# Service difficulty reports: N740EV

A list on [N740EV](https://openairdocs.org/aircraft/N740EV.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 · 282 reports

- [SDR SWIA2025100600005](https://openairdocs.org/sdr/SWIA2025100600005.md): A/C Pack · failed · Oct 5, 2025 · N740EV · Cndair CL6002C10 · Cabin Cooling System
  > L PACK AUTOFAIL. AFTER LANDING BURNING SMELL COMING THROUGH PACKS THEN WE GOT THE L PACK AUTOFAIL CAUTION MESSAGE. TEMP IS 99C ON SYNOPTIC PAGE. (FLIGHT 6351) INTERROGATED MDC, MDC FLAGGING TEMP CTRL VLV1 B1 CODE - 211941 AND PK1 DISCH T SNSR B1 CODE- 00752
- [SDR SWI2025F00769](https://openairdocs.org/sdr/SWI2025F00769.md): Light · loose · Jun 27, 2025 · N740EV · Cndair CL6002C10 · Air Distribution System
  > FLIGHT ATTENDANT REPORTS MECHANICAL BURNING SMELL FROM INSIDE AND/OR NEAR FIRST CLASS COAT CLOSET. 1ST OFFICER SAYS HE COULD SMELL IT WHILE STANDING NEAR THE CLOSET AND THAT IT SMELLS LIKE BURNING RUBBER. FOUND WIRES WITH DAMAGED OUTER COATING IN THE CLOSET.
- [SDR SWIA202403110128](https://openairdocs.org/sdr/SWIA202403110128.md): Intercostal · corroded · Jan 28, 2024 · N740EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD5 AFT IS CORRODED, HN00134302 (C-CHECK RO 3/10/2024) INSTALLED NEW PAX DOOR AFT INTERCOSTAL DD5 IRT DWG 601R31702 REV -N, CRJ700 SRM 51-42-06-001-001-A01. RESTORED FINISH ALL FASTENERS AND APPLIED C.I.C AT REPAIRED LOCATION IAW CRJ
- [SDR SWI202403110199](https://openairdocs.org/sdr/SWI202403110199.md): Frame Angle · corroded · Jan 25, 2024 · N740EV · Cndair CL6002C10 · Fuselage Main, Structure
  > RH FS379.00 FRAME REINFORCING ANGLE (PN: SH670-32119-1) CORRODED AT STR 23R. (C-CHECK RO 3/10/2024) REMOVED AND REPLACED UNSERVICABLE RH FS379.00 FRAME REINFORCING ANGLE (PN: SH670-32119-1) WITH NEW REF. DRWG SH670-32050 REV. J AND CRJ 700 SRM 51-42-06-001
- [SDR SWIA2024031100125](https://openairdocs.org/sdr/SWIA2024031100125.md): Window Frame · cracked · Jan 25, 2024 · N740EV · Cndair CL6002C10 · Fuselage Main, Structure
  > RH WINDSHIELD POST IS CRACKED. (C-CHECK RO 3/10/2024) REMOVED AND INSTALLED NEW R/H WINDSHIELD SIDE POST CRJ 700 SRM 51-42-21-001-001-A01 AND DWG CC670-33055 REV. -F. LEAK CHECK GOOD. COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWI20240311000193](https://openairdocs.org/sdr/SWI20240311000193.md): Intercostal · cracked · Jan 24, 2024 · N740EV · Cndair CL6002C10 · Passenger/Crew Doors
  > POSSIBLE CRACK ON PAX DOOR AFT DD7 INTERCOSTAL JOB # HN00134589 (C-CHECK RO 3/10/2024) REMOVED AND INSTALLED NEW PAX DOOR AFT INTERCOSTAL DD7 IRT DWG 601R31702 REV -N, CRJ700 SRM 51-42-06-001-001-A01, LEAK CHECK GOOD. COMPLIED WITH TASK 51-900-1002-SKY
- [SDR SWI202403110192](https://openairdocs.org/sdr/SWI202403110192.md): Intercostal · cracked · Jan 24, 2024 · N740EV · Cndair CL6002C10 · Passenger/Crew Doors
  > POSSIBLE CRACK ON PAX DOOR FWD DD7 INTERCOSTAL JOB # HN00134589 (C-CHECK RO 3/10/2024) REMOVED CRACKED AND INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD7 - REF IRT DWG 601R31702 REV -N AND CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SK
