# Service difficulty reports: N14173

A list on [N14173](https://openairdocs.org/aircraft/N14173.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 · 80 reports

- [SDR JJBA20221129029](https://openairdocs.org/sdr/JJBA20221129029.md): Skin · dented · Nov 26, 2022 · N14173 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENT HAS CREASE/GOUGE. DENT IS 3.75" X 2.25" AT FR 23-24, STR 12L-13L. DEPTH 0.125, FR 23 TO DENT IS 1", FR24 TO DENT IS 1.5", STR 13L TO DENT IS.75", STR 12L TO DENT IS 2.5". REMOVED SKIN CREASE/GOUGE. DENT FR 23-24 BTW STR 12L-13L. PERFORMED H
- [SDR JJBA20211228037](https://openairdocs.org/sdr/JJBA20211228037.md): None · none · Dec 28, 2021 · N14173 · Emb EMB145XR · Emergency Lighting
  > OVERWING EMERGENCY EXIT COVERS ARE LOOSE. RESECURED EMERGENCY EXIT COVERS
- [SDR JJBA20211205005](https://openairdocs.org/sdr/JJBA20211205005.md): None · none · Dec 5, 2021 · N14173 · Emb EMB145XR · Emergency Lighting
  > ROW 18 EMERGENCY LIGHTS DO NOT COME ON WHEN SWITCH IS ACTIVATED. CHARGED EMERGENCY LIGHT BATTERIES USING AC POWER. OPS CHECK OF EMERGENCY LIGHTS SAT. NO OTHER DEFECTS NOTED.
- [SDR JJBA20210803024](https://openairdocs.org/sdr/JJBA20210803024.md): Light · unsecure · Aug 3, 2021 · N14173 · Emb EMB145XR · Emergency Lighting
  > EMERGENCY PATH LIGHTING STRIP NEAR 1A IS DISLODGED. SECURED IN PLACED EMERGENCY PATH LIGHTING STRIP NEAR 1A WITH TAPE.
- [SDR JJBA20210528029](https://openairdocs.org/sdr/JJBA20210528029.md): Fan · odor · May 28, 2021 · N14173 · Emb EMB145XR · Air Distribution Fan
  > PLASTIC BURNING SMELL NEAR ROW 18, WITH VISIBLE SMOKE COMING FROM FLOOR VENT IN THE ISLE. FOUND CONDENSATION COMING FROM DISCONNECTED FAN #2 HOSE. RECONNECTED FAN #2 HOSE. NO SMOKE AND SMELL NOTED. OPS CHECK SAT.
- [SDR JJBA20210510001](https://openairdocs.org/sdr/JJBA20210510001.md): Instrument Panel · multiple fail · May 8, 2021 · N14173 · Emb EMB145XR · Electrical Power System
  > AVIONICS MASTER 2 LIGHTED WHILE PRESSED IN, CA MFD INOPERATIVE, FO PFD INOPERATIVE, #2 FMS INOPERATIVE, #2 RMU INOPERATIVE. R&R AVIONICS MASTER #2 PUSH BUTTON. PERFORMED AVIONICS MASTER SWITCH TEST. OPS CHECK SAT
- [SDR JJBA20210415051](https://openairdocs.org/sdr/JJBA20210415051.md): Sealant · missing · Apr 15, 2021 · N14173 · Emb EMB145XR · Main Landing Gear
  > REMOVED SEALANT AROUND THE RH AND LH MLG LOWER SIDE STRUT BEARING FLANGE. APPLIED SEALANT AROUND RH AND LH MLG LOWER SIDE STRUT BEARING.
- [SDR JJBA20210304002](https://openairdocs.org/sdr/JJBA20210304002.md): Light · misinstalled · Mar 4, 2021 · N14173 · Emb EMB145XR · Emergency Lighting
  > LH AND RH EXTERIOR OVER-WING EMERGENCY EXIT LIGHTS ARE INSTALLED UPSIDE DOWN. REMOVED AND REINSTALLED LH AND RH EXTERIOR OVER-WING EMERGENCY LIGHT EXIT PANELS.
