# Service difficulty reports: N904EV

A list on [N904EV](https://openairdocs.org/aircraft/N904EV.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 · 266 reports

- [SDR SWIA2026041475691](https://openairdocs.org/sdr/SWIA2026041475691.md): Oxygen Mask · leaking · Apr 14, 2026 · N904EV · Cndair CL6002B19 · Crew Oxygen System
  > OBERSERVOR O2 MASK HAS LEAK. STARTED IN CRUISE COULDN€™T STOP LEAK. (FLIGHT 6064 - FILED CLOSED)REMOVED AND REPLACED CREW OBSERVER OXYGEN MASK ASSY IN REFERENCE TO AMM 35-11-12. REMOVED AND REPLACED CREW OBSERVER OXYGEN MASK STOWAGE BOX ASSY IN REFERENCE TO
- [SDR SWIA2025071400012](https://openairdocs.org/sdr/SWIA2025071400012.md): Wire Harness · broken · Jul 12, 2025 · N904EV · Cndair CL6002B19 · Landing Gear System Wiring
  > GEAR DISAGREE AFTER TAKEOFF. CLEARED VIA CHECKLIST. NOSE WHEEL WAS THE AFFECTED DOWN (FLIGHT 5555 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30474800 WITH THE FOLLOWING CORRECTIVE ACTION: "FOUND NOSE LANDING GEAR ELECTRICAL HARNESS ASSY. BR
- [SDR SWIA202506061211](https://openairdocs.org/sdr/SWIA202506061211.md): Trunnion · misaligned · Dec 11, 2024 · N904EV · Cndair CL6002B19 · Fuselage, Landing Gear Attach Fittings
  > COMPLY WITH SB 601R-57-048 (WINGS €“ CENTER WING PRIMARY STRUCTURE €“ COLD WORK OF HOLES ON THE WEB OF THE MAIN LANDING GEAR (MLG) TRUNNION), DUE TO RH MLG TRUNNION REPLACEMENT (C-CHECK RO 06/05/2025)COMPLIED WITH SB 601R-57-048 (WINGS €“ CENTER WING PRIMA
- [SDR SWIA202506061119](https://openairdocs.org/sdr/SWIA202506061119.md): Floor Panel · cracked · Nov 19, 2024 · N904EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > ELECTRICAL BAY FLOOR PANEL @ FS 193 HAS A CRACK ON LH SIDE @ ACCUMLATER GAUGE BRACKET. (C-CHECK RO 06/05/2025)REPAIRED ELECTRICAL BAY FLOOR PANEL AT FS 193 IAW REO 601R-53-11-081
- [SDR SWIA20250606725](https://openairdocs.org/sdr/SWIA20250606725.md): Trunnion · cracked · Jul 25, 2024 · N904EV · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA44221-601R-57-21-2831-N904EV-PR - THE RHS WING PLANK, TRUNNION, AND STEEL STRAP STACKUP HAS 4 EA CRACK INDICATIONS IN FASTENER HOLES WS65.75. REPAIRED IN REF TO REO 601R-57-21-2831, REV--, DTD 07/31/2018. **THE
- [SDR SWI2023F00570](https://openairdocs.org/sdr/SWI2023F00570.md): Unknown · damaged · Dec 8, 2023 · N904EV · Cndair CL6002B19 · Wing Spar
  > INSPECTION REQUIRED FOR AIRCRAFT WING DAMAGE BETWEEN WS 407.08 AND WS 377.40 AND BETWEEN FORWARD WING SPAR AND AFT WING SPAR. (FILED CLOSED)PERFORMED INSPECTION OF THE DAMAGE TO RH WING BETWEEN WS 407.08 AND WS 377.40 AND BETWEEN FORWARD WING SPAR AND AFT WI
- [SDR SWIA20231214008](https://openairdocs.org/sdr/SWIA20231214008.md): Unknown · unknown · Dec 8, 2023 · N904EV · Cndair CL6002B19 · Wing, Plate/Skin
