# Service difficulty reports: N912EV A list on [N912EV](https://openairdocs.org/aircraft/N912EV.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 · 188 reports - [SDR SWIA2026031777080](https://openairdocs.org/sdr/SWIA2026031777080.md): Pressure Web · cracked · Mar 17, 2026 · N912EV · Cndair CL6002B19 · Fuselage Main, Structure > INSIDE THE AIRCRAFT CABIN AT APPROX FS. 461.00 PRESSURE BOX SKIN SURFACE BETWEEN RBL9 AND LBL 9 SHOWS SIGNS OF CRACKS (2 CRACKS) (C-CHECK RO 08/31/2026)REPAIRED TO PRESSURE FLOOR WEB AT FS 461.00 BETWEEN LBL 9 AND RBL 9 IAW CRJ200 MHIRJ REO 601R-53-41-3419 R - [SDR SWIA2026020677086](https://openairdocs.org/sdr/SWIA2026020677086.md): Stringer · damaged · Feb 6, 2026 · N912EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer > STRINGER 26R FOUND TO HAVE DAMAGE FROM AFT NLG DOOR HINGE PIN. REPAIRED STRINGER 26R AT FS 231.50 BELLOW HINGE ATTACHMENT FITTING IAW REO 601R-53-11-4059 REV. -- DATE 2026-03-12. ANALYSIS TO DETERMINE ADDITIONAL REQUIREMENTS WILL BE COMPLETED WITHIN 12 MON - [SDR SWIA2026012177085](https://openairdocs.org/sdr/SWIA2026012177085.md): Stringer · out of limits · Jan 21, 2026 · N912EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer > STRINGER 20R BETWEEN FS319.00 TO FS349.00 HAS A PREVIOUS UNAPPROVED REPAIR ACCOMPLISHED AT AFT END (C-CHECK RO 08/31/2026)REPAIRED STGR 20R BETWEEN FS 319.70 AND FS 349.00 IAW CRJ200 MHIRJ REO 601R-53-21-3823 REV. -- DATE 2026-07-14 SRM 51-42-21, SRM 51-42-0 - [SDR SWIA2026011977097](https://openairdocs.org/sdr/SWIA2026011977097.md): Frame · corroded · Jan 19, 2026 · N912EV · Cndair CL6002B19 · Fuselage Main, Frame > CORROSION AT BS 364, APPROX STR 25R. REMOVED AND REPLACED FRAME SECTION ON BS 364, STR 25R, IAW SRM 51-42-21, SRM 51-42-06, SRM 51-42-34, SRM 51-42-13,SRM 51-42-02,SRM 51-21-06, SRM 51-40-11, SRM 51-25-01,SRM 53-00-00, AMM 31-41-05, AMM 31-41-04, AMM 53-01- - [SDR SWIA2026011477083](https://openairdocs.org/sdr/SWIA2026011477083.md): Floorbeam · cracked · Jan 14, 2026 · N912EV · Cndair CL6002B19 · Fuselage Main, Floor Beam > INSIDE CABIN RIGHT HAND SIDE F.S. 559.00 RBL18 TEE CAP CRACKED (C-CHECK RO 08/31/2026)REPAIRED TCAP AT FS 559.00 RBL18 IAW REO 601R-53-41-3384, REV --, DATE 2026-01-23. RESTORED SURFACE FINISH IAW CRJ200 SRM 51-25-16. - [SDR SWIA2026011277094](https://openairdocs.org/sdr/SWIA2026011277094.md): Skin · gouged · Jan 12, 2026 · N912EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin > SKIN GOUGED ON INTERNAL SIDE AT BS 668, STR 22L - 23L. REPAIRED SKIN ON LT SIDE OF AFT FUSELAGE AT BS 668 AND BTWN STR 22L & 23L IAW SRM 53-00-31, REPAIR 3. - [SDR SWIA2026010777098](https://openairdocs.org/sdr/SWIA2026010777098.md): Frame · corroded · Jan 7, 2026 · N912EV · Cndair CL6002B19 · Fuselage Main, Frame > CORROSION ON FRAME AT BS 333, STR 25R, OTBD AND AFT OF BOTTOM AFT OXYGEN BOTTLE MOUNT. REMOVED AND REPLACED FRAME SECTION AT BS 333, STR 25R IAW SRM 53-00-00, SRM 51-21-06, SRM 