# Service difficulty reports: N755EV

A list on [N755EV](https://openairdocs.org/aircraft/N755EV.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 · 255 reports

- [SDR SWIA2026081076760](https://openairdocs.org/sdr/SWIA2026081076760.md): Motor · warning message · Aug 10, 2026 · N755EV · Cndair CL6002C10 · Hydraulic Pump (Electric/Engine), Main
  > HYD 3 LOW PRESSURE DURING CLIMB OUT. RAN QRH. MESSAGE REMAINED. (FLIGHT 6481) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 32805095. REF CP 32808417 FOR CORRECTIVE ACTION AND WORK PERFORMED.
- [SDR SWI2026F00081](https://openairdocs.org/sdr/SWI2026F00081.md): Warning Message · illuminated · Jan 18, 2026 · N755EV · Cndair CL6002C10 · Door Warning System
  > PASSENGER DOOR WARNING RECEIVED IN FLIGHT. RAN QRH PROCEDURE. FLIGHT ATTENDANT REPORTED A POPPING NOISE FROM THE MCD IN FLIGHT BEFORE WARNING RECEIVED. (FLIGHT 4957) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31562889 WITH THE FOLLOWING CORRECTIVE ACTION:
- [SDR SWI2026F00079](https://openairdocs.org/sdr/SWI2026F00079.md): Warning Message · activated · Jan 18, 2026 · N755EV · Cndair CL6002C10 · Door Warning System
  > PASSENGER DOOR WARNING RECEIVED IN FLIGHT. RAN QRH PROCEDURE. FLIGHT ATTENDANT REPORTED A POPPING NOISE FROM THE MCD IN FLIGHT BEFORE WARNING RECEIVED. (FLIGHT 4957) OPEN
- [SDR SWIA2024110831](https://openairdocs.org/sdr/SWIA2024110831.md): Latch · cracked · Oct 31, 2024 · N755EV · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > RH AFT TRU BAY LATCH RECESS APPEARS TO BE CRACKED IN TWO LOCATION. (C-CHECK RO 11/6/2024) STOP DRILLED CRACK AT RH AFT TRU BAY LATCH AND COMPLIED WITH ALL STEPS OF REO 670-53-11-2044 REV--, DATED 2024-11-01. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA20241108012](https://openairdocs.org/sdr/SWIA20241108012.md): Floor Support · corroded · Oct 12, 2024 · N755EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > GALLEY 1 MOST FWD INBD FLOOR STRUCTURE MOUNT IS CORRODED. (MARKED) MX # 28984538. (C-CHECK RO 11-6/2024) REMOVED AND REPLACED NEW PLATE FITTING ON GALLEY 1 MOST FWD INBD FLOOR STRUCTURE MOUNT AT FS485 RBL15 REF CRJ700 SRM 51-42-21-001-001-A01 AND DRW# S
- [SDR SWIA2024110803](https://openairdocs.org/sdr/SWIA2024110803.md): Slider · damaged · Oct 3, 2024 · N755EV · Cndair CL6002C10 · Engine Thrust Reverser
  > COMPLY WITH REO 670-54-22-088 REV A, FOR DAMAGE TO LH ENGINE UPPER C-DUCT TRANSCOWL SLIDER MOUNT HOLE. (C-CHECK RO 11/6/2024) COMPLIED WITH ALL STEPS OF REO 670-54-22-088 REV A DATED 2024-10-02, FOR DAMAGE TO LH ENGINE UPPER C-DUCT TRANSCOWL SLIDER MO
- [SDR SWI2024F01190](https://openairdocs.org/sdr/SWI2024F01190.md): Duct · gouged · Sep 20, 2024 · N755EV · Cndair CL6002C10 · Engine Thrust Reverser
  > LH LOWER THRUST REVERSER C-DUCT GOUGED NEAR FLOATING TIE BAR ATTACHING POINTS (C-CHECK RO 11-6/2024) BLENDED-OUT GOUGED AND RESTORED FINISH REWORKED AREA ON LH LOWER THRUST REVERSER C-DUCT NEAR FLOATING TIE BAR ATTACHING POINTS, COMPLIED TO ALL STEPS
- [SDR SWIA20241108920](https://openairdocs.org/sdr/SWIA20241108920.md): Duct · gouged · Sep 20, 2024 · N755EV · Cndair CL6002C10 · Engine Thrust Reverser