  > UPON FURTHER INSPECTION OF RH WING DAMAGE, FOUND 2 DOUBLERS FROM WS 407.08 AND WS 377.40 AND BETWEEN FWD SPAR AND AFT SPAR DAMAGE BEYONG LIMITS. DOUBLERS REQUIRE REPLACEMENT AND IS CONSIDERED MAJOR REPAIR. REFERENCE SRM 57-31-31 FIG 1 SHEET 2 ITEM 34 AND 36. R
- [SDR SWIA202266908](https://openairdocs.org/sdr/SWIA202266908.md): Sensor · failed · Nov 19, 2022 · N904EV · Cndair CL6002B19 · Landing Gear Position and Warning
  > ON CLIMB OUT CALLED FOR GEAR UP, BOTH MLG WENT UP NORMALLY FOLLOWED BY GEAR DISAGREE WARNING MSG, AND SUBSEQUENT NOSE DOOR OPEN CAUTION MSG. EICAS INDICATED MLG UP AND LOCKED AND NLG DOWN. COMPLIED WITH QRH AND THEN ALL LANDING GEAR INDICATED DOWN AND GREEN. R
- [SDR SWIA202158784](https://openairdocs.org/sdr/SWIA202158784.md): Fitting · damaged · May 14, 2021 · N904EV · Cndair CL6002B19 · Vertical Stabilizer
  > V-STAB FWD STEADY BLOCK SUPPORT FITTING FOUND TOOLING DAMAGE ON VERTICAL STAB AT ATTACH HOLES. (C-CHECK RO 6/11/2021) REPAIRED V-STAB FWD STEADY BLOCK SUPPORT FITTING FOUND TOOLING DAMAGE ON VERTICAL STAB AT ATTACH HOLES. IAW MHIRJ REO'S 601R-55-31-375
- [SDR SWIA202158808](https://openairdocs.org/sdr/SWIA202158808.md): Support Fitting · damaged · May 12, 2021 · N904EV · Cndair CL6002B19 · Vertical Stabilizer
  > V-STAB FWD STEADY BLOCK SUPPORT FITTING REQUIRES MACHINING (C-CHECK RO 6/11/2021) PART WAS DAMAGED DURING REMOVAL AND REPLACED BY A NEW SERVICEABLE PARTON CANP 22795401 JOB 97628103 OP 11 NO FINAL COPY OF REO 601R-55-31-381 REQUIRED DUE TO REPLACEMENT
- [SDR SWIA202158745](https://openairdocs.org/sdr/SWIA202158745.md): Skin · corroded · Apr 13, 2021 · N904EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > MULTIPLE AREAS OF CORROSION AND CHAFF DAMAGE BETWEEN F.S. 559+80 & 559+112 FROM STGR 21R TO 24R (C-CHECK RO 6/11/2021) REMOVED DAMAGE FROM FUSE EXTERIOR SKIN FS 559+80- FS 559+112 FROM STR 21R 24R IAW REO 601R-53-51-582 REV -- DATED 2021-04-27. COMPLIED
- [SDR SWIA202158783](https://openairdocs.org/sdr/SWIA202158783.md): Rib · cracked · Apr 2, 2021 · N904EV · Cndair CL6002B19 · Trailing Edge Flaps
  > TRANSFERED FROM CAMP 22538869 JOB 97628101 OP 493 - L/H I/B FLAP I/B CLOSE OUT RIB HAS A DENT APPROX.200 DEEP AND POSSIBLE CRACK AT A NUTPLATE HOLE LOCATION. (C-CHECK RO 6/11/2021) PERFORMED A MAJOR REPAIR BY REMOVING AND REPLACING THE L/H I/B FLAP I/
- [SDR SWIA202158782](https://openairdocs.org/sdr/SWIA202158782.md): Skin · chafed · Mar 30, 2021 · N904EV · Cndair CL6002B19 · Wing, Plate/Skin
  > CHAFF DAMAGE FOUND AT WING TRAILING EDGE AT LBL 45 (C-CHECK RO 6/11/2021) REPAIRED CHAFE DAMAGE AT LBL45 LH WING TRAILING EDGE IAW MHIRJ REO #601R-57-21-3458 REV-- DATE 2021-04-09. TASK CARD 51-900-1003-SKY COMPLETED, FORM M-337 ATTACHED. NO CHANGE TO
- [SDR SWIA202158781](https://openairdocs.org/sdr/SWIA202158781.md): Skin · chafed · Mar 29, 2021 · N904EV · Cndair CL6002B19 · Wing, Plate/Skin
