# Service difficulty reports: N937EV

A list on [N937EV](https://openairdocs.org/aircraft/N937EV.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 · 138 reports

- [SDR SWI2025F01192](https://openairdocs.org/sdr/SWI2025F01192.md): Fuel Line · leaking · Sep 6, 2025 · N937EV · Cndair CL6002B19 · APU Oil System
  > DURING CABIN CLOSE AND START UP. HEAVY FUMES STARTED TO BUILD IN CABIN. SMELLS LIKE JET FUEL. UNABLE TO DISSIPATE AND CONTINUE TO BECOME BREATHING HAZARD. BOTH PILOTS WERE GETTINGHEADACHE AND DECIDED TO RETURN TO GATE AND DEPLANE. AFTER TURNING EVERYTHING OFF
- [SDR SWIA20240810](https://openairdocs.org/sdr/SWIA20240810.md): Landing Gear · warning message · Aug 10, 2024 · N937EV · Cndair CL6002B19 · Landing Gear Position and Warning
  > D: GEAR DISAGREE AFTER SELECTING GEAR UP. NOSE GEAR DID NOT COME UP. RAN QRH AND MANUALLY RELEASED GEAR. RETURNED TO FIELD. GEAR REMAINED LOCKED AND TAXI IN AS NORMAL.C: MEL 32-30-1CAT: A DUE: 1 FLT DAY**** DUE TO ODI EVENT****MANAGEMENT APPROVAL IS REQUIRED V
- [SDR SWIA202265837](https://openairdocs.org/sdr/SWIA202265837.md): None · failed · Jun 1, 2022 · N937EV · Cndair CL6002B19 · Window/Windshield System
  > TROUBLESHOOT R WINDOW HEAT CAUTION ON CLIMB OUT AT 3K FEET. RAN QRH AND MESSAGE CLEARED. GOT MESSAGE AGAIN DESCENDING THROUGH 5K FEET. (FILED - CLOSED) REPLACED RT SIDE WINDOW IN REFERENCE TO CRJ200 AMM 56-12-01 AND 56-220-1000-SKY. OPS CHECK GOOD. NO L
- [SDR SWIA202265296](https://openairdocs.org/sdr/SWIA202265296.md): None · failed · Apr 9, 2022 · N937EV · Cndair CL6002B19 · Landing Gear Door Actuator
  > GEAR DISAGREE AFTER TAKE OFF FLOW QRH PROCEDURES THEN RTF (FLIGHT 5229 - FILED CLOSED) FDR ANALYSIS INDICATED NOSE GEAR DID NOT FULLY RETRACT WHEN COMMANDED, MAINS DID GO FULL UP AND LOCKED. WHEN GEAR COMMANDED DOWN, ALL GEAR WERE DOWN AND LOCKED, AIRCRAFT
- [SDR SWIA202265169](https://openairdocs.org/sdr/SWIA202265169.md): None · failed · Mar 25, 2022 · N937EV · Cndair CL6002B19 · Cabin Pressure Indicator
  > DURING CLIMB OUT AT FL200 GOT THE CABIN ALT CAUTION MESSAGE. RAN THE QRH AND THE MANUAL PRESSURE CONTROLLER WAS NOT STOPPING THE CABIN ALT FROM CLIMBING. GOT THE CABIN ALT WARNING AND RETURNED TO KAMA. (FLIGHT 6941 - FILED CLOSED) REMOVED AND REPLACED BOT
- [SDR SWIA202054938](https://openairdocs.org/sdr/SWIA202054938.md): Line · chafed · Dec 30, 2020 · N937EV · Cndair CL6002B19 · Detection System
  > FOUND STAINLESS LINE TO NR 1 HYDRAULIC ACMP RUBBING THROUGH LEFTHAND FRAME FS 718.00 BETWEEN STGR 16A AND STGR 17. DAMAGE OUT OF LIMITS AND FOUND TO BE A MAJOR REPAIR, PER GMM 3-26 FORM M-337 REQUIRED. PERFORMED TEMPORARY REPAIR NR 2, IN REFERENCE TO CRJ 200
- [SDR SWIA2020072251399](https://openairdocs.org/sdr/SWIA2020072251399.md): Floor Support · corroded · Jul 2, 2020 · N937EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH FLOOR SUPPORT RBL 9, BS 558 TO 559+10 WAS CORRODED AROUND NUTPLATE LOCATION INBOARD AND OUTBOARD SIDES. COMPLIED WITH REPAIR IAW REO, ALL STEPS COMPLIED WITH, CHECKS OKAY, COMPLETED TASK.
