# Service difficulty reports: N18102, cancelled Mar 13, 2025

A list on [N18102, cancelled Mar 13, 2025](https://openairdocs.org/deregistered/N18102-2025-03-13.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 RAIA2019080631001](https://openairdocs.org/sdr/RAIA2019080631001.md): Angle · corroded · Jul 31, 2019 · N18102 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CUTOUT FWD LATERAL "L" SHAPE ANGLE HAVE CORROSION AT FRAME 65 LOWER CORNER IN 3 PLACES. REMOVED AND REPLACED L ANGLE
- [SDR RAIA201905190001](https://openairdocs.org/sdr/RAIA201905190001.md): Control System · inoperative · May 19, 2019 · N18102 · Emb EMB145XR · Power Indicating System
  > E1 OPERATING 9% BELOW N1 RATING DURING CLIMBOUT. A/C IS STILL IN WORK. SUPPLIMENTAL INFORMATION FROM ORIGINAL ENTRY. R&R CONTROL STAND ASSEMBLY. OPS CHECK GOOD.
- [SDR RAIA2018082960001](https://openairdocs.org/sdr/RAIA2018082960001.md): Fuel Cell · leaking · Aug 26, 2018 · N18102 · Emb EMB145XR · Fuel Storage
  > LEFT WING HAD FLUID COMING FROM IT DURING FLT. FOUND FUEL TO BE LEAKING FROM BOTTOM OF LT WING 18 INCHES FWD OF THE JACK POINT FROM SKIN JOINT. CLASSIFIED AS RUNNING LEAK IN TYPE I AREA. SEALED THE INNER SKIN OF FUEL TANK. LEAK CHECKED GOOD.
- [SDR RAIA201806050001](https://openairdocs.org/sdr/RAIA201806050001.md): Fan · malfunctioned · Jun 5, 2018 · N18102 · Emb EMB145XR · Air Distribution Fan
  > COCKPIT RECIR FAN INOP IN FLIGHT. R&R RECIRC FAN OPS TEST GOOD.
- [SDR RAIA201803160001](https://openairdocs.org/sdr/RAIA201803160001.md): Hydraulic System · malfunctioned · Mar 16, 2018 · N18102 · Emb EMB145XR · Hydraulic System, Main
  > IN FLIGHT, THE NR 1 HYDRALIC PUMP FAILED, CAUSING THE NR 1 HYDRAULIC SYSTEM TO FAIL. INSPECTED THE NR 1 HYDRALIC SYSTEM FLUID LEVEL, FOUND GOOD. GV INSPECTED BOTH PUMPS, RAN BOTH PUMPS INDIVIDUALLY AND TOGETHER MOVING FLIGHT CONTROLS AND APLYING BRAKES. A
- [SDR RAIA201705120001](https://openairdocs.org/sdr/RAIA201705120001.md): Bolt · broken · May 12, 2017 · N18102 · Emb EMB145XR · Main Landing Gear Strut/Axle/Truck
  > LG LEVER DISAGREE EICAS WARNING AFTER DEPARTURE WITH A RED HATCHED BOX OVER LEFT MAIN LANDING GEAR INDICATOR. REMOVED AND REPLACED BROKEN TOP BOLT OF LT SHOCK ABSORBER. FERRIED AIRCRAFT TO STL. REMOVED AND REPLACED LT MAIN LANDING GEAR LEG STRUCTURE ASSY DUE T
- [SDR RAIA201612210001](https://openairdocs.org/sdr/RAIA201612210001.md): Bulb · inoperative · Dec 21, 2016 · N18102 · Emb EMB145XR · Emergency Lighting
  > CEILING EMERGENCY LIGHT AT ROW 18 INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.
- [SDR RAIA201605170001](https://openairdocs.org/sdr/RAIA201605170001.md): Radar · inoperative · May 17, 2016 · N18102 · Emb EMB145XR · Weather Radar System
  > RADAR WILL PAINT AN IMAGE ON THE RT SWEEP BUT ERASES EITHER SOME OR ALL OF THE IMAGE ON THE LT SWEEP. THIS OCCURED ON ALL RANGES AND ON BOTH MFD'S. R & R WEATHER RTA ASSEMBLY. OPS CHECK GOOD.
- [SDR RAIA201605070001](https://openairdocs.org/sdr/RAIA201605070001.md): Control Panel · inoperative · May 7, 2016 · N18102 · Emb EMB145XR · Emergency Lighting
  > ALL EMERGENCY LIGHTS WILL NOT COME ON WITH SWITCH ON F/A'S CONTROL PANEL. R & R F/A CONTROL PANEL. OPS CHECK GOOD.