  > FOUND LH AND RH LOWER AFT WING PLANK BL 45 HAS CHAFED AREAS LH SIDE IS 3 INCHES LONG.025 DEEP AND RH SIDE 3 INCHES LONG.035 DEEP BOTH 1 INCH WIDE (C-CHECK RO 6/11/2021) REPAIRED RH LOWER AFT WING PLANK BL45 IAW MHIRJ REO#601R-57-21-3457 REV-- DATE 20
- [SDR SWIA202158762](https://openairdocs.org/sdr/SWIA202158762.md): Floor Support · corroded · Mar 29, 2021 · N904EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RBL27 FLOORBEAM CAP BETWEEN APPROX. FS 559+8 ANDS FS 559+112 IS CORRODED. (C-CHECK RO 6/11/2021) REMOVED AND REPLACED FLOOR BEAM CAP IAW CRJ 200 SRM 51-42-15, 51-42-21, 51-42-34, AND REO 601R-53-51-578 REV -- DATED 2021-04-14. COMPLIED WITH TASK CARD 51
- [SDR SWIA202158792](https://openairdocs.org/sdr/SWIA202158792.md): Support Beam · cracked · Mar 25, 2021 · N904EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > LOWER AFT ANGLE ON CARGO DOOR SUPPORT BEAM, ATTACHED TO FWD SIDE OF 621 BULKHEAD IS CRACKED. (C-CHECK RO 6/11/2021) REMOVED AND REPLACED LOWER AFT ANGLE ON CARGO DOOR SUPPORT BEAM, ATTACHED TO FWD SIDE OF 621 BULKHEAD IAW CRJ-200 SRM 51-42-21 AND 51-40
- [SDR SWIA202158780](https://openairdocs.org/sdr/SWIA202158780.md): Skin · chafed · Mar 23, 2021 · N904EV · Cndair CL6002B19 · Trailing Edge Flaps
  > CUSTOMER REQUEST REPAIR OF RH IB FLAP VANE CAP FOR CHAFING DAMAGE AT WS 56.30, WS 104.099, AND WS 139.924 (C-CHECK RO 6/11/2021) REMOVED AND REPLACED RH IB FLAP VANE CAPS AT WS 56.30, WS 104.099.AND WS 139.924 IAW CRJ 200 SRM 51-40-11 AND 51-42-13 REV.
- [SDR SWIA202158779](https://openairdocs.org/sdr/SWIA202158779.md): Floor Support · corroded · Mar 20, 2021 · N904EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H FLOOR SILL FROM FS 563 TO FS 621 IS CORRODED BEYOND LIMITS AND NEEDS REPLACED (C-CHECK RO 6/11/2021) REPAIRED R/H FLOOR SILL FROM FS 563 TO FS 621 IAW REO 601R-53-61-5376 REV -A DATED 2018-10-25. REFERENCE CONTINUE CARD FOR DETAILS OF WORK PERFORMED
- [SDR SWIA202158760](https://openairdocs.org/sdr/SWIA202158760.md): Floor Support · corroded · Mar 20, 2021 · N904EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H FLOOR SILL FROM FS 559+16 TO FS 559+80 IS CORRODED BEYOND LIMITS AND REQUIRES REPLACMENT (C-CHECK RO 6/11/2021) REMOVED AND REPLACED RH FLOOR SILL FROM FS 559+16 - FS 559+80 IAW CRJ 200 SRM 51-42-06 REV 38 B 25 NOVEMBER 2020 TASK CARD 51-900-1003-SK
- [SDR SWIA202158754](https://openairdocs.org/sdr/SWIA202158754.md): Intercostal · corroded · Mar 20, 2021 · N904EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H INTERCOSTAL FROM FS 559 TO FS 559+16 IS CORRODED BEYOND LIMITS AND REQUIRES REPLACEMENT (C-CHECK RO 6/11/2021) REMOVED R/H INTERCOSTAL FROM FS 559 TO FS 559+16 IAW: CRJ200-SRM-51-42-06 AND 51-41-02. LOCATED AND DRILLED NEW SERVICABLE INTERCOSTAL PN
- [SDR SWIA202158791](https://openairdocs.org/sdr/SWIA202158791.md): Stop Fitting · cracked · Mar 19, 2021 · N904EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR STOP BRACKET (FITTING) FS 310.00 STR 5L IS CRACKED. (C-CHECK RO 6/11/2021) REMOVED AND REPLACED PAX DOOR STOP FITTING IAW CRJ200 SRM 51-40-11 AND 51-42-21