- [SDR SWIA2020072251398](https://openairdocs.org/sdr/SWIA2020072251398.md): Floor Support · corroded · Jun 30, 2020 · N937EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR BEAM AT LBL 9.00 HAS EXFOLIATION CORROSION AROUND MULTIPLE FLOORBOARD SCREW HOLES IN SECTION APPROX. 2 IN. FORWARD OF FS409.00+64 TO APPROX. 2 IN AFT OF FS409.00+96 (C-CHECK) RO 7/18/2020 REMOVED AND INSTALLED NEW FLOOR BEAM AT LBL 9.00 AT FS 409.00
- [SDR SWIA2020072251397](https://openairdocs.org/sdr/SWIA2020072251397.md): Support Angle · chafed · Jun 24, 2020 · N937EV · Cndair CL6002B19 · Passenger/Crew Doors
  > UPON REMOVAL OF THE FWD PAX DOOR PULL IN LEVER FOUND THE FWD PAX DOOR ANGLE SUPPORT CHAFE. REPAIRED PAX DOOR FWD ANGLE SUPPORT IAW MHIRJ REO.
- [SDR SWIA2020072251396](https://openairdocs.org/sdr/SWIA2020072251396.md): Stiffener · defective · Jun 23, 2020 · N937EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > F.S 409+128 LBL 18 OTBD AFT RADIUS OF VERTICAL POST DEFECT NOTED. (C-CHECK) RO 7/18/2020 REMOVED AND REPLACED FS 409+128 POST REF DWG, AND REO, CHECKS OKAY, COMPLETED TASK CARD
- [SDR SWIA2020072251395](https://openairdocs.org/sdr/SWIA2020072251395.md): Intercostal · cracked · Jun 20, 2020 · N937EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD INTERCOSTAL DD5 AND BRACKET IS CRACK (C-CHECK) RO 7/18/2020 INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD5 AND BRACKET, REF. CRJ200 SRM AND BOMBARDIER DWG, PRESSURE CHECK GOOD AT THIS TIME, NO LEAKS FOUND AT THIS TIME, COMPLIED WITH STRUCTURAL MA
- [SDR SWIA2020072251394](https://openairdocs.org/sdr/SWIA2020072251394.md): Former · corroded · Jun 20, 2020 · N937EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR FWD FORMER F/S 311.75 HAS CORROSION (C-CHECK) RO 7/18/2020 DAMAGE WITHIN LIMITS REF REO, RESTORED ACCESS AND PAX DOOR FWD FORMER REF SRM AND DWG, CHECKS OKAY, COMPLETED TASK CARD
- [SDR SWIA2020072251393](https://openairdocs.org/sdr/SWIA2020072251393.md): Intercostal · corroded · Jun 19, 2020 · N937EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR - AFT DD6 INTERCOSTAL HAS CORROSION. INSTALLED NEW PAX DOOR AFT DD6 INTERCOSTAL, IAW SRM AND DWG, PRESSURE CHECKED GOOD. COMPLIED WITH STRUCTURAL MAJOR REPAIR.
