# Service difficulty reports: N980EV

A list on [N980EV](https://openairdocs.org/aircraft/N980EV.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 3 · 136 reports

- [SDR REXA2020022620214](https://openairdocs.org/sdr/REXA2020022620214.md): Bulb · inoperative · Feb 22, 2020 · N980EV · Cndair CL6002B19 · Emergency Lighting
  > EMER LIGHT AFT OF EXIT SIGN OUT RELAMPED IAW CRJ200 AMM 33-51-16. OPS CHECK GOOD
- [SDR REXA2019121311724](https://openairdocs.org/sdr/REXA2019121311724.md): Bulb · inoperative · Dec 11, 2019 · N980EV · Cndair CL6002B19 · Emergency Lighting
  > LH EXTERIOR EMERGENCY LIGHT INOP REPLAMPED EMREGENCY LIGHT IAW CMM 33-52-06. OPS CHECK GOOD. P/N OFF/ON: 8GH002473-08
- [SDR REXA2019081421232](https://openairdocs.org/sdr/REXA2019081421232.md): Floor Support · corroded · Aug 12, 2019 · N980EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT LBL 9 UPPER INBOARD FLANGE WAS CORRODED AT MULTIPLE LOCATIONS BETWEEN BS 409+128 - 559. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-41-2542 REV.
- [SDR REXA2019081411237](https://openairdocs.org/sdr/REXA2019081411237.md): Landing · corroded · Aug 11, 2019 · N980EV · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING PLANK FUEL PANEL ACCESS HOLE NR 5, 640CB HAS MINOR CORROSION ALONG BACK OF HOLE IN CRITICAL ZONE, WS 76.161.
- [SDR REXA2019081411236](https://openairdocs.org/sdr/REXA2019081411236.md): Landing · corroded · Aug 11, 2019 · N980EV · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING PLANK FUEL PANEL ACCESS HOLE NR 1, 640BB HAS MINOR CORROSION AT INBD AND OUTBD ENDS, WS 54.897 IN NON-CRITICAL ZONE. COMPLIED WITH STEPS 10 AND 11 OF REO 601R-57-21-030 REV L. GAP CHECKED GOOD.
- [SDR REXA2019081411235](https://openairdocs.org/sdr/REXA2019081411235.md): Landing · corroded · Aug 11, 2019 · N980EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING PLANK FUEL ACCESS HOLE NR 8, 540FB, HAS MINOR CORROSION ALONG FRONT OF HOLE IN CRITICAL ZONE, WS 136.676. COMPLIED WITH STEPS 10 AND 11 OF REO 601R-57-21-030 REV L. GAP CHECKED GOOD.
- [SDR REXA2019081411234](https://openairdocs.org/sdr/REXA2019081411234.md): Landing · corroded · Aug 11, 2019 · N980EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING PLANK FUEL ACCESS HOLE NR 7, 540EB, HAS MINOR CORROSION AT INBD AND OUTBD ENDS WS 116.366 IN NON-CRITICAL ZONE. COMPLIED WITH STEPS 10 AND 11 OF REO 601R-57-21-030 REV L. GAP CHECKED GOOD.
- [SDR REXA2019081411233](https://openairdocs.org/sdr/REXA2019081411233.md): Landing · corroded · Aug 11, 2019 · N980EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING PLANK FUEL ACCESS HOLE NR 1, 540BB, HAS MINOR CORROSION AT INBD AND OUTBD ENDS, WS 54.897 IN NON-CRITICAL ZONE. COMPLIED WITH STEPS 10 AND 11 OF REO 601R-57-21-030. GAP CHECKED GOOD.
- [SDR REXA2019081411220](https://openairdocs.org/sdr/REXA2019081411220.md): Floor Support · corroded · Aug 11, 2019 · N980EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CAP ANGLE AT LBL9 HAS MULTIPLE AREAS OF CORROSION BETWEEN FS409+64 TO FS409+128. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-43.
- [SDR REXA2019081491242](https://openairdocs.org/sdr/REXA2019081491242.md): Battery · inoperative · Aug 9, 2019 · N980EV · Cndair CL6002B19 · Emergency Lighting
  > AFT CABIN EMERGENCY LIGHTS FAIL. REMOVED AND REPLACED EMERGENCY BATTERY NR 4 IAW AMM 33-51-04-400-801. OP TEST GOOD.
