# Service difficulty reports: N744EV

A list on [N744EV](https://openairdocs.org/aircraft/N744EV.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 · 326 reports

- [SDR SWIA202412031104](https://openairdocs.org/sdr/SWIA202412031104.md): Fitting · misrepaired · Nov 4, 2024 · N744EV · Cndair CL6002C10 · Emergency Exits
  > INCORRECT MATERIAL USED ON JOB: HN00195752, MX TRANS #29021830 (RIGHT OVERWING EMERGENCY-EXIT DOOR - SUSPECTED CRACK AT THE AFT HOOK FITTING.) (C-CHECK RO 11/30/2024) REPAIRED CRACK AT THE R/H OVERWING EMER DOOR, AFT HOOK FITTING PER REO 670-52-21-104 R
- [SDR SWIA202412031103](https://openairdocs.org/sdr/SWIA202412031103.md): Floor Support · corroded · Nov 3, 2024 · N744EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > MULTIPLE SPOTS OF CORROSION ON THE RIGHT-HAND FLOOR SILL, BETWEEN FS280.00 - FS349.00. (C-CHECK RO 11/30/2024) REMOVED AND INSTALLED NEW R/H FLOOR SILL BETWEEN FS280.00 - FS349.00 REF EO # EO NO: CL-600-2C10-53-L08505 REV: IR DATE:2024.11.07 AND DWG# SH
- [SDR SWIA202412031024](https://openairdocs.org/sdr/SWIA202412031024.md): Skin · dented · Oct 24, 2024 · N744EV · Cndair CL6002C10 · Trailing Edge Flaps
  > MUTIPLE DENTS ON LWR SKIN OF R/H WING INBD FLAP. (C-CHECK RO 11/30/2024) MULTIPLE DENTS ON LWR SKIN OF R/H WING I/B FLAP HAVE BEEN REPAIRED REF CRJ 700 SRM 57-52-01-201-005-A01, FIG. 57-52-01-995-803, SHEET 1 AND 2. COMPLIED FULLY W/SKYCARD 51-900-1002-
- [SDR SWIA202412031020](https://openairdocs.org/sdr/SWIA202412031020.md): Shaft · chafed · Oct 20, 2024 · N744EV · Cndair CL6002C10 · Aileron Tabs
  > CHAFED QTY. 4 VANE ACTUATORS CHROME SHAFT AT RH WING INBOARD FLAP ( MARKED) MX# 29027622 JOB OP# HN00195957 (C-CHECK RO 11/30/2024) PERFORMED REPAIR TO RH INBD FLAP 4EA VANE ACTUATORS. PER REO 670-57-52-257 REV -A DATED 2024-08-20. OPS CHECKS GOOD. CO
- [SDR SWIA202412031019](https://openairdocs.org/sdr/SWIA202412031019.md): Fitting · cracked · Oct 19, 2024 · N744EV · Cndair CL6002C10 · Emergency Exits
  > RIGHT OVERWING EMERGENCY-EXIT DOOR - SUSPECTED CRACK AT THE AFT HOOK FITTING. (MARKED) (C-CHECK RO 11/30/2024) REPAIRED CRACK AT THE R/H OVERWING EMER DOOR, AFT HOOK FITTING PER REO 670-52-21-104 REV -A DATE 2024-10-28 BY IDENTIFYING CRACK LOCATION, REM
- [SDR SWIA202412031017](https://openairdocs.org/sdr/SWIA202412031017.md): Transcowl · cracked · Oct 17, 2024 · N744EV · Cndair CL6002C10 · Engine Thrust Reverser
  > R.H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 11/30/2024) INSTALLED 1 EA. NEW "A"-BRACKET P/N CN624-2082-201 ON INBD. SIDE OF R/H UPPER TRANS COWL. REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3, AND COMPLIED
- [SDR SWIA2024120301307](https://openairdocs.org/sdr/SWIA2024120301307.md): Frame · corroded · Oct 11, 2024 · N744EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME 349.00 AT STGR 25R HAS GALVANIC CORROSION TRANS 28980671 (C-CHECK RO 11/30/2024) UPON ATTEMPTING TO REMOVE THE CORROSION FROM FRAME 349.00 AT STGR 25R FOUND CORROSION TO BE 100% MATERIAL LOSS, FRAME 349.00 NEEDS TO BE REPAIRED. REF: CRJ-700 S.R.M
