# Service difficulty reports: N14143

A list on [N14143](https://openairdocs.org/aircraft/N14143.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 · 72 reports

- [SDR JJBA20260706005](https://openairdocs.org/sdr/JJBA20260706005.md): Ics Box · inoperative · Jul 3, 2026 · N14143 · Emb EMB145XR · Indicating/Recording System
  > IC 1 FAIL ON EICAS AFTER PFD 1, MFD 1 AND EICAS DISPLAYS BLANKED OUT. REMOVED AND REPLACED IC #1 IC-600. OPS CHECK SAT.
- [SDR JJBA20260413011](https://openairdocs.org/sdr/JJBA20260413011.md): Roller · lack of lube · Apr 12, 2026 · N14143 · Emb EMB145XR · Cargo/Baggage Doors
  > MCD DIFFICULT TO OPEN OR CLOSE. LUBRICATED MCD ROLLER. OPS CHECK GOOD.
- [SDR JJBA20250515059](https://openairdocs.org/sdr/JJBA20250515059.md): Unknown · odor · May 14, 2025 · N14143 · Emb EMB145XR · Air Distribution System
  > BURNING RUBBER SMELL AFTER TAKE OFF ON CLIMB. PERFORMED FIM PROCEDURES. PERFORMED HIGH POWER ENGINE RUNS. NO SMOKE OR ODOR PRESENT. ALL INDICATIONS NORMAL.
- [SDR JJBA20250328038](https://openairdocs.org/sdr/JJBA20250328038.md): Unknown · odor · Mar 24, 2025 · N14143 · Emb EMB145XR · Air Distribution System
  > WEIRD CHEMICAL SMELL COMING FROM COCKPIT ON DESCENT. PERFORMED WITH ENGINE BLEED 1 AND 2. OC SAT. RAN PACK SYSTEM DURING HIGH POWER RUN ON FULL HOT AND FULL COLD. ENGINES AND PACKS WERE ON TOTAL TIME OF 40 MINUTES. NO DEFECTS OR SMELL WERE NOTED.
- [SDR JJBA20250120017](https://openairdocs.org/sdr/JJBA20250120017.md): Lamp · inoperative · Jan 16, 2025 · N14143 · Emb EMB145XR · Emergency Lighting
  > RIGHT EXTERIOR FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT EXTEIOR FWD EMERGENCY LIGHT. OPS CHECK SAT
- [SDR JJBA20241209006](https://openairdocs.org/sdr/JJBA20241209006.md): A/C Pack · odor · Dec 5, 2024 · N14143 · Emb EMB145XR · Cabin Cooling System
  > DIRTY SOCK SMELL ON DECENT FROM PACK 1. FOLLOWED FIM. DIRTY SOCK SMELL ODOR WAS NOT PRESENT AT THIS TIME. PERFORMED GVI INSPECTION OF THE #1 PACK SYSTEM, NO DEFECTS NOTED. HIGH POWER ENG RUNS PERFORMED. DIRTY SOCK SMELL NOT PRESENT. PERFORMED BORESCOPE INSPECT
- [SDR JJBA20230404002](https://openairdocs.org/sdr/JJBA20230404002.md): Unknown · unknown · Apr 4, 2023 · N14143 · Emb EMB145XR · Aircraft Fuel System
  > CRACK ALONG INTERNAL FUEL TANK DOUBLER UNDER RH WING RIB 9 FOUND CRACK TO BE MIGRATING ACROSS DOUBLER THROUGH 3 HIGH LOCK (FWD) HOLES. REMOVED HILOCK COLLARS FROM SPLICE ON OUTBD SIDE OF RIB 9 AND REMOVED FILLET SEALANT. REMOVED SPLICE BELOW RIB 9. FOUND RH WI
- [SDR JJBA20220711008](https://openairdocs.org/sdr/JJBA20220711008.md): Lamp · inoperative · Jul 9, 2022 · N14143 · Emb EMB145XR · Emergency Lighting
  > LH FORWARD EXTERNAL EMERGENCY LIGHT INOP. R/R LH FORWARD EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK SAT