- [SDR SWI20240311000191](https://openairdocs.org/sdr/SWI20240311000191.md): Intercostal · corroded · Jan 24, 2024 · N740EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD1A BETWEEN FS338.963 & FS347.250 IS CORRODED, HN00134669 (C-CHECK RO 3/10/2024) REMOVED CORRODED AND INSTALLED NEW PAX DOOR AFT INTERCOSTAL DD1A BETWEEN FS338.963 & FS347.250 - REF IRT DWG 601R31702 REV -N & CRJ700 SRM 51-42-06-001-0
- [SDR SWI202403110190](https://openairdocs.org/sdr/SWI202403110190.md): Former · cracked · Jan 24, 2024 · N740EV · Cndair CL6002C10 · Passenger/Crew Doors
  > POSSIBLE CRACK FOUND ON PAX DOOR AFT FORMER JOB # HN00134599 (C-CHECK RO 3/10/2024) REMOVED CRACKED AND INSTALLED NEW PAX DOOR AFT FORMER IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 AND IAW DWG 601R31702 REV. N. COMPLIED WITH
- [SDR SWI202403110189](https://openairdocs.org/sdr/SWI202403110189.md): Intercostal · cracked · Jan 24, 2024 · N740EV · Cndair CL6002C10 · Passenger/Crew Doors
  > POSSIBLE CRACK ON PAX DOOR FWD DD1 INTERCOSTAL JOB # (C-CHECK RO 3/10/2024) REMOVED CRACKED AND INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD1 IRT DWG 601R31702 REV -N, CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR R
- [SDR SWI202403110195](https://openairdocs.org/sdr/SWI202403110195.md): Intercostal · corroded · Jan 24, 2024 · N740EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD7A BETWEEN FS320.163 & FS327.763 IS CORRODED, HN00134622 (C-CHECK RO 3/10/2024) REMOVED CORRODED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD7A BETWEEN FS320.163 & FS327.763 - REF IRT DWG 601R31702 REV -N AND CRJ700 SRM 51-42-06-001-001
- [SDR SWIA2024031100124](https://openairdocs.org/sdr/SWIA2024031100124.md): Intercostal · corroded · Jan 24, 2024 · N740EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID DD1 INTERCOSTAL IS CORRODED JOB # HN00134604 (C-CHECK RO 3/10/2024) REMOVED CORRODED AND INSTALLED NEW PAX DOOR MID DD1 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01 AND DWG 601R31702 REV. N. COMPLIED WI
- [SDR SWI20240311000189](https://openairdocs.org/sdr/SWI20240311000189.md): Intercostal · cracked · Jan 24, 2024 · N740EV · Cndair CL6002C10 · Passenger/Crew Doors
  > POSSIBLE CRACK ON PAX DOOR FWD DD1 INTERCOSTAL JOB # (C-CHECK RO 3/10/2024) REMOVED CRACKED AND INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD1 IRT DWG 601R31702 REV -N, CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY STRUCTURAL MAJOR R
- [SDR SWI202403110201](https://openairdocs.org/sdr/SWI202403110201.md): Stringer · corroded · Jan 20, 2024 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS BAY STR 23R CORRODED BETWEEN FS364.00 AND FS379.00. (C-CHECK RO 3/10/2024) REMOVED AND INSTALLED NEW STR 23R FROM FS356.00 TO FS379.00 REF. DRWG SH690-31350 REV. M AND CRJ 700 SRM 51-42-06-001-001-A01,CRJ 700 SRM 53-00-03-201-001-A01 REV. 38