  > LH UPPER THRUST REVERSER C-DUCT, GOUGED NEAR FLOATING TIE BAR ATTACHING POINTS (C-CHECK RO 11-6/2024) BLENDED-OUT GOUGED AND RESTORED FINISH TO REWORKED AREA ON LH UPPER THRUST REVERSER C-DUCT NEAR FLOATING TIE BAR ATTACHING POINTS, COMPLIED TO ALL STE
- [SDR SWIA20241108915](https://openairdocs.org/sdr/SWIA20241108915.md): Frame · corroded · Sep 15, 2024 · N755EV · Cndair CL6002C10 · Fuselage Main, Frame
  > AFT CARGO BELOW FLOOR HAS CORROSION ON FRAME FS1051.30 RBL2 MX# 28848636 (C-CHECK RO 11/6/2024) PERFORMED SPLICE REPAIR FOR CORROSION DAMAGE TO FS1051.30 LOWER FRAME SECTOR BETWEEN STR26L-STR25R REF REO 670-53-61-2372,REV --, DATED 2024-09-24, CRJ700 S
- [SDR SWIA20241108907](https://openairdocs.org/sdr/SWIA20241108907.md): Frame · cracked · Sep 7, 2024 · N755EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME FS333.00 BETWEEN STGR 1R-2R CRACKED CAMP 28807442 (C-CHECK RO 11/6/2024) COMPLIED WITH ALL STEPS 1-20. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS AT FS333- STGR1R - STGR2R REF REO 670-53-21-2457 REV -A DATE 2024-09-25. COMPLIED WI
- [SDR SWI2024F01189](https://openairdocs.org/sdr/SWI2024F01189.md): Skin · damaged · Sep 6, 2024 · N755EV · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO DOOR EXTERNAL SKIN HAS EDGE DAMAGE ON THE LWR AFT CORNER (C-CHECK RO 11/6/2024) REPAIRED AFT CARGO DOOR EXTERNAL SKIN DAMAGE REF REO 670-52-31-147 REV.--, DATED 2024-09-12. COMPLIED WITH AALL STEPS OF REO 670-52-31-147 REV.--, DATED 2024-09-12
- [SDR SWIA20241108906](https://openairdocs.org/sdr/SWIA20241108906.md): Skin · corroded · Sep 6, 2024 · N755EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN UNDER AFT DRAIN MAST IS CORRODED. CAMP# 28804960 (C-CHECK RO 11-6/2024) REMOVED CORROSION FROM FUSELAGE SKIN UNDER AFT DRAIN MAST, COMPLIED TO ALL THE STEPS REF REO 670-53-61-2365 REV-- DATED 2024-09-12. COMPLIED WITH TASK CARD 51-900-1002
- [SDR SWI2024F01198](https://openairdocs.org/sdr/SWI2024F01198.md): Slider · chafed · Sep 4, 2024 · N755EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LOWER TRANSCOWL OUTBD SLIDER CHAFED AT FWD END. (C-CHECK RO 11-6/2024) COMPLIED WITH CRJ 700 REO# 670-54-21-1659, REV --, DATED 9/11/24 FOR L/H LOWER TRANSCOWL OUTBD SLIDER. COMPLIED WITH MANUAL EXTENSION/RETRACTION OF THE LH ENGINE LOWER THRUST RE
- [SDR SWI2024F01197](https://openairdocs.org/sdr/SWI2024F01197.md): Slider · chafed · Sep 4, 2024 · N755EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LOWER TRANSCOWL INBD SLIDER CHAFED AT FWD END. (C-CHECK RO 11-6/2024) COMPLIED WITH CRJ 700 REO# 670-54-21-1659, REV --, DATED 9/11/24. COMPLIED WITH MANUAL EXTENSION/RETRACTION OF THE LH ENGINE THRUST REVERSER REF CRJ 700 AMM TASK 78-30-00-980-801
- [SDR SWI2024F01196](https://openairdocs.org/sdr/SWI2024F01196.md): Coaming · chafed · Sep 4, 2024 · N755EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LOWER TRANSCOWL LATCH COAMING CHAFED AT FWD EDGE BY FWD LATCH. (C-CHECK RO 11-6/2024) COMPLIED W/FINAL VERSION OF MHIRJ REO 670-54-21-1660, REV --, DATED 9/24/24. ALL STEPS OF REO COMPLETED IN THEIR ENTIRETY. SEE CONTINUATION STEPS FOR MORE DETAILS.
