# Service difficulty reports: N750EV

A list on [N750EV](https://openairdocs.org/aircraft/N750EV.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 6 · 265 reports

- [SDR SWIA2026011900006](https://openairdocs.org/sdr/SWIA2026011900006.md): Trim Switch · faulted · Jan 16, 2026 · N750EV · Cndair CL6002C10 · Stabilizer Position Indicating
  > STAB TRIM RUNAWAY NOSE DOWN JUST AFTER TAKEOFF. PREFORMED QRC, THEN QRH. LANDED FLAPS 20. (FLIGHT 6262) B1-007955 THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31555299 WITH THE FOLLOWING CORRECTIVE ACTION: REFER TO CP 31556697 FOR CORRECTIVE ACTION OF FIRS
- [SDR SWIA202502261218](https://openairdocs.org/sdr/SWIA202502261218.md): Guide Fitting · gouged · Dec 18, 2024 · N750EV · Cndair CL6002C10 · Trailing Edge Flaps
  > LEFT OUTBOARD FLAP, INBOARD GUIDE FITTING GOUGED. (C-CHECK RO 2/25/2025) PERFORMED REPAIR AREA ON LH OB FLAP IB GUIDE FITTING IAW REO 670-57-51-587 REV-- DATE 2025-01-17, CRJ700 SRM 51-24-11, 53-00-00, 51-12-00.
- [SDR SWIA202502261212](https://openairdocs.org/sdr/SWIA202502261212.md): Housing · cracked · Dec 12, 2024 · N750EV · Cndair CL6002C10 · Wing Main, Frame Structure
  > CRACK IN SLAT TRACK HOUSING INSIDE FUEL PANEL 551AB (C-CHECK RO 2/25/2025) REPAIRED DAMAGED SLAT TRACK HOUSING INSIDE FUEL PANEL 551AB IAW REO 670-57-42-577 REV-- DATE 2016-12-02 AND CRJ700 AMM 20-70-00, 28-11-00.
- [SDR SWIA202502261211](https://openairdocs.org/sdr/SWIA202502261211.md): Housing · cracked · Dec 11, 2024 · N750EV · Cndair CL6002C10 · Wing Main, Frame Structure
  > SLAT TRACK HOUSING HAS CRACK INSIDE FUEL PANEL 651AB (C-CHECK RO 2/25/2025) REPAIRED DAMAGED SLAT TRACK HOUSING INSIDE FUEL PANEL 651AB IAW REO 670-57-42-577 REV-- DATE 2016-12-02 AND CRJ700 SRM 51-21-11, 51-25-06, AMM 20-70-00, 27-81-41, 27-81-39, 28-1
- [SDR SWIA202502261206](https://openairdocs.org/sdr/SWIA202502261206.md): Floorbeam · cracked · Dec 6, 2024 · N750EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LBL12 COCKPIT FLOOR BEAM CRACKED AT BOTTOM WHERE IT ATTACHES TO 280 BEAM (C-CHECK RO 2/25/2025) PERFORMED REPAIR AREA ON LBL12 COCKPIT FLOOR BEAM TO 280 BEAM IAW REO 670-53-11-896 REV-- DATE: 2015-03-17, CRJ700 AMM 20-70-00, CRJ700 SRM 51-42-06, 51-42-1
- [SDR SWI2025F00173](https://openairdocs.org/sdr/SWI2025F00173.md): Drag Angle · cracked · Dec 6, 2024 · N750EV · Cndair CL6002C10 · Horizontal Stabilizer Structure
  > RH REAR FUSELAGE TO VERTICAL DRAG ANGLE CRACKED (C-CHECK RO 2/25/2025) REPAIRED DAMAGED DRAG ANGLE AND FILLER ON RH REAR FUSELAGE IAW REO 670-55-31-018 REV-A DATE 2016-11-10. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S121824-2, P.O# 174
- [SDR SWI2025F00172](https://openairdocs.org/sdr/SWI2025F00172.md): Drag Angle · cracked · Dec 6, 2024 · N750EV · Cndair CL6002C10 · Horizontal Stabilizer Structure
  > LH REAR FUSELAGE TO VERTICAL FWD AND AFT DRAG ANGLES CRACKED (C-CHECK RO 2/25/2025) PERFORMED REPAIR ON LH REAR FUSELAGE TO VERTICAL STABILIZER AT FWD AND AFT DRAG ANGLES IAW BOMBARDIER REO 670-55-31-018 REV-A DATE: 2016-11-10 AND IAW CRJ 700 SRM 51-25