- [SDR SWIA202403110020](https://openairdocs.org/sdr/SWIA202403110020.md): Door Frame · corroded · Jan 20, 2024 · N740EV · Cndair CL6002C10 · Fuselage Main, Structure
  > FORWARD WATER-WASTE DOOR SURROUND STRUCTURE LOWER DIAPHRAGM PN: SH670-32284-3 CORRODED. (C-CHECK RO 3/10/2024) INSTALLED NEW FORWARD WATER-WASTE DOOR SURROUND STRUCTURE LOWER DIAPHRAGM REF. DRWG SH670-32280 REV. H AND CRJ 700 SRM 51-42-06-001-001-A01. LOCA
- [SDR SWIA2024031100115](https://openairdocs.org/sdr/SWIA2024031100115.md): Frame · corroded · Jan 15, 2024 · N740EV · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION ON FRAME FS 379.00 BETWEEN STGR 21R - 23R, ACCESSED ON THE EXTERIOR OF AIRCRAFT THROUGH FWD WASTE WATER DOOR (HN00133395) (C-CHECK RO 3/10/2024) REMOVED AND INSTALLED NEW FS379.00 FRAME FROM STR 20R TO STR 25R REF. CRJ-700 DRWG SH670-32280 REV. H
- [SDR SWI20240311000197](https://openairdocs.org/sdr/SWI20240311000197.md): Attach Bracket · cracked · Jan 13, 2024 · N740EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT WING SLAT TRACK CANISTER ATTACHING BRACKET FOR 1-3 IS CRACKED. (FLAGGED & MARKED) (C-CHECK RO 3/10/2024) REPAIRED LH SLAT TRACK CANISTER ATTACHING BRACKET FOR 1-3 PER REO 670-57-42-577 REV -- DATED 2016-12-02 LEAK CHECK GOOD. COMPLIED WITH SKYWEST TAS
- [SDR SWIA20240311003](https://openairdocs.org/sdr/SWIA20240311003.md): Attach Bracket · cracked · Jan 13, 2024 · N740EV · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT WING SLAT TRACK CANISTER ATTACHING BRACKET FOR 1-3 IS CRACKED. (FLAGGED & MARKED) (C-CHECK RO 3/10/2024) REPAIRED RH SLAT TRACK CANISTER ATTACHING BRACKET FOR 1-3 PER REO 670-57-42-577 REV -- DATED 2016-12-02 LEAK CHECK GOOD. COMPLIED WITH SKYWEST
- [SDR SWI202403110202](https://openairdocs.org/sdr/SWI202403110202.md): Hinge · gouged · Jan 12, 2024 · N740EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASSENGER DOOR PIANO HINGE (DOOR SIDE) LUG #24 IS GOUGED. (MARKED) (C-CHECK RO 3/10/2024) REMOVED AND INSTALLED NEW PAX DOOR PIANO HINGE (DOOR SIDE) IAW CRJ 700 SRM 52-11-01-201-002-A01 STEP 4R, 4T AND DWG 601R31702 REV. N. APPLIED FILLET SEAL AROUND NEW
- [SDR SWIA2024031100112](https://openairdocs.org/sdr/SWIA2024031100112.md): Hinge · gouged · Jan 12, 2024 · N740EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASSENGER DOOR PIANO HINGE (FUSELAGE SIDE) LAND #27 IS GOUGED. (C-CHECK RO 3/10/2024) REPAIRED GOUGE ON PASSENGER DOOR PIANO HINGE (FUSELAGE SIDE) LAND #27 IRT REO 670-53-21-582 REV -F DATED 2017-08-02 TYPE IV:, COMPLIED WITH 51-900-1002-SKY
- [SDR SWI202403110196](https://openairdocs.org/sdr/SWI202403110196.md): Stand Off · cracked · Jan 10, 2024 · N740EV · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > R/H UPPER TRANSCOWL INBD A BRACKET IS CRACKED (C-CHECK RO 3/10/2024) R/H UPPER TRANSCOWL I/B "A" BRACKET HAS BEEN REMOVED AND REPLACED REF REO# 670-54-21-971, REV B, DATED 11/28/23. REFER TO CONTINUATION SHEET FOR DETAILS. COMPLIED W/SKYCARD 51-900-1002 S