- [SDR SWIA2024120306](https://openairdocs.org/sdr/SWIA2024120306.md): Frame · corroded · Oct 11, 2024 · N744EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME 333.00 AT STGR 25R HAS GALVANIC CORROSION TRANS 28980680 (C-CHECK RO 11/30/2024) REMOVED CORROSION FROM THE FRAME 333.00 AT STGR 25R REF: CRJ-700 S.R.M.51-21-06-001-001- A01. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW FRAME SECTOR AND A
- [SDR SWIA2024120301348](https://openairdocs.org/sdr/SWIA2024120301348.md): Stringer · corroded · Oct 10, 2024 · N744EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 25R BETWEEN FS333.00 - 364.00 HAS CORROSION TRANS 28971183 (C-CHECK RO 11/30/2024) REMOVED AND INSTALLED NEW STRINGER BETWEEN F.S. 333.00 AND F.S. 364.00 REF: CRJ-700 S.R.M. 51-42-06-001-001-A01, 51-42-21-001-001-A01, DWG-SH670-32103 REV-A. COMPLIE
- [SDR SWIA202412031010](https://openairdocs.org/sdr/SWIA202412031010.md): Stringer · corroded · Oct 10, 2024 · N744EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 25R BETWEEN FS280.00 - FS333.00 HAS CORROSION TRANS 28971174 (C-CHECK RO 11/30/2024) REMOVED AND INSTALLED NEW STRINGER BETWEEN F.S. 280.00 AND F.S. 333.00 REF: CRJ-700 S.R.M. 51-42-06-001-001-A01, 51-42-21-001-001-A01, DWG-SH670-31212 REV -NC. COM
- [SDR SWIA2024120301342](https://openairdocs.org/sdr/SWIA2024120301342.md): Hinge · grooved · Oct 9, 2024 · N744EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE (DOOR SIDE) HAS GROVES AT THE LUG LAND BETWEEN LUGS 15-23, 24-25, 26-27 (C-CHECK RO 11/30/2024) REPAIRED PAX DOOR HINGE DOOR SIDE IAW CRJ 700 SRM 52-11--01-201-007-A01 AND COMPLIED WITH TASK CARD 51-900-1002-SKY (CL600-2C10).
- [SDR SWIA20241203009](https://openairdocs.org/sdr/SWIA20241203009.md): Spar · corroded · Oct 9, 2024 · N744EV · Cndair CL6002C10 · Wing Spar
  > STRUCTURAL CORROSION ON MATING SURFACES INSIDE AUXILIARY SPAR SECTION BEHIND PANEL 642AZ. (C-CHECK RO 11/30/2024) REMOVED CORRODED AND INSTALLED NEW RETAINING ANGLE PN CC670-10338-2 FOR PANEL 642AZ AT R/H WING AUX SPAR PER CRJ700 SRM TASK 51-42-21-001-0
- [SDR SWIA2024120301347](https://openairdocs.org/sdr/SWIA2024120301347.md): Skin · chafed · Oct 5, 2024 · N744EV · Cndair CL6002C10 · Ailerons
  > RIGHT AILERON UPPER LEADING EDGE HAS CHAFING IN MULTIPLE AREAS. (MARKED IN RED) (C-CHECK RO 11/30/2024) REMOVED AND INSTALLED NEW UPPER LEADING EDGE SKIN P/N CC670-13052-4, LOCATED, FIT, DRILLED AND COUNTERSUNK IAW CRJ 700 SRM 51-40-11-001-001-A01. FIT
- [SDR SWIA2024120301346](https://openairdocs.org/sdr/SWIA2024120301346.md): Hinge · grooved · Oct 5, 2024 · N744EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE ON THE FUSELAGE SIDE LAND 27 IS GROOVED. (C-CHECK RO 11/30/2024) REPAIRED PAX DOOR HINGE FUSELAGE SIDE LAND #27 IAW CRJ 700 SRM 53-21-23-201-010-A01 TYPE IV. COMPLIED WITH TASK CARD 51-900-1002-SKY (CL600-2C10) AND FORM M-337.
