# Service difficulty reports: N741EV

A list on [N741EV](https://openairdocs.org/aircraft/N741EV.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 7 · 325 reports

- [SDR SWIA2026062476310](https://openairdocs.org/sdr/SWIA2026062476310.md): Reservoir · leaking · Jun 24, 2026 · N741EV · Cndair CL6002C10 · Humidity Control System
  > STRONG BURNT PLASTIC SMELL ROWS 11-15 IN THE BACK OF THE CABIN (FLIGHT 6337) TROUBLESHOT STRONG BURNT PLASTIC SMELL ROWS 11-15 IN THE BACK OF THE CABIN, IAW FIM 21-22-00-810-806, IT WAS DISCOVERED THAT THE NR 2 HYD SYSTEM RESERVOIR HAD BEEN LEAKING HYD FLUID
- [SDR SWI2025F00447](https://openairdocs.org/sdr/SWI2025F00447.md): Cabin Pressure · pressure loss · Apr 11, 2025 · N741EV · Cndair CL6002C10 · Cabin Pressure Control System
  > LOSS OF CABIN PRESSURE AT F200. EMERGENCY DESCENT. MASKS DEPLOYED. CREW OXYGEN MASKS USED (FLIGHT 6269 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29962820 WITH THE FOLLOWING CORRECTIVE ACTION: "CARRIED FORWARD FOR RESCHEDULING. NOT SC
- [SDR SWIA2025012200012](https://openairdocs.org/sdr/SWIA2025012200012.md): Window · cracked · Jan 12, 2025 · N741EV · Cndair CL6002C10 · Flight Compartment Windows
  > TRANSFER FROM EAML 1512385: FO RIGHT SIDE WINDOW SHATTERED (SPIDER WEB) DURING TAXI IN (FLIGHT 6500) REMOVED AND REPLACED RH WINDOW IN REF. TO AMM 56-12-01. INSTALLED UP TO STEP 28 IN AMM 56-12-01. FINAL TORQUE HAS BEEN COMPLIED WITH ON SIDE WINDOW. SI
- [SDR SWIA202501132](https://openairdocs.org/sdr/SWIA202501132.md): Window · failed · Jan 12, 2025 · N741EV · Cndair CL6002C10 · Flight Compartment Windows
  > TRANSFER FROM EAML 1512385: FO RIGHT SIDE WINDOW SHATTERED (SPIDER WEB) DURING TAXI IN (FLIGHT 6500 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWI2024F00915](https://openairdocs.org/sdr/SWI2024F00915.md): Intercostal · corroded · Jul 29, 2024 · N741EV · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > INTERCOSTAL FWD OF AVIONICS DOOR LEFT OF STGR27 HAS SIGNS OF CORROSION ON INBD WEB (C-CHECK RO 10/6/2024) (FILED CLOSED)REMOVED AND REPLACED INNER COSTAL FWD AVIONICS DOOR AT STGR 27 IB WEB IAW CRJ700 SRM 51-42-06, 51-42-21, 51-40-11, 51-21-11, 51-25-06, 51-42
- [SDR SWIA20240729](https://openairdocs.org/sdr/SWIA20240729.md): Fairing · corroded · Jul 29, 2024 · N741EV · Cndair CL6002C10 · Fuselage Main, Structure
  > SIGNS OF CORROSION FOUND UNDER RAM AIR FAIRING ON FUSELAGE FASTENERS BETWEEN FS1144.00-1162.00 BETWEEN STR 0-1L (C-CHECK RO 10/6/2024) (FILED CLOSED)INSTALLED EWIS PROTECTION ABOVE AND BELOW RAM AIR FAIRING IAW CRJ700 AMM 20-70-00. REMOVED FASTENERS BETWEEN FS
- [SDR SWIA20240727](https://openairdocs.org/sdr/SWIA20240727.md): Floorbeam · corroded · Jul 27, 2024 · N741EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RBL9 FLOOR BEAM HAS SIGNS OF CORROSION AT FS581. EVALUATED CORROSION AT RBL9 FS. 581.FOUND TO BE WITHIN LIMITS IAW REO 670-53-31-921 AND AMM 53-00-49. APPLIED ALODINE, PRIMER AND TOPCOAT IAW CRJ700 SRM 51-21-11, SRM 51-25-06 AND SRM 51-25-16. REINSTALLED SEAT