- [SDR JJBA20220619014](https://openairdocs.org/sdr/JJBA20220619014.md): None · inoperative · Jun 19, 2022 · N14143 · Emb EMB145XR · Air Conditioning System
  > SMOKE SMELL FROM COCKPIT DURING DEP CLIMB OUT. REMOVED AND REPLACED SLEEVES BETWEEN DUAL TEMP CONTROL VALVE AND Y-DUCT ON #2 PACK VALVE. REMOVED AND REPLACED #2 ACM. O-RING BETWEEN TURBINE OUTLET DUCT AND ACM STILL NEEDS TO BE INSTALLED. INSTALLED O-RING. OPS/
- [SDR JJBA20220401002](https://openairdocs.org/sdr/JJBA20220401002.md): Lamp · inoperative · Apr 1, 2022 · N14143 · Emb EMB145XR · Emergency Lighting
  > EMERGENCY CEILING LIGHT IN COCKPIT INOPERATIVE. REMOVED AND REPLACED EMERGENCY CEILING LIGHT IN COCKPIT. OPS CHECK SAT
- [SDR JJBA20211125047](https://openairdocs.org/sdr/JJBA20211125047.md): Unknown · unknown · Nov 25, 2021 · N14143 · Emb EMB145XR · Fuselage Structure (General)
  > RH FWD FUSELAGE I, TWO LIGHTING STRIKES SUSPECTED BTW FR 1A & 2 AND ABOVE STR 13R. DURING LIGHTING STRIKE INVESTIGATION MULTIPLE STRIKE SPOTS BLENDED WITHIN LIMITS, SOME ACCEPTED AS IS AND 2 BLEND OUT FOUN OUT OF LIMITS AND NEED A EXTERNAL DOUBLER REPAIR. FIRS
- [SDR JJBA20211125045](https://openairdocs.org/sdr/JJBA20211125045.md): Unknown · unknown · Nov 25, 2021 · N14143 · Emb EMB145XR · Fuselage Structure (General)
  > MULTIPLE DENTS FOUND ON EXTERNAL SKIN OF MAIN DOOR BTW STR 06L AND STR 08L, STR 12L AND STR 15L. MULTIPLE DENTS ON EXT SIGN OF MAIN DOOR BTW STR 06L-08L AND STR 12L-15L STRIPPED FOR INVESTIGATION ON EXT SKIN OF MAIN DOOR BTW STR 06L-08L AND STR 12L-15L DENTS 1
- [SDR JJBA20211125044](https://openairdocs.org/sdr/JJBA20211125044.md): None · none · Nov 25, 2021 · N14143 · Emb EMB145XR · Fuselage Structure (General)
  > CF1, SKIN FOUND WITH EXISTING BLEND BTW FR 20-21 STR 11-12L. CF1, SKIN BTW FR 20-21 AND STR 11-12L FOUND BLENDED OUT OF LIMITS. REPAIR WAS MADE.
- [SDR JJBA20211124046](https://openairdocs.org/sdr/JJBA20211124046.md): Unknown · unknown · Nov 24, 2021 · N14143 · Emb EMB145XR · Wing Structure
  > RIVET FOUND ON LEADING EDGE II RH. DENT AT RIVET LOCATION OF LEADING EDGE II RH FOUND OUT OF LIMITS AND NEEDS REPAIR PARTS FOR REPAIR SPLICE AND FILLER FABRICATED. REPAIR SPLICE AND FILLER INSTALLED
- [SDR JJBA20211124043](https://openairdocs.org/sdr/JJBA20211124043.md): None · none · Nov 24, 2021 · N14143 · Emb EMB145XR · Fuselage Structure (General)
  > CENTER FUSE II, FRAME 25 CRACKED BTW STR 16R-15R. FRAME REPAIRED
- [SDR JJBA20211124041](https://openairdocs.org/sdr/JJBA20211124041.md): None · none · Nov 24, 2021 · N14143 · Emb EMB145XR · Fuselage Structure (General)
  > CRACK FOUND ON LH FRAME 59 BTW STR 15L-16L IN CF IV AREA. FRAME REPAIRED
