# Service difficulty reports: N24103

A list on [N24103](https://openairdocs.org/aircraft/N24103.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 · 75 reports

- [SDR JJBA20220926040](https://openairdocs.org/sdr/JJBA20220926040.md): Light · misinstalled · Sep 25, 2022 · N24103 · Emb EMB145XR · Emergency Lighting
  > RH AFT OVER WING EMERGENCY LIGHT IS INSTALLED UPSIDE DOWN. RE-INSTALLED RH EXTERNAL EMERGENCY LIGHT REFLECTOR.
- [SDR JJBA20220618013](https://openairdocs.org/sdr/JJBA20220618013.md): None · none · Jun 18, 2022 · N24103 · Emb EMB145XR · Crew Oxygen System
  > O2 MASK WONT TEST. RESECURED O2 MASK BOX. OPS CHECK GOOD.
- [SDR JJBA20220131031](https://openairdocs.org/sdr/JJBA20220131031.md): Lamp · inoperative · Jan 31, 2022 · N24103 · Emb EMB145XR · Lighting System
  > EXTERNAL EMERGENCY MAIN DOOR LIGHT INOPERATIVE. REMOVED AND REPLACED EXTERNAL EMERGENCY MAIN DOOR LIGHT. OPS CHECK SAT
- [SDR ASOA202001247011](https://openairdocs.org/sdr/ASOA202001247011.md): Bushing · missing · Jan 22, 2020 · N24103 · Emb EMB145XR · Spoilers
  > ACTUATOR ATTACH POINT ON R/H GROUND SPOILER HAT BUSHING MISSING. REAMED BOTH BUSHING HOUSINGS, INSTALLED NEW HAT BUSHINGS. AIRCRAFT STILL IN C CHECK.
- [SDR ASOA202001237008](https://openairdocs.org/sdr/ASOA202001237008.md): Support Frame · cracked · Jan 22, 2020 · N24103 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > TYS- CRACK ON FRAME FWD OF LH COCKPIT CEILING SPEAKER BETWEEN FRAME 10-11. THE CRACKED SECTION WAS REMOVED A SUPPORT AND SPLICE WERE FABRICATED AND INSTALLED IAW ENGINEERING DOCUMENT PROVIDED.
- [SDR ASOA202001217006](https://openairdocs.org/sdr/ASOA202001217006.md): Support · cracked · Jan 21, 2020 · N24103 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > TYS A/C WAS FOUND WITH THE NLG UP LOCK SUPPORT FRAME ON THE AFT SIDE CRACKED. MAINTENANCE REPLACED THE UP LOCK SUPPORT BRACKET IAW EMB 145XR SRM 51-40-02. ALL WORK ACCOMPLISHED AND WAS RELEASED TO SERVICE.
- [SDR ASOA201906253036](https://openairdocs.org/sdr/ASOA201906253036.md): Engine · odor · Jun 25, 2019 · N24103 · Emb EMB145XR · Engine (Turbine/Turboprop)
  > THE CREW REPORTED STRONG OIL ODOR DURING DESCENT WHEN THROTTLES WERE AT IDLE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD.