- [SDR SWI2024F00922](https://openairdocs.org/sdr/SWI2024F00922.md): Seat Track · corroded · Jul 24, 2024 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH FLOOR SEAT TRACK (LBL9) HAS SIGNS OF CORROSION AT FS517-FS553.00. (C-CHECK RO 10/6/2024) (FILED CLOSED)EVALUATED LH FLOOR SEAT TRACK (LBL9) BETWEEN AT FS 517.00 TO FS 553.00 AND DAMAGE WAS FOUND 80% OF THE MATERIAL THEREFORE IT IS OUT LIMITS IAW CRJ 700 SRM
- [SDR SWI2024F00921](https://openairdocs.org/sdr/SWI2024F00921.md): Seat Track · corroded · Jul 24, 2024 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL HAS SIGNS OF CORROSION FROM FS909.00 - FS911.00 (C-CHECK RO 10/6/2024) (FILED CLOSED)REPAIRED DAMAGE AT LH SIDE SEAT RAIL FROM FS909.00-FS911.00 IAW CRJ700 SRM 53-51-49CAL TOOL DEPTH GAUGE AV7277 DUE-AUG2024
- [SDR SWI2024F00920](https://openairdocs.org/sdr/SWI2024F00920.md): Seat Track · corroded · Jul 24, 2024 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL HAS SIGNS OF CORROSION FROM FS708.00 - FS761.85 (C-CHECK RO 10/6/2024) (FILED CLOSED)OK TO INSTAL BJ910267REMOVED AND REPLACED LH SIDE SEAT RAIL FS708.00 - FS 761.85 IAW CRJ 700 AMM 53-41-49, CRJ700 AMM 53-00-49P/N- SH670-37509-1 S/N- UNKCAL
- [SDR SWI2024F00919](https://openairdocs.org/sdr/SWI2024F00919.md): Seat Track · corroded · Jul 24, 2024 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL HAS SIGNS OF CORROSION FROM FS677.00 TO FS708.00 (C-CHECK RO 10/6/2024) (FILED CLOSED)EVALED AND FOUND TO BE OUT OF LIMITS. REPLACED LH SIDE SEAT RAIL FROM FS 677.00 TO 708.00 IAW CRJ 700 AMM 53-00-49, SRM 53-41-49 AND SRM 51-42-34.CAL TOOL:T
- [SDR SWI2024F00918](https://openairdocs.org/sdr/SWI2024F00918.md): Seat Track · corroded · Jul 24, 2024 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 FLOOR SEAT TRACK HAS SIGNS OF CORROSION AT FS379.00 (C-CHECK RO 10/6/2024) (FILED CLOSED)REMOVED CORROSION ON SEAT TRACK AT LBL 9 FS. 379 IAW CRJ700 SRM 51-21-06 AND SRM 53-21-49 SRM 51-21-11. CORROSION REMOVED WITHIN LIMITS IAW CRJ700 SRM 51-21-06CAL TO
- [SDR SWI2024F00917](https://openairdocs.org/sdr/SWI2024F00917.md): Seat Track · corroded · Jul 24, 2024 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH FLOOR SEAT TRACK (RBL9) HAS SIGNS OF CORROSION FROM FS349.00-FS485.00. (C-CHECK RO 10/6/2024) (FILED CLOSED)REPAIRED CORRODED RH FLOOR SEAT TRACK (RBL9) FROM FS 349.00 - FS 485.00 (2) PLACES.POST BLEND DIMENSIONS ARE L=5.00" W=0.90" D=0.0083" (2) L=1.6" W=0
