# Service difficulty reports: N907EV

A list on [N907EV](https://openairdocs.org/aircraft/N907EV.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 4 · 161 reports

- [SDR SWIA201904125761](https://openairdocs.org/sdr/SWIA201904125761.md): Pump · failed · Apr 11, 2019 · N907EV · Cndair CL6002B19 · Engine Fuel Pump
  > ON TAKEOFF AT 1000 FEET. THE LEFT ENGINE HAD A FLAMEOUT. CREW HEARD A BANG AND THE ENGINE ROLLED BACK. ITT SPIKED TO 973 FOR 11 SECONDS. NO RELIGHT WAS ATTEMPTED. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. LANDED WITHOUT INCIDENT. (FLT#5313) REMOVE
- [SDR SWIA2018052144688](https://openairdocs.org/sdr/SWIA2018052144688.md): Sensor · out of adjust · May 19, 2018 · N907EV · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE AND NOSE GEAR DOOR WARNING MESSAGES. ADJUSTED THE SENSOR IAW AMM 32-61-00. NO OTHER DEFECTS NOTED. ACFT OK FOR SERVICE.
- [SDR SWIA201844129](https://openairdocs.org/sdr/SWIA201844129.md): Bracket · failed · Jan 5, 2018 · N907EV · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE MESSAGE. RETURN TO FIELD. INSTALLED NLG CENTERING SENSOR BRACKET IAW AMM ANC FMM. RETRACTION & EXTENSION CYCLE OF MLG GOOD. OPS CHECKED GOOD.
- [SDR SWIA201743642](https://openairdocs.org/sdr/SWIA201743642.md): Switch · failed · Aug 15, 2017 · N907EV · Cndair CL6002B19 · Stabilizer Control System
  > MACH AND STAB TRIM CAUTION MESSAGES DURING CLIMB OUT, WOULD NOT REENGAGE, AUTOPILOT PITCH WOULD NOT ENGAGE. DECLARED EMERGENCY. REPLACED CA YOKE TRIM DISCONNECT SWITCH IAW AMM. OPS CHECKED GOOD. MACH & STAB TRIM & AUTO PILOT PITCH TRIM OPERATE NORMALLY.
- [SDR SWIA201743532](https://openairdocs.org/sdr/SWIA201743532.md): Skin · chafed · Jun 20, 2017 · N907EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LOWER RT WING PLANK IS CHAFED AT RBL 45 AND T/E 1.000" X 4.000" X APPROXIMATELY.040" DEEP. REPAIRED THE WING PLANK IAW REO.
- [SDR SWIA201743533](https://openairdocs.org/sdr/SWIA201743533.md): Structure · cracked · Jun 14, 2017 · N907EV · Cndair CL6002B19 · Wing Main, Frame Structure
  > INDICATION NOTED AT RT WING BL5 WATER DRAIN FWD SCREW HOLE. REPAIRED IAW REO.
- [SDR SWIA201743526](https://openairdocs.org/sdr/SWIA201743526.md): Skin · dented · Jun 14, 2017 · N907EV · Cndair CL6002B19 · Vertical Stabilizer, Plate/Skin
  > LEFT VERTICAL STAB HAS ONE DENT 10 INCHES FROM T/E AND JUST ABOVE THE NR 2 RIB. REPAIRED VERTICAL STAB IAW REO.
- [SDR SWIA201743529](https://openairdocs.org/sdr/SWIA201743529.md): Angle · corroded · Jun 9, 2017 · N907EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR LOWER MOUNTING ANGLE CORRODED IN MULTIPLE LOCATIONS. REMOVED AND REPLACED THE ANGLE IAW SRM.
- [SDR SWIA201743528](https://openairdocs.org/sdr/SWIA201743528.md): Floor Support · corroded · Jun 9, 2017 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT CORRODED AT BS 310, LBL 36. REMOVED CORROSION IAW SRM.