- [SDR SWIA20240311011](https://openairdocs.org/sdr/SWIA20240311011.md): Transcowl · chafed · Jan 10, 2024 · N740EV · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > R/H UPPER TRANSCOWL INBD SLIDER IS WORN/CHAFED (C-CHECK RO 3/10/2024) COMPLIED WITH ALL STEPS OF REO 670-54-21-1610 REV €“ DATED: 2024-01-26, DISPOSITION FOR BLENDED CHAFE DAMAGE TO THE RH UPPER TRANSCOWL UPPER INBOARD SLIDER. COMPLIED WITH SKYWEST TASK C
- [SDR SWIA2024031100109](https://openairdocs.org/sdr/SWIA2024031100109.md): Stand Off · cracked · Jan 9, 2024 · N740EV · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > L/H UPPER TRANSCOWL INBD "A" BRACKET IS CRACKED. (C-CHECK RO 3/10/2024) INSTALLED 1 EA. NEW STAND-OFF P/N CN624-2082-201 ON L/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28
- [SDR SWIA2024031100106](https://openairdocs.org/sdr/SWIA2024031100106.md): Web · damaged · Jan 6, 2024 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DRILL START NOTED ON FWD CARGO DOOR WEB SILL AT APPROX.FS566 AND STRG26L (MARKED) (C-CHECK RO 3/10/2024) FWD CARGO DOOR WEB SILL AT APPROX.FS566 AND STRG26L REPAIRED PER MHIRJ REO 670-53-31-850 REV -- DATE 2024-02-08, COMPLIED WITH ALL STEPS OF TASK CARD 5
- [SDR SWI202403110198](https://openairdocs.org/sdr/SWI202403110198.md): Drag Angle · cracked · Jan 5, 2024 · N740EV · Cndair CL6002C10 · Vertical Stabilizer
  > CRACK NOTED ON VERTICAL STAB L/H FWD DRAG ANGLE (MARKED) (C-CHECK RO 3/10/2024) REPAIRED VERTICAL STAB LH FWD DRAG ANGLE REF CRJ700SRM 55-31-00-201-001-A01.COMPLETED SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWIA2024031100105](https://openairdocs.org/sdr/SWIA2024031100105.md): Drag Angle · cracked · Jan 5, 2024 · N740EV · Cndair CL6002C10 · Ventral Structure
  > CRACK NOTED ON L/H AFT VERTICAL STAB DRAG ANGLE (MARKED) (C-CHECK RO 3/10/2024) REPAIRED VERTICAL STAB LH AFT DRAG ANGLE REF CRJ700SRM 55-31-00-201-001-A01.COMPLETED SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWIA2024031100104](https://openairdocs.org/sdr/SWIA2024031100104.md): Skin · dented · Jan 4, 2024 · N740EV · Cndair CL6002C10 · Wing, Plate/Skin
  > L/H LOWER EXTERNAL SKIN IS SCRATCHED AND DENTED BETWEEN. WS350-WS370 AND 2" FROM L/E (MARKED) (C-CHECK RO 3/10/2024) REPAIRED SCRATCH AND DENT ON L/H LOWER EXTERNAL SKIN IS BETWEEN. WS350-WS370 AND 2" FROM L/E BY COMPLYING WITH REO 670-57-21-968 REV -- DA
- [SDR SWI20240311000194](https://openairdocs.org/sdr/SWI20240311000194.md): Slat Track · grooved · Dec 30, 2023 · N740EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT WING SLAT TRACK 1-1 HAS GROOVE IN INBOARD TRACK AS MARKED (C-CHECK RO 3/10/2024) COMPLIED WITH ALL STEPS OF REO 670-57-42-1479 REV -A DATED: 2024-02-27, DISPOSITION FOR BLENDED GOUGE DAMAGE TO SLAT TRACK 1-1, LHS. COMPLIED WITH SKYWEST TASK CARD: 51-9
- [SDR SWIA2024031100230](https://openairdocs.org/sdr/SWIA2024031100230.md): Landing · cracked · Dec 30, 2023 · N740EV · Cndair CL6002C10 · Fuselage Main, Structure