- [SDR JJBA20210121034](https://openairdocs.org/sdr/JJBA20210121034.md): Shear Tie · corroded · Jan 21, 2021 · N14173 · Emb EMB145XR · Fuselage Internal Mounting Structure
  > CORROSION ON AFT SHEAR CLIP OF CARGO DOOR, AT FR 68 BETWEEN STR 15L-16L. ON AFT SHEAR CLIP OF CARGO DOOR, AT FR 68 BETWEEN STR 15L-16L CORROSION BLENDED OUT OF LIMITS. ON AFT SHEAR CLIP OF CARGO DOOR, AT FR 68 BETWEEN STR 15L-16L CUT. ON AFT SHEAR CLIP OF C
- [SDR JJBA20210121028](https://openairdocs.org/sdr/JJBA20210121028.md): Floor Support · corroded · Jan 21, 2021 · N14173 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CENTER OMEGA BEAM CORRODED ON TOP SURFACE (AFTER REMOVAL OF GUSSET) CORROSION LEVEL 2. CENTER OMEGA BEAM CORRODED ON TOP SURFACE BLENDED OUT OF LIMIT AT TWO PLACES. CENTER OMEGA DOUBLER REPAIRED PART LOCALLY FABRICATED. CENTER OMEGA BEAM AFT OF FR 59 AND FW
- [SDR JJBA20210121027](https://openairdocs.org/sdr/JJBA20210121027.md): Floor Support · corroded · Jan 21, 2021 · N14173 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > RT OMEGA BEAM CORRODED ON TOP SURFACE (AFTER REMOVAL OF GUSSET) CORROSION LEVEL 2. RT OMEGA BEAM CORRODED ON TOP SURFACE BLENDED OUT OF LIMIT AT TWO PLACES. RT OMEGA BEAM DOUBLER REPAIRED PART LOCALLY FABRICATED. RT OMEGA BEAM CUT OUT AFT OF FR 59 AMD FWD O
- [SDR JJBA20210121022](https://openairdocs.org/sdr/JJBA20210121022.md): Skin · chafed · Jan 21, 2021 · N14173 · Emb EMB145XR · Rudder, Plate/Skin
  > LT SIDE RUDDER 1, FRONT SPAR SKIN CHAFED ON 2 PLACES BETWEEN RIB ZV 2601.0 AND RIB ZV 3179.0. LT SIDE RUDDER 1, FRONT SPAR SKIN CHAFED ON 2 PLACES BETWEEN RIB ZV2601 AND ZV3179 BLENDED AREA FOR INVESTIGATION, CUT OUT DONE. LT SIDE RUDDER 1, FRONT SPAR SKIN R
- [SDR JJBA20210121021](https://openairdocs.org/sdr/JJBA20210121021.md): Doubler · corroded · Jan 21, 2021 · N14173 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > CARGO AREA UNDER FLOOR CORROSION FOUND RAD ALT ANTENNA. CORROSION LEVEL 2: AT REAR FUSELAGE RADIO ALT ANTENNA, DOUBLER AND LOUVER FOR INVESTIGATION CUT OUT DONE. CARGO AREA UNDER FLOOR RAD ALT ANTENNA REPAIR CARRIED OUT.
- [SDR JJBA20210120036](https://openairdocs.org/sdr/JJBA20210120036.md): Spar · cracked · Jan 20, 2021 · N14173 · Emb EMB145XR · Nacelle/Pylon, Main Frame
  > LT AND RT PYLON SPAR II 2X CRACK (ONE EACH SIDE) ON RIVET HOLE. 1 BUSHING (FLUSH-PYLON) LOCALLY FABRICATED, 1 BUSHING (PYLON) LOCALLY FABRICATED. DAMAGED HOLES ON LT + RT PYLON SPAR II AT ENGINE ATTACHMENT FITTINGS REPAIRED.