- [SDR SWIA20250226924](https://openairdocs.org/sdr/SWIA20250226924.md): Skin · dented · Sep 24, 2024 · N750EV · Cndair CL6002C10 · Rudder, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA78985-670-55-41-107 750EV MXCODEID62683-PR - DENT ON THE RIGHT SIDE RUDDER SKIN AT (RHS DWG: CC670-22031, POCKET THICKNESS AT SUBJECT LOCATION 0.25" +/- 0.004",REF) BETWEEN RS 102.520-RS 108.250. DENT MEASURES 0.383"
- [SDR SWIA202401250003](https://openairdocs.org/sdr/SWIA202401250003.md): Duct · warning message · Jan 23, 2024 · N750EV · Cndair CL6002C10 · Ice/Rain Protection System
  > DURING DECENT WE TURNED ON WINGS AND COWLS ANTI-ICE. WE RECEIVED ANTI ICE DUCT CAUTION MESSAGE FOLLOWED BY ANTI ICE DUCT WARNING AND L/R DUCT FAIL. WE RAN THE QRH FOR BOTH WARNING AND CAUTION. WE DECLARED AN EMERGENCY AND DESCENDED IMMEDIATELY. ONCE WE LEVELED
- [SDR SWIA202401240003](https://openairdocs.org/sdr/SWIA202401240003.md): Duct · warning message · Jan 23, 2024 · N750EV · Cndair CL6002C10 · Airfoil Anti/De-ice System
  > DURING DECENT WE TURNED ON WINGS AND COWLS ANTI-ICE. WE RECEIVED ANTI ICE DUCT CAUTION MESSAGE FOLLOWED BY ANTI ICE DUCT WARNING AND L/R DUCT FAIL. WE RAN THE QRH FOR BOTH WARNING AND CAUTION. WE DECLARED AN EMERGENCY AND DESCENDED IMMEDIATELY. ONCE WE LEVELED
- [SDR SWIA202311280017](https://openairdocs.org/sdr/SWIA202311280017.md): Unknown · warning message · Nov 27, 2023 · N750EV · Cndair CL6002C10 · Airfoil Anti/De-ice System
  > WING OVHT WARNING MESSAGE ON CLIMB OUT, AROUND 600 FT. NOT IN ICING CONDITIONS, WING ANTI/ICE OFF. THEN MESSAGE CLEARED. RAN QRH. MESSAGE DID NOT RETURN. (FLIGHT 4944 FILED CLOSED)PERFORMED OPS CHECK OF WING A/I PER CRJ700 AMM 30-12-00, OPS CHECK GOOD
- [SDR SWIA20230809008](https://openairdocs.org/sdr/SWIA20230809008.md): Unknown · damaged · Aug 8, 2023 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > THE I/B SEAT TRACK AT SEATS 3C, 4C & 15C ARE DAMAGED. (FILED CLOSED)REMOVED AND REPLACED THE I/B SEAT TRACK AT SEATS 3C, 4C & 15C IN REF TO AMM 25-21-01.
- [SDR SWIA2021071459550](https://openairdocs.org/sdr/SWIA2021071459550.md): Window · delaminated · Jul 13, 2021 · N750EV · Cndair CL6002C10 · Flight Compartment Windows
  > RIGHT SIDE WINDOW SHOWING DELAMINATION REQUIRES REPLACEMENT. (FILED CLOSED) REMOVED FO SIDE WINDOW IN REFERENCE TO AMM 56-12-01.SEE CP 23112089-1 FOR INSTALLATION.
- [SDR SWIA202054874](https://openairdocs.org/sdr/SWIA202054874.md): Seal · out of position · Dec 30, 2020 · N750EV · Cndair CL6002C10 · Passenger/Crew Doors
  > LOUD NOISE HAPPENED WHILE CLIMBING THROUGH FL200. NO PRESSURIZATION ISSUES IDENTIFIED. NO CAUTION NO WARNING NO STATUS MESSAGES ON EICAS ALERTING US OF AN ISSUE. CREW REPORTED THE LANDING WEIGHT WAS 65K AND VSI WAS LESS THAN 360FPM. PERFORMED INSPECTION RE
- [SDR SWIA202054660](https://openairdocs.org/sdr/SWIA202054660.md): Stringer Splice · corroded · Nov 25, 2020 · N750EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER JOINT PIECE AT FS 333.00 COMMON TO STGR 23R. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW STRINGER JOINT PIECE AT FS 333.00 COMMON TO STGR 23R, REF CRJ 700 SRM AND DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.