  > * R/H TRU BAY DOOR BOTTOM LANDING IS CRACKED AT THE AFT LATCH CUTOUT, MARKED. (C-CHECK RO 3/10/2024) REMOVED AND REPLACED LANDING AT R/H TRU BAY DOOR BOTTOM REF DRWG CC670-33040 REV. G, REO 670-53-11-1916 REV. -- DATED 2024-01-15 AND CRJ700 SRM 51-42-06-00
- [SDR SWI2024031100200](https://openairdocs.org/sdr/SWI2024031100200.md): Skin · chafed · Dec 29, 2023 · N740EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CHAFFING ON LOWER FUSELAGE SKIN AT FS974 (MARKED, CHAFFING FROM SUPPORT STRAP ON PANEL 196DR). (C-CHECK RO 3/10/2024) REPAIRED CHAFING ON LOWER FUSELAGE SKIN AT FS974 IAW ALL STEPS OF REO 670-53-00-718 REV -- DATED 2024-01-26 AND REO 670-53-00-290 REV-F, D
- [SDR SWIA20240311229](https://openairdocs.org/sdr/SWIA20240311229.md): Skin · dented · Dec 29, 2023 · N740EV · Cndair CL6002C10 · Ailerons
  > *DENT NOTED AT R/H INBD FLAP LOWER EXTERNAL SKIN AT APPROX. FLS29 AND 4" FROM T/E (MARKED) (C-CHECK RO 3/10/2024) INSTALLED -1 REPAIR DOUBLER AND -2 REPAIR FILLER ON R/H INBOARD FLAP LOWER SKIN REF CRJ 700 SRM 57-52-01-201-001-A01 TYPE IV REPAIR. COMPLIED
- [SDR SWIA202266352](https://openairdocs.org/sdr/SWIA202266352.md): None · smoke · Aug 28, 2022 · N740EV · Cndair CL6002C10 · Air Conditioning System
  > DURING CLIMB OUT OF DFW ABOUT 2800 FEET FAS CALLED WITH THE SMELL OF SMOKE AND ACTUAL SMOKE IN CABIN COMING FROM GALLEY AREA. / WE DECLARED AN EMERGENCY AND RETURNED TO DFW. SMOKE DISSIPATED IN FLIGHT AND LANDING WAS ROUTINE. WE DID LAND SLIGHTLY OVER WEIGHT
- [SDR SWIA202266216](https://openairdocs.org/sdr/SWIA202266216.md): None · odor · Aug 2, 2022 · N740EV · Cndair CL6002C10 · Air Conditioning System
  > AT APPROX FLT LEVEL 300FL FA REPORTED TO THE FLT DECK A BURNING ELECTRICAL SMELL. CAPT VERIFIED BURNING SMELL AROUND THE FLT DECK AND FWD FA JP SEAT AREA. NO SIGNS OF SMOKE OR FIRE. NO OTHER OBSERVED FAULTS OR ABNORMAL INDICATIONS. PACKS WERE NORMAL, ENGINES W
- [SDR SWIA202265283](https://openairdocs.org/sdr/SWIA202265283.md): None · cracked · Apr 6, 2022 · N740EV · Cndair CL6002C10 · Window/Windshield System
  > APPROXIMATELY 10 INCH HAIRLINE CRACK IN CAPTAINS SIDE WINDOW. (FLIGHT 3137 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24629586 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED L/H SIDE COCKPIT WINDOW ASSEMBLY IAW TASK CARD#
- [SDR SWIA202263823](https://openairdocs.org/sdr/SWIA202263823.md): None · inoperative · Jan 16, 2022 · N740EV · Cndair CL600* · Steering Unit
  > STEERING INOP CAUTION MESSAGE WHEN EXTENDING LANDING GEAR. QRH UNHELPFUL. NOSE GEAR WOULD NOT RETRACT FULLY AFTERWARDS, BUT IT DID FULLY EXTEND AGAIN. (FLIGHT 3050 - FILED CLOSED) UPON INVESTIGATION OF NOSE LANDING GEAR FOUND STRUT TO BE IN NEED OF SERVIC
- [SDR SWIA2020081251783](https://openairdocs.org/sdr/SWIA2020081251783.md): Floorbeam · damaged · Jul 31, 2020 · N740EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLOORBEAM FLANGE DAMAGED. PERFORMED RBL9 FLOOR BEAM FLANGE REPAIR REF REO. ALL STEPS COMPLETED AT THIS TIME. ST CARD COMPLETE.
