# Service difficulty reports: N719EV A list on [N719EV](https://openairdocs.org/aircraft/N719EV.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 · 269 reports - [SDR SWIA2025092400022](https://openairdocs.org/sdr/SWIA2025092400022.md): A/C Pack · odor · Sep 22, 2025 · N719EV · Cndair CL6002C11 · Cabin Cooling System > ERRONEOUS TEMPERATURE READINGS ON ESC PAGE ON AIR DUCT FROM PACKS, UNABLE TO MAKE TEMPERATURE ADJUSTMENTS, STRANGE ALMOST BURNING SMELL THROUGHOUT FLIGHT DECK AND PASSENGER CABIN (FLIGHT 4294) DEFERRED BOTH PACK TEMP AUTO MODE PER CRJ 550 MEL 21-61-1C. VE - [SDR SWIA2025092300022](https://openairdocs.org/sdr/SWIA2025092300022.md): Acm · odor · Sep 22, 2025 · N719EV · Cndair CL6002C11 · Cabin Cooling System > ERRONEOUS TEMPERATURE READINGS ON ESC PAGE ON AIR DUCT FROM PACKS, UNABLE TO MAKE TEMPERATURE ADJUSTMENTS, STRANGE ALMOST BURNING SMELL THROUGHOUT FLIGHT DECK AND PASSENGER CABIN. MEL 21-61-1CCAT: C DUE: 2OCT25. ERRONEOUS TEMPERATURE READINGS ON ESC PAGE ON - [SDR SWI2025F00651](https://openairdocs.org/sdr/SWI2025F00651.md): Warning Message · illuminated · May 21, 2025 · N719EV · Cndair CL6002C11 · Airfoil Anti/De-ice System > ANTI-ICE DUCT, L WING A/I AND R WING A/I CAUTION MESSAGES CLEARED WITH QRH. VERY LIGHT SMOKE IN CABIN DURING TAXI IN. (FLIGHT 4305 - FILED CLOSED)SEE EAML 1610159 FOR TROUBLESHOOTING THE CABIN SMOKE TO THE L PACK FAILURE, AND EAML 1610161 AND 1610171 FOR TROU - [SDR SWI2025F00640](https://openairdocs.org/sdr/SWI2025F00640.md): Actuator · faulted · May 13, 2025 · N719EV · Cndair CL6002C11 · Elevator Tab Control System > PITCH FEEL CAUTION MESSAGE DURING CLIMB. (FLIGHT 4229 - FILED CLOSED)INSPECTED MDC AND FOUND B1# 007978 PITCH FEEL ACT2/MOTOR. TROUBLESHOT PER FIM 27-31-23. REMOVED AND REPLACED #2(RIGHT SIDE) LINEAR PITCH FEEL ACTUATOR IN REF TO AMM 27-31-23. OPS CHECK GOOD F - [SDR SWIA20240808614](https://openairdocs.org/sdr/SWIA20240808614.md): Structure · corroded · Jun 14, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Structure > INTERNAL STRUCTURE AT FS893.0 ON AFT SIDE BETWEEN STGR 27 AND STGR26R HAVE SUPECTED CORROSION AS MARKED (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED REPAIRED FS 893 ON AFT SIDE BETWEEN STGR27 AND STRG26R REF REO 670-53-51-287 REV. -- DATED 2024-06-27. CO - [SDR SWIA20240808604](https://openairdocs.org/sdr/SWIA20240808604.md): Stringer · corroded · Jun 4, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > STRINGER 20L BETWEEN FRAMES FS 421.00 AND FS 379.00 IS CORRODED. (C-CHECK RO 8/4/2024) REPAIRED STRINGER 20L BETWEEN FRAMES FS 421 AND FS 379.00 REF CRJ700 SRM TASK 53-00-03-201-001-A01 AND MHI RJ REO 670-53-21-2408 REV. -- DATED 2024-06-07 DWG# SH670-3 - [SDR SWIA2024F00619](https://openairdocs.org/sdr/SWIA2024F00619.md): Floor Panel · dented · May 30, 2024 · N719EV · Cndair CL6002C10 · Fuselage Floor Panel > DENTS (4EA) NOTED ON R/H COCKPIT FLOOR PANEL AT APPROX. FS262 AND RBL16 AND FS249 BETWEEN RBL13-RBL19 (MARKED) (C-CHECK RO 8/4/2024) COMPLIED WITH CUTOUT AND INSTALLED DOUBLER TO DENTS ON RH COCKPIT FLOOR REF REO 670-53-11-1976 REV -- 2024-06-25 & REO 6 - [SDR SWIA20240808530](https://openairdocs.org/sdr/SWIA20240808530.md): Floor Panel · dented · May 30, 2024 · N719EV · Cndair CL6002C10 · Fuselage Floor Panel > DENT NOTED AT L/H COCKPIT FLOOR PANEL AT APPROX. FS257 AND LBL18 (MARKED) (C-CHECK RO 8/4/2024) REWORKED ON DENT AT L/H COCKPIT FLOOR PANEL