSSETT.
- [SDR RAIA201903180001](https://openairdocs.org/sdr/RAIA201903180001.md): Door Sill · corroded · Mar 18, 2019 · N13124 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LAV RT FLOOR SILL HAS CORROSION AT FR 59. REMOVED AND REPLACED RT LAV FLOOR SILL.
- [SDR RAIA201903160004](https://openairdocs.org/sdr/RAIA201903160004.md): Shear Tie · cracked · Mar 16, 2019 · N13124 · Emb EMB145XR · Fuselage Internal Mounting Structure
  > SHEAR CLIP AT FRAME 15 AND STR 15R IS CRACKED. REMOVED AND REPLACED SHEER CLIP AT FRAME 15 AND STR 15R.
- [SDR RAIA201903160002](https://openairdocs.org/sdr/RAIA201903160002.md): Angle · corroded · Mar 16, 2019 · N13124 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CARGO DOOR LOWER THRESHOLD Z ANGLE IS CORRODED. REMOVED AND REPLACED CARGO DOOR THRESHOLD Z ANGLE.
- [SDR RAIA201903160001](https://openairdocs.org/sdr/RAIA201903160001.md): Door Sill · corroded · Mar 16, 2019 · N13124 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL AT FRAME 19-21 IS CORRODED. REMOVED AND REPLACED SERVICE DOOR SILL AT FRAME 19-21.
- [SDR RAIA201902020001](https://openairdocs.org/sdr/RAIA201902020001.md): Proximity Switch · dirty · Feb 2, 2019 · N13124 · Emb EMB145XR · Landing Gear Position and Warning
  > LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS. CLEANED DIRT AND DEBRIS OFF ALL PROX SWITCHES. OPS CHECK GOOD AT THIS TIME.
- [SDR RAIA201810040003](https://openairdocs.org/sdr/RAIA201810040003.md): Indication Sys · malfunctioned · Oct 4, 2018 · N13124 · Emb EMB145XR · Fuel Indicating System
  > TOTAL FUEL QUANTITY SHOWES AMBER DASHES INTERMITTENTLY THROUGHOUT FLT. RESET FUEL SYSTEM IAW 28-41-00. SYSTEM CHECK GOOD.
- [SDR RAIA201806090001](https://openairdocs.org/sdr/RAIA201806090001.md): O-Ring · damaged · Jun 9, 2018 · N13124 · Emb EMB145XR · Pneumatic Distribution System
  > BLEED 1 LEAK AFTER TAKE OFF. REMOVED AND REPLACED JOINT 28 O-RINGS. PERFORMED LEAK CHECK OF BLEED SYSTEM. OPS CHECK/LEAK CHECK GOOD AT THIS TIME.
- [SDR RAIA201801050001](https://openairdocs.org/sdr/RAIA201801050001.md): Duct · disconnected · Jan 5, 2018 · N13124 · Emb EMB145XR · Cabin Cooling System
  > NR 2 PACK VALVE CLOSED MESSAGE. TROUBLESHOT AND FOUND THE DUCT DISCONNECTED ON THE NR 2 PACK VALVE. SECURED THE DUCT AND OPS CHECKED GOOD.
- [SDR RAIA201707290002](https://openairdocs.org/sdr/RAIA201707290002.md): Flap Track · cracked · Jul 29, 2017 · N13124 · Emb EMB145XR · Trailing Edge Flaps
  > FLAP OVERSPEED 290 KNOTS AT FLAPS 9. PERFORMED MAX FLAP EXTENDED SPEED INSPECTION, FAILED NDI TESTING ON LEFT WING O/B FLAP INBD TRACK AND RIGHT WING O/B FLAP INBD TRACK.
- [SDR RAIA201701170001](https://openairdocs.org/sdr/RAIA201701170001.md): Transducer · inoperative · Jan 17, 2017 · N13124 · Emb EMB145XR · Ice/Rain Protection System
  > NR 2 ENGINE ANTI ICE EICAS CAME ON. RAN CHECK LIST TEST AND VALVE NEVER OPENED AFTER MULTIPLE ATTEMPTS. R & R THE NR 2 ENG ANTI ICE PRESSURE TRANSDUCER. OPS CHECKED GOOD
- [SDR RAIA201611280001](https://openairdocs.org/sdr/RAIA201611280001.md): Anti-Ice Valve · inoperative · Nov 28, 2016 · N13124 · Emb EMB145XR · Air Intake Anti/De-Ice System
  > NR 1 AND 2 ENGINE ANTI ICE FAILED MESSAGE WHEN BOTH ANTI ICE VALVES HAVE BEEN DEFERRED. R & R THE ANTI ICE VALVE IAW AMM 30-21-01, OPS CHECKED GOOD.
- [SDR RAIA201601280001](https://openairdocs.org/sdr/RAIA201601280001.md): Bulb · inoperative · Jan 28, 2016 · N13124 · Emb EMB145XR · Emergency Lighting
  > RIGHT WING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. RELAMPED RT EXTERIOR EMERGENCY LIGHT. OPS CHECK GOOD.

Next page: https://openairdocs.org/aircraft/N13124/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 = 'N13124' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N13124/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.