- [SDR JJBA20210120035](https://openairdocs.org/sdr/JJBA20210120035.md): Rivet · missing · Jan 20, 2021 · N14173 · Emb EMB145XR · Fuselage Main, Structure
  > BAGGAGE DOOR FWD TRACK RIVET MISSING LOWER END. AFTER INVESTIGATION BAGGAGE DOOR FWD TRACK FOUND CORRODED AND BLENDED OUT OF LIMITS AT RIVET HOLE LOCATION & 1 ANCHOR NUT HOLES BAGGAGE DOOR FWD 2 FRAME 65 REPAIRED.
- [SDR JJBA20210120033](https://openairdocs.org/sdr/JJBA20210120033.md): Doubler · corroded · Jan 20, 2021 · N14173 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE ANTENNA RAD ALT NO 1 INTERNAL DOUBLER CORRODED. CUT OUT DONE. DOUBLER HOLES PATTERN DRILLED ON SKIN. DOUBLER INSTALLED WITH FILLER.
- [SDR JJBA20210120032](https://openairdocs.org/sdr/JJBA20210120032.md): Floor Support · damaged · Jan 20, 2021 · N14173 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > DAMAGE ON LT CENTER FUSE 1 BETWEEN FR 23 JUNCTION 03 AND BETWEEN STR 19L-20L. DAMAGE ON LT CENTER FUSE 1 BETWEEN FR 23 JUNCTION 03 AND BETWEEN STR 19L-20L, AREA STRIPPED FOR INVESTIGATION. AN EXISTING BLEND IS FOUND ON LT CENTER FUSE 1 BETWEEN FR 23 - JUNCTI
- [SDR JJBA20210120031](https://openairdocs.org/sdr/JJBA20210120031.md): Skin · corroded · Jan 20, 2021 · N14173 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > CARGO AREA UNDER FLOOR FR 67 AROUND WATER DRAIN SKIN SHOW SIGN OF CORROSION, CORROSION LEVEL 2. CARGO AREA UNDER FLOOR FR 67 AROUND WATER DRAIN SKIN SHOW SIGN OF CORROSION OUT OF LIMITS REMOVED BY CUT OUT. REPAIR PARTS FAB, REPAIR CARRIED OUT. FOR SKIN REPR
- [SDR JJBA20210120030](https://openairdocs.org/sdr/JJBA20210120030.md): Skin · cracked · Jan 20, 2021 · N14173 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > RF 1 LT FUSELAGE SKIN AT FR 75.700 BELOW STGR 2L 2 CRACK FOUND AT ONE RIVET LOCATION. ON RF1 LT FUSELAGE SKIN AT FR 75.700 BELOW STGR 2L CUT OUT DONE. ON RF1 LT FUSELAGE SKIN AT FR 75.700 BELOW STGR 2L SKIN REPAIRED.
- [SDR JJBA20210120029](https://openairdocs.org/sdr/JJBA20210120029.md): Doubler · damaged · Jan 20, 2021 · N14173 · Emb EMB145XR · Fuselage Main, Bulkhead
  > PRESS BULKHEAD DOUBLER REPAIR EVALUATION FWD PRESS BULKHEAD AND REMOVE THE DOUBLER INSTALLED ON THE FORWARD PRESSURE BULKHEAD. DOUBLER REMOVED FOR REPAIR EVALUATION. NEW DOUBLER FABRICATED. INSTALLED NEW DOUBLER. NTD INSPECTION C/OUT BT MAGNIFYING GLASS X30
- [SDR JJBA20210112012](https://openairdocs.org/sdr/JJBA20210112012.md): Floor Support · cracked · Jan 12, 2021 · N14173 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CF3, LT OMEGA BEAM OUTBD ANGLE CRACKED. CF3, LT OMEGA BEAM OUTBD ANGLE REPAIRED.