- [SDR SWI2024F00916](https://openairdocs.org/sdr/SWI2024F00916.md): Seat Track · corroded · Jul 24, 2024 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH FLOOR SEAT TRACK (RBL9) HAS SIGNS OF CORROSION FROM FS581.00-FS683.00 (C-CHECK RO 10/6/2024) (FILED CLOSED)OK TO INSTALL BJ 910267REMOVED AND REPLACED RH FLOOR SEAT TRACK (RBL9) FROM FS 581.00-FS 683.00 IAW CRJ 700 AMM 53-00-49 AND SRM 53-31-49.CAL TOOL: TO
- [SDR SWIA20240724](https://openairdocs.org/sdr/SWIA20240724.md): Seat Track · corroded · Jul 24, 2024 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH FLOOR SEAT TRACK (LBL9) HAS SIGNS OF CORROSION AT FS629.00-FS632.00 (C-CHECK RO 10/6/2024) (FILED CLOSED)REMOVED AND REPLACED LH FLOOR SEAT TRACK BETWEEN FS 565.00 TO 632.00 IAW CRJ 700 AMM 53-00-49BLENDED LH FLOOR SEAT TRACK BETWEEN FS 565.00 TO 632.00 MAT
- [SDR SWIA20240720](https://openairdocs.org/sdr/SWIA20240720.md): Vane · chafed · Jul 20, 2024 · N741EV · Cndair CL6002C10 · Trailing Edge Flaps
  > LH INBD FLAP VANE CHAFFED AT INBD HINGE LOCATION (C-CHECK RO 10/6/2024) (FILED CLOSED)REMOVED AND REPLACED LH INBD FLAP VANE. NDT PERFORMED BY BARRON NDT LLC, FAA CRS #5NDR545D, REPORT #S072924-5 P.O. #173177 DATE OF INSPECTION 29JUL2024, SEE REPORT FOR DETAIL
- [SDR SWI2024F00909](https://openairdocs.org/sdr/SWI2024F00909.md): Transcowl · gouged · Jul 19, 2024 · N741EV · Cndair CL6002C10 · Engine Thrust Reverser
  > LH TRANS COWL INBD SLIDER GOUGED (C-CHECK RO 10/6/2024) (FILED CLOSED)PERFORMED REPAIR ON CHAFE DAMAGE AT L/H TRANSCOWL INBD SLIDER IAW REO 670-78-34-384 REV D DATED 2018-11-27CAL TOOL: DIGITAL CALIPER ID: AV-7805 CAL DUE: JAN-2025PERFORMED NDT PT INSPECTION B
- [SDR SWIA20240719](https://openairdocs.org/sdr/SWIA20240719.md): Tripler · chafed · Jul 19, 2024 · N741EV · Cndair CL6002C10 · Fuselage Main, Structure
  > THE REPAIR LOCATED AT FS969.00 STR 27, HAS CHAFFING ON FASTENERS AND CHAFFING ON THE TRIPLER. PERFORMED REPAIR LOCATED AT FS969.00 STR 27 IAW REO 670-53-00-290 REV-F DATE: 2019-04-26, CRJ700 SRM 25-82-06, 53-61-01, 51-25-01, AMM 25-08-06, 21-31-00, NDT PERFOR
- [SDR SWIA202411151241](https://openairdocs.org/sdr/SWIA202411151241.md): Frame · damaged · Jul 18, 2024 · N741EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME FS1144.00 DAMAGED NEAR STR 9R BY WATER INJECTION LINE (C-CHECK RO 10/6/2024) (FILED CLOSED)EVALUATED DAMAGE ON FRAMS FS. 1144.00 NEAR SRT 9RH FOUND TO BE OUT OF LIMITS IAW CRJ700 SRM 53-61-06. FABRICATED REPAIR ANGLE ON FRAME FS 1144.00 NEAR STR 9RH BY W
- [SDR SWIA20241115 718](https://openairdocs.org/sdr/SWIA20241115%20718.md): Skin · chafed · Jul 18, 2024 · N741EV · Cndair CL6002C10 · Trailing Edge Flaps
  > CHAFFING NOTED ON LH INBOARD FLAP LOWER SKIN WHERE CANOE FAIRING IS INSTALLED, INBOARD FAIRING. (C-CHECK RO 10/6/2024) (FILED CLOSED)REPAIRED ON LH IB FLAP LWR SKIN(PN CC670-14061-3, BATCH# 173054) WHERE CANOE FAIRING AT IB FAIRING IAW CRJ700 SRM 57-52-01, 51-