- [SDR SWIA20241108904](https://openairdocs.org/sdr/SWIA20241108904.md): Bracket · cracked · Sep 4, 2024 · N755EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL INBD "A" BRACKET STIFFENER CRACKED. (C-CHECK RO 11-6/2024) REMOVED AND REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD
- [SDR SWI2024F01188](https://openairdocs.org/sdr/SWI2024F01188.md): Floorbeam · corroded · Aug 30, 2024 · N755EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > R/H RBL 9 FLOOR BEAM CORRODED ON TOP FROM APROX FS 477- FS 570 MARKED (C-CHECK RO 11-6/2024) REPAIRED RH RBL9 FLOOR BEAM FROM APPROX FS477-FS570 REF-CRJ 700 REO 670-53-31-937 REV -- DATED 2024-09-12, EO NO: CL-600-2C10-53-L08306 REV.IR DATED 10/3/2024,
- [SDR SWIA2024110830](https://openairdocs.org/sdr/SWIA2024110830.md): Floorbeam · corroded · Aug 30, 2024 · N755EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > R/H RBL 9 FLOOR BEAM CORRODED ON TOP FROM APROX FS 570 TO FS 680 MARKED (C-CHECK RO 11-6/2024) REPAIRED RBL 9 FLOOR BEAM APROX FS 570 TO FS 680. COMPLIED WITH ALL STEPS OF CRJ 700 SRM 53-00-41-201-001-A01, AND REO 670-53-31-950 REV:-A DATE: 2024-10-07,
- [SDR SWI2024F01170](https://openairdocs.org/sdr/SWI2024F01170.md): Frame Splice · corroded · Aug 29, 2024 · N755EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME SPLICE STRAP IS CORRODED AT FS319 APPROX. WL72 (RH SIDE) (C-CHECK RO 11-6/2024) REMOVED AND REPLACED NEW FRAME SPLICE BRACKET LOCATED AT FS319.00 APPROX. WL72, R/H SIDE, FLOOR LEVEL REF CRJ 700 SRM 51-42-21-001-001-A01 AND SRM 51-42-13-001-001
- [SDR SWI2024F01169](https://openairdocs.org/sdr/SWI2024F01169.md): Slat Track · worn · Aug 29, 2024 · N755EV · Cndair CL6002C10 · Leading Edge Devices
  > LH WING SLAT TRACK 3-3 HAS WEAR GROVES ON LOWER SURFACE (C-CHECK RO 11-6/2024) BLENDED OUT WEAR GROVES, AT LH WING SLAT TRACK 3-3, ON LOWER SURFACE, 4EA SPOTS, REF. CRJ-700, SRM 51-12-00-001-001-A01. AND FOUND NO LIMITS IN SRM AND COMPLIED WITH ALL STEP
- [SDR SWIA2024110829](https://openairdocs.org/sdr/SWIA2024110829.md): Slat Track · worn · Aug 29, 2024 · N755EV · Cndair CL6002C10 · Leading Edge Devices
  > LH WING SLAT TRACK 1-1 HAS WEAR GROVES ON LOWER SURFACE (C-CHECK RO 11-6/2024) BLENDED OUT WEAR GROVES, AT LH WING SLAT TRACK 1-1, ON LOWER SURFACE, 3EA SPOTS, REF. CRJ-700, SRM 51-12-00-001-001-A01. AND FOUND NO LIMITS IN SRM AND COMPLIED WITH ALL STEP
- [SDR SWI2024F01195](https://openairdocs.org/sdr/SWI2024F01195.md): Guide · chafed · Aug 28, 2024 · N755EV · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO DOOR SURROUND GUIDE FITTINGS CHAFED (MARKED). (C-CHECK RO 11-6/2024) REPAIRED DAMAGE TO AFT CARGO DOOR SURROUND GUIDE FITTINGS REF REO-670-53-61-2361 REV -- DATE 2024-09-10, BY COMPLYING WITH ALL STEPS. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2024110828](https://openairdocs.org/sdr/SWIA2024110828.md): Doubler · gouged · Aug 28, 2024 · N755EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > AFT LOWER SKIN DOUBLER REPAIR HAS SEVERAL GOUGES FROM WING TO BODY FAIRING (C-CHECK RO 11-6/2024) REMOVED AND REPLACED EXISTING DOUBLER REPAIR AT AFT LOWER SKIN WING TO BODY FAIRING REF REO 670-53-00-290, REV -F, DATED 2019/04/26. PRESSURE LEAK CHECK GO