- [SDR SWIA2024120305](https://openairdocs.org/sdr/SWIA2024120305.md): Hinge · grooved · Oct 5, 2024 · N744EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASSENGER DOOR HINGE ON THE DOOR LUGS 24 TO 27 HAVE GROOVING DAMAGE. (MARKED IN RED) (C-CHECK RO 11/30/2024) REPAIRED PAX DOOR HINGE ON THE DOOR LUGS 24 TO 27 IAW CRJ 700 SRM 52-11-01-201-007-A01 AND COMPLIED WITH TASK CARD 51-900-1002-SKY (CL600-2C10).
- [SDR SWIA2024120301327](https://openairdocs.org/sdr/SWIA2024120301327.md): Stringer · corroded · Sep 27, 2024 · N744EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR26R HAS CORROSION AROUND ONE FASTENER BETWEEN FS453.00 & FS469.00. (MARKED) (C-CHECK RO 11/30/2024) REPAIRED CORROSION ON STGR26R ON FASTENERS BETWEEN FS469.00-FS485.00 REF REO 670-53-21-2474, REV -- DATE 2024-10-15. SEE CONTINUATION FOR DETAILS. CO
- [SDR SWIA2024120301326](https://openairdocs.org/sdr/SWIA2024120301326.md): Frame · corroded · Sep 27, 2024 · N744EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME FS295.00 HAS CORROSION ON THE LOWER FLANGE STGR25L - 24R. (MARKED) (C-CHECK RO 11/30/2024) REMOVED CORROSION FROM LOWER FLANGE COMMON TO BELLY SKIN, AT FS295.00 BETWEEN STGR25L - STGR24R, AND EVALUATED AS 'OUT-OF-LIMITS'. REPAIRED FRAME FLANGE. RE
- [SDR SWIA2024120301325](https://openairdocs.org/sdr/SWIA2024120301325.md): Frame · corroded · Sep 27, 2024 · N744EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME FS310.00 HAS CORROSION ON THE UPPER FLANGE FROM STGR24L - STGR26R. (MARKED) (C-CHECK RO 11/30/2024) REMOVED CORROSION FROM FRAME UPPER FLANGE AT FS310.00 STGR24L-STGR26R PER CRJ700SRM 51-21-06-001-001-A01 AND FOUND OUT OF LIMITS. REPAIRED FRAME PE
- [SDR SWIA2024120301324](https://openairdocs.org/sdr/SWIA2024120301324.md): Plate · corroded · Sep 27, 2024 · N744EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD CARGO DOOR SURROUND STRUCTURE FORWARD JOINT PLATE FS535.00 STGR25L HAS CORROSION AROUND MULTIPLE FASTENERS. (MARKED) (C-CHECK RO 11/30/2024) REMOVED CORROSION FROM THE FWD CARGO SURROUND STRUCTURE JOINT PLATE AT FS535.00 AND FOUND NO DAMAGE ALLO
- [SDR SWIA202412030927](https://openairdocs.org/sdr/SWIA202412030927.md): Stringer Splice · corroded · Sep 27, 2024 · N744EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE FS333.00 STGR25R HAS GALVANIC CORROSION. (C-CHECK RO 11/30/2024) REMOVED CORROSION FROM STRINGER SPLICE AT FS333.00, STGR25R. STRINGER SPLICE HAD 100% MATERIAL LOSS. REPLACED STRINGER SPLICE WITH NEW STRINGER SPLICE. REF. CRJ700 SRM 51
- [SDR SWIA20241203924](https://openairdocs.org/sdr/SWIA20241203924.md): Slat Track · worn · Sep 24, 2024 · N744EV · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 2-3 HAS 1 AREA WITH WEAR MARKS. (MARKED) (C-CHECK RO 11/30/2024) REMOVED WEAR MARKS FROM R/H SLAT TRACK 2-3 PER CRJ700SRM 51-12-00-001-001-A01 AND FOUND NO PUBLISHED LIMITS. REPAIRED R/H SLAT TRACK 2-3 PER REO 670-57-42-1761 REV -- DATE