- [SDR RAIA201603220001](https://openairdocs.org/sdr/RAIA201603220001.md): Engine · leaking · Mar 22, 2016 · N18102 · Emb EMB145XR · Turbine Engine Oil System
  > ON TAKEOFF AT 100 KNOTS, STRONG SMOKE/BURNING ODOR WITH A LIGHT BLUE HAZE IN THE COCKPIT, ALSO NOTICED IN THE CABIN, EMERGENCY LANDING. MAINTENANCE REPLACED NR 1 ENGINE, LEAK AND OPS CHECK GOOD.
- [SDR RAIA201603170001](https://openairdocs.org/sdr/RAIA201603170001.md): Light · inoperative · Mar 17, 2016 · N18102 · Emb EMB145XR · Emergency Lighting
  > LARGE EMERGENCY EXIT LIGHT ON SIDEWALL PANEL AT ROW 18A IS INOPERATIVE. MAINTENANCE DISCONNECTED CONNECTORS, INSPECTED, RECONNECTED CONNECTORS, NO DEFECTS NOTED, OPS CHECK GOOD.
- [SDR RAIA201602280001](https://openairdocs.org/sdr/RAIA201602280001.md): Hydraulic System · unknown · Feb 28, 2016 · N18102 · Emb EMB145XR · Hydraulic System, Main
  > STEADY LOSS OF HYDRAULIC FLUID IN FLIGHT. DID A FULL HYDRAULIC TEST AND LEAK CHECK OF NR 1 SYSTEM HYDRAULICS. NO DEFECTS FOUND AT THIS TIME. SERVICE HYDRAULIC FLUID TO FULL.
- [SDR RAIA201507280002](https://openairdocs.org/sdr/RAIA201507280002.md): Light · unknown · Jul 28, 2015 · N18102 · Emb EMB145XR · Emergency Lighting
  > PAX DOOR SWING ARM EMERGENCY LIGHT IS INOPERATIVE. OPS CHECKED EMERGENCY LIGHT. OPS CHECKED GOOD.
- [SDR ASOA20121117132](https://openairdocs.org/sdr/ASOA20121117132.md): Frame · cracked · Nov 18, 2012 · N18102 · Emb EMB145XR · Fuselage Main, Frame
  > DURING C-CHECK, FRAME 10 CRACKED UNDER RT DV WINDOW CUTOUT. VERIFIED WITH EDDY CURRENT. MX R & R FRAME 10 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121117131](https://openairdocs.org/sdr/ASOA20121117131.md): Frame · cracked · Nov 17, 2012 · N18102 · Emb EMB145XR · Fuselage Main, Frame
  > DURING C-CHECK, FRAME 10 CRACKED UNDER LT DV WINDOW CUTOUT. VERIFIED WITH EDDY CURRENT. MX R & R FRAME 10 UNDER LT DV WINDOW IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121117130](https://openairdocs.org/sdr/ASOA20121117130.md): Frame · bent · Nov 17, 2012 · N18102 · Emb EMB145XR · Fuselage Main, Frame
  > DURING C-CHECK, FRAME 72 BENT AT STRINGER 15L-16L. MX R & R FRAME 72, BETWEEN 16L AND 13R IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121117129](https://openairdocs.org/sdr/ASOA20121117129.md): Frame Splice · cracked · Nov 17, 2012 · N18102 · Emb EMB145XR · Fuselage Main, Frame
  > DURING C-CHECK, FRAME 72 SPLICE CRACKED AT STRINGER 15L-16L. MX R & R FRAME 72 SPLICE AT FRAME 72, STRINGER 15L AND 16L IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121117128](https://openairdocs.org/sdr/ASOA20121117128.md): Frame · cracked · Nov 17, 2012 · N18102 · Emb EMB145XR · Fuselage Main, Frame
  > DURING C-CHECK,K FRAME 72 CRACKED AT RIVET ON STRINGER 16L. MX R & R FRAME 72 BETWEEN STRINGER 16L AND 13R IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121117127](https://openairdocs.org/sdr/ASOA20121117127.md): Floorbeam · corroded · Nov 17, 2012 · N18102 · Emb EMB145XR · Fuselage Main, Floor Beam
  > DURING C-CHECK CENTER FLOORBEAM AT FRAME 49 AREA HAS CORROSION. MX COMPLETED AND INSTALLED THE FABRICATED REPAIR DOUBLER AT CENTER FLOORBEAM AT FRAME 49 AREA IAW EC5310-01466. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121117126](https://openairdocs.org/sdr/ASOA20121117126.md): Floorbeam · corroded · Nov 17, 2012 · N18102 · Emb EMB145XR · Fuselage Main, Floor Beam