- [SDR JJBA20211124040](https://openairdocs.org/sdr/JJBA20211124040.md): Skin · damaged · Nov 24, 2021 · N14143 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > FWD FUSELAGE 1 RH SKIN AT FR 3 BTW STR 01R-13R SEVERAL RIVETS NOT PROPERLY INSTALLED. PAINT STRIPPED ON FWD FUSELAGE I RH, STR 01R-13R FOR INVESTIGATION ON FWD FUSELAGE I RH SKIN AT FR3 BTW STR 01R-13R IMPROPERLY INSTALLED RIVETS REMOVED. RIVETS HOLES FOUND TO
- [SDR JJBA20211124039](https://openairdocs.org/sdr/JJBA20211124039.md): Doubler · corroded · Nov 24, 2021 · N14143 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON ANTENNA INNER DOUBLER BTW FR 65-66 AND STR 21LH + STR 21RH. REMOVED R. ALT ANTENNA FOR ACCESS, REMOVED INNER AND OTHER DOUBLER FOR INVESTIGATION. AFTER FURTHER INVESTIGATION FOUND OUTER SKIN CRACK OUT OF LIMITS AT R. ALT ANTENNA LOCATION. PE
- [SDR JJBA20211118038](https://openairdocs.org/sdr/JJBA20211118038.md): Skin · dented · Nov 18, 2021 · N14143 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > LH FWD FUSELAGE II, DENT FOUND ON EXTERNAL SKIN BTW FR 8-9 AND STR 18L-20L. DENT REMOVED BY CUT OUT ON LH FWD FUSE II EXTERNAL SKIN BTW FR 8-9 AND STR 18L-20L. PATCH DOUBLER LOCALLY FABRICATED. AT LH FWD FUSELAGE II, EXTERNAL SKIN BTW FR 8-9 AND STR 18L-20L DE
- [SDR JJBA20211118034](https://openairdocs.org/sdr/JJBA20211118034.md): None · none · Nov 18, 2021 · N14143 · Emb EMB145XR · Fuselage Structure (General)
  > CF1 FLOOR STRUCTURE PROFILE OMEGA BTW FR 20-23 LH CORRODED. AFTER FURTHER INVESTIGATION OMEGA BEAM FOUND CRACKED AT FASTENERS LOCATION. CF1 FLOOR STRUCTURE, OMEGA BEAM REPLACED.
- [SDR JJBA202108030026](https://openairdocs.org/sdr/JJBA202108030026.md): Glowstrip · cracked · Jul 30, 2021 · N14143 · Emb EMB145XR · Emergency Equipment
  > PHOTOLUMINESCENT STRIP CRACKED AT SEAT 1A. R/R PHOTOLUMINECENT STRIP
- [SDR JJBA2021310002](https://openairdocs.org/sdr/JJBA2021310002.md): Seat Frame · cracked · Mar 10, 2021 · N14143 · Emb EMB145XR · Passenger Compartment Equipment
  > FOUND SEATS 23A, 22A, 24A, 21A, 7A, 5A HAVE A CRACK BELOW ARMREST ON STRUCTURE. R&R 23A, 22A, 24A, 21A, 7A, 5A SEATS. OPS CHECK SAT. NO DEFECTS NOTED.
- [SDR JJBA202006242006](https://openairdocs.org/sdr/JJBA202006242006.md): Electronic Unit · inoperative · Jun 22, 2020 · N14143 · Emb EMB145XR · Landing Gear Retraction/Extension System
  > LG AIR GROUND FAIL EICAS MESSAGE IMMEDIATELY AFTER TAKE OFF. ADJUST NLG TORQUE LINK TARGET. PERFORM GEAR SWINGS FAIL. TROUBLESHOT TO LGEU. R&R LGEU AND GEAR SWINGS 5 TIMES. OPS CHECK SAT. NO OTHER DEFECTS NOTED.
- [SDR JJBA202006054003](https://openairdocs.org/sdr/JJBA202006054003.md): Charger · inoperative · Jun 4, 2020 · N14143 · Emb EMB145XR · Emergency Lighting
  > FORWARD EXTERNAL EMERGENCY LIGHTS FWD OF WING INOPERATIVE. REMOVED AND REPLACED NR 2 BATTERY CHARGER ASSEMBLY. REMOVED AND REPLACED BURNT OUT BULBS. OPS CHECK SAT.