- [SDR SWIA202412031338](https://openairdocs.org/sdr/SWIA202412031338.md): Slat Track · worn · Sep 24, 2024 · N744EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 2-3 HAS 1 AREA WITH WEAR MARKS. (MARKED) (C-CHECK RO 11/30/2024) REMOVED WEAR MARKS FROM L/H SLAT TRACK 2-3 PER CRJ700SRM 51-12-00-001-001-A01 AND FOUND NO PUBLISHED LIMITS. REPAIRED L/H SLAT TRACK 2-3 PER REO 670-57-42-1774 REV -- DATE
- [SDR SWIA202412031337](https://openairdocs.org/sdr/SWIA202412031337.md): Slat Track · damaged · Sep 24, 2024 · N744EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 2-2 HAS 2 AREAS WITH LIGHT PITTING. (MARKED) (C-CHECK RO 11/30/2024) REMOVED PITTING CORROSION FROM L/H SLAT TRACK 2-2 PER CRJ700SRM 51-21-06-001-001-A01 AND FOUND NO PUBLISHED LIMITS. REPAIRED L/H SLAT TRACK 2-2 PER REO 670-57-42-1767
- [SDR SWIA202412031336](https://openairdocs.org/sdr/SWIA202412031336.md): Slat Track · worn · Sep 24, 2024 · N744EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 2-1 HAS 1 AREA WITH WEAR MARKS. (MARKED) (C-CHECK RO 11/30/2024) REMOVED WEAR MARKS FROM L/H SLAT TRACK 2-1 PER CRJ700SRM 51-12-00-001-001-A01 AND FOUND NO PUBLISHED LIMITS. REPAIRED L/H SLAT TRACK 2-1 PER REO 670-57-42-1773 REV -- DATE
- [SDR SWIA202412031335](https://openairdocs.org/sdr/SWIA202412031335.md): Slat Track · damaged · Sep 24, 2024 · N744EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 1-2 HAS 2 AREAS WITH LIGHT PITTING. (MARKED) (C-CHECK RO 11/30/2024) REMOVED PITTING CORROSION FROM L/H SLAT TRACK 1-2 PER CRJ700SRM 51-21-06-001-001-A01 AND FOUND NO PUBLISHED LIMITS. REPAIRED L/H SLAT TRACK 1-2 PER REO 670-57-42-1764 R
- [SDR SWIA202412031334](https://openairdocs.org/sdr/SWIA202412031334.md): Slat Track · worn · Sep 24, 2024 · N744EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 1-1 HAS 1 AREA WITH WEAR MARKS. (MARKED) (C-CHECK RO 11/30/2024) REMOVED WEAR MARKS FROM L/H SLAT TRACK 1-1 PER CRJ700SRM 51-12-00-001-001-A01 AND FOUND NO PUBLISHED LIMITS. REPAIRED L/H SLAT TRACK 1-1 PER REO 670-57-42-1769 REV -- DATE
- [SDR SWIA2024120301341](https://openairdocs.org/sdr/SWIA2024120301341.md): Slat Track · worn · Sep 24, 2024 · N744EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 3-3 HAS 1 AREA WITH WEAR MARKS. (MARKED) (C-CHECK RO 11/30/2024) REMOVED WEAR MARKS FROM L/H SLAT TRACK 3-3 PER CRJ700SRM 51-12-00-001-001-A01 AND FOUND NO PUBLISHED LIMITS. REPAIRED L/H SLAT TRACK 3-3 PER REO 670-57-42-1776 REV -- DATE
- [SDR SWIA2024120301340](https://openairdocs.org/sdr/SWIA2024120301340.md): Slat Track · damaged · Sep 24, 2024 · N744EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 3-2 HAS 2 AREA WITH LIGHT PITTING. (MARKED) (C-CHECK RO 11/30/2024) REMOVED PITTING CORROSION FROM L/H SLAT TRACK 3-2 PER CRJ700SRM 51-21-06-001-001-A01 AND FOUND NO PUBLISHED LIMITS. REPAIRED L/H SLAT TRACK 3-2 PER REO 670-57-42-1777 R