51-42-06, SRM 51-42-21, SRM 51-40-11, SRM 51-25-06, SRM 51-21-11, SRM 51-25-16, AM - [SDR SWIA2026010777096](https://openairdocs.org/sdr/SWIA2026010777096.md): Floor Support · corroded · Jan 7, 2026 · N912EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > INSIDE THE AIRCRAFT CABIN RT SIDE BS 550 (APPROX) PRESSURE FLOOR SILL SHOW SIGNS OF CORROSION. REMOVED CORROSION INSIDE THE AIRCRAFT CABIN RIGHT SIDE BS 550 (APPROX) PRESSURE FLOOR SILL IAW SRM 51-21-06. MEASURED AREA ORIGINAL THICKNESS IS 0.080" AND MINIMUM - [SDR SWIA2026010777095](https://openairdocs.org/sdr/SWIA2026010777095.md): Frame · corroded · Jan 7, 2026 · N912EV · Cndair CL6002B19 · Fuselage Main, Frame > FRAME AT BS 394, APPROX STR 23L, CORRODED. REMOVED AND REPLACED FRAME SECTION BS 394 BTWN STR 23L - 15L IAW SRM 51-42-06 AND SRM 51-42-21 REF: SRM 53-00-00, SRM 51-21-06, SRM 51-42-34, SRM 51-40-11, SRM 51-41-02, SRM 51-26-00, SRM 51-25-01, ESPM 20-12-00, AMM - [SDR SWIA2026010777093](https://openairdocs.org/sdr/SWIA2026010777093.md): Skin · corroded · Jan 7, 2026 · N912EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > INSIDE AIRCRAFT CABIN RIGHT SIDE BS 464 - 449 (APPROX) PRESSURE FLOOR SILL SHOW SIGNS OF CORROSION IN MULTIPLE AREAS. REMOVED CORROSION INSIDE THE AIRCRAFT CABIN RIGHT SIDE BS 464 - 449 (APPROX) PRESSURE FLOOR SILL IAW SRM 51-21-06. MEASURED AREA ON RT PRESS - [SDR SWIA2026010777091](https://openairdocs.org/sdr/SWIA2026010777091.md): Floor Support · corroded · Jan 7, 2026 · N912EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > INSIDE AIRCRAFT CABIN LT SIDE BS 409+128 - 428 (APPROX) PRESSURE FLOOR SILL SHOWS SIGN OF CORROSION IN MULTIPLE AREAS. REMOVED CORROSION INSIDE THE AIRCRAFT CABIN LT SIDE BS 409+128 - 428 (APPROX) PRESSURE FLOOR SILL IAW SRM 51-21-06. MEASURED AREA ON PRESS - [SDR SWIA2026010777090](https://openairdocs.org/sdr/SWIA2026010777090.md): Floor Support · corroded · Jan 7, 2026 · N912EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > INSIDE AIRCRAFT CABIN RT SIDE FROM BS 529 - 513 (APPROX) PRESSURE FLOOR SILL SHOW SIGNS OF CORROSION IN MULTIPLE AREAS. REMOVED CORROSION INSIDE AIRCRAFT CABIN RT SIDE FROM BS 529 - 513 (APPROX) PRESSURE FLOOR SILL IAW SRM 51-21-06. MEASURED AREA ON RT PRESS - [SDR SWIA2026010777088](https://openairdocs.org/sdr/SWIA2026010777088.md): Floor Support · corroded · Jan 7, 2026 · N912EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > INSIDE THE AIRCRAFT CABIN LT SIDE BS 478 - 492 (APPROX) PRESSURE FLOOR SILL SHOWS SIGNS OF CORROSION IN MULTIPLE AREAS. REMOVED CORROSION FROM CABIN LT SIDE PRESSURE FLOOR SILL AT BS 478 - 492 (APPROX) IAW SRM 51-21-06. MEASURED AREA ON PRESSURE FLOOR SILL - [SDR SWIA2026010777087](https://openairdocs.org/sdr/SWIA2026010777087.md): Floor Support · corroded · Jan 7, 2026 · N912EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > INSIDE THE AIRCRAFT CABIN LT SIDE FROM BS 459 - 468 (APPROX) PRESSURE FLOOR SILL SHOWS SIGNS OF