- [SDR JJBA202006052002](https://openairdocs.org/sdr/JJBA202006052002.md): Fastener · loose · Jun 2, 2020 · N14143 · Emb EMB145XR · Emergency Exits
  > RIGHT PASSENGER CABIN, ESCAPE HATCH DOOR TOOK SEVERAL MINUTES TO REMOVE DOOR TO FOM. FOUND FASTENERS THAT ATTACH SIDEWALL PANEL TO EMERGENCY EXIT DOOR FRAME LOOSE CAUSING DOOR TO JAM ON FASTENERS. RESECURED FASTENERS. OPS CHECK SAT.
- [SDR JJBA2020031108003](https://openairdocs.org/sdr/JJBA2020031108003.md): Warning System · false activation · Mar 8, 2020 · N14143 · Emb EMB145XR · Landing Gear Position and Warning
  > LG LEVER DISAGREE ON TAKE-OFF. PERFORMED GVI OF NLG, MLG, AND WHEEL WELLS WITH NO DEFECTS. CHECKED CMC WITH NO FAULTS. PERFORMED GEAR SWINGS. FOUND TO BE TRANSITORY.
- [SDR JJBA2020012219005](https://openairdocs.org/sdr/JJBA2020012219005.md): Warning Message · false activation · Jan 19, 2020 · N14143 · Emb EMB145XR · Landing Gear Selector
  > LG LEVER DISAGREE MASTER WARNING ON TAKE OFF. CHECKED FOR PROPER UP LOCK HOOK POSITIONS. NO FAULTS FOUND. CHECKED PROX SWITCHES FOR CONDITION AND SECURITY. NO DEFECTS FOUND. PERFORMED MULTIPLE EXTENSION AND RETRACTION TESTS. OPS CHECK SAT. NO DEFECTS NOTED. NO
- [SDR JJBA20200117004](https://openairdocs.org/sdr/JJBA20200117004.md): Charger · inoperative · Jan 17, 2020 · N14143 · Emb EMB145XR · Emergency Lighting
  > BOTH OVER WING EMERGENCY LIGHTS INOPERATIVE. R&R #4 EMERGENCY LIGHT BATTERY. OPS CHECK FAILED. R&R BATTERY CHARGER ASSEMBLY. OPS CHECK SAT. ORIGINAL BATTERY STILL INSTALLED.
- [SDR JJBA20190920006](https://openairdocs.org/sdr/JJBA20190920006.md): Unknown · noisy · Sep 20, 2019 · N14143 · Emb EMB145XR · Emergency Exits
  > LEFT OVER WING EMERGENCY EXIT WHISTLES. REMOVED AND REINSTALLED EMERGENCY EXIT AND THEN PERFORMED PRESSURIZATION PROCEDURE. NO DEFECTS NOTED AND LEAK CHECK SAT AT THIS TIME.
- [SDR JJBA20190830014](https://openairdocs.org/sdr/JJBA20190830014.md): Electronic Unit · faulty · Aug 30, 2019 · N14143 · Emb EMB145XR · Landing Gear System
  > ON APU START SEVERAL EICAS MESSAGES APPEARED AND REMAIN ON. R&R AC STATIC INVERTER. OPS CHECK SAT. ONLY FOR THE MESSAGE 115 VAC BUS OFF. OPS CHECK FAIL FOR ALL OTHER MESSAGES. FOUND FAULTY LGEU. R&R LGEU. OPS CHECK SAT. ALL EICAS FAULTS CLEARED. NO DEFECTS NOT
- [SDR JJBA2019082917013](https://openairdocs.org/sdr/JJBA2019082917013.md): Electronic Unit · inoperative · Aug 17, 2019 · N14143 · Emb EMB145XR · Landing Gear Position and Warning
  > LANDING GEAR AIR/GROUND FAIL ON ROTATION, GEAR WILL NOT RETRACT. R&R LEGU. JACKED AND SWUNG GEAR MULTIPLE TIMES. OPS CHECK SAT. NO OTHER DEFECTS NOTED.