- [SDR SWI2024F01187](https://openairdocs.org/sdr/SWI2024F01187.md): Skin · corroded · Aug 27, 2024 · N755EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > INNER CLOSING SKIN HAS CORROSION IN MULTIPLE AREAS FS536.00 - 578.00 STGR25L. (MARKED IN RED) (C-CHECK RO 11-6/2024) REMOVED CORROSION FROM INNER CLOSING SKIN IN MULTIPLE AREAS FS536.00 - 578.00 STGR25L PER CRJ700 SRM 51-21-06-001-001-A01 AND FOUND TO B
- [SDR SWI2024F01186](https://openairdocs.org/sdr/SWI2024F01186.md): Track · gouged · Aug 27, 2024 · N755EV · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO DOOR FWD TRACK ASSY HAS MULTIPLE AREAS GOUGED (C-CHECK RO 11-6/2024) REMOVED AND REPLACED AFT BAGGAGE BAY DOOR FWD TRACK ASSEMBLY REF. CRJ 700 SRM 53-61-58-001-001-A01 AND CRJ 700 SRM 53-61-58-201-002-A01. OPS TEST GOOD. COMPLIED WITH TASK CAR
- [SDR SWI2024F01185](https://openairdocs.org/sdr/SWI2024F01185.md): Door Frame · corroded · Aug 27, 2024 · N755EV · Cndair CL6002C10 · Fuselage Main, Structure
  > FORWARD BAGGAGE BAY SURROUND STRUCTURE - FORWARD INNER UPPER JOINT PLATE HAS MULTIPLE AREAS OF CORROSION. (MARKED IN RED) (C-CHECK RO 11-6/2024) REMOVED AND REPLACED WITH NEW FWD BAGGAGE BAY SURROUND FWD INNER JOINT PLATE REF CRJ700 SRM 51-42-21-001-001
- [SDR SWI2024F01184](https://openairdocs.org/sdr/SWI2024F01184.md): Track · gouged · Aug 27, 2024 · N755EV · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO DOOR AFT TRACK ASSY HAS MULTIPLE AREAS GOUGED (C-CHECK RO 11-6/2024) REMOVED AND REPLACED AFT BAGGAGE BAY DOOR AFT TRACK ASSEMBLY REF. CRJ 700 SRM 53-61-58-201-002-A01 AND CRJ 700 SRM 53-61-58-201-002-A01. OPS TEST GOOD. COMPLIED WITH TASK CAR
- [SDR SWI2024F01183](https://openairdocs.org/sdr/SWI2024F01183.md): Drain Mast · corroded · Aug 27, 2024 · N755EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT CARGO BELOW FLOOR DRAIN MAST CHANNEL HAS CORROSION (C-CHECK RO 11-6/2024) EVALUATED CORROSION AND FOUND TO BE BEYOND LIMITS PER CRJ700 SRM 53-61-04-101-003-A01. FABRICATED AND INSTALLED NEW CHANNEL AT AFT CARGO BELOW FLOOR DRAIN MAST REF CRJ700 SRM
- [SDR SWI2024F01182](https://openairdocs.org/sdr/SWI2024F01182.md): Angle · corroded · Aug 27, 2024 · N755EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SPLICE ANGLE ON STGR26R BETWEEN FS333.00 & FS349.00 HAS AREAS OF CORROSION. (C-CHECK RO 11-6/2024) BLENDED OUT CORROSION ON SPLICE ANGLE, STGR26R BETWEEN FS333.00 AND FS349.00. REF CRJ 700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS. REMOVED AN