AT APPROX. FS257 AND LBL18 AND COMPLIED TO ALL THE STEPS GIVEN ON REF REO 670-53-11-1975 REV -- DATE: 2024-06-14 - [SDR SWIA20240808529](https://openairdocs.org/sdr/SWIA20240808529.md): Cleat · corroded · May 29, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings > BRACKET ( CLEAT) AT APPROX. FS 295.00 AND STGR 20L IS CORRODED. CAMP 28305038. (C-CHECK RO 8/4/2024) REPLACED STRINGER CLEAT 20L AT FS295 REF CRJ700 SRM 51-42-06 -001-001-A01 AND DRAWING SH670-31550 REV G. COMPLIED WITH SKY CARD 51-900-1002-SKY STRUC - [SDR SWIA2024F00639](https://openairdocs.org/sdr/SWIA2024F00639.md): Door Sill · corroded · May 28, 2024 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure > PASSENGER DOOR FLOOR SILL AT STGR17L BETWEEN FS310.00 AND FS349.00 HAS MULTIPLE SPOTS OF CORROSION AS MARKED (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR LOWER SILL (KICKPLATE) PN SH670-31875-7 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH6 - [SDR SWIA2024F00638](https://openairdocs.org/sdr/SWIA2024F00638.md): Plate · corroded · May 28, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin > AFT ATG ANTENNA RETAINING PLATE ASSY HAS CORROSION ROUND FWD COAX CABLE HOLE (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW AFT ATG ANTENNA DOUBLER PN P16492 REF. CRJ700 SRM 51-42-20-001-001-A01 AND GOGO DRAWING P13112-20110 REV H DATED 5/04/2011. COM - [SDR SWIA2024F00644](https://openairdocs.org/sdr/SWIA2024F00644.md): Floor Support · corroded · May 26, 2024 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure > PASSENGER DOOR BELOW FLOOR STRUCTURE BETWEEN FS333.00 AND FS349.00 AT STGR21L CORRODED AS MARKED (C-CHECK RO 8/4/2024) REPLACED CORRODED BACKUP SILL AT STR 21L BETWEEN FS333 - FS349 WITH NEW PN SH670-31823-1 REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG - [SDR SWIA20240808526](https://openairdocs.org/sdr/SWIA20240808526.md): Frame · corroded · May 26, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Frame > CORROSION ON FRAME FRONT FACE AND AFT FACE AT FS295.00 STGR20L AS MARKED (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW LOWER FRAME SECTOR FS295 BETWEEN STR 20L -STR25R REF CRJ-700 SRM 51-42-21-001-001-A01 AND SRM 53-00-06-201-006-A01. COMPLIED WITH 51 - [SDR SWIA2024F00637](https://openairdocs.org/sdr/SWIA2024F00637.md): Stringer · corroded · May 25, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > EVIDENCE OF CORROSION ON STGR26R BETWEEN FS295.00 AND FS310.00 AS MARKED (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW STRG 26R BETWEEN FS 280 TO FS 333 REF CRJ-700-SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV K. COMP - [SDR SWIA2024F00636](https://openairdocs.org/sdr/SWIA2024F00636.md): Skin · gouged · May 25, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Frame > MULTIPLE SPOTS OF CORROSION AND GOUGES NOTED AT FWD CARGO LOWER CLOSE SKIN (THRESHOLD) BETWEEN FS533-FS581 (MARKED)REPAIRED FWD CARGO LOWER CLOSE SKIN (THRESHOLD) BETWEEN FS533-FS581 REF REO 670-53-31-890 REV -- DATED 2024-07-04. COMPLIED WITH 51-900-1002-SKY - [SDR SWIA2024F00635](https://openairdocs.org/sdr/SWIA2024F00635.md): Tie Down · corroded · May 25, 2024 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > CORROSION NOTED AT FWD CARGO TIE DOWN SUPPORT PLATE COMMON TO FRAME 533 BETWEEN STRG 22L-23L (MARKED) (C-CHECK RO 8/4/2024) REMOVED CORRODED FWD CARGO TIE DOWN SUPPORT PLATE AND INSTALLED 1EA NEW TIE DOWN SUPPORT PLATE