  > DURING C-CHECK, LT FLOORBEAM AT FRAME 38 CROSSBEAM AREA HAS CORROSION. MX COMPLETED REPAIR ON LT FLOORBEAM AT FRAME 38 IAW SRM 53-00-10. DETERMINED TO BE A MINOR IAW SOP 5702. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121117125](https://openairdocs.org/sdr/ASOA20121117125.md): Floor Support · corroded · Nov 17, 2012 · N18102 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, LT OMEGA BEAM AT FRAME 59 CROSSBEAM AREA HAS CORROSION. MX COMPLETED INSTALL OF LT OMEGA BEAM REPAIR AT FRAME 59 CROSSBEAM AREA IAW EC5310-01466 ORIG AND IAW SRM 53-00-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121117124V](https://openairdocs.org/sdr/ASOA20121117124V.md): Floor Support · corroded · Nov 17, 2012 · N18102 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DURING C-CHECK, RT OMEGA BEAM AT FRAME 23 IS CORRODED AT NUTPLATE. MX FABRICATED AND INSTALLED REPAIR DOUBLER AT RT OMEGA BEAM AT FRAME 23 AT NUTPLATE IAW EC5320-01443, REV C. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201112140008](https://openairdocs.org/sdr/ASOA201112140008.md): Control Unit · failed · Dec 14, 2011 · N18102 · Emb EMB145XR · Communications System
  > ADC 1 WENT OUT IN FLIGHT. R & R NR 1 COMMS UNIT IAW AMM 23-00-01. OPS CHECKED GOOD, ACFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA11IA220](https://openairdocs.org/sdr/C2XA11IA220.md): Apu · malfunctioned · Sep 17, 2011 · N18102 · Emb EMB145XR · APU Core Engine
  > IAH - FLIGHT 2373 THE CREW REPORTED THAT THE APU FAILED ON ROTATION OUT OF JAX WITH AN APU OIL LO PRESS MESSAGE AND A BURNING OIL ODOR. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU AND PLACED IT ON MEL 49-00-0
- [SDR C2XA11TY125](https://openairdocs.org/sdr/C2XA11TY125.md): Case · fod · Jul 25, 2011 · N18102 · Emb EMB145XR · Turbine Engine Air Inlet Section
  > TYS - A/C WAS FERRIED FRON BNA TO TYS FOR FOD DAMAGE WHERE MAINTENANCE REMOVED AND REPLACED THE FAN CASE (PN-145-75001-409-SN-NC1476); MULTIBLE BYPASS VANES (PN-23067033) BOROSCOPE NR 1 ENGINE IAW RR MM 05--50-200-804 AND RR MM 72-50-00-801, NO DAMAGE OR DEFEC
- [SDR C2XA11RI085](https://openairdocs.org/sdr/C2XA11RI085.md): Controller · defective · May 23, 2011 · N18102 · Emb EMB145XR · Cabin Pressure Controller
  > FLIGHT 2398 - EWR - FLIGHT CREW REPORTED PRESSURIZATION DIFFERENTIAL READS ABOUT 1-2 PSI LOWER THAN IT SHOULD AT ALL ALTITUDES - FL350- 5.9 PSI. EWR MX REMOVED AND REPLACED DIGITAL AND MANUAL PRESSURIZATION CONTROLLERS. EWR MX PERFORMED OPERATIONAL CHECK SUC
- [SDR C2XA11RI084](https://openairdocs.org/sdr/C2XA11RI084.md): Controller · defective · May 23, 2011 · N18102 · Emb EMB145XR · Cabin Pressure Controller
  > FLIGHT 2398 - EWR - FLIGHT CREW REPORTED PRESSURIZATION DIFFERENTIAL READS ABOUT 1-2 PSI LOWER THAN IT SHOULD AT ALL ALTITUDES - FL350- 5.9 PSI. EWR MX REMOVED AND REPLACED DIGITAL AND MANUAL PRESSURIZATION CONTROLLERS. EWR MX PERFORMED OPERATIONAL CHECK SUC
- [SDR C2XA11SH046](https://openairdocs.org/sdr/C2XA11SH046.md): Floor Support · corroded · Feb 21, 2011 · N18102 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 20. REPLACED OMEGA BEAM IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA11SH045](https://openairdocs.org/sdr/C2XA11SH045.md): Skin · cracked · Feb 21, 2011 · N18102 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > SHV - DURING C-CHECK FUSELAGE SKIN IS CRACKED AROUND RIVETS AT FR 80. REPAIRED SKIN IAW EC5330-02364. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR C2XA10RI153](https://openairdocs.org/sdr/C2XA10RI153.md): Controller · inoperative · Dec 2, 2010 · N18102 · Emb EMB145XR · Cabin Pressure Controller