- [SDR SWIA202158752](https://openairdocs.org/sdr/SWIA202158752.md): Skin · corroded · Mar 19, 2021 · N904EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > UPON REMOVAL OF AFT POTABLE WATER DRAIN FOUND EXTERIOR FUSE SKIN CORRODED BETWEEN F.S. 605 - F.S. 621 STRINGER 26R - 25R (C-CHECK RO 6/11/2021) REPAIRED FUSE SKIN CORROSION UNDER AFT POTABLE WATER DRAIN AT FS605 - FS621 STGR 26R - 25R IAW MHIRJ REO 601R
- [SDR SWIA202158748](https://openairdocs.org/sdr/SWIA202158748.md): Bulkhead Web · damaged · Mar 16, 2021 · N904EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS 2 AREAS WITH MULTIPLE INDICATIONS NOTED 1) RBL9.5 WL74.5 1.5 INCHES LONG 100 %FSH AND 2) LBL18.00 WL75.5 1 ICH LONG 90%FSH BOTH AREAS FAILED NDT INSPECTION (C-CHECK RO 6/11/2021) REMOVED DAMAGE FROM REAR PRESSURE BU
- [SDR SWIA202158805](https://openairdocs.org/sdr/SWIA202158805.md): Bolt · corroded · Mar 15, 2021 · N904EV · Cndair CL6002B19 · Trailing Edge Flaps
  > L/H I/NB FLAP O/B UPPER FITTING THROUGHT BOLT AND NUT HARDWARE CORRODED. (C-CHECK RO 6/11/2021) REPLACED L/H I/B FLAP O/B UPPER FITTING THROUGH BOLT AND NUT HARDWARE. TO BE INSTALLED ON CAMP CP22000952.
- [SDR SWIA202158778](https://openairdocs.org/sdr/SWIA202158778.md): Access Panel · corroded · Mar 15, 2021 · N904EV · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT LOWER WING PLANK FUEL ACCESS HOLE AT 650DB HAS CORROSION IN THE CRITICAL AND NON-CRITICAL AREAS. (C-CHECK RO 6/11/2021) REMOVED CORROSION FROM 650DB IN CRICTICAL AND NON-CRITICAL AREAS IAW REO 601R-57-21-030 REV L DATED 2014-02-05, COMPLIED WITH S
- [SDR SWIA202158777](https://openairdocs.org/sdr/SWIA202158777.md): Access Panel · corroded · Mar 15, 2021 · N904EV · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT LOWER WING PLANK FUEL ACCESS HOLE AT 650FB HAS CORROSION IN THE CRITICAL AND NON-CRITICAL AREAS. (C-CHECK RO 6/11/2021) REMOVED CORROSION FROM 650FB IN CRICTICAL AND NON-CRITICAL AREAS IAW REO 601R-57-21-030 REV L DATED 2014-02-05, COMPLIED WITH S
- [SDR SWIA202158776](https://openairdocs.org/sdr/SWIA202158776.md): Access Panel · corroded · Mar 15, 2021 · N904EV · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT LOWER WING PLANK FUEL ACCESS HOLE AT 650GB HAS CORROSION IN THE CRITICAL AND NON-CRITICAL AREAS. (C-CHECK RO 6/11/2021) REMOVED CORROSION FROM 650GB IN CRICTICAL AND NON-CRITICAL AREAS IAW REO 601R-57-21-030 REV L DATED 2014-02-05, COMPLIED WITH S
- [SDR SWIA202158775](https://openairdocs.org/sdr/SWIA202158775.md): Access Panel · corroded · Mar 15, 2021 · N904EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT LOWER WING PLANK FUEL TANK ACCESS HOLE AT 550GB HAS CORROSION IN CRITICAL AND NON-CRITICAL AREAS. (C-CHECK RO 6/11/2021) REMOVED CORROSION FROM 550GB IN CRICTICAL AND NON-CRITICAL AREAS IAW REO 601R-57-21-030 REV L DATED 2014-02-05, COMPLIED WITH S