- [SDR ASOA201905024015](https://openairdocs.org/sdr/ASOA201905024015.md): Skin · corroded · May 2, 2019 · N24103 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > IAH - DURING INSPECTION THE FORWARD RADIO ALTIMETER ANTENNA WAS FOUND TO HAVE CORROSION INSIDE THE BASE IN THE CARGO COMPARTMENT. MAINTENANCE REMOVED THE CORRODED SKIN BETWEEN FRAMES 68-69 STR 21L-21R, PERFORMED HFEC WITH NO DEFECTS NOTED AND INSTALLED A FILLE
- [SDR ASOA201905024014](https://openairdocs.org/sdr/ASOA201905024014.md): Skin · corroded · May 2, 2019 · N24103 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > IAH - DURING INSPECTION THE FORWARD RADIO ALTIMETER ANTENNA WAS FOUND TO HAVE CORROSION INSIDE THE BASE IN THE CARGO COMPARTMENT. MAINTENANCE REMOVED THE CORRODED SKIN BETWEEN FRAMES 64-65 STR 21L-21R, PERFORMED HFEC WITH NO DEFECTS NOTED AND INSTALLED A FILLE
- [SDR ASOA20190415053](https://openairdocs.org/sdr/ASOA20190415053.md): Bulb · inoperative · Apr 10, 2019 · N24103 · Emb EMB145XR · Emergency Lighting
  > DURING MX INSPECTION THE EMERGENCY LIGHT OVER SEAT 18CD WAS INOP. MX REMOVED AND REPLACED THE BULB WITH OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20190415052](https://openairdocs.org/sdr/ASOA20190415052.md): Bulb · inoperative · Apr 10, 2019 · N24103 · Emb EMB145 · Emergency Lighting
  > DURING MX INSPECTION THE EMERGENCY LIGHT OVER SEAT 18A WAS INOP. MX REMOVED AND REPLACED THE BULB WITH OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201808214043](https://openairdocs.org/sdr/ASOA201808214043.md): Engine · leaking · Aug 18, 2018 · N24103 · Emb EMB145XR · Engine (Turbine/Turboprop)
  > FLIGHT 4178, THE CREW REPORTED STRONG OIL FUMES POSSIBLY COMING FROM THE NR 1 PACK. THE AIRCRAFT RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NR 1 ENGINE. OPS CHECKED WITH NO DEFECTS NOTED
- [SDR ASOA201602121576](https://openairdocs.org/sdr/ASOA201602121576.md): Stringer · corroded · Dec 12, 2016 · N24103 · Emb EMB145XR · Fuselage Main, Longeron/Stringer
  > DURING C-CK STRINGER 18R CORRODED AT FR 23. REMOVED STRINGER AND SPLICED IN A NEW STRINGER IAW SRM 53-00-03. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160315019H](https://openairdocs.org/sdr/ASOA20160315019H.md): Display · shorted · Mar 13, 2016 · N24103 · Emb EMB145XR · Attitude and Direction Data System
  > THE CREW REPORTED THAT AT LEVEL CRUISE AT FL360, F/O PFD WENT RED, THEN BLANK AND THEN HAD AN INTENSE SULFUR/ELECTRICAL FIRE ODOR OCCURRED IN THE COCKPIT. THE ACFT LANDED WITHOUT INCIDENT WHERE CONTRACT MAINTENANCE PLACED THE F/O PFD ON MEL 34-22-01-01, AND TH
- [SDR ASOA2016114004T](https://openairdocs.org/sdr/ASOA2016114004T.md): Smoke Detector · inoperative · Jan 12, 2016 · N24103 · Emb EMB145LR · Smoke Detection
  > AFT BAGGAGE SMOKE DETECTOR FAILED. R & R SMOKE DETECTOR. ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR ASOA20150907050C](https://openairdocs.org/sdr/ASOA20150907050C.md): Inverter · inoperative · Sep 7, 2015 · N24103 · Emb EMB145XR · Emergency Lighting
  > THE CREW REPORTED EMERGENCY EXIT LIGHT IDENTIFER ABOVE THE F/A JUMPSEAT DID NOT ILLUMINATE WHEN TESTED. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPS CHECKS WERE GOOD.
- [SDR ASOA20140608117](https://openairdocs.org/sdr/ASOA20140608117.md): Support Bracket · corroded · Jun 8, 2014 · N24103 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING C-CHECK CORROSION, ON VENTRAL TANK FWD FACE AT SUPPORT BRACKET FOR FUEL LINE. REPAIRED SUPPORT BRACKET IAW EC5320-01942 REV. ORIG. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140608116](https://openairdocs.org/sdr/ASOA20140608116.md): Receptacle · corroded · Jun 8, 2014 · N24103 · Emb EMB145XR · Fuselage Main, Bulkhead Fuselage wiring
  > DURING C-CHECK, CORROSION ON VENTRAL TANK FWD FACE AROUND THREE CONNECTOR RECEPTACLES. REPAIRED IAW EC5320-01942 REV. ORIG. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140608115](https://openairdocs.org/sdr/ASOA20140608115.md): Structure · chafed · Jun 8, 2014 · N24103 · Emb EMB145XR · Fuel Storage
  > DURING C-CHECK VENTRAL TANK CHAFED ON LT SIDE FRAME 51-52. MAINTENANCE REPAIRED VENTRAL TANK IAW EC5320-01941 REV ORIG. ACFT APPROVED FOR RETURN SERVICE.