- [SDR JJBA201902273013](https://openairdocs.org/sdr/JJBA201902273013.md): Unknown · malfunctioned · Feb 23, 2019 · N14143 · Emb EMB145XR · Cabin Pressure Control System
  > CABIN WILL NOT MAINTAIN PRESSURIZATION OPERATING ON ONE PACK. PERFORMED AIRCRAFT PRESSURIZATION WITH BOTH PACKS OPERATIVE. NO PRESSURE LOSS NOTED. OPS CHECK SAT.
- [SDR JJBA20190128036](https://openairdocs.org/sdr/JJBA20190128036.md): Sensor · inoperative · Jan 28, 2019 · N14143 · Emb EMB145XR · Smoke Detection
  > ON DECENT FROM 8-6000 FEET CREW HAD AURAL AND EICAS MESSAGE. LAV SMOKE WARNING IN FLIGHT PROCEDURE PER QRH PULLED C/B E9 AND E10. NO APU RUNNING. NO SMOKE NOTED AND NO ODOR NOTED. R&R LAV SMOKE DETECTOR SENSOR. OPS CHECK SAT. PERFORMED HIGH POWER RUNS WITH NO
- [SDR JJBA20180524011](https://openairdocs.org/sdr/JJBA20180524011.md): Floorbeam · corroded · May 24, 2018 · N14143 · Emb EMB145XR · Fuselage Main, Floor Beam
  > CENTER FLOORBEAM IS CORRODED AT FR 50-61. FABRICATED AND INSTALLED REPAIR DOUBLER ONTO CENTER FLOORBEAM AT FR 59-61. HFEC INSPECTION FOUND NOTED NO DEFECTS IN CUT OUT OF FLOORBEAM.
- [SDR JJBA20180312002](https://openairdocs.org/sdr/JJBA20180312002.md): Light · defective · Mar 12, 2018 · N14143 · Emb EMB145XR · Emergency Lighting
  > EXTERNAL EMERGENCY LIGHT AT MAIN DOOR INOP. TROUBLE SHOT TO BAD CONTACT ASSY. R&R MAIN CABIN DOOR LIGHT ASSY. OPS CK SAT MEL CLEARED.
- [SDR JJBA20180312001](https://openairdocs.org/sdr/JJBA20180312001.md): Wire · broken · Mar 12, 2018 · N14143 · Emb EMB145XR · Light System Wiring
  > EXTERNAL EMERGENCY LIGHT AT LT FORWARD LOWER FAIRING INOP. REMOVED AND REPLACED NR 1 BATTERY CHARGER ASSY FOR EMERGENCY LIGHTS. OPS CHECK FAILED. FOUND BROKEN/CHAFFED WIRE. REPAIRED BY SPLICING. OPS CHECK SAT.
- [SDR ASOA20161002057C](https://openairdocs.org/sdr/ASOA20161002057C.md): Button · failed · Oct 2, 2016 · N14143 · Emb EMB145XR · Windshield/Door Rain/Ice Removal
  > THE CREW REPORTED WINDSHIELD HEAT NR 1 FAILED IN FLIGHT AND HAD ELECTRICAL BURNING ODOR. MAINTENANCE REPLACED THE WINDSHIELD HEAT SYSTEM PUSH BUTTON. OPS CHECKED GOOD.