- [SDR SWI2024F01181](https://openairdocs.org/sdr/SWI2024F01181.md): Door Frame · damaged · Aug 27, 2024 · N755EV · Cndair CL6002C10 · Fuselage Main, Structure
  > FORWARD CARGO DOOR SURROUND STRUCTURE - INNER SKIN BETWEEN THE FORWARD AND AFT JOINT PLATES HAS DAMAGE ON THE EDGE BEHIND THE FORWARD AND AFT DOOR HINGES. (MARKED IN RED) (C-CHECK RO 11-6/2024) REPAIRED FORWARD CARGO DOOR SURROUND STRUCTURE - INNER SKIN
- [SDR SWI2024F01180](https://openairdocs.org/sdr/SWI2024F01180.md): Door Frame · corroded · Aug 27, 2024 · N755EV · Cndair CL6002C10 · Fuselage Main, Structure
  > FORWARD BAGGAGE BAY SURROUND STRUCTURE - AFT INNER JOINT PLATE HAS MULTIPLE AREAS OF CORROSION FS578.00 STGR25L. (MARKED IN RED) (C-CHECK RO 11-6/2024) REMOVED AFT INNER JOINT PLATE (LOWER EXTERNAL), FROM FORWARD BAGGAGE BAY SURROUND STRUCTURE, FS578.0
- [SDR SWIA2024110827](https://openairdocs.org/sdr/SWIA2024110827.md): Stringer · corroded · Aug 27, 2024 · N755EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR26R BETWEEN FS349.00 & 364.00. (MARKED IN RED) (C-CHECK RO 11-6/2024) BLENDED OUT CORROSION ON STGR 26R BETWEEN FS349.00 & FS364.00. REF CRJ 700 SRM 51-21-06-001-001-A01 AND FOUND DAMAGE ALLOWED IN AREA. REPAIRED USING REO 670-53-21-245
- [SDR SWI2024F01178](https://openairdocs.org/sdr/SWI2024F01178.md): Skin · gouged · Aug 24, 2024 · N755EV · Cndair CL6002C10 · Cargo/Baggage Doors
  > FWD BAG BAY DOOR INNER SKIN AND STRUCTURE GOUGED AND CHAFFED AT R/H FWD CORNER (MARKED) (C-CHECK RO 11-6/2024) REPAIRED CHAFFE ON FWD BAGGAGE BAY DOOR, INNER SKIN AND STRUCTURE AT R/H FWD CORNER AND COMPLIED ALL STEPS REF REO 670-52-35-503 REV.--, DATE
- [SDR SWIA2024110824](https://openairdocs.org/sdr/SWIA2024110824.md): Skin · gouged · Aug 24, 2024 · N755EV · Cndair CL6002C10 · Cargo/Baggage Doors
  > FWD BAG BAY DOOR INNER SKIN AND STRUCTURE GOUGED AND CHAFFED AT R/H AFT CORNER (MARKED) (C-CHECK RO 11-6/2024) REPAIRED FWD CARGO DOOR INNER SKIN AND EDGE FRAMES IAW REO 670-52-35-503 REV. -- DATED 2024-09-10 ALL STEPS 1 THRU 5. COMPLIED WITH TASK CARD
- [SDR SWI2024F01179](https://openairdocs.org/sdr/SWI2024F01179.md): Panel · corroded · Aug 23, 2024 · N755EV · Cndair CL6002C10 · Wing, Plate/Skin
  > PANEL 541DB HAS FRETTING CORROSION AT MULTIPLE POINTS ON THE PANEL (MARKED) MX#28736038 (C-CHECK RO 11-6/2024) REMOVED CORROSION ON INNER MATTING SURFACE AT PANEL 541DB REF CRJ700 SRM 51-21-06-001-001-A01 AND FOUND TO BE OUT OF LIMITS AND REPAIR REF REO
- [SDR SWI2024F01194](https://openairdocs.org/sdr/SWI2024F01194.md): Nut Plate · missing · Aug 22, 2024 · N755EV · Cndair CL6002C10 · Elevator Structure
  > R/H ELEVATOR PANEL HINGE 342BB HAS A MISSING NUT-PLATE WHERE MARKED. MX # 28730250. (C-CHECK RO 11-6/2024) REPAIRED R/H ELEVATOR PANEL HINGE 342BB RIB REF. EO NO: CL-600-2C10-55-L08260 REV: A DATE: 9/19/2024 AND CRJ 700 SRM 51-42-06-001-001-A01. SEE CO