- [SDR SWIA2024120301339](https://openairdocs.org/sdr/SWIA2024120301339.md): Slat Track · damaged · Sep 24, 2024 · N744EV · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 3-1 HAS 1 AREA WITH LIGHT PITTING. (MARKED) (C-CHECK RO 11/30/2024) REMOVED PITTING CORROSION FROM L/H SLAT TRACK 3-1 PER CRJ700SRM 51-21-06-001-001-A01 AND FOUND NO PUBLISHED LIMITS. REPAIRED L/H SLAT TRACK 3-1 PER REO 670-57-42-1775 R
- [SDR SWIA2024120301333](https://openairdocs.org/sdr/SWIA2024120301333.md): Slat Track · worn · Sep 24, 2024 · N744EV · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 3-1 HAS 2 AREA WITH WEAR MARKS. (MARKED) (C-CHECK RO 11/30/2024) REMOVED WEAR MARKS FROM R/H SLAT TRACK 3-1 PER CRJ700SRM 51-12-00-001-001-A01 AND FOUND NO PUBLISHED LIMITS. REPAIRED R/H SLAT TRACK 3-1 PER REO 670-57-42-1768 REV -- DATE
- [SDR SWIA2024120301332](https://openairdocs.org/sdr/SWIA2024120301332.md): Slat Track · damaged · Sep 24, 2024 · N744EV · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 3-2 HAS 1 AREA WITH LIGHT PITTING. (MARKED) (C-CHECK RO 11/30/2024) REMOVED PITTING CORROSION FROM R/H SLAT TRACK 3-2 PER CRJ700SRM 51-21-06-001-001-A01 AND FOUND NO PUBLISHED LIMITS. REPAIRED R/H SLAT TRACK 3-2 PER REO 670-57-42-1758
- [SDR SWIA2024120301331](https://openairdocs.org/sdr/SWIA2024120301331.md): Slat Track · damaged · Sep 24, 2024 · N744EV · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 2-2 HAS 2 AREAS WITH LIGHT PITTING. (MARKED) (C-CHECK RO 11/30/2024) REMOVED PITTING CORROSION FROM R/H SLAT TRACK 2-2 PER CRJ700SRM 51-21-06-001-001-A01 AND FOUND NO PUBLISHED LIMITS. REPAIRED R/H SLAT TRACK 2-2 PER REO 670-57-42-1770
- [SDR SWIA2024120301330](https://openairdocs.org/sdr/SWIA2024120301330.md): Slat Track · damaged · Sep 24, 2024 · N744EV · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 1-2 HAS 1 AREA WITH LIGHT PITTING. (MARKED) (C-CHECK RO 11/30/2024) REMOVED PITTING CORROSION FROM R/H SLAT TRACK 1-2 PER CRJ700SRM 51-21-06-001-001-A01 AND FOUND NO PUBLISHED LIMITS. REPAIRED R/H SLAT TRACK 1-2 PER REO 670-57-42-1757 R
- [SDR SWIA2024120301329](https://openairdocs.org/sdr/SWIA2024120301329.md): Slat Track · damaged · Sep 24, 2024 · N744EV · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 1-1 HAS 1 AREA WITH LIGHT PITTING. (MARKED) (C-CHECK RO 11/30/2024) REMOVED PITTING CORROSION FROM R/H SLAT TRACK 1-1 PER CRJ700SRM 51-21-06-001-001-A01 AND FOUND NO PUBLISHED LIMITS. REPAIRED R/H SLAT TRACK 1-1 PER REO 670-57-42-1784 R