- [SDR SWIA202158774](https://openairdocs.org/sdr/SWIA202158774.md): Access Panel · corroded · Mar 15, 2021 · N904EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT LOWER WING PLANK FUEL TANK ACCESS HOLE AT 550CB HAS CORROSION IN CRITICAL AND NON-CRITICAL AREAS. (C-CHECK RO 6/11/2021) REMOVED CORROSION FROM 550CB IN CRICTICAL AND NON-CRITICAL AREAS IAW REO 601R-57-21-030 REV L DATED 2014-02-05, COMPLIED WITH S
- [SDR SWIA202158773](https://openairdocs.org/sdr/SWIA202158773.md): Access Panel · corroded · Mar 15, 2021 · N904EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT LOWER WING PLANK FUEL TANK ACCESS HOLE AT 540BB HAS CORROSION IN CRITICAL AND NON-CRITICAL AREAS. (C-CHECK RO 6/11/2021) REMOVED CORROSION BY BLENDING IAW REO# 601R-57-21-030 REV-L DATED 2014-02-05. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED
- [SDR SWIA202158772](https://openairdocs.org/sdr/SWIA202158772.md): Access Panel · corroded · Mar 15, 2021 · N904EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT LOWER WING PLANK FUEL TANK ACCESS HOLE AT 540AB HAS CORROSION IN CRITICAL AND NON-CRITICAL AREAS. (C-CHECK RO 6/11/2021) REMOVED CORROSION FROM 540AB IN CRICTICAL AND NON-CRITICAL AREAS IAW REO 601R-57-21-030 REV L DATED 2014-02-05, COMPLIED WITH S
- [SDR SWIA202158771](https://openairdocs.org/sdr/SWIA202158771.md): Access Panel · corroded · Mar 15, 2021 · N904EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT LOWER WING PLANK FUEL TANK ACCESS HOLE AT 510AB HAS CORROSION IN CRITICAL AND NON-CRITICAL AREAS. (C-CHECK RO 6/11/2021) REMOVED CORROSION FROM 510 AB FUEL PANEL CUTOUT IN NON-CRITICA AND CRITICAL AREAS IAW REO 601R-57-21-030 REV L DATED 2014-02-05
- [SDR SWIA202158742](https://openairdocs.org/sdr/SWIA202158742.md): Access Panel · corroded · Mar 15, 2021 · N904EV · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT LOWER WING PLANK FUEL ACCESS HOLE AT 610BB HAS CORROSION IN THE CRITICAL AND NON-CRITICAL AREAS. (C-CHECK RO 6/11/2021) REMOVED CORROSION FROM 610 BB FUEL PANEL CUTOUT IN NON-CRITICA AND CRITICAL AREAS IAW REO 601R-57-21-030 REV L DATED 2014-02-05
- [SDR SWIA202158804](https://openairdocs.org/sdr/SWIA202158804.md): Nut · corroded · Mar 14, 2021 · N904EV · Cndair CL6002B19 · Spoilers
  > LEFT SPOILERON INBOARD HINGE NUT CORRODED, AND INBOARD AND OUTBOARD RETAINING PLATE BOLTS CORRODED. (C-CHECK RO 6/11/2021) REPLACED SPOILERON INBOARD HINGE NUT AND INBOARD AND OUTBOARD RETAINING PLATE BOLTS IAW CRJ 200-AMM 27-64-01-400-801.
- [SDR SWIA202158803](https://openairdocs.org/sdr/SWIA202158803.md): Nut · corroded · Mar 14, 2021 · N904EV · Cndair CL6002B19 · Spoilers
  > LEFT SPOILERON OUTBOARD HINGE NUT CORRODED. (C-CHECK RO 6/11/2021) INSTALLED NEW NUT AND COTTER PIN ON LEFT SPOILERON OUTBOARD HINGE IAW CRJ-200 AMM 27-64-01-400-801.