- [SDR SWIA2020072251392](https://openairdocs.org/sdr/SWIA2020072251392.md): Doubler · cracked · Jun 18, 2020 · N937EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR - AFT PULL IN CAM DOUBLER IS CRACKED REMOVED AND INSTALLED NEW PAX DOOR PULL IN CAM DOUBLER IAW CRJ 200 SRM AND BOMBARDIER DWG. COMPLIED WITH SKYWEST SKYCARD COMPLETED FORM M-337
- [SDR SWIA2020072251391](https://openairdocs.org/sdr/SWIA2020072251391.md): Door Frame · corroded · Jun 18, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR AFT FORMER AT FS347.27 HAS CORROSION (C-CHECK) RO 7/18/2020 REMOVED AND REPLACED PAX DOOR AFT FORMER REF SRM AND DWG, COMPLETED TASK CARD, CHECKS OKAY
- [SDR SWIA2020072251412](https://openairdocs.org/sdr/SWIA2020072251412.md): Fitting · corroded · Jun 17, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Structure
  > PAX DOOR SURROUND, AFT HANDRAIL CLOSING FITTING ASSEMBLY HAS CORROSION. BLENDED OUT CORROSION ON THE PAX DOOR SURROUND, AFT HANDRAIL CLOSING FITTING WITH-IN ALLOWABLE LIMITS IAW SRM. RESTORED FINISH TO REWORK AREA IAW SRM. REMOVED AND REPLACE THREE NUTPLATES
- [SDR SWIA2020072251411](https://openairdocs.org/sdr/SWIA2020072251411.md): Fitting · corroded · Jun 17, 2020 · N937EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR SURROUND - FWD HANDRAIL CLOSING FITTING ASSEMBLY HAS CORROSION. BLENDED OUT CORROSION ON THE PAX DOOR SURROUND - FWD HANDRAIL CLOSING FITTING (SILL CUP CLEAT) WITH-IN ALLOWABLE LIMITS IAW SRM. RESTORED FINISH TO REWORK AREA IAW SRM. REMOVED AND REPL
- [SDR SWIA2020072251409](https://openairdocs.org/sdr/SWIA2020072251409.md): Door Frame · chafed · Jun 17, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Structure
  > THE CARGO DOOR CUTOUT INETRIOR SURROUND LOWER COMBING FWD SIDE IS CHAFED. REMOVED AND REPLACED CARGO DOOR COAMING REF SRM, CHECK OKAY
- [SDR SWIA2020072251408](https://openairdocs.org/sdr/SWIA2020072251408.md): Door Frame · chafed · Jun 17, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Structure
  > THE CARGO DOOR CUTOUT INTERIOR SURROUND UPPER COMBING IS CHAFFED IN THE CENTER. REMOVED AND REPLACED CARGO DOOR UPPER COAMING REF SRM, CHECK OKAY
- [SDR SWIA2020072251407](https://openairdocs.org/sdr/SWIA2020072251407.md): Anchor Fitting · corroded · Jun 17, 2020 · N937EV · Cndair CL6002B19 · Passenger/Crew Doors
  > *PAX DOOR SURROUND - AFT ANCHOR FITTING - LAMINATED SHIM PLATE HAS CORROSION. (C-CHECK) RO 7/18/2020 REMOVED AND REPLACED THE AFT PASSENGER DOOR ANCHOR FITTING, REF CRJ 200 AMM.
- [SDR SWIA2020072251406](https://openairdocs.org/sdr/SWIA2020072251406.md): Anchor Fitting · corroded · Jun 17, 2020 · N937EV · Cndair CL6002B19 · Passenger/Crew Doors
  > *PAX DOOR SURROUND - FWD ANCHOR FITTING - SERRATED PLATE HAS CORROSION. PASSENGER DOOR FWD ANCHOR FITTING REMOVED AND REPLACED WITH NEW. REF AMM. FUNCTIONAL TEST CHECKED GOOD.
- [SDR SWIA2020072251390](https://openairdocs.org/sdr/SWIA2020072251390.md): Floor Support · corroded · Jun 17, 2020 · N937EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > *PAX DOOR SURROUND - LOWER FLOOR SUPPORT ANGLE HAS CORROSION AT FASTNER HOLES. PASSENGER DOOR LOWER FLOOR SUPPORT ANGLE REMOVED AND REPLACED WITH NEW, IAW SRM AND DWG. COMPLIED WITH TASK CARD.
- [SDR SWIA2020072251389](https://openairdocs.org/sdr/SWIA2020072251389.md): Frame · cracked · Jun 17, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME SECTOR APPROX BS 333, STRINGER 1L, CRACKED AT TOOLING HOLE. REMOVED AND INSTALLED A NEW FRAME IAW DRAWING, AND SRM. COMPLIED WITH TASK CARD. ALL CHECKS GOOD.