- [SDR SWIA202054659](https://openairdocs.org/sdr/SWIA202054659.md): Stringer Splice · corroded · Nov 23, 2020 · N750EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER JOINT PIECE STGR 24R AT FS 333.00. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW STRINGER JOINT PIECE STGR 24R AT FS 333.00, REF. CRJ 700 SRM AND DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.
- [SDR SWIA202054700](https://openairdocs.org/sdr/SWIA202054700.md): Attach Angle · corroded · Nov 22, 2020 · N750EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > ATTACHMENT ANGLE LOCATED ON STGR 26L BETWEEN FS 349-FS 364 HAS SEVERE CORROSION ON AFT CORNER, MARKED. C-CHECK RO 12/14/2020. INSTALLED NEW ATTACHMENT ANGLE LOCATED AT STGR 26L BETWEEN FS 349-FS 364, PER CRJ 700 SRM.
- [SDR SWIA202054658](https://openairdocs.org/sdr/SWIA202054658.md): Door Sill · damaged · Nov 18, 2020 · N750EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SEVERAL ELONGATED HOLES IN PAX DOOR FLOOR SILL STRUCTURE, MARKED. C-CHECK RO 12/14/2020. UPSIZED HOLES AND INSTALLED NEW FASTENERS, REF MHIRJ REO FOR REPAIR TO ELONGATED HOLES IN PAX DOOR FLOOR SILL STRUCTURE.
- [SDR SWIA202054657](https://openairdocs.org/sdr/SWIA202054657.md): Skin · dented · Nov 18, 2020 · N750EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > EXTERNAL SKIN HAS DENT LOCATED APPROXIMATELY AT FS 1015.00 TO FS 1031 BETWEEN STRINGER 23L AND STGR 24L. C-CHECK RO 12/14/2020. CUT DAMAGE OUT AND INSTALLED DOUBLER AT EXTERNAL SKIN AT FS 1015.00 TO FS 1031 BETWEEN STRINGER 23L AND STGR 24L, REF CRJ 700 SRM.
- [SDR SWIA202054656](https://openairdocs.org/sdr/SWIA202054656.md): Diaphragm · corroded · Nov 16, 2020 · N750EV · Cndair CL6002C10 · Fluid Service Doors
  > WHILE REMOVING FRAME SECTOR AT FS 379.00 FOUND CORROSION ON WATER WASTE SERVICE DOOR LOWER DIAPHRAGM P/N SH670-32284-3. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW SERVICABLE DIAPHRAGM ON LOWER FWD WATER WASTE DOOR SURROUND STRUCTURE, REF DWG AND CRJ 70
- [SDR SWIA202054698](https://openairdocs.org/sdr/SWIA202054698.md): Seat Track · corroded · Nov 12, 2020 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT TRACK BETWEEN FS 428.00-485.00 LBL 27, MUTIPLE AREAS MARKED. C-CHECK RO 12/14/2020. REMOVED AND REPLACED NEW SEAT TRACK AT LBL 27 BETWEEN FS 428 TO FS 485, PER CRJ 700 AMM TOOL USED TUC8834 CAL:01-JUN-20 DUE:30-JUN-21.
- [SDR SWIA202054655](https://openairdocs.org/sdr/SWIA202054655.md): Intercostal · corroded · Nov 12, 2020 · N750EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON RT LATCH PIN INTERCOSTAL LOCATED BETWEEN FS 349.00-FS 364.00 AND BETWEEN STGR 27-STGR 26R. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW RT LATCH PIN INTERCOSTAL LOCATED BETWEEN FS 349.00-FS 364.00 AND BETWEEN STGR 27-STGR 26R, REF CRJ
- [SDR SWIA202054654](https://openairdocs.org/sdr/SWIA202054654.md): Stringer · corroded · Nov 12, 2020 · N750EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER 27 BETWEEN FS 333.00 AND FS 349.00. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW STRINGER 27 BETWEEN FS 333.00 AND FS 349.00, REF CRJ 700 SRM & DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.