- [SDR ASOA20140608113](https://openairdocs.org/sdr/ASOA20140608113.md): Support Bracket · corroded · Jun 8, 2014 · N24103 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, LOWER CENTER FUEL LINE SUPPORT BRACKET ON RIB 1 OF VENTRAL TANK CORRODED. MAINTENANCE R & R SUPPORT BRACKET IAW SRM 53-20-07. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140608112](https://openairdocs.org/sdr/ASOA20140608112.md): Shear Tie · corroded · Jun 8, 2014 · N24103 · Emb EMB145XR · Fuselage Internal Mounting Structure
  > DURING C-CHECK, SHEAR TIE AT FRAME 9 BETWEEN STRINGER 20-21L CORRODED. MAINTENANCE R & R SHEAR TIE IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140608111V](https://openairdocs.org/sdr/ASOA20140608111V.md): Shear Tie · corroded · Jun 8, 2014 · N24103 · Emb EMB145XR · Fuselage Internal Mounting Structure
  > DURING C-CHECK, SHEAR TIE CORRODED, AT FRAME 13 BETWEEN STRINGERS 20-21R. MAINTENANCE R & R SHEAR TIE IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140608110](https://openairdocs.org/sdr/ASOA20140608110.md): Skin Splice · corroded · Jun 8, 2014 · N24103 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C-CHECK, SKIN SPLICE CORRODED, BETWEEN FRAMES 13-14 STRINGERS 20R-20L. MAINTENANCE PERFORMED REPAIR ON SKIN SPLICE IAW SRM 53-00-02, FIG 201. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140607109](https://openairdocs.org/sdr/ASOA20140607109.md): Skin · corroded · Jun 7, 2014 · N24103 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C-CHECK THE FORWARD FUSELAGE II SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 11-12 AND STRINGERS 20-21R. MAINTENANCE R & R THE SKIN IAW SRM 51-20-01. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140607108](https://openairdocs.org/sdr/ASOA20140607108.md): Stringer · corroded · Jun 7, 2014 · N24103 · Emb EMB145XR · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, STRINGER 21R WAS FOUND TO BE CORRODED BETWEEN FRAMES 12-14. MAINTENANCE R & R THE STRINGER IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140607107](https://openairdocs.org/sdr/ASOA20140607107.md): Beam · corroded · Jun 7, 2014 · N24103 · Emb EMB145XR · 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. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140604098](https://openairdocs.org/sdr/ASOA20140604098.md): Door Sill · corroded · Jun 4, 2014 · N24103 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140604097](https://openairdocs.org/sdr/ASOA20140604097.md): Stringer · corroded · Jun 4, 2014 · N24103 · Emb EMB145XR · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK, STRINGER 21L WAS FOUND TO BE CORRODED BETWEEN FRAMES 17-18. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A SPLICE REPAIR IAW EC5320-01940. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120530116](https://openairdocs.org/sdr/ASOA20120530116.md): Sill · corroded · May 25, 2012 · N24103 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CORROSION BEYOND LIMITS ON SILL. R & R SILL.
- [SDR ASOA20120530115](https://openairdocs.org/sdr/ASOA20120530115.md): Floor Support · corroded · May 25, 2012 · N24103 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LT OMEGA BEAM CORRODED BEYOND LIMITS. R & R GUSSET.
- [SDR ASOA20120530114](https://openairdocs.org/sdr/ASOA20120530114.md): Floor Support · cracked · May 25, 2012 · N24103 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > R & R OMEGA BEAM SUPPORT CRACKED. R & R SUPPORT.