- [SDR JJBA202002109002](https://openairdocs.org/sdr/JJBA202002109002.md): Light · inoperative · Feb 9, 2020 · N14173 · Emb EMB145XR · Emergency Lighting
  > ISLE PATH EMERGENCY PHOTO-LUMINESCENT INCORRECT AT 1A WITH EMERGENCY RED MARKS. R&R PHOTO-LUMINESCENT FLOOR STRIP LIGHT. NO FURTHER DEFECTS NOTED.
- [SDR JJBA2020013029008](https://openairdocs.org/sdr/JJBA2020013029008.md): Light · inoperative · Jan 29, 2020 · N14173 · Emb EMB145XR · Emergency Lighting
  > SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R&R SERVICE DOOR EXTERNAL EMERGENCY LIGHT.
- [SDR JJBA201912165005](https://openairdocs.org/sdr/JJBA201912165005.md): Lamp · inoperative · Dec 15, 2019 · N14173 · Emb EMB145XR · Emergency Lighting
  > SERVICE DOOR EXTERNAL EMERGENCY LIGHT FLICKERS. REMOVED AND REPLACED EMERGENCY LIGHT LAMP. OPS CHECK SAT.
- [SDR JJBA201904264016](https://openairdocs.org/sdr/JJBA201904264016.md): Sign · unsecure · Apr 24, 2019 · N14173 · Emb EMB145XR · Emergency Lighting
  > EXIT SIGN AT ROW 18 UNSECURED. RE-SECURED EXIT SIGN ON ROW 18. OPS CHECK SAT.
- [SDR JJBA2019040331015](https://openairdocs.org/sdr/JJBA2019040331015.md): Selector · malfunctioned · Mar 31, 2019 · N14173 · Emb EMB145XR · Trailing Edge Flap Control System
  > WHEN FLAP HANDLE WAS PLACED TO 0, FLAPS 9 INDICATED ON EICAS. R&R FLAP SELECTOR LEVER.
- [SDR JJBA20190319007](https://openairdocs.org/sdr/JJBA20190319007.md): Acm · seized · Mar 19, 2019 · N14173 · Emb EMB145XR · Cabin Cooling System
  > SMOKE IN THE COCKPIT AND CABIN. FOUND NR 1 ACM SEIZED. REMOVED AND REPLACED ACM. OPS CHECK OF NR 1 ACM SAT.
- [SDR JJBA20190103003](https://openairdocs.org/sdr/JJBA20190103003.md): Power Supply · inoperative · Jan 3, 2019 · N14173 · Emb EMB145XR · Emergency Lighting
  > BOTH OVER WING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY FOR OVER WING EXTERIOR EMERGENCY LIGHTS. OPS CHECK SAT.
- [SDR JJBA20181229032](https://openairdocs.org/sdr/JJBA20181229032.md): Cradle · defective · Dec 29, 2018 · N14173 · Emb EMB145XR · Emergency Lighting
  > LT AND RT EXTERNAL EMERGENCY LIGHTS ON CENTER FAIRINGS INOPERATIVE. R&R NR 4 EMERGENCY BATTERY CRADLE. OPS CHECK SAT.
- [SDR JJBA201812076004](https://openairdocs.org/sdr/JJBA201812076004.md): Skin · corroded · Dec 6, 2018 · N14173 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > AIRCRAFT DATA PLATE FORWARD RIGHT RIVET IS LOOSE AND SKIN AREA AT FORWARD SIDE HAS SURFACE CORROSION. CORROSION EXTENDS 100% THROUGH SKIN AND REQUIRES CUT-OUT AND REPAIR. PERFORMED CUT-OUT AND FABRICATED DOUBLER OUT OF ALCLAD 2024T3, 040" AND FILLER OUT OF ALC
- [SDR ASOA201710247023](https://openairdocs.org/sdr/ASOA201710247023.md): Structure · corroded · Oct 24, 2017 · N14173 · Emb EMB145XR · Vertical Stabilizer Miscellaneous Structure
  > A/C IS IN A C-CHECK STATUS WHEN INSPECTION FOUND THE RT VERTICAL STAB WITH CORROSION. MAINTENANCE REMOVED THE CORROSION IAW WITH SRM 55-30-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR ASOA201710247022](https://openairdocs.org/sdr/ASOA201710247022.md): Structure · corroded · Oct 24, 2017 · N14173 · Emb EMB145XR · Vertical Stabilizer Miscellaneous Structure
  > A/C IS IN A C-CHECK STATUS WHEN INSPECTION FOUND THE LT VERTICAL STAB WITH CORROSION. MAINTENANCE REMOVED THE CORROSION OF THE VERTICAL STAB IAW SRM 55-30-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.
