# Service difficulty reports: N14180

A list on [N14180](https://openairdocs.org/aircraft/N14180.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 · 85 reports

- [SDR JJBA20221121016](https://openairdocs.org/sdr/JJBA20221121016.md): Actuator Cable · jammed · Nov 18, 2022 · N14180 · Emb EMB145XR · Passenger/Crew Doors
  > MAIN CABIN DOOR WON'T OPEN, ACTUATING MECHANISM JAMMED. INSPECTED AND FOUND MAIN DOOR FORWARD LOCK JAMMING. ADJUSTED MAIN CABIN DOOR CABLE D TO FRONT LOCK BOX. FOUND AFT LOCKING-MECHANISM CAM OVER CENTER. THE LOCKING FORCE OUT OF LIMITS (ON LOW SIDE WITH FORCE
- [SDR JJBA20211027060](https://openairdocs.org/sdr/JJBA20211027060.md): None · none · Oct 27, 2021 · N14180 · Emb EMB145XR · Emergency Lighting
  > MCD EXTERIOR EMERGENCY LIGHT INOPERATIVE. R&R MCD EXT EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT.
- [SDR JJBA20210611019](https://openairdocs.org/sdr/JJBA20210611019.md): Skin · dented · Jun 11, 2021 · N14180 · Emb EMB145XR · Wing, Plate/Skin
  > LH WING INBD LEADING EDGE HAS A DENT. ACCOMPLISHED PERMANENT REPAIR TO THE LEFT HAND WING LEADING EDGE 1 BY REMOVING DAMAGE, NDT PERFORMED. FABRICATED AND INSTALLED REPAIR PARTS
- [SDR JJBA20210607013](https://openairdocs.org/sdr/JJBA20210607013.md): Floor Support · corroded · Jun 7, 2021 · N14180 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORTS IN MIDDLE SECTION (FR 23-FR 59) POSSIBLE CORROSION. EVALUATED AREA RH FLOOR SUPPORT BTW FR 23-25, FR53-57. FOUND TO BE IN LIMIT, APPLIED ALODINE AND PRIME. AREA AT RH BTW FR 25-36, FR 37-41, LH BTW FR 21-23, FR 23-25, FR 28-40, FR 29-35, F
- [SDR JJBA20210606012](https://openairdocs.org/sdr/JJBA20210606012.md): Floorbeam · corroded · Jun 6, 2021 · N14180 · Emb EMB145XR · Fuselage Main, Floor Beam
  > LAV FLOOR BEAMS BL 19L, BL 0, BL 19R SIGNS OF CORROSION. EVALUATED AND REMOVED CORROSION ON LAV FLOOR BEAMS. FOUND TO BE 100% OUT OF LIMITS. REMOVED AND INSTALLED NEW GUSSETS ON BL 0 AND BL 19. REMOVED AND FABRICATED NEW GUSSET FOR LBL19 AND INSTALLED NEW GUSS
- [SDR JJBA20210604011](https://openairdocs.org/sdr/JJBA20210604011.md): Seat Track · damaged · Jun 4, 2021 · N14180 · Emb EMB145XR · Fuselage, Seat/Cargo Attach Fittings
  > LH COCKPIT SEAT TRACK HAVE ELONGATED HOLES (LH AND RH SIDE) AND CHAFFED. EVALUATED LH COCKPIT SEAT TRACK. FOUND TO BE OUT OF LIMITS. COUNTER SIDE EXCEEDS THE MINIMUM REQUIREMENT. REMOVED AND REPLACED SEAT TRACK LH.
- [SDR JJBA20210602007](https://openairdocs.org/sdr/JJBA20210602007.md): Floor Support · corroded · Jun 2, 2021 · N14180 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORTS IN FWD SECTION (FWD OF FR 23) POSSIBLE CORROSION. REMOVED CORROSION ON GUSSET AND BEAM ASTER EVAL. FOUND BOTH PARTS TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW GUSSET AND BEAM AT FR 16 TO FR 24 BL-O AND FR 20 BL-O. TREATED, PRIMED, TOP
- [SDR JJBA20210522026](https://openairdocs.org/sdr/JJBA20210522026.md): Seat Track · damaged · May 22, 2021 · N14180 · Emb EMB145XR · Fuselage, Seat/Cargo Attach Fittings
  > RH COCKPIT SEAT TRACK HAVE ELONGATED HOLES (LH SIDE AND RH SIDE) AND CHAFED. REMOVED AND REPLACED 2 EA TRACKS AT RH COCKPIT (LH SIDE AND RH SIDE).