- [SDR SWIA201743534](https://openairdocs.org/sdr/SWIA201743534.md): Bulkhead Web · cracked · Jun 6, 2017 · N907EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED 1) LBL9.5 WL 134 APPROX 3 INCHES LONG 60%FSH 2) RBL9.5 WL 134 APPROX 2 INCHES LONG 50%FSH 3) RBL18 WL 134 4 INCHES LONG 90%FSH 4) RBL27.50 WL 134 APPROX 1 INCH 50% FSH 5) RBL27.50 WL111 APPROX 5 INCHES
- [SDR SWIA201743531](https://openairdocs.org/sdr/SWIA201743531.md): Skin · dented · Jun 4, 2017 · N907EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN DENTED, BS 656 BETWEEN STRINGERS 26 AND 27R. REPAIRED THE SKIN IAW REO.
- [SDR SWIA201743530](https://openairdocs.org/sdr/SWIA201743530.md): Skin · gouged · Jun 4, 2017 · N907EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > THE SKIN HAD SEVERAL SMALL NICKS AND GOUGES FROM BS 589 TO 605 BETWEEN STRINGER 21R & 23R. REPAIRED THE SKIN IAW SRM.
- [SDR SWIA201743527](https://openairdocs.org/sdr/SWIA201743527.md): Skin · dented · Jun 4, 2017 · N907EV · Cndair CL6002B19 · Trailing Edge Flaps
  > RT INBOARD FLAP HAS A DENT ON THE LOWER SKIN INBOARD SIDE. REPAIRED THE FLAP SKIN IAW REO.
- [SDR SWIA201743525](https://openairdocs.org/sdr/SWIA201743525.md): Panel · damaged · May 19, 2017 · N907EV · Cndair CL6002B19 · Standard Practices/Structures
  > TWO OVERSIZED HOLES IN PANEL 131AL. REPAIRED TWO OVERSIZED HOLES IN PANEL 131AL AT 10 O'CLOCK AND 9 O'CLOCK POSITIONS IAW REO.
- [SDR ASOA20161112155A](https://openairdocs.org/sdr/ASOA20161112155A.md): Floor Support · corroded · Nov 12, 2016 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING C CHECK, FOUND RT FLOOR SUPPORT CORRODED BETWEEN BS 409+32 - 409+96. REPAIRED IAW EC/TC REO 601R53-00-530.
- [SDR ASOA20161112154A](https://openairdocs.org/sdr/ASOA20161112154A.md): Floor Support · corroded · Nov 12, 2016 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING C CHECK, FOUND RBL 46 FLOOR SUPPORT CORRODED AT BS 559+80. REPAIRED IAW EC/TC REO 601R-53-00-526.
- [SDR ASOA20161112153](https://openairdocs.org/sdr/ASOA20161112153.md): Floor Support · corroded · Nov 12, 2016 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING C CHECK, FOUND LBL 46 FLOOR SUPPORT CORRODED BETWEEN BS 559+16 - 559+48. REPAIRED IAW EC/TC REO 601R-53-00-526.
- [SDR ASOA20161112152A](https://openairdocs.org/sdr/ASOA20161112152A.md): Floor Support · corroded · Nov 12, 2016 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING C CHECK, FOUND RBL 46 FLOOR SUPPORT CORRODED BETWEEN BS 582-621. REPAIRED IAW EC/TC REO 601R-53-00-526.
- [SDR ASOA20161108148](https://openairdocs.org/sdr/ASOA20161108148.md): Stiffener · cracked · Nov 8, 2016 · N907EV · Cndair CL6002B19 · Passenger/Crew Doors
  > DURING C CHECK, FOUND PAX DOOR ASSIST MOTOR AFT SIDE PANEL STIFFENER CRACKED AT LOWER SECTION. C/W EC/TC REO 601R-52-11-1376 REV A.
- [SDR ASOA20161108099](https://openairdocs.org/sdr/ASOA20161108099.md): Skin · damaged · Nov 8, 2016 · N907EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING C CHECK, FOUND FASTENER HOLE DAMAGED ON FUSELAGE SKIN DURING INSTALLATION OF PANEL 132AL. REPAIRED THE SKIN IAW REO 601R-53-11-162 & EC/TC REO 601R-53-11-162. MAJOR REPAIR.