- [SDR ASOA201710047021](https://openairdocs.org/sdr/ASOA201710047021.md): Shear Tie · corroded · Oct 4, 2017 · N14173 · Emb EMB145XR · Fuselage Internal Mounting Structure
  > CARGO DOOR CUT-OUT AT FRAME 65 LOWER SHEAR TIE CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE SHEAR TIE.
- [SDR ASOA201710047017](https://openairdocs.org/sdr/ASOA201710047017.md): Profile · damaged · Oct 4, 2017 · N14173 · Emb EMB145XR · Cargo/Baggage Doors
  > CARGO DOOR LOWER PROFILE IS DAMAGED ON FORWARD LOWER CORNER. REMOVED AND REPLACED LOWER PROFILE, PRIMED AND PAINTED.
- [SDR ASOA201612187008](https://openairdocs.org/sdr/ASOA201612187008.md): Battery · discharged · Dec 17, 2016 · N14173 · Emb EMB145XR · Emergency Lighting
  > EMERGENCY LIGHTS OPERATING OFF THE NR 2 EMERGENCY LIGHT BATTERY ARE INOP. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY. OPS CHECK GOOD.
- [SDR ASOA201612187009](https://openairdocs.org/sdr/ASOA201612187009.md): Carbon Seal · leaking · Dec 5, 2016 · N14173 · Emb EMB145XR · Turbine Engine Oil System
  > WHEN OPERATING ON ENGINE BLEEDS WITH PACKS ON, THERE WAS A SMELL OF OIL IN THE FLIGHT DECK WHEN AT LOW POWER SETTINGS. REMOVED AND REPLACED CARBON SEAL. OPS AND LEAK CHECKED GOOD. THIS AIRCRAFT WAS OUT OF SERVICE FROM 12/5/16 TO 12/18/16
- [SDR ASOA20160530034](https://openairdocs.org/sdr/ASOA20160530034.md): Acm · failed · May 30, 2016 · N14173 · Emb EMB145XR · Cabin Cooling System
  > THE CREW REPORTED SMOKE IN COCKPIT AND CABIN. MAINTENANCE INSPECTED AND REPLACED THE PACK NR 1 ACM. OPS CHECKS WERE GOOD.
- [SDR ASOA20160205004](https://openairdocs.org/sdr/ASOA20160205004.md): Battery Pack · inoperative · Feb 5, 2016 · N14173 · Emb EMB145XR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION THE CEILING EMERGENCY LIGHTS ABOVE ROW 12 AND LT/RT OVERWING EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE R & R NR 4 EMERGENCY LIGHT BATTERY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20151103056R](https://openairdocs.org/sdr/ASOA20151103056R.md): Battery Pack · inoperative · Nov 3, 2015 · N14173 · Emb EMB145XR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, THE NR 3 EMERGENCY LIGHT BATTERY WAS DISCOVERED INOPERATIVE. MAINTENANCE R & R THE NR 3 EMERGENCY LIGHT BATTERY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150821046](https://openairdocs.org/sdr/ASOA20150821046.md): Inverter · inoperative · Aug 21, 2015 · N14173 · Emb EMB145XR · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE LT SERVICE DOOR EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT INVERTER. OPS CHECKS WERE GOOD.