- [SDR REXA2019081451238](https://openairdocs.org/sdr/REXA2019081451238.md): Floor Support · corroded · Aug 5, 2019 · N980EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT RBL 9 UPPER INBD FLANGE WAS CORRODED AT MULTIPLE LOCATIONS BETWEEN BS 409+128 TO 559. INSTALLED A NEW SERVICEABLE FLOOR SUPPORT IAW SRM 51-42-06, 51-42-13, 51-42-21, AND REO 601R-53-41-2537 REV--.
- [SDR REXA201908141240](https://openairdocs.org/sdr/REXA201908141240.md): Frame · corroded · Aug 4, 2019 · N980EV · Cndair CL6002B19 · Fuselage Main, Frame
  > AFT FUSELAGE FS 589.00 FRAME CORRODED BETWEEN STRINGERS 26R TO 21L. INCLUDES JOB 8775971 OP 318 AND 349. REMOVED AND REPLACED LOWER FRAME SECTOR AND REINFORCEMENT ANGLE IAW SRM 51-42-06 AND 51-42-21. LEAK CHECKED GOOD.
- [SDR REXA201908141239](https://openairdocs.org/sdr/REXA201908141239.md): Frame · corroded · Aug 4, 2019 · N980EV · Cndair CL6002B19 · Fuselage Main, Frame
  > AFT FUSELAGE FS 589.00 FRAME CORRODED BETWEEN STRINGERS 26R TO 21L. INCLUDES JOB 8775971 OP 318 AND 349. REMOVED AND REPLACED LOWER FRAME SECTOR AND REINFORCEMENT ANGLE IAW SRM 51-42-06 AND 51-42-21. LEAK CHECKED GOOD.
- [SDR REXA201908141214](https://openairdocs.org/sdr/REXA201908141214.md): Retainer · gouged · Aug 4, 2019 · N980EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR HAS 3 EA GOUGES ON TOP CENTER SEAL RETAINER, WITH DOOR OPEN. REMOVED AND REPLACED PAX DOOR UPPER SEAL RETAINER IAW BOMBARDIER GREO 601R-52-11-915 AND CRJ 200 SRM 51-42-06 AND 51-42-13. LEAK CHECK GOOD. WVAC EMP 769 STAMP
- [SDR REXA20190814217](https://openairdocs.org/sdr/REXA20190814217.md): Floor Support · corroded · Aug 2, 2019 · N980EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CAP ANGLE AT RBL 9 HAS MULTIPLE AREAS OF CORROSION BETWEEN BS 409 - 409+128. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-11, TR 51-42, 51-42-06, 51-42-21, 51-42-15, 51-45-00.
- [SDR REXA2019081401218](https://openairdocs.org/sdr/REXA2019081401218.md): Bulkhead Web · cracked · Jul 31, 2019 · N980EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND 9 INDICATIONS IN HEEL OF Z-MEMBER FWD FACE OF BS 621 REAR PRESSURE BULKHEAD RBL 18, WL 126 - 135, 40%FSH, BL 0 WL 126 - 135, 45% RSH, LBL 18 WL 126 - 133, 40% FSH, RBL 27.5 WL 107-109 70% FSH, RBL 18 WL 99-104 80%FSH, BL 0, WL 107-113 45% FSH, LB
- [SDR REXA2019081401222](https://openairdocs.org/sdr/REXA2019081401222.md): Bracket · gouged · Jul 21, 2019 · N980EV · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT WING OTBD FLAP, O/B LUG FITTING HAS A SMALL GOUGE ON BRACKET APPX.300 X.300 X.010 DEEP. REPAIRED AREA ON THE LT WING OTBD FLAP, OTBD LUG FITTING IAW REO 601R-57-21-3105 REV--.
- [SDR REXA2019081401221](https://openairdocs.org/sdr/REXA2019081401221.md): Crossbeam · corroded · Jul 21, 2019 · N980EV · Cndair CL6002B19 · Fuselage Main, Structure
  > FS 280 CROSSBEAM UPPER FLANGE HAS CORROSION AT SEVERAL LOCATING BETWEEN LBL 4 TO RBL 17. ACCOMPLIISHED FS 280 REPAIR IAW REO 601R53-11-926 REV B.