- [SDR ASOA2016081715279](https://openairdocs.org/sdr/ASOA2016081715279.md): Wire · misinstalled · Aug 17, 2016 · N907EV · Cndair CL6002B19 · Light System Wiring
  > NUMBERS 1, 2, AND 7 EXTERNAL EMERGENCY LIGHTS INOPERTIVE. ACFT NOT OPERATED AT NIGHT. FOUND WIRES TO FORWARD NR 1 SERVICE DOOR EMERGENCY LIGHT INCORRECTLY INSTALLED. R & R NR 1 LT AND RT EMERGENCY LIGHT SOCKETS AND REPLACED FUSE TO NR 1 BATTERY PACK. R & R
- [SDR ASOA2016080515193](https://openairdocs.org/sdr/ASOA2016080515193.md): Lamp · burned out · Aug 5, 2016 · N907EV · Cndair CL6002B19 · Emergency Lighting
  > NR 2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR ASOA2016080515192](https://openairdocs.org/sdr/ASOA2016080515192.md): Lamp · burned out · Aug 5, 2016 · N907EV · Cndair CL6002B19 · Emergency Lighting
  > NR 2 CABIN EMERGENCY CEILING FLOOD LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 3-51-16. OPS CHECKED GOOD.
- [SDR ASOA2016061914945](https://openairdocs.org/sdr/ASOA2016061914945.md): Light · inoperative · Jun 19, 2016 · N907EV · Cndair CL6002B19 · Emergency Lighting
  > RIGHT NR 3 EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R RT NR 3 EXTERIOR EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECK GOOD.
- [SDR ASOA2015122114236](https://openairdocs.org/sdr/ASOA2015122114236.md): Sign · damaged · Dec 21, 2015 · N907EV · Cndair CL6002B19 · Emergency Lighting
  > LIGHTED FLOOR-LEVEL EXIT SIGN AT SERVICE DOOR DAMAGED. R & R SIGN IAW AMM 33-51-10. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2015110213995](https://openairdocs.org/sdr/ASOA2015110213995.md): Inverter · failed · Nov 2, 2015 · N907EV · Cndair CL6002B19 · Emergency Lighting
  > LIGHTED FLOOR-LEVEL EXIT SIGN AT RT OVERWING EMERGENCY EXIT INOPERATIVE. R & R AFFECTED INVERTER IAW 33-51-07. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.
- [SDR ASOA2014121111861](https://openairdocs.org/sdr/ASOA2014121111861.md): Sign · inoperative · Dec 7, 2014 · N907EV · Cndair CL6002B19 · Emergency Lighting
  > RT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. OPS CHECKED EMERGENCY LIGHT IAW AMM 33-51-00. OPS CHECKED GOOD.
- [SDR ASOA2014111211636](https://openairdocs.org/sdr/ASOA2014111211636.md): Frame · corroded · Oct 29, 2014 · N907EV · Cndair CL6002B19 · Fuselage Main, Frame
  > BS 364, FRAME IS CORRODED BETWEEN STR 26L AND 26R. REPAIRED.
- [SDR ASOA2014111211635](https://openairdocs.org/sdr/ASOA2014111211635.md): Post · cracked · Oct 27, 2014 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128, RBL 18 INBD VERT POST HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69 APPROX.5" LONG X 50 PERCENT FSH. FAILED NDT INSP. REMOVED LT AND RT VERTICAL POSTS AT FS 409+128, RBL 18 IAW SRM 51-42-06 AND 51-42-22. C/W ECTC REO: 601R-53-41-889
- [SDR ASOA2014111011625](https://openairdocs.org/sdr/ASOA2014111011625.md): Stiffener · cracked · Oct 27, 2014 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128, BL 0 VERT POST RT SIDE HAS AN INDICATION NOTED IN THE AFT FLANGE RADIUS AT WL 69, APPROX.250" LONG BY 50 PERCNET FSH. FAILED NDT. R & R RT VERT POST AT BL 0 PN 601R32208-132 IAW CRJ 200 51-42-22, 51-42-06. COMPLIED WITH EC/TC REO 601R-53-41-889
- [SDR ASOA2014111211634](https://openairdocs.org/sdr/ASOA2014111211634.md): Pin · corroded · Oct 25, 2014 · N907EV · Cndair CL6002B19 · Standard Practices/Structures
  > LT AND RT LATCH IN INTERCOSTALS ARE CORRODED BETWEEN FS 349 AND FS 364. REMOVED LT AND RT LATCH PIN INTERCOSTALS IAW SRM 51-42-06 AND 51-42-21. INSTALLED LT LATCH PIN INTERCOSTAL 601R31049-9 AND RT LATCH PIN INTERCOSTAL 601R31049-10 IAW SRM 51-42-06, 51-42-2
- [SDR ASOA2014111011624](https://openairdocs.org/sdr/ASOA2014111011624.md): Isolator · cracked · Oct 23, 2014 · N907EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD FWD FACE OF WEB HAS A MISSING ISOLATOR AND A BENT AND CRACKED ISOLATOR AT RBL 27.50 AND WL 75.00. R & R ISOLATOR BRACKET AND INSTALLED NEW ISOLATOR IAW SRM 51-42-06.