- [SDR JJBA20210519021](https://openairdocs.org/sdr/JJBA20210519021.md): Reinforcement · corroded · May 19, 2021 · N14180 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > PAX DOOR THRESHOLD REINFORCING STRUCTURE HAS CORROSION THREE DIFFERENT BRACKETS. REMOVED AND REPLACED 2 NEW BRACKETS ON PAX DOOR OUTBD BRACKETS PAINT DAMAGE ONLY.
- [SDR JJBA20210518019](https://openairdocs.org/sdr/JJBA20210518019.md): Hinge · worn · May 18, 2021 · N14180 · Emb EMB145XR · Fuselage, Door Hinge
  > PAX DOOR, UPPER SIDE HINGE ATTACHMENT FITTING HAS WEAR MARKS AND GAUGING. BLENDED OUT DAMAGE.
- [SDR JJBA20210518018](https://openairdocs.org/sdr/JJBA20210518018.md): Hinge · cracked · May 18, 2021 · N14180 · Emb EMB145XR · Fuselage, Door Hinge
  > PAX DOOR, LWR SIDE HINGE ATTACHMENT FITTING HAS CRACK MARK. BLENDED OUT DAMAGE.
- [SDR JJBA20210518017](https://openairdocs.org/sdr/JJBA20210518017.md): Floorbeam · corroded · May 18, 2021 · N14180 · Emb EMB145XR · Fuselage Main, Floor Beam
  > FRM 23, 15R, RBL 0.0'-27.0" FLOOR BOARD SUPPORT BEAM HAS CORROSION (FLOOR STRUCTURE). REMOVED AND REPLACED ANGLE (SUPPORT).
- [SDR ASOA2020031184003](https://openairdocs.org/sdr/ASOA2020031184003.md): Light · overheated · Mar 8, 2020 · N14180 · Emb EMB145XR · Passenger Compartment Lighting
  > IAH - FLIGHT 4328, THE CREW REPORTED CEILING LIGHT SMOKE SMELL 1A & 2A. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE AFFECTED CEILING LIGHT ON MEL 33-20-00-2, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE
- [SDR ASOA2019041065049](https://openairdocs.org/sdr/ASOA2019041065049.md): Ground Stud · damaged · Apr 6, 2019 · N14180 · Emb EMB145XR · Light System Wiring
  > CREW REPORTED ROW 18 EMERGENCY LIGHTS WILL NOT ILLUMINATE FACING A/C FRONT BACK SIDE WORKS. MX INSPECTED AND FOUND W192-8819-22N (GROUND STUD GS8517DC) DAMAGED REPAIRED ITEMS OPERATIONAL CHECKS GOOD IAW EMB 145 XRJ AMM 33-50-50 (20-13-05) A/C WAS APPROVED FOR
- [SDR ASOA201807095161](https://openairdocs.org/sdr/ASOA201807095161.md): Inverter · inoperative · Jul 9, 2018 · N14180 · Emb EMB145LR · Emergency Lighting
  > DURING MX INSPECTION THE LOWER EMERGENCY LIGHT ON THE SERVICE DOOR WAS INOP. MX REMOVED AND REPLACED THE NR 2 INVERTER WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA201806267116](https://openairdocs.org/sdr/ASOA201806267116.md): Fitting · cracked · Jun 26, 2018 · N14180 · Emb EMB145XR · Nacelle/Pylon Miscellaneous Structure
  > TYS A/C CAME IN FOR A 2A INSPECTION WHEN INSPECTION FOUND THE LEFT ENGINE LOWER FWD AFT FITTING CRACKED AND VERIFIED BY NDT METHODS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW EA 26-2014-063. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AFTER ALL WORK IS C
- [SDR ASOA201702020046](https://openairdocs.org/sdr/ASOA201702020046.md): Skin · cracked · Feb 2, 2017 · N14180 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DURING C-CK. FUSELAGE SKIN CRACK AT FR 75 BTW STR 2L-3L. REPAIRED FUSELAGE SKIN IAW SRM 53-31-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160912046](https://openairdocs.org/sdr/ASOA20160912046.md): Computer · faulted · Sep 12, 2016 · N14180 · Emb EMB145XR · Central Computers
  > CREW REPORTED THE ACFT GOES INTO R/O AND G/A MODE DURING TAKEOFF AND ON APPROACH AND UNABLE TO SWITCH OUT OF IT. MAINTENANCE R & R IC-600 NR 2 WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20160912049C](https://openairdocs.org/sdr/ASOA20160912049C.md): Computer · malfunctioned · Sep 12, 2016 · N14180 · Emb EMB145XR · Flight Control System
  > THE CREW REPORTED THE AIRCRAFT GOES INTO A ROLL AND GA MODE DURING TAKOFF AND ON APPROACH AND UNABLE TO SWITCH OUT OF IT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 IC600 COMPUTER. OPS CHECKED GOOD.