- [SDR SWIA2024120301328](https://openairdocs.org/sdr/SWIA2024120301328.md): Slat Track · worn · Sep 24, 2024 · N744EV · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 1-1 HAS 1 AREA WITH WEAR MARKS. (MARKED) (C-CHECK RO 11/30/2024) REMOVED WEAR MARKS FROM R/H SLAT TRACK 1-1 PER CRJ700SRM 51-12-00-001-001-A01 AND FOUND NO PUBLISHED LIMITS. REPAIRED R/H SLAT TRACK 1-1 PER REO 670-57-42-1784 REV -- DATE
- [SDR SWIA2024120301290](https://openairdocs.org/sdr/SWIA2024120301290.md): Bushing · gouged · Sep 23, 2024 · N744EV · Cndair CL6002C10 · Trailing Edge Flaps
  > LH FLAP HINGE BOX ASSEMBLY AT WS178 UPPER PRESSED BUSHINGS 4EA ARE GOUGED AND CHAFED. REQUIRES REPLACEMENT. (C-CHECK RO 11/30/2024) REMOVED AND REPLACED LH FLAP HINGE BOX ASSEMBLY AT WS178 4EA UPPER PRESSED BUSHINGS REF CRJ700 AMM 20-31-00-000-801-A01 A
- [SDR SWIA2024120301289](https://openairdocs.org/sdr/SWIA2024120301289.md): Transcowl · cracked · Sep 23, 2024 · N744EV · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 11/30/2024) INSTALLED 1 EA. NEW "A"-BRACKET P/N CN624-2082-201. ON INBD. SIDE OF L/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3. AND COMPLIE
- [SDR SWIA2024120300923](https://openairdocs.org/sdr/SWIA2024120300923.md): Rivet · sheared · Sep 23, 2024 · N744EV · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL Z STIFFENER RIVETS ARE SHEARED (C-CHECK RO 11/30/2024) R/H LWR TRANSCOWL HAS BEEN REPAIRED REF REO# 670-54-21-1675, REV --, DATED 10-16-24. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY. REFER TO CONTINUATION SHEET FOR DETAILS.
- [SDR SWIA20241203288](https://openairdocs.org/sdr/SWIA20241203288.md): Beam · damaged · Sep 21, 2024 · N744EV · Cndair CL6002C10 · Wing Main, Frame Structure
  > LEFT INBOARD FLAP OUTBOARD FLAP VANE ACTUATOR BEAM HAS FLAT SPOTS ON LOWER SURFACE. (MARKED IN RED) (C-CHECK RO 11/30/2024) DAMAGE (FLAT SPOTS), REMOVED BY BLENDING FROM LEFT INBOARD FLAP, INBOARD FLAP VANE ACTUATOR BEAM (OUTER TUBE), UPPER AND LOWER S
- [SDR SWIA202412031288](https://openairdocs.org/sdr/SWIA202412031288.md): Beam · damaged · Sep 21, 2024 · N744EV · Cndair CL6002C10 · Wing Main, Frame Structure
  > LEFT INBOARD FLAP OUTBOARD FLAP VANE ACTUATOR BEAM HAS FLAT SPOTS ON LOWER SURFACE. (MARKED IN RED) (C-CHECK RO 11/30/2024) DAMAGE (FLAT SPOTS), REMOVED BY BLENDING FROM LEFT INBOARD FLAP, INBOARD FLAP VANE ACTUATOR BEAM (OUTER TUBE), UPPER AND LOWER S
- [SDR SWIA20241203919](https://openairdocs.org/sdr/SWIA20241203919.md): Vane · chafed · Sep 19, 2024 · N744EV · Cndair CL6002C10 · Trailing Edge Flaps
  > LH INBD FLAP VANE L/E IS CHAFED AT APPROX. WS 80 (C-CHECK RO 11/30/2024) REMOVED AND REPLACED WITH NEW LH INBD FLAP CENTER VANE AT APPX WS80 REF CRJ700 SRM 51-42-13-001-001-A01 AND DWG CC670-14010, REV -F. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SK