- [SDR SWI2024F01100](https://openairdocs.org/sdr/SWI2024F01100.md): Skin · dented · Jul 18, 2024 · N741EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR SKIN AT FS.310.00 LOWER SECTION HAS A DENT EVAL (C-CHECK RO 10/6/2024) (FILED CLOSED)PERFORMED DRESS BACK ON PASSENGER DOOR SKIN AT FS 310.00 LOWER SECTION IAW BOMBARDIER REO 670-51-00-085 REV-A DATE: 2017-08-23, MHIRJ REO 670-53-21-2455 REV-- D
- [SDR SWI2024F01099](https://openairdocs.org/sdr/SWI2024F01099.md): Door Frame · gouged · Jul 18, 2024 · N741EV · Cndair CL6002C10 · Fuselage Main, Structure
  > PASSENGER DOOR FRAME SKIN AT FS349.00 UPPER SECTION GOUGED EVAL (C-CHECK RO 10/6/2024) (FILED CLOSED)PERFORMED BLEND OUT REPAIR ON PASSANGER DOOR FRAME SKIN AT FS349.00 UPPER SECTION, FOUND WITHIN LIMITS IAW REO 670-53-21-2460 REV-- DATE: 2024-09-12, CRJ700
- [SDR SWI2024F01098](https://openairdocs.org/sdr/SWI2024F01098.md): Frame · damaged · Jul 18, 2024 · N741EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME FS1144.00 DAMAGED NEAR STR 9R BY WATER INJECTION LINE (C-CHECK RO 10/6/2024) (FILED CLOSED)EVALUATED DAMAGE ON FRAMS FS. 1144.00 NEAR SRT 9RH FOUND TO BE OUT OF LIMITS IAW CRJ700 SRM 53-61-06. FABRICATED REPAIR ANGLE ON FRAME FS 1144.00 NEAR STR 9RH BY W
- [SDR SWI2024F01097](https://openairdocs.org/sdr/SWI2024F01097.md): Skin · gouged · Jul 18, 2024 · N741EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR SKIN AT FS310.00 UPPER SECTION GOUGED EVAL (C-CHECK RO 10/6/2024) (FILED CLOSED)REMOVED DAMAGE AND EVALUATED AREA AT PASSENGER DOOR SKIN AT FS 310.00 UPPER SECTION,DIMENSIONS L=1.710" W=0.325",REMAINING THICKNESS 0.125",FOUND TO BE WITH IN LIM I
- [SDR SWI2024F00914](https://openairdocs.org/sdr/SWI2024F00914.md): Floorbeam · corroded · Jul 18, 2024 · N741EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > SIGNS OF CORROSION NOTED ON COCKPIT AND CABIN FLOOR LANDINGS ON THE FS280.00 BEAM, LBL9 -RBL9. (C-CHECK RO 10/6/2024) (FILED CLOSED)REMOVED AND REPLACE NEW ANGLE P/N CC670-34095-3S ON COCKPIT FS280.00 BEAM, LBL9 TO RBL9 AND EVALUATED AREA ON CABIN FLOOR LANDIN
- [SDR SWI2024F00913](https://openairdocs.org/sdr/SWI2024F00913.md): Vane · chafed · Jul 18, 2024 · N741EV · Cndair CL6002C10 · Trailing Edge Flaps
  > ON THE LH INBOARD FLAP VANE, THERE IS CHAFFING ON THE CENTER LEADING EDGE OF THE VANE. (C-CHECK RO 10/6/2024) (FILED CLOSED)REMOVED AND REPLACED L/H INBD FLAP VANE CENTER LEADING EDGE CAP VANE IAW CRJ700 SRM 51-42-13, SRM 51-21-11, SRM 51-25-06, SRM 51-25-16,
- [SDR SWI2024F00912](https://openairdocs.org/sdr/SWI2024F00912.md): Skin · dented · Jul 18, 2024 · N741EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR SKIN AT FS.310.00 LOWER SECTION HAS A DENT EVAL (C-CHECK RO 10/6/2024) (FILED OPEN)PERFORMED DRESS BACK ON PASSENGER DOOR SKIN AT FS 310.00 LOWER SECTION IAW BOMBARDIER REO 670-51-00-085 REV-A DATE: 2017-08-23, MHIRJ REO 670-53-21-2455 REV-- DAT