- [SDR ASOA20150815045](https://openairdocs.org/sdr/ASOA20150815045.md): Yoke · cracked · Aug 15, 2015 · N14180 · Emb EMB145XR · Nacelle/Pylon, Main Frame
  > DURING MAINTENANCE THE NR 2 ENGINE FORWARD LOWER YOKE FITTING WAS FOUND CRACKED. MAINTENANCE REPLACED THE NR 2 ENGINE YOKE FITTING IAW STS EA 26-2014-063.
- [SDR ASOA20150620059](https://openairdocs.org/sdr/ASOA20150620059.md): Inverter · inoperative · Jun 20, 2015 · N14180 · Emb EMB145XR · Emergency Lighting
  > DURING PREFLIGHT THE EXIT ROW EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20150318019](https://openairdocs.org/sdr/ASOA20150318019.md): Controller · failed · Mar 18, 2015 · N14180 · Emb EMB145XR · Windshield/Door Rain/Ice Removal
  > THE CREW REPORTED WINDSHIELD HEAT NR 1 FAIL RESULTING IN ELECTRICAL OVERHEAT SMELL. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS WINDSHIELD HEAT TEMP CONTROLLER, OPS CHECKS WERE GOOD.
- [SDR ASOA20141016114R](https://openairdocs.org/sdr/ASOA20141016114R.md): Inverter · inoperative · Oct 16, 2014 · N14180 · Emb EMB145XR · Emergency Lighting
  > DURING MAINTENANCE INSPECTION, THE FWD EMERGENCY EXIT ROW AISLE LIGHT WOULD NOT ILLUMINATE. MX R & R THE NR 6 EMERGENCY LIGHT SYSTEM INVERTER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20140930083](https://openairdocs.org/sdr/ASOA20140930083.md): Light · inoperative · Sep 30, 2014 · N14180 · Emb EMB145XR · Emergency Lighting
  > THE CREW REPORTED OVERHEAD EMERGENCY EXIT LIGHT AT ROW 12 DID NOT ILLUMINATE DURING TEST. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY EXIT LIGHT AT ROW 12. OPS CHECKED GOOD.
- [SDR ASOA20140705092](https://openairdocs.org/sdr/ASOA20140705092.md): Light · inoperative · Jul 5, 2014 · N14180 · Emb EMB145XR · Emergency Lighting
  > DURING PREFLIGHT THE CREW REPORTED THAT THE EMERGENCY LIGHT WAS INOPERATIVE OVER SEAT 18C ON THE FORWARD SIDE. MAINTENANCE R & R THE AFFECTED LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR V0XD201405250122](https://openairdocs.org/sdr/V0XD201405250122.md): Skin · dented · May 29, 2014 · N14180 · Emb EMB145XR · Fuselage Main, Plate/Skin
  > DENT ON REAR FUSELAGE SKIN, FRAME 78 STRINGER 6L. REPAIRED DENT IAW EC 5330-02473.
- [SDR V0XD2014052518021](https://openairdocs.org/sdr/V0XD2014052518021.md): Structure · corroded · May 28, 2014 · N14180 · Emb EMB145XR · Fuselage Main, Structure
  > WASTE DRAIN VALVE COMPARTMENT CORRODED. R & R WASTE DRAIN VALVE COMPARTMENT IAW SRM 51-40-02.
- [SDR V0XD2014052518020](https://openairdocs.org/sdr/V0XD2014052518020.md): Floor Support · corroded · May 25, 2014 · N14180 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CORROSION ON RT FLOOR SUPPORT FRAMES 41-48. R & R RT FLOOR SUPPORT IAW SRM 51-40-02, 51-40-04, 51-40-06.
- [SDR V0XD2014052518019](https://openairdocs.org/sdr/V0XD2014052518019.md): Channel · corroded · May 25, 2014 · N14180 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > SERVICE DOOR FRAME CHANNEL CORRODED AT THREE NUT PLATE LOCATIONS. R & R SERVICE DOOR FRAME CHANNEL IAW SRM 51-40-02, 51-20-03.