- [SDR SWIA202158802](https://openairdocs.org/sdr/SWIA202158802.md): Nut · corroded · Mar 14, 2021 · N904EV · Cndair CL6002B19 · Spoilers
  > LEFT FLIGHT SPOILER OUTBOARD HINGE NUT CORRODED. (C-CHECK RO 6/11/2021) REMOVED AND REPLACED LH FLT SPOILER OB HINGE NUT IAW CRJ 200 AMM 27-64-05-400-801. OPS CHECK "GOOD"
- [SDR SWIA202158801](https://openairdocs.org/sdr/SWIA202158801.md): Nut · corroded · Mar 14, 2021 · N904EV · Cndair CL6002B19 · Spoilers
  > LEFT FLIGHT SPOLIER INBOARD ACTUATOR HAS A CORRODED LOWER MOUNT NUT. (C-CHECK RO 6/11/2021) REMOVED AND REPLACED LH FLT SPOILER IB ACTUATOR LOWER MOUNT NUT IAW CRJ 200 AMM 27-62-01-400-801. OPS CHECK "GOOD"
- [SDR SWIA202158800](https://openairdocs.org/sdr/SWIA202158800.md): Nut · corroded · Mar 14, 2021 · N904EV · Cndair CL6002B19 · Spoilers
  > LEFT OUTBOARD GROUND SPOLIER INBOARD AND OUTBOARD HINGE NUTS ARE CORRODED. (C-CHECK RO 6/11/2021) REMOVED AND REPLACED LH OB GND SPOILER IB AND OB HINGE NUTS IAW CRJ 200 AMM 27-65-01-400-801. OPS CHECK "GOOD"
- [SDR SWIA202158806](https://openairdocs.org/sdr/SWIA202158806.md): Door Frame · chafed · Mar 12, 2021 · N904EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR TOP AFT CORNER OF FRAME IS CHAFED. (C-CHECK RO 6/11/2021) REMOVED AND REPLACED DAMAGED CARGO DOOR SUPPORT BEAM IAW CRJ200 SRM 51-42-06 AND 51-42-21
- [SDR SWIA202158799](https://openairdocs.org/sdr/SWIA202158799.md): Nut · corroded · Mar 12, 2021 · N904EV · Cndair CL6002B19 · Spoilers
  > RIGHT WING OUTBOARD GROUND SPOILER, OUTBOARD HINGE BOLT NUT CORRODED. (C-CHECK RO 6/11/2021) INSTALLED NEW HARDWARE NUT PN# MS17825-5 WASHER NAS1149CO563B AND BUSHING PN# 600-10300-597 ON RH OTBD GROUND SPOILER OTBD HINGE IAW CRJ 200 AMM27-65-01-400-801
- [SDR SWIA202158798](https://openairdocs.org/sdr/SWIA202158798.md): Bolt · corroded · Mar 12, 2021 · N904EV · Cndair CL6002B19 · Spoilers
  > RIGHT HAND WING INBOARD GROUND SPOILER, OUTBOARD HINGE BOLT NUT CORRODED. (C-CHECK RO 6/11/2021) RECIEVED NEW SERVICABLE BOLT AND NUT REFERENCE JOB 97628105 OP 858 CAMP #22354738 FOR INSTALL
- [SDR SWIA202158797](https://openairdocs.org/sdr/SWIA202158797.md): Nut · corroded · Mar 12, 2021 · N904EV · Cndair CL6002B19 · Spoilers
  > RIGHT WING FLIGHT SPOILER INBOARD HINGE BOLT NUTS AND RETAINING BRACKET HARDWARE CORRODED. (C-CHECK RO 6/11/2021) REMOVED AND REPLACED RH WING FLIGHT SPOILER IB HINGE BOLT NUTS AND RETAINING BRACKET HARDWARE IAW CRJ AMM 27-64-05-400-801. OPS CHECK "GOOD
- [SDR SWIA202158796](https://openairdocs.org/sdr/SWIA202158796.md): Nut · corroded · Mar 12, 2021 · N904EV · Cndair CL6002B19 · Spoilers
  > RIGHT HAND WING SPOILERON HINGE BOLT NUTS AND RETAINING BRACKET HARDWARE CORRODED. (C-CHECK RO 6/11/2021) REMOVED AND REPLACED RH WING SPOILERON HINGE BOLTS AND RETAINING HARDWARE IAW CRJ 200 AMM 27-64-01-400-801. OPS CHECK "GOOD"