- [SDR ASOA2014111011623](https://openairdocs.org/sdr/ASOA2014111011623.md): Bulkhead Web · cracked · Oct 23, 2014 · N907EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT BL 0.0, WL 108-112, 3.5" L, 70 PERCNET FSH. FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-61-1285 AND GREO 601R-53-61-1285, REV D.
- [SDR ASOA2014111011622](https://openairdocs.org/sdr/ASOA2014111011622.md): Bulkhead Web · cracked · Oct 23, 2014 · N907EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATIONS NOTED AT BL 0.0, WL 131-134, 2.5" L, 50 PERCENT FSH. FAILED NDT INSPECTION. COMPLIED WITH EC/TC REO 601R-53-61-1285 AND REO 601R-53-61-1285, REV D.
- [SDR ASOA2014111211633](https://openairdocs.org/sdr/ASOA2014111211633.md): Floor Support · corroded · Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON LT UPPER SURFACE OF PRESSURE FLOOR SUPPORT BS 409+128 - 559.00. BLENDED CORROSION IAW REO 601R-53-41-666 2.2 DISP A AND B. PERFORMED EDDY CURRENT REWORKED AREAS IAW REO 601R-53-41-666, REV C 1.2, STEP C. NO INDICATIONS NOTED AT THIS TIME.
- [SDR ASOA2014110711621](https://openairdocs.org/sdr/ASOA2014110711621.md): Cargo Track · corroded · Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK AT RBL 9 BS 559+110 - 568 CORRODED. R & R THE CARGO TRACK SEGMENT IAW SRM 51-41-02-00, 51-41-04-00.
- [SDR ASOA2014110711620](https://openairdocs.org/sdr/ASOA2014110711620.md): Seat Track · corroded · Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK AT RBL 9, BS 559+87-559+96 CORRODED. R & R THE CARGO TRACK SEGMENT IAW SRM 51-41-02-00, 51-41-04-00.
- [SDR ASOA2014110711619](https://openairdocs.org/sdr/ASOA2014110711619.md): Cargo Track · corroded · Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK AT RBL 27 BS 559+79 - 559+95 HAS CORROSION. R & R THE CARGO TRACK SEGMENT IAW SRM 51-41-02-00, 51-41-04-00.
- [SDR ASOA2014110611610](https://openairdocs.org/sdr/ASOA2014110611610.md): Cargo Track · corroded · Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK AT LBL 27, BS 559 HAS CORROSION AT ATTACHMENT HOLES. R & R THE CARGO TRACK SEGMENT IAW SRM 51-41-02-00, 51-41-04-00.
- [SDR ASOA2014110611609](https://openairdocs.org/sdr/ASOA2014110611609.md): Cargo Track · corroded · Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK AT LBL 9, BS 612-617 HAS CORROSION AT ATTACHMENT HOLES. R & R THE CARGO TRACK SEGMENT IAW SRM 51-42-02-00, 51-41-04-00.
- [SDR ASOA2014110611608](https://openairdocs.org/sdr/ASOA2014110611608.md): Cargo Track · corroded · Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK AT LBL 9 BS 559+110 - 568 HAS CORROSION. R & R THE CARGO TRACK SEGMENT IAW SRM 51-41-02-00, 51-41-04-00.