- [SDR ASOA20120530113](https://openairdocs.org/sdr/ASOA20120530113.md): Sill · corroded · May 25, 2012 · N24103 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > RT OTBD SILL CORRODED BEYOND LIMITS. R & R SILL.
- [SDR ASOA20120530112](https://openairdocs.org/sdr/ASOA20120530112.md): Floor Support · corroded · May 25, 2012 · N24103 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > RT OMEGA BEAM GUSSET CORRODED BEYOND LIMITS. R & R GUSSET.
- [SDR ASOA20120530111T](https://openairdocs.org/sdr/ASOA20120530111T.md): Floor Support · corroded · May 25, 2012 · N24103 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CENTER OMEGA BEAM CORRODED BEYOND LIMITS. R & R GUSSET.
- [SDR ASOA20120516100](https://openairdocs.org/sdr/ASOA20120516100.md): Floor Support · corroded · May 11, 2012 · N24103 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LEFT SIDE OMEGA BEAM, FRAME 59 THRU 61 CORRODED BEYOND LIMITS AT NUT PLATES.
- [SDR ASOA20120516099](https://openairdocs.org/sdr/ASOA20120516099.md): Sill · corroded · May 11, 2012 · N24103 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > SILL HAS CORROSION BEYOND LIMITS AT FRAME 61 LT SILL.
- [SDR C2XA11TY165](https://openairdocs.org/sdr/C2XA11TY165.md): Actuator · malfunctioned · Oct 25, 2011 · N24103 · Emb EMB145XR · Stabilizer Actuator
  > MASTER WARMING PITCH TRIM INOP ON EICAS. REMOVED AND REPLACED HORZ STAB ACTUATOR IAW EMB 145XR AMM 27-40-02. OPS CHECK GOOD.
- [SDR C2XA11IA237](https://openairdocs.org/sdr/C2XA11IA237.md): Smoke Detector · malfunctioned · Oct 18, 2011 · N24103 · Emb EMB145XR · Smoke Detection
  > IAH - FLIGHT 4183, THE CREW REPORTED THAT THE LAV SMOKE DETECTOR WENT OFF TWICE WITH NO SIGNS OF FIRE OR SMOKE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR PANEL, AND LAV SMOKE DETECTOR, OPERATIONA
- [SDR C2XA11IA236](https://openairdocs.org/sdr/C2XA11IA236.md): Control Panel · malfunctioned · Oct 18, 2011 · N24103 · Emb EMB145XR · Smoke Detection
  > IAH - FLIGHT 4183, THE CREW REPORTED THAT THE LAV SMOKE DETECTOR WENT OFF TWICE WITH NO SIGNS OF FIRE OR SMOKE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR PANEL, AND LAV SMOKE DETECTOR, OPERATIONA
- [SDR C2XA11TY132](https://openairdocs.org/sdr/C2XA11TY132.md): Proximity Switch · out of adjust · Aug 22, 2011 · N24103 · Emb EMB145XR · Landing Gear Position and Warning
  > TYS - A/C WAS LEAVING BNA ON CLIMBOUT, THE CREW GOT A EICAS MESSAGE OF AIR-GROUND FAIL. A/C RETURN TO BNA WHERE MAINTENANCE ADJUSTED THE PROX SWITCHES AND TARGETS AT THE LT FOWARD, RT FOWARD AND AFT PROX SWITCHES, OPS CHECK GOOD AND WAS RELEASED. NO PARTS IN
- [SDR C2XA11IA137](https://openairdocs.org/sdr/C2XA11IA137.md): Fadec · inoperative · Jul 1, 2011 · N24103 · Emb EMB145XR · Fuel Controlling System
  > IAH - FLIGHT 3038, THE CREW REPORTED THAT THE NUMBER TWO ENGINE FADEC WAS COMMANDING THE HIGHEST THRUST RATING AND WOULD NOT STAY SET AT A LOWER RATING. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FADEC 2A,
- [SDR C2XA11CL152](https://openairdocs.org/sdr/C2XA11CL152.md): Line · failed · Jun 22, 2011 · N24103 · Emb EMB145XR · Pneumatic Distribution System