- [SDR SWIA202054653](https://openairdocs.org/sdr/SWIA202054653.md): Intercostal · corroded · Nov 12, 2020 · N750EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON BACK-UP SILL AT STGR 21L BETWEEN FS 333.00 AND FS 349.00. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW BACK-UP SILL AT STGR 21L BETWEEN FS 333.00 AND FS 349.00, REF CRJ 700 SRM DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.
- [SDR SWIA202054652](https://openairdocs.org/sdr/SWIA202054652.md): Intercostal · corroded · Nov 12, 2020 · N750EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL AT 21L FROM FS 310.00 TO FS 333.00. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW INTERCOSTAL AT 21 L FROM FS 310.00 TO 333.00, REF CRJ 700 SRM DWG. COMPLIED WITH TASK CARD. PRESSURE CHECKS GOOD.
- [SDR SWIA202054651](https://openairdocs.org/sdr/SWIA202054651.md): Intercostal · corroded · Nov 11, 2020 · N750EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL ON STRG 20R BETWEEN FS 319.70 AND FS 349.00 IS CORRODED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW INTERCOSTAL ON STRG 20R BETWEEN FS 319.70 AND FS 349.00, REF CRJ 700 SRM DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.
- [SDR SWIA202054650](https://openairdocs.org/sdr/SWIA202054650.md): Intercostal · corroded · Nov 11, 2020 · N750EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL ON STRG 20R BETWEEN FS 310 & FS 319.70 IS CORRODED. C-CHECK RO 12/14/2020. REPLACED INTERCOSTAL ON STRG 20R BETWEEN FS 310 & FS 319.70 PN: SH670-32047-1, IAW DWG, CRJ700 SRM, AND COMPLIED WITH SKYCARD.
- [SDR SWIA202054703](https://openairdocs.org/sdr/SWIA202054703.md): Clamp · broken · Nov 10, 2020 · N750EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR FWD FRAME FS 319.70 HAS BROKEN TEFLON CLAMP AT APPROXIMATELY STGR 15 HINGE AREA, MARKED. C-CHECK RO 12/14/2020. REPLACED BROKEN TEFLON CLAMP WITH 1 EA NEW TEFLON CLAMP, REF CRJ 700 AMM.
- [SDR SWIA202054699](https://openairdocs.org/sdr/SWIA202054699.md): Seat Track · corroded · Nov 10, 2020 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT TRACK BETWEEN FS 349.00-428.00 LBL 27, MULTIPLE AREAS MARKED. C-CHECK RO 12/14/2020. REMOVED AND REPLACED SEAT TRACK AT LBL 27 FROM FS 349 TO FS 428, PER CRJ 700 AMM TOOLS USED TUC8834 CAL: 01-JUN-20 DUE:30-JUN-21.
- [SDR SWIA202054697](https://openairdocs.org/sdr/SWIA202054697.md): Seat Track · corroded · Nov 10, 2020 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT SIDE SEAT TRACK BETWEEN FS 572.00-669.00. C-CHECK RO 12/14/2020. REMOVED AND REPLACED RT SIDE SEAT TRACK FROM FS 573.00 TO FS 675.00, P/N SH670-33558-3, PER CRJ700 AMM USING CALIBRATED TOOL TUC5658 DUE: 31-JUL-21.
- [SDR SWIA202054696](https://openairdocs.org/sdr/SWIA202054696.md): Seat Track · corroded · Nov 10, 2020 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT SIDE SEAT TRACK BETWEEN FS 572.00-669.00. C-CHECK RO 12/14/2020. REMOVED AND REPLACED LT SIDE SEAT TRACK FROM FS 573.00 TO FS 675.00, P/N SH670-33558-3 PER CRJ700 AMMS 53-00-49-000-801-A17 AND USING CALIBRATED TOOL TUC5658 DUE: 31-JUL-21.
- [SDR SWIA202054695](https://openairdocs.org/sdr/SWIA202054695.md): Seat Track · corroded · Nov 10, 2020 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT SIDE SEAT TRACK BETWEEN FS 485.00-572.00. C-CHECK RO 12/14/2020. REMOVED AND REPLACED RT SIDE SEAT TRACK FROM FS 483.00 TO FS 573, P/N SH670-32234-951 PER CRJ700 AMM USING CALIBRATED TOOL TUC5658 DUE: 31-JUL-21.