- [SDR REXA2019081491241](https://openairdocs.org/sdr/REXA2019081491241.md): Separator · chafed · Jul 19, 2019 · N980EV · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > PANEL 422DB IS CHAFED. REMOVED AND REPLACED FWD AND AFT SEPERATORS ON PANEL 422DB IAW CRJ200 SRM 51-41-06 WVAC EMP STAMP 771
- [SDR REXA2019081491227](https://openairdocs.org/sdr/REXA2019081491227.md): Separator · chafed · Jul 19, 2019 · N980EV · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
  > PANEL 422DB IS CHAFED. REMOVED AND REPLACED FWD AND AFT SEPERATORS ON PANEL 422DB IAW SRM 51-41-06.
- [SDR REXA2019081400223](https://openairdocs.org/sdr/REXA2019081400223.md): Fitting · cracked · Jul 18, 2019 · N980EV · Cndair CL6002B19 · Fuselage Main, Structure
  > COPILOTS WINDSHIELD POST LOWER AFT FITTING CRACKED. INSTALLED A NEW FITTING IAW SRM 51-42-21.
- [SDR REXA20190814219](https://openairdocs.org/sdr/REXA20190814219.md): Stiffener · chafed · Jul 18, 2019 · N980EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 REAR PRESSURE BULKHEAD AFT VERTICAL STIFFENER AT B.L. 0 AT WL 140 IS CHAFED APROX -.5 WIDE & 0.030 DEEP. REPAIRED AREA IAW REO 601R-53-61-7060, AND GREO 601R-53-61-1523.
- [SDR REXA2019081461226](https://openairdocs.org/sdr/REXA2019081461226.md): Seat Track · corroded · Jul 16, 2019 · N980EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK IS CORRODED FS 449. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR REXA2019081461225](https://openairdocs.org/sdr/REXA2019081461225.md): Frame · cracked · Jul 16, 2019 · N980EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 333 FRAME CRACKED ABOVE PAX DOOR CUTOUT BETWEEN STRINGER 0 AND 1L. LOCATED, DRILLED, AND INSTALLED A NEW SERVICEABLE FRAME SEGMENT IAW SRM 51-42-06, 51-42-21, AND 51-40-11.
- [SDR REXA2019081401224](https://openairdocs.org/sdr/REXA2019081401224.md): Fitting · cracked · Jul 16, 2019 · N980EV · Cndair CL6002B19 · Fuselage Main, Structure
  > PILOT WINDSHIELD SIDE POST LOWER AFT FITTING CRACKED. REPLACED THE FITTING IAW SRM 51-42-21.
- [SDR REXA2019081491231](https://openairdocs.org/sdr/REXA2019081491231.md): Seat Track · corroded · Jul 9, 2019 · N980EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT TRACK IS CORRODED BS 449 - 499. INSTALLED A NEW SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR REXA2019081491229](https://openairdocs.org/sdr/REXA2019081491229.md): Seat Track · damaged · Jul 9, 2019 · N980EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK, LBL 9, BETWEEN BS 365 TO 400 WAS CORRODED AND GOUGED AT MULTIPLE LOCATIONS. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR REXA2019081491228](https://openairdocs.org/sdr/REXA2019081491228.md): Seat Track · corroded · Jul 9, 2019 · N980EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK WAS CORRODED BS 406+112 - 449. REMOVED & REPLACED THE SEAT TRACK IAW AMM 53-01-11-400-802.
- [SDR REXA2019070901215](https://openairdocs.org/sdr/REXA2019070901215.md): Seat Track · gouged · Jul 9, 2019 · N980EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT TRACK SEGMENT IS GOUGED BS 364 - 409+16. INSTALLED NEW SEAT TRACK RAIL IAW AMM 51-01-11-400-802.
- [SDR REXA2019081481230](https://openairdocs.org/sdr/REXA2019081481230.md): Seat Track · corroded · Jul 8, 2019 · N980EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK WAS GOUGED, BS 364 - 409+16. INSTALLED A NEW SEAT TRACK IAW AMM 51-01-11-400-802.
- [SDR REXA201908014216](https://openairdocs.org/sdr/REXA201908014216.md): Seat Track · corroded · Jul 8, 2019 · N980EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT TRACK IS CORRODED FS409+112 - 449 INSTALLED NEW SEAT RAIL IAW AMM 53-01-11-400-802.