- [SDR SWIA2020072251388](https://openairdocs.org/sdr/SWIA2020072251388.md): Attach Angle · cracked · Jun 17, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > *PAX DOOR SURROUND - UPPER SILL ATTACH ANGLES AT STGR3L, APPROX. FS280 APPEAR CRACKED. (C-CHECK) RO 7/18/2020 REMOVED AND REPLACED STR3 CLIPS REF DWG AND SRM, CHECK OKAY, COMPLETED TASK CARD
- [SDR SWIA2020072251387](https://openairdocs.org/sdr/SWIA2020072251387.md): Pressure Panel · corroded · Jun 17, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Structure
  > * THE RH PRESSURE FLOOR SILL PANEL HAS MULTIPLE LOCATIONS OF CORROSION BETWEEN FS439.00 AND FS499.00. REMOVED CORROSION ON RH PRESSURE FLOOR SILL PANEL BETWEEN FS439.00 AND FS499.00 IN 5 LOCATIONS. ALL BLENDS WITHIN LIMITS. SEE CONTINUE CARD FOR FURTHER DETA
- [SDR SWIA2020072251386](https://openairdocs.org/sdr/SWIA2020072251386.md): Pressure Panel · corroded · Jun 17, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Structure
  > * THE LH PRESSURE FLOOR SILL PANEL HAS CORROSION BETWEEN FS424.00 AND FS473.00. (MARKED) (C-CHECK) RO 7/18/2020 REMOVED CORROSION ON LH PRESSURE FLOOR SILL PANEL BETWEEN FS424.00 AND FS473.00 IN 7 LOCATIONS. ALL BLENDS WITHIN LIMITS. SEE CONTINUE CARD FO
- [SDR SWIA2020072251405](https://openairdocs.org/sdr/SWIA2020072251405.md): Seat Track · corroded · Jun 16, 2020 · N937EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > * THE SEAT TRACK AT LBL 9.00 HAS CORROSION FROM FS364.00 TO JUST AFT FS394.00. REMOVED AND REPLACE PART - THE NEW SEAT TRACK ALONG WITH NEW FASTENERS AT LBL 9.0 AT FS364.00 - FS394.00. REF CRJ200 AMM.
- [SDR SWIA2020072251404](https://openairdocs.org/sdr/SWIA2020072251404.md): Seat Track · corroded · Jun 16, 2020 · N937EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > THE SEAT TRACK AT RBL 9 WAS CORRODED FROM BS 364 TO JUST AFT OF BS 394. REMOVED AND REPLACED THE SEAT TRACK IAW AMM.
- [SDR SWIA2020072251403](https://openairdocs.org/sdr/SWIA2020072251403.md): Cargo Track · corroded · Jun 16, 2020 · N937EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK BETWEEN BS 559+96 AND 559+112 CORRODED. CORROSION COMPLETELY COVERS ALL 3 ANCHOR PLATES AND IS OUT OF LIMITS IAW SRM. REMOVED THE ANCHOR PLATES IAW AMM. INSTALLED THE REPLACEMENT ANCHOR PLATES IAW AMM.
- [SDR SWIA2020072251402](https://openairdocs.org/sdr/SWIA2020072251402.md): Seat Track · corroded · Jun 16, 2020 · N937EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL 9, BETWEEN JUST AFT OF BS 559 AND TO JUST AFT OF BS 559+80 WAS CORRODED AND GOUGED. REPLACED THE SEAT TRACK.
- [SDR SWIA2020072251401](https://openairdocs.org/sdr/SWIA2020072251401.md): Panel · cracked · Jun 16, 2020 · N937EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT WEB PANEL HAS CRACK IN LOWER CORNER. REMOVED AND INSTALLED NEW AFT STAIR WEB PANEL IAW SRM.
- [SDR SWIA2020072251385](https://openairdocs.org/sdr/SWIA2020072251385.md): Fitting · corroded · Jun 16, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > * THE WARDROBE FITTING JUST FWD OF FS310.00 AT LH FLOOR SILL HAS CORROSION. (MARKED) (C-CHECK) RO 7/18/2020 REMOVED AND REPLACED WARDROBE FITTING JUST FWD OF FS310.00 AT LH FLOOR SILL. SEE CONT CARD FOR DETAILS. REF: CRJ200 NDTM, CRJ200 SRM AND DWG
- [SDR SWIA2020072251384](https://openairdocs.org/sdr/SWIA2020072251384.md): Frame · corroded · Jun 16, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Frame
  > *CORROSION ON FRAME AT FS 605.00 ON FWD FACE BETWEEN STRG 24R STGR 26R (C-CHECK) RO 7/18/2020 REPLACED FS605.00 FRAME BETWEEN STGR 20R AND STGR 20L. REF BOMBARDIER DWG AND CRJ 200 SRM. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.