- [SDR SWI2024F00911](https://openairdocs.org/sdr/SWI2024F00911.md): Door Frame · gouged · Jul 18, 2024 · N741EV · Cndair CL6002C10 · Fuselage Main, Structure
  > PASSENGER DOOR FRAME SKIN AT FS349.00 UPPER SECTION GOUGED EVAL (C-CHECK RO 10/6/2024) (FILED OPEN)PERFORMED BLEND OUT REPAIR ON PASSANGER DOOR FRAME SKIN AT FS349.00 UPPER SECTION, FOUND WITHIN LIMITS IAW REO 670-53-21-2460 REV-- DATE: 2024-09-12, CRJ700 SR
- [SDR SWI2024F00910](https://openairdocs.org/sdr/SWI2024F00910.md): Frame · damaged · Jul 18, 2024 · N741EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME FS1144.00 DAMAGED NEAR STR 9R BY WATER INJECTION LINE (C-CHECK RO 10/6/2024) (FILED OPEN)EVALUATED DAMAGE ON FRAMS FS. 1144.00 NEAR SRT 9RH FOUND TO BE OUT OF LIMITS IAW CRJ700 SRM 53-61-06. FABRICATED REPAIR ANGLE ON FRAME FS 1144.00 NEAR STR 9RH BY WAT
- [SDR SWI2024F01106](https://openairdocs.org/sdr/SWI2024F01106.md): Drag Angle · cracked · Jul 17, 2024 · N741EV · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous Structure
  > L/H VERTICAL STABLIZER DRAG ANGLES CRACKED FWD AND AFT. (C-CHECK RO 10/6/2024) (FILED CLOSED)REPAIRED L/H VERTICAL STABILIZER DRAG ANGLES FWD AND AFT IAW REO 670-55-31-018 REV-- DATE: 2024-08-29, REO 670-55-31-018 REV-A DATE: 2016-11-10, CRJ700 SRM 51-26-01, N
- [SDR SWI2024F00908](https://openairdocs.org/sdr/SWI2024F00908.md): Skin · chafed · Jul 17, 2024 · N741EV · Cndair CL6002C10 · Ailerons
  > LH AILERON LOWER LEADING EDGE CHAFFING DAMAGE. (C-CHECK RO 10/6/2024) (FILED CLOSED)REPAIRED DAMAGE LH AILERON LOWER LEADING EDGE IAW CRJ700 SRM 51-42-06, SRM 57-61-01, SRM 51-21-11, SRM 51-25-06, & SRM 51-25-16. NDT PERFORMED BY BARRON NDT, LLC FAA CRS #5NDR
- [SDR SWI2024F00907](https://openairdocs.org/sdr/SWI2024F00907.md): Drag Angle · cracked · Jul 17, 2024 · N741EV · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous Structure
  > L/H VERTICAL STABLIZER DRAG ANGLES CRACKED FWD AND AFT. (C-CHECK RO 10/6/2024) (FILED OPEN)REPAIRED L/H VERTICAL STABILIZER DRAG ANGLES FWD AND AFT IAW REO 670-55-31-018 REV-- DATE: 2024-08-29, REO 670-55-31-018 REV-A DATE: 2016-11-10, CRJ700 SRM 51-26-01, NDT
- [SDR SWIA20240717](https://openairdocs.org/sdr/SWIA20240717.md): Drag Angle · cracked · Jul 17, 2024 · N741EV · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous Structure
  > R/H VERTICAL STABLIZER DRAG ANGLES CRACKED FWD AND AFT. (C-CHECK RO 10/6/2024) (FILED OPEN)REPAIRED R/H VERTICAL STABILIZER AFT DRAG ANGLE IAW BOMBARDIER REO 670-55-31-177 REV.-- DATE:2024/08/22, REO 670-55-31-018 REV.-A DATE: 2016-11-10, CRJ700 SRM 51-26-01,
- [SDR SWIA20240714](https://openairdocs.org/sdr/SWIA20240714.md): Skin · damaged · Jul 14, 2024 · N741EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD CORNER SKIN PNL DENTED WITH A DAMAGED RIVET. (C-CHECK RO 10/6/2024) (FILED CLOSED)REMOVED AND REPLACED DAMAGED PASSENGER DOOR FWD CORNER PANEL IAW CRJ700 SRM 51-21-11, SRM 51-25-06, SRM 51-42-06, SRM 51-42-13, SRM 51-25-16, SRM 51-40-11, AND SRM52