  > FLIGHT 2451 - STL - FLIGHT CREW REPORTED AUTO PRESS INOP IN FLIGHT AND DECLARED EMERGENCY DESCENT INTO STL. IAH MX REMOVED AND REPLACED AUTO PRESS CONTROLLER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09TY200](https://openairdocs.org/sdr/C2XA09TY200.md): Sill · corroded · Jul 30, 2009 · N18102 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > TYS - A/C CURRENTLY IN C-CHECK WHEN INSPECTION FOUND CORROSION ON THE RIGHT FLOOR SILLS FROM FRAME 29 THRU FRAME 48 OUT OF MFG LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILLS IAW EMB 145XR SRM 51040-02. A/C WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR C2XA09TY198](https://openairdocs.org/sdr/C2XA09TY198.md): Sill · corroded · Jul 30, 2009 · N18102 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > TYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE LEFT FLOOR SILLS FROM FRAME 19A TO FRAME 36 CORRODED BEYOND MFG'S LIMITS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILLS IAW EMB 145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEA
- [SDR C2XA09TY205](https://openairdocs.org/sdr/C2XA09TY205.md): Floor Support · corroded · Jul 29, 2009 · N18102 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LT OMEGA BEAM TOP CAP IN LAV BETWEEN FRM 59-62 IS CORRODED AROUND RIVETS AND NUT PLATES. BLENDED OUT CORROSION AND IS WITHIN LIMITS, ALODINED, PRIMED AND PAINTED.
- [SDR C2XA09TY204](https://openairdocs.org/sdr/C2XA09TY204.md): Mount · corroded · Jul 29, 2009 · N18102 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LT FRM MOUNT FOR LT CARBON FIBER BEAM BULKHEAD SUPPORT AT FRM 61 HAS CORROSION AT LOWER EDGE. BLENDED CORRODED AREA, FABRICATED EXTERNAL DOUBLERS, ALODINED, PRIMED AND PAINTED IAW EC5320-01462.
- [SDR C2XA09TY202](https://openairdocs.org/sdr/C2XA09TY202.md): Flange · corroded · Jul 29, 2009 · N18102 · Emb EMB145XR · Nacelle/Pylon Miscellaneous Structure
  > NR 1 ENG INLET ATTACH FLANGE HAS CORROSION AROUND BOLT HOLES. REAMED AND INSTALLED BUSHING IAW EC5420-01158.
- [SDR C2XA09TY196](https://openairdocs.org/sdr/C2XA09TY196.md): Sill · corroded · Jul 29, 2009 · N18102 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > RT FLOORBOARD SILL BETWEEN FRM 53-60 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL.
- [SDR C2XA09TY195](https://openairdocs.org/sdr/C2XA09TY195.md): Sill · corroded · Jul 29, 2009 · N18102 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LT FLOORBOARD SILL BETWEEN FRMS 53-60 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOOR SILL.
- [SDR C2XA09TY194](https://openairdocs.org/sdr/C2XA09TY194.md): Floor Support · corroded · Jul 29, 2009 · N18102 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > RT OMEGA BEAM TOP CAP IN LAV HAS CORROSION UNDER CARBON BEAM AT FRM 61. REMOVED AND REPLACED TOP CAP.
- [SDR C2XA09TY191](https://openairdocs.org/sdr/C2XA09TY191.md): Floor Support · corroded · Jul 28, 2009 · N18102 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LT OMEGA BEAM TOPCAP IN LAV BETWEEN FRMS 59-62 IS CORRODED AROUND RIVETS AND NUT PLATES. BLENDED OUT CORROSION, IS WITHIN LIMITS. ALODINED, PRIMED AND PAINTED.
- [SDR C2XA09TY190](https://openairdocs.org/sdr/C2XA09TY190.md): Sill · corroded · Jul 28, 2009 · N18102 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LT SIDE FLOORBOARD SILL BETWEEN FRM 41-48 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SILL.