- [SDR ASOA2014110611607](https://openairdocs.org/sdr/ASOA2014110611607.md): Cargo Track · corroded · Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK AT LBL 9 BS 559+87- 559-96 HAS CORROSION AT ATTACHMENT HOLES. R & R THE CARGO TRACK SEGMENT IAW SRM 51-41-02-00, 51-41-04-00.
- [SDR ASOA2014110611606](https://openairdocs.org/sdr/ASOA2014110611606.md): Floor Support · corroded · Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT CARGO FLOOR SILL FROM FS 559.00+112 TO FS 621.00 HAS FILIFORM CORROSION AT FLOORBOARD SCREW HOLES. REMOVED NUTPLATES FROM RT CARGO FLOOR SILL FROM FS 559.00+112 TO FS 621.00 IAW SRM 51-54-10. INSTALLED 13 NEW SERVICEABLE NUTPLATES, PN MS21059L3 IAW SRM 5
- [SDR ASOA2014110611605](https://openairdocs.org/sdr/ASOA2014110611605.md): Frame · corroded · Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS 333.00 BETWEEN LBL STGR 24 AND RBL STGR 24. REMOVED POSTS AT FS 333 RBL 20 AND LBL 20 IAW SRM 51-42-06 & 51-42-21. UPON FURTHER INVESTIGATION, FOUND TO BE BETWEEN STR 24 & 23L AND STR 24 & 23R, INSTALLED SAME SERVICEABLE VERTICAL POS
- [SDR ASOA2014110611604](https://openairdocs.org/sdr/ASOA2014110611604.md): Frame · corroded · Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage Main, Frame
  > CORROSION ON FRAME AT FS 349.00 BETWEEN LBL STR 24 AND RBL STGR 24. REMOVED CORRODED FRAME SECTOR AT FS 349.00 BETWEEN STR 23L-23R IAW SRM 51-42-06 AND 51-42-21. LOCATED AND DRILLED NEW SERVICEABLE FS 349.00 FRAME SECTOR IAW SRM 51-40-11. INSTALLED IAW SNIE
- [SDR ASOA2014110611603](https://openairdocs.org/sdr/ASOA2014110611603.md): Bracket · cracked · Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage Main, Structure
  > PILOTS SIDE WINDOWS AFT BRACKET IS CRACKED APPROX.250"L AT BOTTOM OF POST. REMOVED AFT, PILOT SIDE WINDSCREEN FITTING IAW SRM 51-42-21. INSTALLED NEW FITTING IAW SRM 51-42-21. LOCATED AND DRILLED NEW BRACKET IAW SRM 51-40-11. COMPLIED WITH SNIEO 601R33007
- [SDR ASOA2014110511601](https://openairdocs.org/sdr/ASOA2014110511601.md): Floorbeam · corroded · Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL 9 - 27 FLOORBEAM CAP BS 559+96 CORRODED. REPAIRED IAW REO 601R-53-00-005.
- [SDR ASOA2014110511600](https://openairdocs.org/sdr/ASOA2014110511600.md): Floorbeam · corroded · Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > RBL 9 - 27 FLOORBEAM TEE AT BS 559+112 HAS CORROSION. REPAIRED IAW REO 601R-53-090-005.
- [SDR ASOA2014110511599](https://openairdocs.org/sdr/ASOA2014110511599.md): Floor Support · corroded · Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT CARGO FLOOR SUPPORT FROM BS 574 - 621 HAS CORROSION AT FLOORBOARD SCREW HOLES. REPAIRED IAW REO 601R-53-00-526 AND GREO 601R-53-00-526 REV.
- [SDR ASOA2014110511598](https://openairdocs.org/sdr/ASOA2014110511598.md): Floor Support · corroded · Oct 22, 2014 · N907EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON LT FLOOR SUPPORT AT BS 349 JUST AFT OF PAX DOOR. REPAIRED IAW REO 601R-53-00-530.

Next page: https://openairdocs.org/aircraft/N907EV/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 = 'N907EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N907EV/reports

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