- [SDR SWIA202054694](https://openairdocs.org/sdr/SWIA202054694.md): Seat Track · corroded · Nov 10, 2020 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT SIDE SEAT TRACK BETWEEN FS 485.00-572.00. C-CHECK RO 12/14/2020. REMOVED AND REPLACED LT SIDE SEAT TRACK FROM FS 483.00 TO FS 573.00, P/N SH670-32234-951 PER CRJ700 AMM USING CALIBRATED TOOL TUC5658 DUE: 31-JUL-21.
- [SDR SWIA202054693](https://openairdocs.org/sdr/SWIA202054693.md): Seat Track · corroded · Nov 10, 2020 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT SIDE SEAT TRACK BETWEEN FS 364.00-485.00. C-CHECK RO 12/14/2020. INSTALLED NEW REPLACEMENT LT SIDE SEAT TRACK AT FS 378.00-FS 483.00, REF CRJ700 AMM. TOOL NR TUC7824 CAL: 01-JUN-20 DUE: 30-JUN-21.
- [SDR SWIA202054692](https://openairdocs.org/sdr/SWIA202054692.md): Seat Track · corroded · Nov 10, 2020 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LT SIDE SEAT TRACK BETWEEN FS 364.00-485.00. C-CHECK RO 12/14/2020. INSTALLED NEW REPLACEMENT LT SIDE SEAT TRACK AT FS 378.00-FS 483.00, REF CRJ700 AMM. TOOL NR TUC7824 CAL: 01-JUN-20 DUE: 30-JUN-21.
- [SDR SWIA202054649](https://openairdocs.org/sdr/SWIA202054649.md): Bracket · corroded · Nov 10, 2020 · N750EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > FS 1031 STGR 22L CORNER BRACKET CORRODED, AS MARKED. C-CHECK RO 12/14/2020. REMOVED AND REPLACED CORNER STRINGER CLIP WITH NEW AT FS 1031.00 STR 22L, REF CRJ700 SRM & DWG, FIT CHECK GOOD. RESTORED FINISH. COMPLIED WITH SKYWEST TASK CARD.
- [SDR SWIA202054648](https://openairdocs.org/sdr/SWIA202054648.md): Stringer Splice · corroded · Nov 10, 2020 · N750EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER JOINT PIECE FS 333.00 COMMON TO STGR 25L. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW STRINGER JOINT PIECE FS 333.00 COMMON TO STGR 25L, REF CRJ 700 SRM DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.
- [SDR SWIA202054647](https://openairdocs.org/sdr/SWIA202054647.md): Floor Support · corroded · Nov 10, 2020 · N750EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON RT FLOOR SILL FS 280-FS 319.70. C-CHECK RO 12/14/2020. REMOVED CORROSION ON RT FLOOR SILL AT FS 280-FS 319.70 FOUND 100% MATERIAL LOSS CRJ700 SRM. INSTALLED NEW FLOOR SILL AT RT FS 280-319.70, REF DRW AND CRJ700 SRM. PERFORMED PRESSURE CHECK
- [SDR SWIA202054646](https://openairdocs.org/sdr/SWIA202054646.md): Channel · corroded · Nov 10, 2020 · N750EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DRAIN MAST DOUBLER BETWEEN STGRS 27/26R AND FS 1031/1047 CORRODED, AS MARKED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED NEW DRAIN MAST DOUBLER BETWEEN STGRS 27/26R AND FS 1031/1047, REF CRJ 700 SRM DWG. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD.
- [SDR SWIA202054691](https://openairdocs.org/sdr/SWIA202054691.md): Seat Track · corroded · Nov 9, 2020 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RT FLOOR SEAT RAIL CORRODED BETWEEN FS 847.00-985.00 RBL 9, MULTIPLE AREAS MARKED. C-CHECK RO 12/14/2020. REMOVED AND REPLACED CORRODED SEAT TRACK WITH NEW SEAT TRACK, REF CRJ 700 AMM AND CRJ 700 SRM. SEE CONTINUATION CARD FOR DETAILS USING CALIBRATED TOOL
- [SDR SWIA202054690](https://openairdocs.org/sdr/SWIA202054690.md): Seat Track · corroded · Nov 9, 2020 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED LBL 9 FROM FS 708.00 THRU FS 847.00. C-CHECK RO 12/14/2020. REMOVED AND REPLACED CORRODED SEAT TRACK WITH NEW SEAT TRACK, REF CRJ 700 AMM AND CRJ 700 SRM. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202054689](https://openairdocs.org/sdr/SWIA202054689.md): Seat Track · corroded · Nov 9, 2020 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED RBL 9 FROM FS 581.00 TO FS 708.00. C-CHECK RO 12/14/2020. INSTALLED 2 EA NEW REPLACEMENT SEAT TRACKS AT RBL 9.00 FROM FS 581.00-FS 683.50 AND FS 683.50-FS 837.00, REF CRJ700 AMM. TOOL NR TUC7824 CAL: 01-JUN-20 DUE: 30-JUN-21.