- [SDR SWIA202158790](https://openairdocs.org/sdr/SWIA202158790.md): Angle · cracked · Mar 11, 2021 · N904EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > R/H INTERCOSTAL ANGLE IS CRACKED AT FS621.0 TO FS625.0 BL45, STR14, WL 97.5. (C-CHECK RO 6/11/2021) REMOVED AND REPLACED R/H INTERCOSTAL ANGLE AT FS621.0 TO FS625.0 BL45, STR14, WL 97.5 IAW CRJ 200 SRM 51-40-11, 51-42-21, AND 51-25-16
- [SDR SWIA202158789](https://openairdocs.org/sdr/SWIA202158789.md): Angle · cracked · Mar 11, 2021 · N904EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > L/H INTERCOSTAL ANGLE IS CRACKED AT FS621.0 TO FS625.0 BL45, STR14, WL 97.5. (C-CHECK RO 6/11/2021) REMOVED AND REPLACED INTERCOSTAL ANGLE AT F.S.621.0 TO F.S. 625.0 BL45, STRG14, WL 97.5 IAW SRM 51-40-11, 51-42-21, AND 51-25-16
- [SDR SWIA202158756](https://openairdocs.org/sdr/SWIA202158756.md): Window Post · cracked · Mar 10, 2021 · N904EV · Cndair CL6002B19 · Fuselage Main, Structure
  > LH WINDSHIELD SIDE POST SUPPORT FRAME BETWEEN FS 220 AND FS 235 BELOW WL 110 IS CRACKED. (C-CHECK RO 6/11/2021) REMOVED AND REPLACED ANGLE FOR LH WINDSHIELD SIDE POST SUPPORT FRAME BETWEEN FS 220- FS FS 235 AT WL 110 IAW CRJ 200 SRM 51-42-06 AND DWG 60
- [SDR SWIA202158755](https://openairdocs.org/sdr/SWIA202158755.md): Window Frame · cracked · Mar 10, 2021 · N904EV · Cndair CL6002B19 · Fuselage Main, Structure
  > RH WINDSHIELD SIDE POST SUPPORT FRAME BETWEEN FS 220 AND FS 235 BELOW WL 110 IS CRACKED. (C-CHECK RO 6/11/2021) REMOVED AND REPLACED ANGLE FOR RH WINDSHIELD SIDE POST SUPPORT FRAME BETWEEN FS 220- FS FS 235 AT WL 110 IAW CRJ 200 SRM 51-42-06 AND DWG 60
- [SDR SWIA202158795](https://openairdocs.org/sdr/SWIA202158795.md): Crossbeam · corroded · Mar 9, 2021 · N904EV · Cndair CL6002B19 · Fuselage Main, Structure
  > CROSSBEAM CAP AT FS559.00+112 HAS MULTIPLE SPOTS OF CORROSION BETWEEN LBL27 AND LBL45 (C-CHECK RO 6/11/2021) REMOVED AND REPLACED CROSSBEAM CAP AT F.S. 559+112 BETWEEN LBL27 AND LBL 45 IAW CRJ200 SRM 51-42-06
- [SDR SWIA202158788](https://openairdocs.org/sdr/SWIA202158788.md): Intercostal · cracked · Mar 9, 2021 · N904EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL APPEARS TO BE CRACKED IN INBOARD UPPER RADIUS AT FS484, RBL36-RBL45, UNDER THE PRESSURE FLOOR. (C-CHECK RO 6/11/2021) REMOVED AND REPLACED CRACKED INTERCOSTAL WITH NEW INTERCOSTAL AT F.S, 484 RBL 36 TO RBL 45 IAW CRJ 200 SRM 51-40-11, 51-42
- [SDR SWIA202158770](https://openairdocs.org/sdr/SWIA202158770.md): Stringer · corroded · Mar 9, 2021 · N904EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRGR 27 HAS MULTIPLE SPOTS OF CORROSION FROM FS605.00 TO FS621.00 (C-CHECK RO 6/11/2021) REMOVED AND REPLACED STR 27 FROM FS 559+112 - FS 621 IAW CRJ 200 SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED FORM 337. NO WEIGHT CHANGE NOTED.

Next page: https://openairdocs.org/aircraft/N904EV/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 = 'N904EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N904EV/reports

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