- [SDR V0XD2014052518018](https://openairdocs.org/sdr/V0XD2014052518018.md): Support · corroded · May 25, 2014 · N14180 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CORROSION ON LT SUPPORT AT FRAME 64 S15L. BLENDED CORROSION MATERIAL LOSS WAS.003" WITHIN LIMITS IAW SRM 53-31-10.
- [SDR V0XD2014052518017](https://openairdocs.org/sdr/V0XD2014052518017.md): Beam · corroded · May 25, 2014 · N14180 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > LAV LT BEAM CAP CORRODED. BLENDED CORROSION, REMOVED.005" OF MATERIAL LOSS. FOUND TO BE WITHIN LIMITS IAW SRM 53-24-10, WO 80225, WC 1184.
- [SDR V0XD2014052518016](https://openairdocs.org/sdr/V0XD2014052518016.md): Cap · corroded · May 25, 2014 · N14180 · Emb EMB145XR · Fuselage, Landing Gear Attach Fittings
  > LEFT NLG TRUNNION CAP HAS PITTING. REMOVED MINOR PITTING ON LT NLG TRUNNION CAP IAW SRM 53-11-08, WO 80225, W/C 1177.
- [SDR V0XD2014052518015](https://openairdocs.org/sdr/V0XD2014052518015.md): Floor Support · corroded · May 25, 2014 · N14180 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CORROSION ON RT FLOOR SUPPORT AFT OF FRAME 50. R & R RT FLOOR SUPPORT FROM FRAMES 48-52 IAW SRM 51-40-02, 51-20-03.
- [SDR V0XD2014052518014](https://openairdocs.org/sdr/V0XD2014052518014.md): Floorbeam · corroded · May 25, 2014 · N14180 · Emb EMB145XR · Fuselage Main, Floor Beam
  > RT FLOORBEAM ANGLE CORRODED AT FRAME 23. R & R RT FLOORBEAM ANGLE IAW SRM 51-40-02, WO 80225, WC 1183.
- [SDR V0XD2014052518013](https://openairdocs.org/sdr/V0XD2014052518013.md): Floor Support · corroded · May 25, 2014 · N14180 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CORROSION ON LT FLOOR SUPPORT. R & R LT FLOOR SUPPORT FROM FRAMES 18 - 24 IAW SRM 51-40-02, 51-40-09, 51-20-03.
- [SDR V0XD2014052518012](https://openairdocs.org/sdr/V0XD2014052518012.md): Floorbeam · corroded · May 25, 2014 · N14180 · Emb EMB145XR · Fuselage Main, Floor Beam
  > CORROSION UNDER LAV FLOOR PANEL 261DF ON FLOORBEAM. R & R FLOORBEAM ANGLE IAW SRM 51-40-02.
- [SDR V0XD2014052518011](https://openairdocs.org/sdr/V0XD2014052518011.md): Floor Support · corroded · May 25, 2014 · N14180 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CORROSION ON LT FLOOR SUPPORT AT FRAME 49. BLENDED CORROSION AND FOUND WITHIN LIMITS IAW SRM 53-23-10. NDT PERFORMED.
- [SDR V0XD2014052318010](https://openairdocs.org/sdr/V0XD2014052318010.md): Floor Support · corroded · May 22, 2014 · N14180 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR SUPPORT CORRODED AT FRAME 65. BLENDED CORROSION IAW SRM 53-31-10, FOUND TO BE WITH IN LIMITS IAW SRM 53-31-10, SWPM 20-21-00, AND CPM 51-21-04, 51-21-05. NDT PERFORMED, NO DEFECTS NOTED.
- [SDR V0XD2014052318009](https://openairdocs.org/sdr/V0XD2014052318009.md): Splice · corroded · May 22, 2014 · N14180 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CONNECTION SPLICE CORRODED AT FRAME 35 UNDER FLOORBOARD 252AF. BLENDED CORRODED AREA IAW SRM 53-23-10, AREA LESS THAN 10 PERCENT MATERIAL LOSS, FOUND TO BE WITH IN LIMITS.
- [SDR V0XD2014052318008](https://openairdocs.org/sdr/V0XD2014052318008.md): Floor Support · corroded · May 22, 2014 · N14180 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT FROM FRAMES 24-36 IS CORRODED. REMOVED CORRODED FLOOR SUPPORT AND INSTALLED NEW IAW SRM 51-4-02, AND SWPM 20-21-00.