- [SDR SWIA202054688](https://openairdocs.org/sdr/SWIA202054688.md): Seat Track · corroded · Nov 9, 2020 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED LBL 9 FROM FS 581.00 TO FS 708.00. C-CHECK RO 12/14/2020. REMOVED AND REPLACED NEW SEAT TRACK AT LBL 9 FROM FS 581 TO FS 708, PER CRJ 700 AMM. TOOLS USED TUC8834 CAL: 01-JUN-20 DUE: 30-JUN-21.
- [SDR SWIA202054687](https://openairdocs.org/sdr/SWIA202054687.md): Seat Track · corroded · Nov 9, 2020 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED RBL 9 FROM 485.00 TO FS 581.00. C-CHECK RO 12/14/2020. INSTALLED NEWLY FABRICATED SEAT TRACK FROM RBL 9 FS 485.00 THRU FS 581.00, IAW CRJ 700 AMM. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202054686](https://openairdocs.org/sdr/SWIA202054686.md): Seat Track · corroded · Nov 9, 2020 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED LBL 9 FROM 485.00 TO FS 581.00. C-CHECK RO 12/14/2020. REMOVED AND REPLACED NEW SEAT TRACK AT LBL 9 FROM FS 485 TO FS 581, PER CRJ 700 AMM.
- [SDR SWIA202054685](https://openairdocs.org/sdr/SWIA202054685.md): Seat Track · corroded · Nov 9, 2020 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED LBL 9 FROM FS 349.00 THRU FS 485.00. C-CHECK RO 12/14/2020. REMOVED AND REPLACED NEW SEAT TRACK AT LBL 9 FROM FS 349 TO FS 485, PER CRJ 700 AMM.
- [SDR SWIA202054684](https://openairdocs.org/sdr/SWIA202054684.md): Seat Track · corroded · Nov 9, 2020 · N750EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACKS CORRODED RBL 9 FROM FS 349.00 THRU FS 485.00. C-CHECK RO 12/14/2020. REPLACED CORRODED SEAT TRACK RBL 9 FROM FS 349.00 THRU FS485.00, IAW CRJ 700 AMM CONFIG A03. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202054645](https://openairdocs.org/sdr/SWIA202054645.md): Strap · corroded · Nov 9, 2020 · N750EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UNDERFLOOR CORROSION ON FUSELAGE STRAP AT FS 280.00 BETWEEN STGR 26L-25R, AREAS MARKED. C-CHECK RO 12/14/2020. REMOVED COROSION TO ACCEPTABLE LIMITS AT UNDERFLOOR FUSELAGE STRAP AT FS 280.00 BETWEEN STGR 26L-25R, REF REO AND CRJ700 SRM. VERIFIED ALL CONDITI
- [SDR SWIA202054644](https://openairdocs.org/sdr/SWIA202054644.md): Attach Angle · corroded · Nov 9, 2020 · N750EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CORROSION ON ATTACHING ANGLE TO STGR 19L AND FRAME FS 295.00, MARKED. C-CHECK RO 12/14/2020. REMOVED AND INSTALLED "NEW" STRINGER CLEAT LOCATED ON STGR 19L AT FS 295, AS REQUIRED REF CRJ700 SRM AND DWG. SEE CONTINUE CARD FOR DETAILS.
- [SDR SWIA202054643](https://openairdocs.org/sdr/SWIA202054643.md): Stringer · corroded · Nov 9, 2020 · N750EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 23R BETWEEN FS 319.00-333.00, MARKED. C-CHECK RO 12/14/2020. STGR 23R LOCATED BETWEEN FS 280-FS 333 OUT OF LIMITS. REMOVED AND REPLACED WITH NEW AND RESTORED FINISH, REF CRJ 700 SRM AND DRAWING. TASK CARD COMPLIED WITH. CHECK GOOD SEE CO

Next page: https://openairdocs.org/aircraft/N750EV/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 = 'N750EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N750EV/reports

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