- [SDR SWIA2020081251782](https://openairdocs.org/sdr/SWIA2020081251782.md): Floor Support · damaged · Jul 31, 2020 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PERFORM RBL9 FLOOR BEAM FLANGE REPAIR REF. REO 670-53-41-463. PERFORMED RBL9 FLOOR BEAM FLANGE REPAIR REF REO. ALL STEPS COMPLETED AT THIS TIME.
- [SDR SWIA2020081251781](https://openairdocs.org/sdr/SWIA2020081251781.md): Splice · corroded · Jul 31, 2020 · N740EV · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION FOUND ON I/B TOP SPLICE FOR RBL9 AT FS572.00. REPLACED IB TOP SPLICE ON RBL9 FLOORBEAM AT FS572.00 PER SRM, AND DWGS.
- [SDR SWIA2020081251780](https://openairdocs.org/sdr/SWIA2020081251780.md): Splice · corroded · Jul 30, 2020 · N740EV · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION ON RBL9 SPLICE AT FS 686 IB AND OB TOP SPLICE. REPLACED IB & OB TOP SPLICE AT RBL9 FLOORBEAM, FS686 PER SRM, BOMBARDIER DWG AND BOMBARDIER DWG. COMPLIED WITH SKYWEST TASKCARD
- [SDR SWIA2020081251779](https://openairdocs.org/sdr/SWIA2020081251779.md): Splice · corroded · Jul 30, 2020 · N740EV · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION FOUND ON OB TOP SPLICE FOR RBL9 AT FS572.00. REPLACED OB TOP SPLICE FOR RBL9 FS572.00 IAW SRM, AND DWGS.
- [SDR SWIA2020081251778](https://openairdocs.org/sdr/SWIA2020081251778.md): Stringer · corroded · Jul 25, 2020 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 22R FS333-FS349 HAD CORROSION. REMOVED AND INSTALLED NEW STRINGER 22R FROM FS 319.00 TO FS 349.00 REF. CRJ 700 SRM. AND DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.
- [SDR SWIA2020081251777](https://openairdocs.org/sdr/SWIA2020081251777.md): Frame Angle · cracked · Jul 23, 2020 · N740EV · Cndair CL6002C10 · Fuselage Main, Structure
  > CLIP CRACKED COMMON TO FS333 FRAME AND WATER DRAIN MAST CHANNEL STGR 25R-24R. REMOVED CRACKED AND INSTALLED NEW CLIP REF. DWG AND SRM.
- [SDR SWIA2020081251776](https://openairdocs.org/sdr/SWIA2020081251776.md): Stringer · corroded · Jul 23, 2020 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 22R BETWEEN F.S. 319 AND F.S. 333 HAS EVIDENCE OF CORROSION (C-CHECK) RO 8/10/2020 REMOVED AND INSTALLED NEW STRINGER AT STGR 22R AT FS 315 TO 349 REF. CRJ 700 SRM AND DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.