  > EWR FLT 2370 THE CREW REPORTED A BLEED 1 OVERTEMP MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE BLEED LINE TO THE LOW TEMPERATURE THERMOSTAT. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA11TY079](https://openairdocs.org/sdr/C2XA11TY079.md): Proximity Switch · faulty · Jun 7, 2011 · N24103 · Emb EMB145XR · Landing Gear Position and Warning
  > L/G AIR GROUND FAIL MESSAGE ON EICAS ON EXTENSION. REMOVED AND REPLACED RT MLG UPPER PROX SWITCH IAW EMB145 AMM32-63-01 OPS CHECK GOOD IAW EMB 145XR AMM 32-63-05. AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA11TY024](https://openairdocs.org/sdr/C2XA11TY024.md): Wire · broken · Mar 8, 2011 · N24103 · Emb EMB145XR · Fire Protection System Wiring
  > TYS - ENGINE 2 FIRE DETECT FAIL MESSAGE APPEARED FOR APPROXIMATELY 10 SEC ON SHORT FINAL APPROACH. MAINTENANCE REPAIRED WIRE W407-0012-20 NEAR CONNECTER PO 915 IAW EMB 145 SWPM 2021-00. OPS CHECK GOOD AND WAS THEN RELEASED.
- [SDR C2XA11IA039](https://openairdocs.org/sdr/C2XA11IA039.md): Light · inoperative · Mar 3, 2011 · N24103 · Emb EMB145XR · Emergency Lighting
  > IAH - DURING A-CHECK INSPECTION THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND 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 C2XA10IA145](https://openairdocs.org/sdr/C2XA10IA145.md): Inverter · inoperative · Apr 24, 2010 · N24103 · Emb EMB145XR · Emergency Lighting
  > MCI - DURING MAINTENANCE INSPECTION THE LT OVERWING EXIT UPPER AFT EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO S
- [SDR C2XA10IA059](https://openairdocs.org/sdr/C2XA10IA059.md): Filter · dirty · Feb 10, 2010 · N24103 · Emb EMB145XR · Pneumatic Distribution System
  > IAH - FLIGHT 2037, THE CREW REPORTED A BLEED ONE AND TWO OVERTEMP IN ICING CONDITIONS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AND TWO FAN AIR VALVE FILTERS, OPERATIONALLY, AND LEAK CHECK
- [SDR C2XA09RI156](https://openairdocs.org/sdr/C2XA09RI156.md): Sensor · inoperative · Sep 7, 2009 · N24103 · Emb EMB145XR · Outside Air Temperature Indicator/Sensor
  > FLIGHT 2463 - EWR - FLIGHT CREW REPORTED "TAT 2 HEAT INOP" INDICATION ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED TAT CURRENT SENSOR AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. ACFT WAS APPROVED TO RETURN
- [SDR C2XA09RI026](https://openairdocs.org/sdr/C2XA09RI026.md): Apu · leaking · Feb 19, 2009 · N24103 · Emb EMB145XR · APU Core Engine
  > FLT 2602 - EWR - FLIGHT CREW REPORTED STRONG FUEL SMELL ON T/O IN EWR AND XNA. RIC MX REMOVED AND REPLACED APU AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09CL018](https://openairdocs.org/sdr/C2XA09CL018.md): Line · cracked · Feb 9, 2009 · N24103 · Emb EMB145XR · APU Engine Fuel and Control
  > CLE FLIGHT NR 2267 THE CREW REPORTED A FUEL ODOR FOR 2-3 MINUTES AFTER APU SHUTDOWN. MX INSPECTED AND REPLACED THE FORWARD FUEL LINE FROM THE APU FUEL FILTER TO THE FUEL CONTROL UNIT. OPS CHECKS WERE GOOD AND NO FUEL ODOR WAS PRESENT.

Next page: https://openairdocs.org/aircraft/N24103/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 = 'N24103' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N24103/reports

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