- [SDR REXA2018121181208](https://openairdocs.org/sdr/REXA2018121181208.md): Bulkhead Web · gouged · Dec 8, 2018 · N980EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > SCRATCH/GOUGE/DENT NOTED ON RPB @FS621 2.25" OB OF RIVET CENTER LINE FOR LBL18.00 22" UP FROM THE FLOOR 1.5"L X 1.25"W X.025" DEPTH DEEPEST DEPTH IS AT END OF GOUGE REATHER SHARP IN NATURE COMPLIED WITH TEMP REPAIR IAW REO 601R-53-61-6808 NDT COMPLIED WITH RE
- [SDR REXA2018121181207](https://openairdocs.org/sdr/REXA2018121181207.md): Bulkhead · damaged · Dec 8, 2018 · N980EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING COMPLIANCE OF T/C 53-280-607 NOTED MULTIPLE RIVET HEAD STRIKE DAMAGE ON THE FWD FACE OF THE REAR PRESSURE BULKHEAD @FS621. LOCATIONS LBL36.20 LBL27.5 LBL18 LBL9.5 RBL18.0 RBL27.5 AND RBL36.2 ALL 13" UP FROM THE FLOOR AND IN LINE HORIZONTAL REMOVED AND
- [SDR REXA2018121181206](https://openairdocs.org/sdr/REXA2018121181206.md): Bulkhead Web · damaged · Dec 8, 2018 · N980EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING COMPLETION OF T/C53-280-607 NOTED MULTIPLE AREAS OF HARDWARE STRIKE DAMAGE TO THE RPB FWD FACE SKIN LOCATIONS LBL27.5 LBL18.0 RBL18 RBL27.5 RBL36.2 ALL ARE 30" UP FROM THE FLOOR AND IN A LINE HORIZONTALLY ALL ARE ON A RIVET LINE COMPLETED REPAIRS TO NO
- [SDR REXA2018081540700](https://openairdocs.org/sdr/REXA2018081540700.md): Bulb · inoperative · Aug 14, 2018 · N980EV · Cndair CL6002B19 · Emergency Lighting
  > GALLEY DOOR, EMERGENCY EXIT LIGHT, ONE BULB WAS INOPERATIVE. PERFORMED AN OPS TEST OF THE EMERGENCY LIGHT IAW AMM 33-51-00. OPS CHECKED GOOD
- [SDR REXA2018081530699](https://openairdocs.org/sdr/REXA2018081530699.md): Lamp · inoperative · Aug 13, 2018 · N980EV · Cndair CL6002B19 · Emergency Lighting
  > SERVICE DOOR EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR REXA2018061850491](https://openairdocs.org/sdr/REXA2018061850491.md): Flashlight · inoperative · Jun 15, 2018 · N980EV · Cndair CL6002B19 · Emergency Equipment
  > ON A ROUTINE 200 NOTICE, FIRST OFFICER`S FLASHLIGHT LED INOPERATIVE. R & R THE FLASHLIGHT IAW AMM 25-61-02. OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR REXA2018060530436](https://openairdocs.org/sdr/REXA2018060530436.md): Seal · broken · Jun 3, 2018 · N980EV · Cndair CL6002B19 · Emergency Equipment
  > SEAL ON CABIN PBE WAS BROKEN. REPLACED THE SEAL ON THE AFT PBE.
- [SDR REXA2018051760386](https://openairdocs.org/sdr/REXA2018051760386.md): Flashlight · inoperative · May 16, 2018 · N980EV · Cndair CL6002B19 · Emergency Equipment
  > FORWARD FA FLASHLIGHT, OK LIGHT NOT BLINKING AND UNIT VERY WARM TO THE TOUCH. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 25-61-02. OPS CHECKED GOOD. NO DEFECTS NOTED.
- [SDR REXA2018031200182](https://openairdocs.org/sdr/REXA2018031200182.md): Pbe · damaged · Mar 12, 2018 · N980EV · Cndair CL6002B19 · Emergency Equipment
  > WARDROBE PBE LOST ITS VACUUM. REMOVED AND REPLACED THE PBE IAW AMM 35-30-00.