- [SDR ASOA20150526051](https://openairdocs.org/sdr/ASOA20150526051.md): Fuse · failed · May 26, 2015 · N14173 · Emb EMB145XR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, THE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R A BLOWN FUSE IN THE NR 4 EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED THE LIGHTS WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN
- [SDR ASOA20150218054V](https://openairdocs.org/sdr/ASOA20150218054V.md): Door Sill · corroded · Feb 18, 2015 · N14173 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL CORRODED BETWEEN FRAMES 20-22. R & R DOOR SILL IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150218053V](https://openairdocs.org/sdr/ASOA20150218053V.md): Support · corroded · Feb 18, 2015 · N14173 · Emb EMB145XR · Fuselage Main, Structure
  > CARGO LOWER BEAM CORRODED BETWEEN FRAMES 65-68. R & R CARGO DOOR LOWER CUTOUT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20141111132](https://openairdocs.org/sdr/ASOA20141111132.md): Light · odor · Nov 11, 2014 · N14173 · Emb EMB145XR · Passenger Compartment Lighting
  > THE CREW REPORTED AN ELECTRICAL BURNING ODOR FROM THE LAVATORY LIGHT AFTER THE LATCH WAS CLOSED. THE ACFT LANDED WITHOUT INCIDENT. R & R THE LIGHT BALLAST, OPS TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140927109](https://openairdocs.org/sdr/ASOA20140927109.md): Charger · inoperative · Sep 27, 2014 · N14173 · Emb EMB145XR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, BOTH AFT EXTERIOR OVERWING EMERGENCY LIGHTS WERE DISCOVERED INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY CHARGER ASSY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140922108](https://openairdocs.org/sdr/ASOA20140922108.md): Engine · leaking · Sep 22, 2014 · N14173 · Emb EMB145XR · Engine (Turbine/Turboprop)
  > CREW REPORTED A LAVATORY SMOKE WARNING ON EICAS AFTER TAKEOFF. ACFT PERFORMED AN AIR TURN BACK WHERE IT LANDED WITHOUT INCIDENT. NR 2 ENGINE WAS R & R AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130813149H](https://openairdocs.org/sdr/ASOA20130813149H.md): Skin · cracked · Aug 15, 2013 · N14173 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING 2A INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 79 BELOW STRINGER 05R. MX REMOVED THE DAMAGE AROUND THE RIVET AND PERFORMED A BUSHING REPAIR IAW DER APPROVED TECHL DISPOSITION ETD2013-145-029290, AND THE ACFT WAS APP
- [SDR ASOA2013153](https://openairdocs.org/sdr/ASOA2013153.md): Skin · cracked · Aug 13, 2013 · N14173 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING 2A INSPECTION, THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 77 BELOW STRINGER 03L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR IAW DER APPROVED TECH DISPOSITION ETD2013-145-029290, AND THE ACFT WAS APPROVED FOR RETURN T
- [SDR ASOA20130813152](https://openairdocs.org/sdr/ASOA20130813152.md): Skin · cracked · Aug 13, 2013 · N14173 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING 2A INSPECTION THE LT AFT FUSELAGE SKIN WAS FOUND TO HAVE A CRACK AT A RIVET ON FRAME 77 BELOW STRINGER 08L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR IAW DER APPROVED TECH DISPOSITION ETD2013-145-029290, AND THE ACFT WAS APPROVED FOR RETURN
- [SDR ASOA20130813151H](https://openairdocs.org/sdr/ASOA20130813151H.md): Skin · cracked · Aug 13, 2013 · N14173 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING 2A INSPECTION THE LT AFT FUSELAGE SKIN WAS FOUND TO HAVE 3 EA CRACKS TOTALING 6.74MM (.026") AT A RIVET ON FRAME 79 BELOW STRINGER 05L. MX REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR IAW DER APPROVED TECH DISPOSITION ETD2013-145-029290, AND THE A

Next page: https://openairdocs.org/aircraft/N14173/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 = 'N14173' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N14173/reports

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