- [SDR V0XD2014052318007](https://openairdocs.org/sdr/V0XD2014052318007.md): Floor Support · corroded · May 22, 2014 · N14180 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT FWD OF FRAME 26 LT SIDE. REMOVED CORRODED FLOOR SUPPORT AND INSTALLED NEW IAW SRM 51-40-02, 51-20-03, 51-40-06, AND SWPM 20-22-00.
- [SDR V0XD2014052318006](https://openairdocs.org/sdr/V0XD2014052318006.md): Floorbeam · corroded · May 21, 2014 · N14180 · Emb EMB145XR · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM. R & R FLOORBEAM IAW SRM 51-40-02, 51-20-03 AND, 51-40-02.
- [SDR V0XD2014052318005](https://openairdocs.org/sdr/V0XD2014052318005.md): Window Frame · corroded · May 21, 2014 · N14180 · Emb EMB145XR · Fuselage Main, Structure
  > RIGHT WINDSHIELD ASSY FRAME IS CORRODED IN MULTIPLE AREAS. BLENDED CORRODED AREAS IAW ACMM 56-10-01, FOUND TO BE WITHIN LIMITS IAW MM 56-10-01. NDT PERFORMED, NO DEFECTS NOTED.
- [SDR V0XD2014052318004](https://openairdocs.org/sdr/V0XD2014052318004.md): Window Frame · corroded · May 20, 2014 · N14180 · Emb EMB145XR · Fuselage Main, Structure
  > LEFT WINDSHIELD ASSY FRAME IS CORRODED IN MULTIPLE AREAS. BLENDED CORRODED AREAS IAW ACMM 56-10-01, FOUND TO BE WITHIN LIMITS IAW ACMM 56-10-01. NDT PERFORMED, NO DEFECTS NOTED.
- [SDR ASOA20130305020R](https://openairdocs.org/sdr/ASOA20130305020R.md): Wire · damaged · Mar 5, 2013 · N14180 · Emb EMB145XR · Equipment/Furnishings Wiring
  > CREW REPORTED THE F/O'S FLASHLIGHT WAS NOT CHARGING. MX REPAIRED THE WIRE ON THE F/O'S FLASHLIGHT CHARGER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20121009131](https://openairdocs.org/sdr/ASOA20121009131.md): Light · malfunctioned · Oct 9, 2012 · N14180 · Emb EMB145XR · Emergency Lighting
  > DURING POST FLIGHT INSPECTION, CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT SHUTOFF. SWITCHES WERE CYCLED ON AND OFF AND THE LIGHTS EXTINGUISED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120711051](https://openairdocs.org/sdr/ASOA20120711051.md): Sign · inoperative · Jul 11, 2012 · N14180 · Emb EMB145XR · Emergency Lighting
  > FWD FACING CEILING EMERGENCY SIGN OVERWING FOUND INOPERATIVE. MX R & R EMERGENCY EXIT CEILING SIGN WITH OPS CHECK SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20120604051](https://openairdocs.org/sdr/ASOA20120604051.md): Engine · leaking · Jun 4, 2012 · N14180 · Emb EMB145XR · Engine (Turbine/Turboprop)
  > CREW REPORTED SMOKE IN THE LAVATORY. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. ENGINE LEAKING, MX REPLACED THE NR 2 ENGINE. OPS CHECKED GOOD.
- [SDR ASOA20120508095](https://openairdocs.org/sdr/ASOA20120508095.md): Shear Tie · cracked · May 8, 2012 · N14180 · Emb EMB145XR · Fuselage Internal Mounting Structure
  > SHEAR TIE CRACKED AT FR 73, BETWEEN STR 8BR AND 9BR. MX R & R THE SHEAR TIE IAW SRM 51-10-03 AND 51-40-02.
- [SDR ASOA20120508094](https://openairdocs.org/sdr/ASOA20120508094.md): Floor Support · cracked · May 8, 2012 · N14180 · Emb EMB145XR · Fuselage Miscellaneous Structure
  > SPLICE BRACKET CRACKED AT THE LT OMEGA BEAM BETWEEN FR 16 AND 17. MX R & R THE SPLICE BRACKET IAW SRM 51-20-03 AND 51-40-02. ACFT WILL BE RELEASED AT THE END OF THE CHECK.

Next page: https://openairdocs.org/aircraft/N14180/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 = 'N14180' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N14180/reports

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