- [SDR REXA2018021600129](https://openairdocs.org/sdr/REXA2018021600129.md): Light · inoperative · Feb 16, 2018 · N980EV · Cndair CL6002B19 · Emergency Lighting
  > LEFT FWD EMERGENCY LIGHT OUT (EXTERIOR PAX DOOR). RELAMPED LEFT FWD EMERGENCY LIGHT (EXTERIOR PAX DOOR) IAW AMM 33-51-21. OPS CHECK GOOD.
- [SDR REXA2018011100015](https://openairdocs.org/sdr/REXA2018011100015.md): Light · inoperative · Jan 11, 2018 · N980EV · Cndair CL6002B19 · Emergency Lighting
  > LT OVERWING EXTERIOR EMERGENCY CENTER LIGHT NR 3 INOP. R&R EXTERIOR EMERGENCY OVER WING CENTER LIGHT NR 3 IAW AMM 35-51-21. OPS CHECK GOOD.
- [SDR REXA2017053100646](https://openairdocs.org/sdr/REXA2017053100646.md): Gauge · damaged · May 31, 2017 · N980EV · Cndair CL6002B19 · Portable Oxygen System
  > ENTRANCE AREA OXYGEN BOTTLE HAS DAMAGED GAUGE. REMOVED AND REPLACED PORTABLE OXYGEN BOTTLE IAW AMM 35-31-01.
- [SDR REXA2017030400316](https://openairdocs.org/sdr/REXA2017030400316.md): Light · damaged · Mar 4, 2017 · N980EV · Cndair CL6002B19 · Emergency Lighting
  > SEVERAL SECTIONS OF THE FLOOR EMERGENCY LIGHTS WERE DAMAGED. REPLACED THE LIGHTS, OPS CHECKED GOOD. IAW VCMM 33-60-13.
- [SDR REXA2017030300314](https://openairdocs.org/sdr/REXA2017030300314.md): Lead · disconnected · Mar 3, 2017 · N980EV · Cndair CL6002B19 · Light System Wiring
  > LEFT EMERGENCY EXIT LIGHTED SIGN INOP. CONNECTED LEFT EMERGENCY EXIT LIGHTED SIGN POWER LEADS IAW AMM 33-51-13 OPS CHECKED GOOD.
- [SDR REXA2017022600293](https://openairdocs.org/sdr/REXA2017022600293.md): Socket · unsecure · Feb 26, 2017 · N980EV · Cndair CL6002B19 · Emergency Lighting
  > AFT BLUE SOCKET ON CNT EXIT LIGHT DAMAGED. RESECURED AFT BLUE SOCKET ON CNT EXIT LIGHT IAW AMM 33-51-14.
- [SDR REXA2017020700187](https://openairdocs.org/sdr/REXA2017020700187.md): Hose · damaged · Feb 7, 2017 · N980EV · Cndair CL6002B19 · Crew Oxygen System
  > THE OBSERVER`S OXYGEN MASK HOSE DAMAGED. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12-000-801.
- [SDR ASOA20161106109](https://openairdocs.org/sdr/ASOA20161106109.md): Cargo Track · corroded · Nov 6, 2016 · N980EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK AT BS 559+64 - 559+80, LBL 9 CORRODED. REMOVED AND REPLACED THE CARGO TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20161105106](https://openairdocs.org/sdr/ASOA20161105106.md): Door Sill · corroded · Nov 5, 2016 · N980EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON TOP OF FLOORSILL AT FS 409.00+128- 559.00 AND LBL 36-40. REMOVED CORROSION FROM FLOORSILL IN DISCREPANT AREAS BETWEEN FS 409.00+128 AND 559.00 AND LBL 36-40 REF SRM 51-21-16. COMPLIED WITH EC/TC REO 601R-53-41-666 AND REO 601R-53-41-666 RE
- [SDR ASOA20161105105](https://openairdocs.org/sdr/ASOA20161105105.md): Cargo Track · corroded · Nov 5, 2016 · N980EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO FLOOR TRACK AT 559+64- 559+80 AT LBL 27 IS CORRODED. REMOVED AND REPLACED CARGO FLOOR TRACK AT FS 559+64- 559+80 IAW AMM 53-00-49-000-801 AND 53-00-49-400-801. COMPLIED WITH EC/TC REO 601R-53-00-485 AND REO 601R-53-00-485 REV B AND COMPLIED WITH EC/TC

Next page: https://openairdocs.org/aircraft/N980EV/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 = 'N980EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N980EV/reports

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