- [SDR SWIA2020072251383](https://openairdocs.org/sdr/SWIA2020072251383.md): Floorbeam · cracked · Jun 16, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > *PRESSURE FLOOR SUPPORT CENTER BEAM (BL 0.00) IS CRACKED AT FS 559.00 (C-CHECK) RO 7/18/2020 REPAIRED FLOOR BEAM BETWEEN FS529.00 & FS559.00 AND BL0.0. REF REO. ALL CHECKS GOOD.
- [SDR SWIA2020072251382](https://openairdocs.org/sdr/SWIA2020072251382.md): Seat Track · corroded · Jun 16, 2020 · N937EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > *FLOOR SUPPORT STRUCTURE, AT RBL9, APPROX. FS559+80: TRACK FOR 9G/LAV MOUNT IS CORRODED. (C-CHECK) RO 7/18/2020 REMOVGED AND INSTALLED 1 EACH NEW SERVICEABLE SEAT TRACK SECTION P/N 601R38779-13 AT RBL9 AND FS559+80. REF - CRJ 200 AMM.
- [SDR SWIA2020072251381](https://openairdocs.org/sdr/SWIA2020072251381.md): Bracket · corroded · Jun 16, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > *FLOOR SUPPORT STRUCTURE AFT MOUNT BRACKET FOR AFT CARGO DOOR NETTING HAS CORROSION. (C-CHECK) RO 7/18/2020 CARGO FLOOR SUPPORT STRUCTURE AFT MOUT BRACKET FOR NETTING HAS CORROSION ON MULTIPLE ELEMENTS AND IS OUT OF LIMITS. REMOVED AND REPLACED WITH NEW
- [SDR SWIA2020072251380](https://openairdocs.org/sdr/SWIA2020072251380.md): Bracket · corroded · Jun 16, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > FLOOR SUPPORT STRUCTURE MIDDLE MOUNT BRACKET FOR AFT CARGO DOOR NETTING HAS CORROSION. FLOOR SUPPORT STRUCTURE MIDDLE MOUNT BRACKET FOR AFT CARGO DOOR NETTING HAS CORROSION ON MORE THAN ONE ELEMENT AND COVERS MORE THAN 30% OF PART AND IS OUT OF LIMITS REF
- [SDR SWIA2020072251379](https://openairdocs.org/sdr/SWIA2020072251379.md): Floorbeam · corroded · Jun 16, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM ANGLE AT LEFT SIDE BS 621 BULKHEAD HAS CORROSION. REMOVED AND REPLACED REPAIR ANGLE IN REFERENCE TO REO AND SRM, CHECK OKAY, COMPLETED TASK CARD
- [SDR SWIA2020072251378](https://openairdocs.org/sdr/SWIA2020072251378.md): Floorbeam · corroded · Jun 16, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM AT LBL 27 FOR THE FS621 BULKHEAD MOUNT WAS CORRODED. COMPLIED WITH PERMANENT REPAIR FLOOR FITTING AT BS 621 REF REO, ALL STEPS COMPLIED WITH.
- [SDR SWIA2020072251377](https://openairdocs.org/sdr/SWIA2020072251377.md): Floor Support · corroded · Jun 16, 2020 · N937EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT STRUCTURE ÂT RBL 9, ? TOP WAS CORRODED AT MULTIPLE LOCATIONS BETWEEN APPROXIMATELY BS 559+10 AND 559+80. COMPLIED WITH PERMANENT REPAIR TO THE FLOOR SUPPORT IAW SRM AND REO, ALL APPLICABLE STEPS COMPLIED WITH, COMPLETED TASK CARD.
- [SDR SWIA2020072251376](https://openairdocs.org/sdr/SWIA2020072251376.md): Bulkhead · damaged · Jun 16, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BS 621 PRESSURE BULKHEAD, FWD FACE ABOVE FLOOR, AREA EXIBITS MANY SCREW STARTS AND GOUGES, AND SEVERAL DAMAGED RIVET HEADS. REPAIRED THE BS 621 BULKHEAD IAW REO. COMPLIED WITH TASK CARD.