CORROSION IN MULTIPLE AREAS. REMOVED CORROSION FROM CABIN LT PRESSURE FLOOR SILL AT BS 459 - 468 IAW SRM 51-21-06. MEASURED AREA ON BS 455 - 468.00. ORIGINAL IS 0. - [SDR SWIA2026010777084](https://openairdocs.org/sdr/SWIA2026010777084.md): Floor Support · corroded · Jan 7, 2026 · N912EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > INSIDE THE AIRCRAFT CABIN LEFT SIDE F.S. 510.00 (APPROX) PRESSURE FLOOR SILL SHOWS SIGNS OF CORROSION (AREA MARKED WITH RED GREASE PENCIL) (C-CHECK RO 08/31/2026)REMOVED CORROSION FROM CABIN LEFT HAND SIDE PRESSURE FLOOR SILL AT F.S. 510.00 IAW CRJ200 SRM 5 - [SDR SWIA2026010777082](https://openairdocs.org/sdr/SWIA2026010777082.md): Floor Support · corroded · Jan 7, 2026 · N912EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > INSIDE THE AIRCRAFT CABIN LEFT SIDE BETWEEN F.S. 439.00 TO F.S. 449.00 (APPROX) PRESSURE FLOOR SILL SHOWING SIGNS OF CORROSION IN MULTIPLE AREAS (AREAS MARKED WITH RED GREASE PENCIL) (C-CHECK RO 08/31/2026)REMOVED CORROSION FROM CABIN LEFT HAND SIDE PRESSUR - [SDR SWIA2026010777081](https://openairdocs.org/sdr/SWIA2026010777081.md): Floor Support · corroded · Jan 7, 2026 · N912EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > INSIDE THE AIRCRAFT CABIN RIGHT HAND SIDE F.S. 424.00 (APPROX) PRESSURE FLOOR SILL SHOWS SIGNS OF CORROSION IN MULTIPLE AREAS (AREAS MARKED WITH RED GREASE PENCIL) (C-CHECK RO 08/31/2026)REMOVED CORROSION INSIDE THE AIRCRAFT CABIN RIGHT HAND SIDE F.S. 424.0 - [SDR SWIA2026010777079](https://openairdocs.org/sdr/SWIA2026010777079.md): Floor Support · corroded · Jan 7, 2026 · N912EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > INSIDE THE AIRCRAFT CABIN RIGHT HAND SIDE F.S. 473.00 (APPROX) PRESSURE FLOOR SILL SHOWS SIGNS OF CORROSION (AREA MARKED WITH RED GREASE PENCIL) (C-CHECK RO 08/31/2026)REMOVED CORROSION INSIDE THE AIRCRAFT CABIN RIGHT HAND SIDE FROM F.S 473.00 (APPROX) PRES - [SDR SWIA2026010777078](https://openairdocs.org/sdr/SWIA2026010777078.md): Floor Support · corroded · Jan 7, 2026 · N912EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > INSIDE THE AIRCRAFT CABIN RIGHT HAND SIDE FROM F.S 506.00 TO F.S. 484.00 (APPROX) PRESSURE FLOOR SILL SHOW SIGNS OF CORROSION IN MULTIPLE AREAS (AREAS MARKED WITH RED GREASE PENCIL) (C-CHECK RO 08/31/2026)REMOVED CORROSION INSIDE THE AIRCRAFT CABIN RIGHT HA - [SDR SWIA2026010777077](https://openairdocs.org/sdr/SWIA2026010777077.md): Floor Support · corroded · Jan 7, 2026 · N912EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure > INSIDE THE ACFT CABIN LEFT HAND SIDE FROM F.S. 518.00 TO F.S. 540.00 (APPROX) PRESSURE FLOOR SILL SHOWS SIGNS OF CORROSION IN MULTIPLE AREAS (AREAS MARKED WITH RED GREASE PENCIL) (C-CHECK RO 08/31/2026)REMOVED CORROSION FROM CABIN LEFT HAND SIDE PRESSURE FL - [SDR SWIA2025121977092](https://openairdocs.org/sdr/SWIA2025121977092.md): Skin · corroded · Dec 19, 2025 · N912EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin > PAINT DAMAGED AND POSSIBLE CORROSION FOUND ON SKIN FROM BS 559 - 559+80, STR 24L - 24R. REMOVED CORROSION ON BELLY SKIN FROM BS 559 - 559+80 BTWN STR 24L-24R IAW SRM 51-21-06. DAMAGE FOUND TO BE WITHIN ALLOWABLE LIMITS IAW REO 601R-53-00-930 REV--. REMOVED A - [SDR SWIA2025121877089](https://openairdocs.org/sdr/SWIA2025121877089.md): Skin · corroded · Dec 18, 2025 · N912EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin > PAINT DAMAGE WITH SIGNS OF CORROSION FOUND ON BELLY AT BS 559+80 - 574, STR 24L - 24R. REMOVED CORROSION ON BELLY SKIN AT BS 559+80 - 574, STR 24L-24R IAW SRM 51-21-06. DAMAGE FOUND TO BE WITHIN ALLOWABLE LIMITS IAW REO 601R-53-00-930 REV--. REMOVED AND REP - [SDR SWIA20250217005](https://openairdocs.org/sdr/SWIA20250217005.md): Fitting · damaged · Feb 15, 2025 · N912EV · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings > NOSE DOOR OPEN GEAR DISAGREE (FLIGHT 5442 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29648047 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CP 29651672 FOR INSPECTION OF NLG MAIN FITTING FOR DAMAGE AND REPAIR TO MAIN FITTING.REFEREN - [SDR SWIA20241218](https://openairdocs.org/sdr/SWIA20241218.md): Windshield · cracked · Dec 18, 2024 · N912EV · Cndair CL6002B19 · Flight Compartment Windows > TRANSFER FROM EAML 1494907: LEFT WINDSHIELD CRACKED AND GOT L WSHLD HEAT CAUTION IN FLIGHT. (FLIGHT 5213 - FILED CLOSED) REMOVED AND REPLACED LH WINDSHIELD IN ACCORDANCE WITH AMMM:56-11-01 AND TASK CARD:56-220-1000-SKY. OPS CHECKS AND LEAKS CHEKS GOOD A - [SDR SWI2024110859](https://openairdocs.org/sdr/SWI2024110859.md): Skin · damaged · Aug 8, 2024 · N912EV · Cndair CL6002B19 · Ailerons > LIGHTNING STRIKE FOUND ON L/H AILERON TRAILING EDGE (FILED CLOSED) COMPLIED WITH TEMPORARY REPAIR FOR LIGHTNING STRIKE DAMAGES FOUND ON LH AILERON TRAILING EDGE PER REO 601R-57-61-862 REV-- DATED 2024-08-09. REFERENCE CHILD CAMPS FOR EDDY CURRENT AND CO - [SDR SWI2024F01159](https://openairdocs.org/sdr/SWI2024F01159.md): Skin · damaged · Aug 8, 2024 · N912EV · Cndair CL6002B19 · Ailerons > LIGHTNING STRIKE FOUND ON L/H AILERON TRAILING EDGE (FILED CLOSED) COMPLIED WITH TEMPORARY REPAIR FOR LIGHTNING STRIKE DAMAGES FOUND ON LH AILERON TRAILING EDGE PER REO 601R-57-61-862 REV-- DATED 2024-08-09. REFERENCE CHILD CAMPS FOR EDDY CURRENT AND CO - [SDR SWIA2024081200008](https://openairdocs.org/sdr/SWIA2024081200008.md): Skin · damaged · Aug 8, 2024 · N912EV · Cndair CL6002B19 · Ailerons > LIGHTNING STRIKE FOUND ON L/H AILERON TRAILING EDGE (FILED OPEN) COMPLIED WITH TEMPORARY REPAIR FOR LIGHTNING STRIKE DAMAGES FOUND ON LH AILERON TRAILING EDGE PER REO 601R-57-61-862 REV-- DATED 2024-08-09. REFERENCE CHILD CAMPS FOR EDDY CURRENT AND COND - [SDR SWIA202266569](https://openairdocs.org/sdr/SWIA202266569.md): None · corroded · Aug 29, 2022 · N912EV · Cndair CL6002B19 · Fuselage Main, Frame > LBL27 FLOORBEAM BETWEEN FS559+112 AND FS621 FOUND TO BE CORRODED. (C-CHECK