PN: SH670-33390-1. REF CRJ700 SRM - [SDR SWIA2024F00634](https://openairdocs.org/sdr/SWIA2024F00634.md): Frame · corroded · May 25, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Frame > CORROSION NOTED ON FRAME 549 BETWEEN STRG25L-26L (MARKED) (C-CHECK RO 8/4/2024) REPAIRED FS.549 LOWER SECTOR FRAME BETWEEN STR 26L & STR 27 REF REO 670-53-31-882 REV -- DATED 2024-07-02. COMPLIED WITH 51-900-1002-SKY AND PRESSURE CHECK GOOD. SEE CONTI - [SDR SWIA2024F00633](https://openairdocs.org/sdr/SWIA2024F00633.md): Frame · corroded · May 25, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Frame > EVIDENCE OF CORROSION AT FS310.00 BETWEEN STGR26L AND STGR26R (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW LOWER FRAME SECTOR FS310 BETWEEN STR 25R - STR 25L AND 2EA FRAME SPLICES AND 2EA STRINGER CLEATS REF CRJ-700 SRM 53-00-06-201-006-A01. COMPLI - [SDR SWIA2024F00632](https://openairdocs.org/sdr/SWIA2024F00632.md): Tie Down · corroded · May 25, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Structure > CORROSION NOTED AT FWD CARGO TIE DOWN SUPPORT PLATE COMMON TO FRAME 581 BETWEEN STRG 22L-23L (MARKED) (C-CHECK RO 8/4/2024) REMOVED OUT OF LIMIT DISCREPANT TIE DOWN PLATE AND INSTALLED NEW REPLACEMENT TIE DOWN PLATE WITH NEW FASTENERS AT FS.581 FRAME BE - [SDR SWIA2024F00631](https://openairdocs.org/sdr/SWIA2024F00631.md): Tie Down · corroded · May 25, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Structure > CORROSION NOTED AT FWD CARGO TIE DOWN SUPPORT PLATE COMMON TO FRAME 581 BETWEEN STRG 27-26L (MARKED) (C-CHECK RO 8/4/2024) REPLACED FWD CARGO TIE DOWN SUPPORT PLATE COMMON TO FRAME 581 BETWEEN STRG 27-26L CRJ700 SRM TASK 51-23-00-001-001-A01, SRM TASK 5 - [SDR SWIA2024F00630](https://openairdocs.org/sdr/SWIA2024F00630.md): Stringer · corroded · May 25, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > EVIDENCE OF CORROSION ON STGR26L BETWEEN FS295.00 AND FS310.00 AS MARKED (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW STRG 26L BETWEEN FS 280 TO FS 333 REF CRJ-700-SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV K. COMPLIE - [SDR SWIA20240808525](https://openairdocs.org/sdr/SWIA20240808525.md): Intercostal · chafed · May 25, 2024 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure > IN THE AEB, INTERCOSTAL AT STGR9R BETWEEN FS1144.00 - FS1162.00 IS CHAFFED (C-CHECK RO 8/4/2024) REPLACED INTERCOSTAL PN: AF670-36540-002 BETWEEN FS1144 AND FS1162 AT STGR 9R PER CRJ700 SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01 AND DWG # MM670- - [SDR SWIA2024F00647](https://openairdocs.org/sdr/SWIA2024F00647.md): Floorbeam · corroded · May 24, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Floor Beam > MULTIPLE SPOTS OF CORROSION NOTED ON L/H FLOOR BEAM CAP AT LBL 9 AT APPROX. FS572-FS685 (MARKED) (C-CHECK RO 8/4/2024) REPAIRED L/H FLOOR BEAM CAP AT LBL 9 AT APPROX. FS572-FS685 REF REO 670-53-31-901 REV --DATED 2024-07-02 AND CRJ-700-SRM 53-00-41-201- - [SDR SWIA2024F00646](https://openairdocs.org/sdr/SWIA2024F00646.md): Floorbeam · corroded · May 24, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Floor Beam > MULTIPLE SPOTS OF CORROSION NOTED ON R/H FLOOR BEAM CAP AT RBL 9 AT APPROX. FS477-FS572 (MARKED) (C-CHECK RO 8/4/2024) CLEANED REF CRJ-700 SRM 51-26-00-001-001-A01 AND FOUND NO CORROSION ON RH FLOOR BEAM CAP AT RBL9 FS477 - FS527. REPAIRED RBL 9.0 FLOO - [SDR SWIA2024F00645](https://openairdocs.org/sdr/SWIA2024F00645.md): Structure · corroded · May 24, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Structure > SUSPECTED CORROSION ON CIRCUMFERENTIAL JOINT BETWEEN FS969.00 TO FS985.00 NEXT TO STGR26R AS MARKED (C-CHECK RO 8/4/2024) REPAIRED LOWER SKIN SPLICE STRAP AT FS 977 BETWEEN STR 25R AND STR26R REF REO 670-53-00-729 REV. -- DATED 2024-06-07. COMPLIED WITH - [SDR SWIA2024F00609](https://openairdocs.org/sdr/SWIA2024F00609.md): Window Post · cracked · May 23, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Structure > CRACK NOTED ON L/H WINDSHIELD SIDE POST (MARKED) (C-CHECK RO 8/4/2024) REMOVED AND REPLACED LH WINDSHIELD SIDE POST. REF. CJ700 SRM 51-42-21-001-001-A01 REV. 38 ISSUED 07/25/2020 AND DWG# CC670-33055 REV. -F. LEAK CHECK GOOD WITH NO LEAKS NOTED. SEE CO - [SDR SWIA20240808523](https://openairdocs.org/sdr/SWIA20240808523.md): Post · cracked · May 23, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Structure > CRACK NOTED ON R/H WINDSHIELD SIDE POST (MARKED) (C-CHECK RO 8/4/2024) REMOVED AND REPLACED RH WINDSHIELD SIDE POSTE. REF. CRJ700 SRM 51-42-21-001-001-A01 AND DWG# CC670-33055 REV. -F.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY AND PRESSURE CHECK GO - [SDR SWIA2024F00618](https://openairdocs.org/sdr/SWIA2024F00618.md): Former · corroded · May 21, 2024 · N719EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR FORMER, FS329.41, DD5 AND DD6 HAS INTERGRANULAR CORROSION (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR FORMER, FS329.41, DD5 AND DD6. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH 51-900-1002-SKY - [SDR SWIA20240808521](https://openairdocs.org/sdr/SWIA20240808521.md): Intercostal · corroded · May 21, 2024 · N719EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD7 FS311.75 - FS320.00 HAS INTERGRANULAR CORROSION (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD7 FS311.75 - FS320.00. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH 51-9 - [SDR SWIA2024F00648](https://openairdocs.org/sdr/SWIA2024F00648.md): Frame · corroded · May 20, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Frame > CORROSION FOUND ON FRAME FS349 BETWEEN STGR 26L AND 26R (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW LOWER FRAME AT FS349 FROM STR 23L TO STR24R REF CRJ-700-SRM 51-42-06-001-001-A01. CRJ-700-SRM 51-42-21-001-001-A01 AND DRAWING SH670-31357 REV B. COM - [SDR SWIA20240808520](https://openairdocs.org/sdr/SWIA20240808520.md): Frame · corroded · May 20, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Frame > CORROSION FOUND ON FRAME FS364 BETWEEN STGR 26L AND 26R (HN00161937) (C-CHECK RO 8/4/2024) REPAIRED FRAME FS364 BETWEEN STGR 26L AND 26R REF CRJ-700 SRM 53-21-23-201-008-A01, CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700-SRM 51-42-21-001-001-A01, AND DWG: S - [SDR SWIA2024F00629](https://openairdocs.org/sdr/SWIA2024F00629.md): Intercostal · corroded · May 19, 2024 · N719EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD3 FS311.75 - FS320.00 HAS INTERGRANULAR CORROSION (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD3 FS311.75 - FS320.00. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH 51-9 - [SDR SWIA2024F00628](https://openairdocs.org/sdr/SWIA2024F00628.md): Intercostal · corroded · May 19, 2024 · N719EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD5 FS338.00 - FS347.25 HAS INTERGRANULAR CORROSION (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD5 FS338.00 - FS347.25. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPILED WITH 51-90 - [SDR SWIA2024F00627](https://openairdocs.org/sdr/SWIA2024F00627.md): Door Frame · corroded · May 19, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Structure > PAX DOOR FORMER FS347.25 IS CRACKED @ FASTENER HOLES FOR PULLEY BRACKET AND HAS INTERGRANULAR CORROSION (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR AFT FORMER FS347.25. REF:CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 - [SDR SWIA2024F00626](https://openairdocs.org/sdr/SWIA2024F00626.md): Intercostal · corroded · May 19, 2024 · N719EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD2 FS338.00 - FS347.25 HAS INTERGRANULAR CORROSION (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD2 FS338.00 - FS347.25. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH 51-90 - [SDR SWIA2024F00625](https://openairdocs.org/sdr/SWIA2024F00625.md): Door Frame · corroded · May 19, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Structure > PAX DOOR FRAME, FS313.56, DD4 AND DD5 HAS INTERGRANULAR CORROSION (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR FRAME, FS313.56, DD4 AND DD5. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N COMPLIED WITH 51-900-1002-SKY AND - [SDR SWIA2024F00624](https://openairdocs.org/sdr/SWIA2024F00624.md): Cleat · corroded · May 19, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Structure > 1 EA CLEAT @ PAX DOOR FRAME, FS313.56 AND DD4 HAS INTERGRANULAR CORROSION (C-CHECK RO 8/4/2024) REMOVED AND REPLACED 1 EA CLEAT @ PAX DOOR FRAME, FS313.56 AND DD4. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH 51-900-1 - [SDR SWIA2024F00623](https://openairdocs.org/sdr/SWIA2024F00623.md): Intercostal · cracked · May 19, 2024 · N719EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD1 FS338.00 - FS347.25 IS CRACKED (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD1 FS338.00 - FS347.25. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH 51-900-1002-SKY AND PR - [SDR SWIA2024F00622](https://openairdocs.org/sdr/SWIA2024F00622.md): Intercostal · corroded · May 19, 2024 · N719EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD6 FS320.00 - FS338.00 HAS INTERGRANULAR CORROSION (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD6 FS320.00 - FS338.00. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWING 6 - [SDR SWIA2024F00621](https://openairdocs.org/sdr/SWIA2024F00621.md): Intercostal · corroded · May 19, 2024 · N719EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD1A FS338.00 - FS347.25 HAS INTERGRANULAR CORROSION (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD1A FS338.00 - FS347.25. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH 51- - [SDR SWIA2024F00620](https://openairdocs.org/sdr/SWIA2024F00620.md): Intercostal · corroded · May 19, 2024 · N719EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD1 FS323.00 - FS335.00 HAS INTERGRANULAR CORROSION (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD1 FS323.00 - FS335.00. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWING 6 - [SDR SWIA20240808519](https://openairdocs.org/sdr/SWIA20240808519.md): Intercostal · corroded · May 19, 2024 · N719EV · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR INTERCOSTAL DD4 FS311.75 - FS320.00 HAS INTERGRANULAR CORROSION (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD4 FS311.75 - FS320.00. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH 51-9 - [SDR SWIA2024F00653](https://openairdocs.org/sdr/SWIA2024F00653.md): Seat Track · corroded · May 16, 2024 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > MULTIPLE SPOTS OF CORROSION NOTED ON L/H SIDE SEAT RAIL AT APPROX.FS946-FS969 (MARKED) (C-CHECK RO 8/4/2024) REMOVED CORROSION FROM L/H SIDE SEAT RAIL AT APPROX. FS946-FS969 REF CRJ700 SRM 51-12-00-001-001-A01. DAMAGE WAS FOUND TO BE OUT OF LIMITS. INS - [SDR SWIA2024F00652](https://openairdocs.org/sdr/SWIA2024F00652.md): Seat Track · corroded · May 16, 2024 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > MULTIPLE SPOTS OF CORROSION NOTED ON L/H SIDE SEAT RAIL AT APPROX. FS785-FS797 (MARKED) (C-CHECK RO 8/4/2024) REMOVED CORROSION ON MULTIPLES SPOTS AT L/H SIDE SEAT RAIL AT APPROX. FS785-FS797. REF. CRJ-700 SRM 51-21-06-001-001-A01. DAMAGE FOUND TO BE OU - [SDR SWIA2024F00651](https://openairdocs.org/sdr/SWIA2024F00651.md): Seat Track · corroded · May 16, 2024 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > MULTIPLE SPOTS OF CORROSION NOTED ON R/H SIDE SEAT RAIL ASSY. BETWEEN FS572.00-FS675.00 (MARKED) (C-CHECK RO 8/4/2024) REMOVED CORROSION ON R/H SIDE SEAT RAIL ASSY. BETWEEN FS572.00-FS675.00 REF CRJ700 SRM 51-21-06-001-001-A01. DAMAGE WAS EVALUATED AND - [SDR SWIA2024F00650](https://openairdocs.org/sdr/SWIA2024F00650.md): Seat Track · corroded · May 16, 2024 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > L/H SIDE SEAT RAIL AT FS674-FS713 EXFOLIATED (MARKED) (C-CHECK RO 8/4/2024) REPLACED LH SIDE SEAT RAIL AT APPROX FS674 - FS713 REF CRJ-700 AMM 53-00-49-400-801-A17 - [SDR SWIA2024F00649](https://openairdocs.org/sdr/SWIA2024F00649.md): Seat Track · corroded · May 16, 2024 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > MULTIPLE SPOTS OF CORROSION NOTED ON R/H SIDE SEAT RAIL ASSY. BETWEEN FS483.00-FS572.00 (MARKED) (C-CHECK RO 8/4/2024) REPLACED RH SIDE SEAT RAIL AT APPROX FS483 - FS572 REF CRJ-700 AMM 53-00-49-400-801-A17 - [SDR SWIA2024F00657](https://openairdocs.org/sdr/SWIA2024F00657.md): Seat Track · corroded · May 16, 2024 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > MULTIPLE SPOTS OF CORROSION NOTED ON L/H SIDE SEAT RAIL BETWEEN FS713-FS761 (MARKED) (C-CHECK RO 8/4/2024) REPLACED THE LH SIDE SEAT RAIL BETWEEN APPROX FS713 - FS761 REF CRJ-700 AMM 53-00-49-400-801-A17 - [SDR SWIA2024F00656](https://openairdocs.org/sdr/SWIA2024F00656.md): Seat Track · corroded · May 16, 2024 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > MULTIPLE SPOTS OF CORROSION NOTED ON L/H SIDE SEAT RAIL AT APPROX. FS854-FS868 (MARKED) (C-CHECK RO 8/4/2024) L/H SIDE SEAT RAIL AT APPROX. FS854-FS868 HAD MORE THAN ONE TYPE OF DAMAGE AT THE SAME CROSS SECTION IN MULTIPLE AREAS. INSTALLED NEW L/H SIDE - [SDR SWIA2024F00655](https://openairdocs.org/sdr/SWIA2024F00655.md): Seat Track · corroded · May 16, 2024 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > MULTIPLE SPOTS OF CORROSION NOTED ON R/H SIDE SEAT RAIL AT APPROX.. FS713.00-FS761.00 (MARKED), MX#28245828 (C-CHECK RO 8/4/2024) REPLACED RH SIDE SEAT RAIL AT APPROX FS713 - FS761 REF CRJ-700 AMM 53-00-49-400-801-A01 Next page: https://openairdocs.org/aircraft/N719EV/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 = 'N719EV' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N719EV/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.