- [SDR ASOA20160112001](https://openairdocs.org/sdr/ASOA20160112001.md): Valve · faulty · Jan 12, 2016 · N14143 · Emb EMB145XR · Cabin Pressure Control System
  > PILOT REPORTED LOST PRESSURIZATION GOING THROUGH 10,000 FT. MAINTENANCE R & R AIR DISTRIBUTION GROUND CONNECTION VALVE WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20151226209](https://openairdocs.org/sdr/ASOA20151226209.md): Beam · corroded · Dec 26, 2015 · N14143 · Emb EMB145XR · Fuselage Main, Structure
  > DURING C-CHECK, BAGGAGE DOOR LOWER CUTOUT CORRODED. R & R CARGO DOOR LOWER CUTOUT SUPPORT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20151212206](https://openairdocs.org/sdr/ASOA20151212206.md): Skin · cracked · Dec 12, 2015 · N14143 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C-CHECK. FUSELAGE CRACKED AROUND RIVET FRAME 79, STR 5-6L. REPAIRED RIVET AREA ON FUSELAGE AROUND RIVET FROM 79, STR 5L-6L IAW SRM 53-32-01. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20151212205V](https://openairdocs.org/sdr/ASOA20151212205V.md): Skin · cracked · Dec 12, 2015 · N14143 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C-CHECK. FUSELAGE CRACKED AROUND RIVET FRAME 78, STR 5-6R. REPAIRED AREA ON FUSELAGE AROUND RIVET FROM 78 IAW SRM 53-32-01. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150416023C](https://openairdocs.org/sdr/ASOA20150416023C.md): Fitting · cracked · Apr 16, 2015 · N14143 · Emb EMB145XR · Nacelle/Pylon, Attach Fittings
  > DURING ROUTINE MAINTENANCE THE NR 1 PYLON FOWARD YOKE FITTING WAS FOUND CRACKED. MAINTENANCE REPLACED THE YOKE FITTING IAW STS EA 26-2014-063.
- [SDR ASOA20141020116](https://openairdocs.org/sdr/ASOA20141020116.md): Charger · inoperative · Oct 20, 2014 · N14143 · Emb EMB145XR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, THE FWD OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE R & R THE NR 1 BATTERY CHARGER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20141017111](https://openairdocs.org/sdr/ASOA20141017111.md): Tire · failed · Oct 17, 2014 · N14143 · Emb EMB145XR · Tire
  > DURING TAKEOFF, NR 2 TIRE BLEW FROM FOD DAMAGE CAUSING MULTIPLE DAMAGES TO THE RT GEAR AUX DOOR. MAINTENANCE R & R THE RT MLG AUX DOOR IAW AMM 32-10-07. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF CHECKS.
- [SDR ASOA20141015110](https://openairdocs.org/sdr/ASOA20141015110.md): Engine · fod · Oct 15, 2014 · N14143 · Emb EMB145XR · Engine (Turbine/Turboprop)
  > WHILE ON TAKEOFF THE NR 2 TIRE BLEW APART IMBEDDING PART OF TIRE IN THE NR 2 ENGINE AND DAMAGING THE FLAP. THE NR 2 ENGINE WILL BE CHANGED AND THE FLAP TEMPORARY REPAIRED FOR A FERRY FLIGHT TO REPAIR THE SMALL DAMAGE TO THE FLAP. ALL WORK WILL BE ACCOMPLISHED
- [SDR ASOA20140224020](https://openairdocs.org/sdr/ASOA20140224020.md): Light · burned · Feb 24, 2014 · N14143 · Emb EMB145XR · Passenger Compartment Lighting
  > CREW REPORTED SMOKE COMING FROM CABIN OVERHEAD LIGHTS AT SEAT 23A. MX INSPECTED AND FOUND LIGHT RECEPTACLE BURNED. R & R SIDEWALL LIGHT ASSY WITH OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131109271](https://openairdocs.org/sdr/ASOA20131109271.md): Fitting · worn · Nov 9, 2013 · N14143 · Emb EMB145XR · Wing, Control Surface Attach Fittings
  > DURING C-CHECK, THE LT WING AILERON PCA FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE FITTING IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20131109270](https://openairdocs.org/sdr/ASOA20131109270.md): Floor Support · corroded · Nov 9, 2013 · N14143 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01443. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130624334](https://openairdocs.org/sdr/ASOA20130624334.md): Floor Support · cracked · Jun 23, 2013 · N14143 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CENTER OMEGA BEAM SPLICE BETWEEN FRAMES 16 AND 17 CRACKED ON LT SIDE. R & R OMEGA BEAM SPLICE BETWEEN FRAME 16 AND 17.
- [SDR ASOA20130624333](https://openairdocs.org/sdr/ASOA20130624333.md): Floor Support · cracked · Jun 23, 2013 · N14143 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LEFT OMEGA BEAM, RT AND LT SPLICE BETWEEN FRAMES 16 AND 17 CRACKED. R & R OMEGA BEAM SPLICE BETWEEN FRAME 16 AND 17.

Next page: https://openairdocs.org/aircraft/N14143/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 = 'N14143' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N14143/reports

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