- [SDR C2XA09TY189](https://openairdocs.org/sdr/C2XA09TY189.md): Sill · corroded · Jul 28, 2009 · N18102 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > RT FLOORBOARD SILL BETWEEN FRM 48-53 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOOR SILL.
- [SDR C2XA09TY188](https://openairdocs.org/sdr/C2XA09TY188.md): Sill · corroded · Jul 28, 2009 · N18102 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LT SIDE OF FLOOBOARD SILL BETWEEN FRM 29-35 HAS CORROSION BEYOND LIMITS. REMOVED AND REPLACED FLOOR SILL.
- [SDR C2XA09TY183](https://openairdocs.org/sdr/C2XA09TY183.md): Sill · corroded · Jul 24, 2009 · N18102 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > TYS - THE RIGHT FLOOR SILL BETWEEN FR 59 THRU 61 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLOOR SILL IAW 145XR SRM 51-40-02 AND CPM 51-21-03, 04, 06.
- [SDR C2XA09TY182](https://openairdocs.org/sdr/C2XA09TY182.md): Bracket · corroded · Jul 24, 2009 · N18102 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > TYS - THE LAV FLOOR TOPCAP HAS SURFACE CORROSION UNDER THE POTABLE WATER OVERFILL B-NUT. MAINTENANCE REMOVED AND REPLACED THE WATER POTABLE SUPPORT BRACKET IAW EMB 145XR SRM 51-40-02, 03, 04 AND CPM 51-21-O5. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UP
- [SDR C2XA09TY181](https://openairdocs.org/sdr/C2XA09TY181.md): Sill · corroded · Jul 24, 2009 · N18102 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > TYS - CORROSION WAS FOUND ON THE LEFT SILL BETWEEN FR 59 TO FR 60. MAINTENANCE REMOVED AND REPLACED THE SILL IAW EMB A45XR SRM 51-40-02 AND CPM 51-21-04-05-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR C2XA09TY172](https://openairdocs.org/sdr/C2XA09TY172.md): Attach Fitting · corroded · Jul 22, 2009 · N18102 · Emb EMB145XR · Nacelle/Pylon Miscellaneous Structure
  > NR 2 ENG INLET ATTACH FLANGE HAS CORROSION AROUND 9 NUT PLATE HOLES. REAMED TO REMOVE CORROSION AND INSTALLED BUSHINGS IAW EC5420-01158.
- [SDR C2XA09TY168](https://openairdocs.org/sdr/C2XA09TY168.md): Skin · chafed · Jul 22, 2009 · N18102 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > TYS - A/C IN A C-CHECK STATUS WHEN THE VENTRAL TANK WAS FOUND CHAFING THE LOWER FORWARD EDGE OF BELLY SKIN. MAINTENANCE BLENDED AREA AND FOUND TO BE WITHIN LIMITS. WORK WAS ACCOMPLISHED IAW EMB 145XR SRM 51-10-03. ALODINED, PRIMED AND PAINTED IAW CPM 51-21-
- [SDR C2XA09SH192](https://openairdocs.org/sdr/C2XA09SH192.md): Inverter · inoperative · Jul 6, 2009 · N18102 · Emb EMB145XR · Emergency Lighting
  > RIGHT OVERWING EXIT SHROUD EXIT IDENTIFIER SIGN INOPERATIVE. REMOVED AND REPLACED NR 3 DC/AC INVERTER P/N 7824-1, S/N ILLEGIBLE WITH P/N 7824-1 S/N PT4563 IAW EMB145XR AMM 33-50-11 AND OPS CHECKED GOOD.
- [SDR C2XA09RI122](https://openairdocs.org/sdr/C2XA09RI122.md): Light · broken · Jun 19, 2009 · N18102 · Emb EMB145XR · Emergency Lighting
  > FLIGHT CREW REPORTED EMERGENCY LIGHT STRIP BROKEN. MX REMOVED AND REPLACED LIGHT STRIP AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA09TY082](https://openairdocs.org/sdr/C2XA09TY082.md): Fuse · blown · May 4, 2009 · N18102 · Emb EMB145XR · Emergency Lighting
  > TYS - DURING ROUTINE MX BOTH OVERWING EMERGENCY LIGHTS WERE FOUND INOP. THE NR 4 BATTERY FUSES WERE REMOVED AND REPLACED AND OPS CHECKED GOOD IAW RADIANT POWER CORP VCMM 25-60-03.

Next page: https://openairdocs.org/deregistered/N18102-2025-03-13/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 = 'N18102' AND deregistration_id = 'N18102-2025-03-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N18102-2025-03-13/reports

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