- [SDR SWIA2024110822](https://openairdocs.org/sdr/SWIA2024110822.md): Hinge · damaged · Aug 22, 2024 · N755EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE (PAX SIDE) ROLL PIN INSERT HOLE ELONGATED (C-CHECK RO 11-6/2024) OPENED SPRING HOLE ON PASSENGER DOOR HINGE HALF TO 0.1285", RESTORED FINISH AND INSTALLED A NEW RETENTION SPRING PIN REF REO 670-52-11-1404 REV -- DATED 2024-09-10. ALL STEP
- [SDR SWIA2024110861](https://openairdocs.org/sdr/SWIA2024110861.md): Structure · damaged · Aug 21, 2024 · N755EV · Cndair CL6002C10 · Wing Main, Frame Structure
  > RH WING JACK PAD DOES NOT GO INTO THREADS TRANS#28722388 (C-CHECK RO 11-6/2024) REPLACED RH WING JACK PAD WITH A SERVICEABLE UNIT REF CRJ 700 SRM 51-42-21-001-001-A01 REV. 38, DATED JULY 25, 2020, DWG CC670-10004 REV.-F, DWG CC670-10038 REV.NC. LEAK CHE
- [SDR SWI2024F01161](https://openairdocs.org/sdr/SWI2024F01161.md): Pad · damaged · Aug 21, 2024 · N755EV · Cndair CL6002C10 · Wing Main, Frame Structure
  > RH WING JACK PAD DOES NOT GO INTO THREADS TRANS#28722388 (C-CHECK RO 11-6/2024) REPLACED RH WING JACK PAD WITH A SERVICEABLE UNIT REF CRJ 700 SRM 51-42-21-001-001-A01 REV. 38, DATED JULY 25, 2020, DWG CC670-10004 REV.-F, DWG CC670-10038 REV.NC. LEAK CHE
- [SDR SWIA20241108709](https://openairdocs.org/sdr/SWIA20241108709.md): None · none · Jul 9, 2024 · N755EV · Cndair CL6002C10 · Standard Practices/Structures
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA74310-670-54-22-037 N787SK MXCODEID59647-PR - ENLARGED HOLES, LOG NUMBER 56115, LINE NO. 11. PERFORMED TEMPORARY REPAIR OF ENLARGED HOLES BY ACCOMPLISHING INSTRUCTIONS IN REO 670-54-22-037,. FINAL HOLE IS 0.354. IN
- [SDR SWIA20241108215](https://openairdocs.org/sdr/SWIA20241108215.md): None · none · Feb 15, 2024 · N755EV · Cndair CL6002C10 · Standard Practices/Structures
  > COMPLY WITH: 670BA-53-040 - FUSELAGE - CENTER FUSELAGE, PRIMARY STRUCTURE FS280.00 TO FS295.00 - INSPECTION AND REINFORCEMENT OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR REV C PART(S) B (C-CHECK RO 11-6/2024) COMPLIED WITH: 670BA-53-040 - FUSELAGE
- [SDR SWIA2021081860360](https://openairdocs.org/sdr/SWIA2021081860360.md): Angle · cracked · Jul 28, 2021 · N755EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF F.S 333 FRAME AT STRINGER 21L, FOUND F.S 333 FRAME REINFORCEMENT ANGLE CRACKED. (C-CHECK RO 8/16/2021) REMOVED AND REPLACED CRACKED REINFORCEMENT ANGLE WITH NEW SERVICEABLE ANGLE AT FS333.00 L/H BETWEEN STGR'S 18L AND 21L USING ALL NEW
- [SDR SWIA2021081860359](https://openairdocs.org/sdr/SWIA2021081860359.md): Structure · chafed · Jul 27, 2021 · N755EV · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > RH LOWER TRANSCOWL SPIGOT HOLE CHAFED/WORN. (C-CHECK RO 8/16/2021) REPLACED DAMAGED RH LOWER TRANSCOWL SPIGOT HOLE/DOOR LATCH COAMING WITH NEW (P/N: CN624-2060-207) REF REO 670-54-21-1207, REV A DATED 2015-08-27. COMPLIED WITH ST 51-900-1002-SKY.