- [SDR SWIA20241008520](https://openairdocs.org/sdr/SWIA20241008520.md): Door · installed · May 20, 2024 · N741EV · Cndair CL6002C10 · Standard Practices/Structures
  > COMPLY WITH: 670BA-32-056 - LANDING GEAR - NOSE LANDING GEAR (NLG) AND DOORS - INSTALLATION OF A NEW HINGE FOR THE NLG AFT DOOR ASSEMBLY REV A PART(S) 0 (C-CHECK RO 10/6/2024) (FILED CLOSED)PERFORMED DOUBLER REPAIR ON NOSE LANDING GEAR AT LH DOOR AFT HINGE F
- [SDR SWIA20230428006](https://openairdocs.org/sdr/SWIA20230428006.md): Unknown · cracked · Apr 26, 2023 · N741EV · Cndair CL6002C10 · Flight Compartment Windows
  > LEFT SIDE WINDSHIELD CRACKED. (FLT 3164 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26542290 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED LH SIDE WINDOW REFERENCE APPLICABLE STEPS IN AMM 56-12-01TASK CARD 56-220-1000-SKY COMPLIED
- [SDR SWIA2023042700004](https://openairdocs.org/sdr/SWIA2023042700004.md): Unknown · cracked · Apr 26, 2023 · N741EV · Cndair CL6002C10 · Flight Compartment Windows
  > LEFT SIDE WINDSHIELD CRACKED. (FLT 3164 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA202263763](https://openairdocs.org/sdr/SWIA202263763.md): None · bent · Jan 5, 2022 · N741EV · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > FLOOR SUPPORT STRUCTURE SUPPORT ANGLE LOCATED AT LBL27 BETWEEN FS349 - FS364 IS BENT/DEFORMED. (FILED- OPEN) REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE SUPPORT ANGLE AT LBL27 BETWEEN FS349 - FS364 IN REFERENCE TO SRM 51-42-13.
- [SDR SWIA202263762](https://openairdocs.org/sdr/SWIA202263762.md): None · bent · Jan 5, 2022 · N741EV · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > FLOOR SUPPORT STRUCTURE SUPPORT ANGLE LOCATED AT LBL27 BETWEEN FS333 - FS349 IS BENT/DEFORMED. (FILED- OPEN) REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE SUPPORT ANGLE AT LBL27 BETWEEN FS333 - FS349 IN REFERENCE TO SRM 51-42-13.
- [SDR SWIA202263761](https://openairdocs.org/sdr/SWIA202263761.md): None · bent · Jan 5, 2022 · N741EV · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > FLOOR SUPPORT STRUCTURE SUPPORT ANGLE LOCATED AT LBL27 BETWEEN FS310 - FS333 IS BENT/DEFORMED. (FILED- OPEN) REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE SUPPORT ANGLE AT LBL27 BETWEEN FS310 - FS333 IN REFERENCE TO SRM 51-42-13.
- [SDR SWIA202163760](https://openairdocs.org/sdr/SWIA202163760.md): None · corroded · Dec 26, 2021 · N741EV · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > BACKUP SILL BETWEEN FS 310.00 TO 333.00 AND STGR 21L CORRODED. (FILED- OPEN) REMOVED AND REPLACED BACKUP SILL BETWEEN FS 310.00 TO 333.00 AND STR 21L WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1002-SKY. COMPLETED M-337.