RO 9/28/2022) INSTALLED NEW SERVICEABLE LBL27 FLOORBEAM BETWEEN FS559+112 AND FS621 IAW CRJ 200 SRM 51-42-21AND 51-40-11. COMPLETED MAJOR STRUCTURAL REPAIR SKYCARD 51-900-1003-S - [SDR SWIA202266568](https://openairdocs.org/sdr/SWIA202266568.md): None · corroded · Aug 23, 2022 · N912EV · Cndair CL6002B19 · Doors > FOUND PAX DOOR LOWER AFT CORNER SEAL RETAINER TO BE CORRODED AND CRACKED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED SEAL RETAINER IAW CRJ200 SRM 51-42-06. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. - [SDR SWIA202266567](https://openairdocs.org/sdr/SWIA202266567.md): None · corroded · Aug 22, 2022 · N912EV · Cndair CL6002B19 · Air Conditioning Doors > FOUND CORROSION ON MOUNTING PLATE AT GROUND AIR CONDITION CONNECTION AT FS 574.00 AND FS 589.00 BETWEEN STR 22R AND STR24R (C-CHECK RO 9/28/2022) REMOVED OLD AND INSTALLED NEW MOUNTING PLATE AT GROUND AIR CONDITION CONNECTIOC AT FS 574.00 AND FS 589.00 - [SDR SWIA202266566](https://openairdocs.org/sdr/SWIA202266566.md): None · corroded · Aug 21, 2022 · N912EV · Cndair CL6002B19 · Electrical/Electronic Compartment Doors > AVI BAY DOOR SEAL RETAINERS (4EA) FOUND TO BE CORRODED OUT OF LIMITS. REPLACEMENT REQUIRED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED AVI BAY DOOR SEAL RETAINERS (4EA) IAW CRJ 200 SRM 51-42-06 REV 39 DATED 10 MAR 2022. MAJOR REPAIR TASK CARD 51-900-10 - [SDR SWIA202266565](https://openairdocs.org/sdr/SWIA202266565.md): None · corroded · Aug 21, 2022 · N912EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer > FOUND PAX DOOR INTERCOSTAL DD6 AFT SIDE TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PA.X DOOR INTERCOSTAL DD6 IAW CRJ200 SRM 51-42-06. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE C - [SDR SWIA202266564](https://openairdocs.org/sdr/SWIA202266564.md): None · corroded · Aug 20, 2022 · N912EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer > AVI DOOR INTERCOSTAL FROM F.S. 349.00 TO F.S. 364.00 BETWEEN STGR 27R AND STGR 26R IS CORRODED (C-CHECK RO 9/28/2022) INSTALLED NEW SERVICEABLE INTERCOSTAL IAW CRJ 200 SRM 51-42-06 & CRJ 200 SRM 51-42-21.COMPLETED SKY CARD 51-900-1003-SKY AND COMPLETED - [SDR SWIA202266563](https://openairdocs.org/sdr/SWIA202266563.md): None · cracked · Aug 18, 2022 · N912EV · Cndair CL6002B19 · Fuselage Main, Keel > STRINGER 3L IS CRACKED FWDD OF FS 379.00. (C-CHECK RO 9/28/2022) REPAIRED STR 3L IAW CRJ200 SRM 53-00-03 STRINGERS - SPLICE REPAIRS. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FO - [SDR SWIA202266562](https://openairdocs.org/sdr/SWIA202266562.md): None · corroded · Aug 18, 2022 · N912EV · Cndair CL6002B19 · Fuselage Main, Frame > LBL 9 FLOOR BEAM HAS CORROSION DAMAGE BETWEEN F.S.409.00+80 - F.S.409.00+96 (C-CHECK RO 9/28/2022) REPAIRED CORROSION AT LBL9 BETWEEN F.S.409.00+80 - F.S.409.00+96LBL 9 FLOOR BEAM IAW CRJ 200 SRM 53-00-43. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-10 - [SDR SWIA202266561](https://openairdocs.org/sdr/SWIA202266561.md): None · cracked · Aug 16, 2022 · N912EV · Cndair CL6002B19 · Fuselage Main, Frame > OUTBD FLOORBEAM WEB AT RBL9 BETWEEN FS409+32 AND FS409+48 FOUND TO BE CRACKED. REPLACEMENT REQUIRED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED OUTBD FLOORBEAM WEB AT RBL9 BETWEEN FS409+32 AND FS409+48 WITH NEW SERVICEABLE PART IAW CRJ 200 SRM 51-42-06 - [SDR SWIA202266560](https://openairdocs.org/sdr/SWIA202266560.md): None · cracked · Aug 16, 2022 · N912EV · Cndair CL6002B19 · Fuselage Main, Frame > INBD FLOORBEAM WEB AT RBL9 BETWEEN FS409+32 AND FS409+48 FOUND TO BE CRACKED. REPLACEMENT REQUIRED. (C-CHECK RO 9/28/2022) INSTALLED NEW SERVICABLE FLOOR BEAM WEB IAW CRJ 200 SRM 51-40-11, 51-42-21, 51-42-06. COMPLETED SKY CARD 51--900-1003 SKY AND COMP - [SDR SWIA202266559](https://openairdocs.org/sdr/SWIA202266559.md): None · corroded · Aug 16, 2022 · N912EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer > FOUND PAX DOOR INTERCOSTAL DD1 AFT TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD1 IAW CRJ 200 SRM 51-42-06.REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMP - [SDR SWIA202266558](https://openairdocs.org/sdr/SWIA202266558.md): None · corroded · Aug 16, 2022 · N912EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer > FOUND PAX DOOR INTERCOSTAL DD1A AFT SIDE TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD1A IAW CRJ 200 SRM 51-42-06. REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY A - [SDR SWIA202266557](https://openairdocs.org/sdr/SWIA202266557.md): None · corroded · Aug 16, 2022 · N912EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer > FOUND PAX DOOR INTERCOSTAL DD2 AFT TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD2 IAW CRJ 200 SRM 51-42-06. REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COM - [SDR SWIA202266556](https://openairdocs.org/sdr/SWIA202266556.md): None · corroded · Aug 16, 2022 · N912EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer > FOUND PAX DOOR INTERCOSTAL DD5 AFT TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD5 IAW CRJ 200 SRM 51-42-06.REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMP - [SDR SWIA202266555](https://openairdocs.org/sdr/SWIA202266555.md): None · corroded · Aug 16, 2022 · N912EV · Cndair CL6002B19 · Fuselage Main, Frame > FOUND PAX DOOR FWD FORMER BETWEEN DD4-DD5 TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR FWD FORMER BETWEEN DD4-DD5 IAW CRJ 200 SRM 51-42-06. REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-90 - [SDR SWIA202266554](https://openairdocs.org/sdr/SWIA202266554.md): None · corroded · Aug 16, 2022 · N912EV · Cndair CL6002B19 · Fuselage Main, Frame > FOUND PAX DOOR FWD FORMER TO BE HEAVLY CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED FWD FORMER ON PAX DOOR IAW CRJ 200 SRM 51-42-06 AND 51-42-21REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY A - [SDR SWIA202266553](https://openairdocs.org/sdr/SWIA202266553.md): None · corroded · Aug 16, 2022 · N912EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer > FOUND PAX DOOR INTERCOSTAL DD7 MID TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD7 IAW CRJ 200 SRM 51-42-06.REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMP - [SDR SWIA202266552](https://openairdocs.org/sdr/SWIA202266552.md): None · corroded · Aug 13, 2022 · N912EV · Cndair CL6002B19 · Electrical/Electronic Compartment Doors > AVIONICS DOOR INNER LOWER EDGE ANGLE IS CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED AVIONICS DOOR INNER LOWER EDGE ANGLE IAW CRJ200 SRM 51-42-06 AND 51-42-21. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIG - [SDR SWIA202266551](https://openairdocs.org/sdr/SWIA202266551.md): None · corroded · Aug 13, 2022 · N912EV · Cndair CL6002B19 · Electrical/Electronic Compartment Doors > AVIONICS DOOR INNER UPPER EDGE ANGLE IS CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED AVIONICS DOOR INNER UPPER EDGE ANGLE IAW CRJ 200 SRM 51-42-06. REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SK - [SDR SWIA202266550](https://openairdocs.org/sdr/SWIA202266550.md): None · corroded · Aug 13, 2022 · N912EV · Cndair CL6002B19 · Electrical/Electronic Compartment Doors > AVIONICS DOOR INNER AFT EDGE ANGLE IS CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED AVI DOOR INNER AFT EDGE ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REV39 DATED 3/10/2021.MAJOR REPAIR TASK CARD 51-900-103-SKY AND FORM M-337 COMPLETED AND ATTA - [SDR SWIA202266549](https://openairdocs.org/sdr/SWIA202266549.md): None · corroded · Aug 13, 2022 · N912EV · Cndair CL6002B19 · Electrical/Electronic Compartment Doors > AVIONICS DOOR INNER FWD EDGE ANGLE IS CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED AVIONICS DOOR INNER FWD EDGE ANGLE IAW CRJ200 SRM 51-42-06.REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND - [SDR SWIA202266548](https://openairdocs.org/sdr/SWIA202266548.md): None · cracked · Aug 13, 2022 · N912EV · Cndair CL6002B19 · Fuselage Main, Frame > FS589 FRAME FROM STGR20L TO STGR17L IS CRACKED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED FS. 589 FRAME FROM STGR 20L TO 17L IAW CRJ 200 SRM 51-42-06, 51-42-21 AND 51-40-11 COMPLETED SKY CARD 51-900-1003 AND COMPLETED M-337 FORM ATTACHED. REFERENCE CO - [SDR SWIA202266547](https://openairdocs.org/sdr/SWIA202266547.md): None · corroded · Aug 13, 2022 · N912EV · Cndair CL6002B19 · Fuselage Main, Keel > CAP ANGLE AT F.S.409.00 IS CORRODED FROM STR26.5L TO 26.5R ON BOTH FWD AND AFT ATTACHING FLANGES. (C-CHECK RO 9/28/2022) / COMPLIED WITH MHIRJ REO 601R-53-21-3563 REV. -- DATED 2022-08-16. REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STR Next page: https://openairdocs.org/aircraft/N912EV/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 = 'N912EV' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N912EV/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.