- [SDR SWIA2020072251413](https://openairdocs.org/sdr/SWIA2020072251413.md): Seat Track · damaged · Jun 15, 2020 · N937EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > COPILOTS OUTBOARD SEAT TRACK HAS MISSING AND DAMAGED FASTENER HEADS FOR THE TOP CAP PLATE. PERFORMED PERMANENT REPAIR TO COPILOT'S OTBD SEAT TRACK. REF REO & DWG.
- [SDR SWIA2020072251375](https://openairdocs.org/sdr/SWIA2020072251375.md): Intercostal · corroded · Jun 15, 2020 · N937EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR, MIDDLE INTERCOSTAL AT DD4 WAS CORRODED. INSTALLED A NEW PAX DOOR DD4 INTERCOSTAL IAW SRM AND DWG, PRESSURE LEAK CHECKED GOOD. NO DEFECTS NOTED. COMPLIED WITH STRUCTURAL MAJOR REPAIR.
- [SDR SWIA2020072251374](https://openairdocs.org/sdr/SWIA2020072251374.md): Intercostal · corroded · Jun 15, 2020 · N937EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR, MIDDLE INTERCOSTAL DD6 HAS SIGNS OF CORROSION AND LOSS PF PROTECTIVE COATING. REMOVED AND REPLACED PAX DOOR INTERCOSTAL IAW SRM AND DWG, COMPLETED TASK CARD, CHECKED OKAY.
- [SDR SWIA2020072251373](https://openairdocs.org/sdr/SWIA2020072251373.md): Bracket · corroded · Jun 15, 2020 · N937EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR - CLIP AT APPROX. FS347 FOR THE AFT INTERCOSTAL AT DD6 HAS CORROSION. (C-CHECK) RO 7/18/2020 INSTALLED NEW PAX DOOR CLIP COMMON TO AFT DD6 INTERCOSTAL, REF. CRJ200 SRM AND BOMBARDIER DWG, PRESSURE LEAK CHECK GOOD AT THIS TIME, NO LEAKS FOUND AT
- [SDR SWIA2020072251400](https://openairdocs.org/sdr/SWIA2020072251400.md): Roller · cracked · Jun 14, 2020 · N937EV · Cndair CL6002B19 · Galley Doors
  > SERVICE DOOR: AFT DOWN-LOCK ROLLER IS CRACKED. REMOVED AND REPLACED THE ROLLER AND PIN IAW AMM.
- [SDR SWIA2020072251372](https://openairdocs.org/sdr/SWIA2020072251372.md): Bulkhead · chafed · Jun 14, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > *FS280, RIGHT SIDE BULKHEAD HAS CHAFES ON A REPAIR DOUBLER ON THE AFT SIDE. REMOVED AND REPLACED THE EXISTING CHAFED -1 DOUBLER WITH A NEW -1 DOUBLER REF PREVIOUSLY ACCOMPLISHED REO, SRM AND RESTORED FINISH TO REWORK AREA IAW SRM.
- [SDR SWIA2020072251371](https://openairdocs.org/sdr/SWIA2020072251371.md): Skin · dented · Jun 13, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT IN AIRCRAFT SKIN BS 603, STR 18L. REPAIRED THE DENT WITH GOUGE IAW REO.
- [SDR SWIA2020072251370](https://openairdocs.org/sdr/SWIA2020072251370.md): Hinge Fitting · chafed · Jun 11, 2020 · N937EV · Cndair CL6002B19 · Fuselage, Door Hinge
  > RIGHT EMERGENCY DOOR HINGE FITTINGS FWD AND AFT HAVE ABRASION DAMAGE. COMPLIED WITH PERMANENT REPAIR DOOR HINGE FITTINGS REF REO, ALL STEPS COMPLIED WITH, CHECKS OKAY, COMPLETED TASK CARD
- [SDR SWIA2020072251364](https://openairdocs.org/sdr/SWIA2020072251364.md): Skin · dented · Jun 8, 2020 · N937EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > 6 EA. DENT LOCATED @ APPROX. FS605 BELOW WL 783.50 (MARKED). PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. ALL DENTS REPAIRED WITHIN ALLOWABLE LIMITS REF REO, ALL STEPS COMPLIED WITH

Next page: https://openairdocs.org/aircraft/N937EV/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 = 'N937EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N937EV/reports

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