- [SDR SWIA2020081251774](https://openairdocs.org/sdr/SWIA2020081251774.md): Stringer · corroded · Jul 16, 2020 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 21R BETWEEN FS349 AND FS364 HAS CORROSION. (C-CHECK) RO 8/10/2020 REMOVED AND REPLACED STRINGER 21R BETWEEN FS333.00 AND 379.00. REF BOMBARDIER DWG AND CRJ700 SRM. LEAK CHECK GOOD. COMPLIED WITH TASK CARD.
- [SDR SWIA2020081251798](https://openairdocs.org/sdr/SWIA2020081251798.md): Nut · corroded · Jul 9, 2020 · N740EV · Cndair CL6002C10 · Trailing Edge Flaps
  > RH OB FLAPS HINGE ARM SUB ASSY AT W.S. 264.0 HAS A CORRODED NUT ON THE LWR ATTACH BOLT. REMOVED AND REPLACED RH OB FLAPS HINGE ARM SUB ASSY AT W.S. 264.00 LWR ATTACH BOLT NUT AND WASHER P/N MS17826-8 AND P/N NAS1149D0863K REF AMM TASK
- [SDR SWIA2020081251797](https://openairdocs.org/sdr/SWIA2020081251797.md): Clamp · corroded · Jul 9, 2020 · N740EV · Cndair CL6002C10 · Trailing Edge Flaps
  > RH OB FLAPS MOST OB SKEW DETECTOR HARNESS HAS CORRODED CLAMP HARDWARE. REMOVED AND REPLACED RH OB FLAPS MOST OB SKEW DETECTOR HARNESS CLAMP HARDWARE (SCREW P/N NAS1801-3-7 AND WASHER P/N NAS1149D0332J) REF CRJ 700 AMM TASK.
- [SDR SWIA2020081251796](https://openairdocs.org/sdr/SWIA2020081251796.md): Bolt · corroded · Jul 9, 2020 · N740EV · Cndair CL6002C10 · Trailing Edge Flaps
  > THE FWD 2 MOUNT BOLTS OF THE LH OB FLAP'S OB HINGE BOX ARE CORRODED. REPLACED THE 2EA FWD MOUNT BOLTS OF THE LH OB FLAPS OB HINGE BOX. REF CRJ700 AMM. OPS TEST GOOD. COMPLIED WITH TASK CARD.
- [SDR SWIA2020081251795](https://openairdocs.org/sdr/SWIA2020081251795.md): Bolt · corroded · Jul 9, 2020 · N740EV · Cndair CL6002C10 · Trailing Edge Flaps
  > THE FWD 2 MOUNT BOLTS OF THE RH OB FLAP'S OB HINGE BOX ARE CORRODED. REPLACED THE FWD 2EA MOUNT BOLTS OF THE RH OB FLAPS HINGE BOX. REF AMM. OPS TEST GOOD. COMPLIED WITH TASK CARD.
- [SDR SWIA2020081251773](https://openairdocs.org/sdr/SWIA2020081251773.md): Floor Support · corroded · Jul 8, 2020 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR BEAM TOP SURFACE AT RBL9 BETWEEN FS.572.00 AND FS.686.00 HAS CORROSION AND GOUGING. (C-CHECK) RO 8/10/2020 CORROSION AND DAMAGE REMOVAL NOT ALLOWED FS477 TO FS685 FLOOR SUPPORT STRUCTURE, REFERENCE CRJ700 SRM. REMOVED AND REPLACED RBL9 FLOOR BEAM WI
- [SDR SWIA2020081251772](https://openairdocs.org/sdr/SWIA2020081251772.md): Floor Support · corroded · Jul 8, 2020 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR BEAM TOP SURFACE AT LBL9 BETWEEN FS.572.00 AND FS.686.00 HAS CORROSION AND GOUGING (C-CHECK) RO 8/10/2020 BLENDED CORROSION AND GOUGING FROM FLOOR BEAM TOP CAP AT LBL 9 BETWEEN FS572 - FS686 REF CRJ 700 SRM. EVALUATED AND FOUND NO DAMAGE IS ALLOWED

Next page: https://openairdocs.org/aircraft/N740EV/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 = 'N740EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N740EV/reports

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