- [SDR SWIA2021081860358](https://openairdocs.org/sdr/SWIA2021081860358.md): Duct · damaged · Jul 15, 2021 · N755EV · Cndair CL6002C10 · Engine Thrust Reverser
  > RH ENGINE LOWER THRUST REVERSER C-DUCT, NYLON INSERT MOUNTING SCREW HOLES THROUGH METAL STRUCTURE ARE OBLONG / DAMAGED. (C-CHECK RO 8/16/2021) PERFORMED REPAIR OF RH ENGINE LOWER THRUST REVERSER C-DUCT NYLON ENLONGATED HOLES IAW REO 670-78-30-921 REV-B
- [SDR SWIA2021081860356](https://openairdocs.org/sdr/SWIA2021081860356.md): Stiffener · corroded · Jul 5, 2021 · N755EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LOWER FS250.00 STIFFENER CORRODED AT MULTIPLE AREAS (MARKED) BETWEEN STGR 23R TO STGR 23L. (C-CHECK RO 8/16/2021) LOWER FS250.00 STIFFENER CORROSION EVALUATED AS OUT-O-LIMITS WITH 100% MATERIAL LOSS. REMOVED STIFFENER AT FS250.00 BETWEEN STGR23R - STGR2
- [SDR SWIA2021081860355](https://openairdocs.org/sdr/SWIA2021081860355.md): Angle · cracked · Jul 3, 2021 · N755EV · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > LH UPPER TRANSCOWL "Z" ANGLE APPEARS TO BE DISBONDED. (C-CHECK RO 8/16/2021) LH UPPER TRANSCOWL Z ANGLE FOUND TO BE CRACKED. PERFORMED REPAIR TO LH UPPER TRANSCOWL "Z" ANGLE IAW ALL STEPS OF REO 670-54-21-1460 REV--, DATED 2021-08-02 AND CRJ700 SRM 51-4
- [SDR SWIA2021081860354](https://openairdocs.org/sdr/SWIA2021081860354.md): Structure · chafed · Jul 3, 2021 · N755EV · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > LH UPPER TRANSCOWL SPIGOT HOLE CHAFED/WORN. (C-CHECK RO 8/16/2021) REMOVED DAMAGE AND INSTALLED NEW LH UPPER TRANSCOWL DOOR LATCH COAMING AND SPIGOT DOUBLER PER REO 670-54-21-1207 REV-A, DATED 2015-08-27. COMPLIED WITH ST 51-900-1002-SKY
- [SDR SWIA2021081860353](https://openairdocs.org/sdr/SWIA2021081860353.md): Angle · cracked · Jul 3, 2021 · N755EV · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > RH LOWER TRANSCOWL "Z" ANGLE DISBONDED. (C-CHECK RO 8/16/2021) RH UPPER TRANSCOWL Z ANGLE FOUND TO BE CRACKED. PERFORMED REPAIR TO RH UPPER TRANSCOWL "Z" ANGLE IAW ALL STEPS OF REO 670-54-21-1461 REV--, DATED 2021-08-02 AND CRJ700 SRM 51-42-13-001-001-A
- [SDR SWIA2021081860352](https://openairdocs.org/sdr/SWIA2021081860352.md): Window Post · cracked · Jul 2, 2021 · N755EV · Cndair CL6002C10 · Fuselage Main, Structure
  > RH WINDSHIELD SIDE POST, CRACK RADIATING FORWARD OUT OF THE TOP BARREL NUT HOLE. (C-CHECK RO 8/16/2021) REMOVED AND REPLACED RH WINDSHIELD SIDE POST, REF. CRJ700 SRM 51-42-21-001-001-A01 AND DRAWING 601R33007 REV. U. PRESSURIZATION LEAK CHEAK GOOD. SEE
- [SDR SWIA2021081860351](https://openairdocs.org/sdr/SWIA2021081860351.md): Window Post · cracked · Jul 2, 2021 · N755EV · Cndair CL6002C10 · Fuselage Main, Structure
  > LH WINDSHIELD SIDE POST, CRACK RADIATING FORWARD OUT OF THE TOP BARREL NUT HOLE. (C-CHECK RO 8/16/2021) REMOVED AND REPLACED LH WINDSHIELD SIDE POST, REF. CRJ700 SRM 51-42-21-001-001-A01 AND DRAWING 601R3307 REV. U. PRESSURIZATION LEAK CHEAK GOOD. SEE C

Next page: https://openairdocs.org/aircraft/N755EV/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 = 'N755EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N755EV/reports

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