- [SDR SWIA202163759](https://openairdocs.org/sdr/SWIA202163759.md): None · damaged · Dec 9, 2021 · N741EV · Cndair CL6002C10 · Fuselage Main, Frame
  > DURING THE INCORPORATION OF SB 670SH-53-042 THE BULKHEAD BEAM @ FS693 LBL 27 PN SH670-35884-7 WAS DAMAGED. (FILED- OPEN) REMOVED AND REPLACED BULKHEAD BEAM @ FS693 LBL 27, IN REF. TO 670BA-53-036 AND 670SH-53-042, COMPLETED 51-900-1002-SKY AND M337. REF. C
- [SDR SWIA202163758](https://openairdocs.org/sdr/SWIA202163758.md): None · damaged · Dec 9, 2021 · N741EV · Cndair CL6002C10 · Fuselage Main, Frame
  > DURING THE INCORPORATION OF SB 670SH-53-042 THE BULKHEAD BEAM @ FS693 LBL 18 PN SH670-35886-5 WAS DAMAGED. (FILED- CLOSED) REMOVED AND REPLACED BULKHEAD BEAM @ FS693 LBL 18, IN REF. TO 670BA-53-036 AND 670SH-53-042, COMPLETED 51-900-1002-SKY AND M337. REF.
- [SDR SWIA202163757](https://openairdocs.org/sdr/SWIA202163757.md): None · none · Dec 9, 2021 · N741EV · Cndair CL6002C10 · Fuselage Main, Frame
  > DURING THE INCORPORATION OF SB 670SH-53-042 THE BULKHEAD BEAM @ FS693 LBL 9 PN SH670-35885-5 WAS DAMAGED. (FILED - OPEN) REMOVED AND REPLACED BULKHEAD BEAM @ FS693 LBL 9, IN REF. TO 670BA-53-036 AND 670SH-53-042, COMPLETED 51-900-1002-SKY AND M337. REF. CP
- [SDR SWIA202163755](https://openairdocs.org/sdr/SWIA202163755.md): None · cracked · Dec 4, 2021 · N741EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FOUND CRACKED DIAPHRAGM PN SH670-36115-1 @ FS735, AND LBL36. REPLACE AS NECESSARY. (FILE - CLOSED) REMOVED AND REPLACED DIAPHRAGM @ FS735 AND LBL36 IN REF. SRM 51-42-21, COMPLETED 51-900-1002-SKY AND COMPLETED M-337, REF. CP 23852492 FOR LEAK CHECK
- [SDR SWIA202163756](https://openairdocs.org/sdr/SWIA202163756.md): None · damaged · Oct 18, 2021 · N741EV · Cndair CL6002C10 · Fuselage Main, Frame
  > COMPLY WITH: 670BA-53-036 - FUSELAGE - CENTER FUSELAGE, FS669.40 TO FS855.40 - REPLACEMENT OF THE BEAMS AF LBL36 AND RBL36, AND THE FLOOR ASSEMBLY BETWEEN FS693.00 AND FS847.00 WITH BEAMS INSTALLED AT BL0, LBL9, LBL18, LBL27, RBL9, RBL18 AND RBL27 REV D PART(
- [SDR SWIA202161778](https://openairdocs.org/sdr/SWIA202161778.md): None · damaged · Oct 7, 2021 · N741EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > AIRCRAFT SUSTAINED DAMAGE TO LHS SKIN PANEL BETWEEN FS 193.00 - FS 202.75 AND STR BL22.00 - STR 14L FROM BIRDSTRIKE. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. REF CAMP'S ML 23603273, 23603274, 23603275 AND 23603276. (FILED CLOSED) REMOVED AND REPLACE
- [SDR SWIA202008252071](https://openairdocs.org/sdr/SWIA202008252071.md): Bracket · corroded · Aug 11, 2020 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT STRUCTURE - ENTRANCE STORAGE FWD AMOUNT BRACKETS HAVE CORROSION AROUND AND IN THE BOLT HOLES. REMOVED AND REPLACED FLOOR SUPPORT NEW ENTRANCE STORAGE FWD MOUNT BRACKETS IAW SRM.
- [SDR SWIA202008252070](https://openairdocs.org/sdr/SWIA202008252070.md): Floorbeam · corroded · Aug 4, 2020 · N741EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RBL 9 FLOORBEAM AT BS 581 WAS CORRODED. COMPLIED WITH ALL STEPS OF REO.
- [SDR SWIA202008252069](https://openairdocs.org/sdr/SWIA202008252069.md): Floor Support · corroded · Aug 4, 2020 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR BEAM, FS533 TO FS565 WAS CORRODED. COMPLIED WITH ALL STEPS OF REO.

Next page: https://openairdocs.org/aircraft/N741EV/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 = 'N741EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N741EV/reports

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