- [SDR SWIA20241203916](https://openairdocs.org/sdr/SWIA20241203916.md): Drag Angle · cracked · Sep 16, 2024 · N744EV · Cndair CL6002C10 · Vertical Stabilizer
  > RH FWD DRAG ANGLE AT ROOT OF VERTICAL STAB. HAS POSSIBLE CRACK AT AFT SIDE IN RADIUS (MARKED). (C-CHECK RO 11/30/2024) REMOVED CRACKED DRAG ANGLE AND REPAIRED WITH FABRICATED REPAIR PARTS ON FWD DRAG ANGLE AT RH ROOT OF VERTICAL STAB REF REO 670-55-31-0
- [SDR SWIA20241203912](https://openairdocs.org/sdr/SWIA20241203912.md): Skin · damaged · Sep 12, 2024 · N744EV · Cndair CL6002C10 · Trailing Edge Flaps
  > ADM # N744EV-8276 - L/H I/B FLAP LOWER SKIN, O/B FROM L1 FLAP HINGE FAIRING.25" I/B FROM WS 56.539 AND 4.25" FORWARD OF FLAP TRAILING EDGE. DAMAGE WITHIN LIMITS:.100L X.0800 W X.07D INCHES. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REW
- [SDR SWIA202266739](https://openairdocs.org/sdr/SWIA202266739.md): None · overheated · Nov 8, 2022 · N744EV · Cndair CL6002C10 · Master Cylinder/Brake Valve
  > BRAKE OVER HEAT MASTER WARNING IN DECENT. COME ON SHOWED 12 ON RIGHT INBOARD THE WENT TO 0, WENT AWAY. CAME BACK ON AT 20. FLOWED QRH STAYED RED 0 ALL THE WAY TO THE GATE. (FLIGHT 3083 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25769593
- [SDR SWIA202266208](https://openairdocs.org/sdr/SWIA202266208.md): None · odor · Jul 29, 2022 · N744EV · Cndair CL6002C10 · Air Conditioning System
  > ON APPROACH CREW DETECTED BURNING ELECTRICAL SMELL. AFTER LANDING NOTICED RECIRC FAN FAULT STATUS MESSAGE AND BREAKER 1A5 WAS POPPED. (FLIGHT #3226 FILED CLOSED) COMPLIED WITH FDE SMOKE SMELL IN THE COCKPIT REF CRJ 709 FIM 21-21-00. PERFORMED INSPECTION F
- [SDR SWIA202161605](https://openairdocs.org/sdr/SWIA202161605.md): Battery Pack · odor · Oct 5, 2021 · N744EV · Cndair CL6002C10 · Emergency Lighting
  > ON APPROACH TO DFW FAS REPORTED FUMES AND A VAGUE ELECTRICAL SMELL FROM ROWS 15 THROUGH 17. ROUGHLY 1 MINUTE LATER THE SMELL DISSIPATED AND WAS NOT PRESENT FOR REMAINDER OF FLIGHT. NO INDICATIONS OF SMOKE IN COCKPIT (FLIGHT 3086 - FILED CLOSED) TROUBLE-SH
- [SDR SWIA202160616](https://openairdocs.org/sdr/SWIA202160616.md): Skin · dented · Aug 4, 2021 · N744EV · Cndair CL6002C10 · Wing, Plate/Skin
  > LH LOWER WING SURFACE PN CC670-10046-5 HAS DENT DAMAGE @ WS 255 BETWEEN STR 11 & 12 (FILED CLOSED) REPAIRED L/H WING LOWER SKIN IAW MHIRJ REO 670-57-21-919 REV. -- DATED 8/6/2021. COMPLETED AND ATTACHED SKYWEST STRUCTURAL MAJOR REPAIR TASK 51-900-1003-SKY
- [SDR SWIA202160615](https://openairdocs.org/sdr/SWIA202160615.md): Skin · damaged · Aug 4, 2021 · N744EV · Cndair CL6002C10 · Trailing Edge Flaps
  > LH OB FLAP LOWER SKIN AND TRAILING EDGE DAMAGED BETWEEN FS 254.96 TO FS 262.76 (FILED CLOSED) REPAIRED L/H O/B FLAP LOWER SKIN AND T/E DAMAGE IAW CRJ-700 SRM 57-53-01-201-001-A01 TYPE IV REPAIR. COMPLETED AND ATTACHED SKYWEST STRUCTURAL MAJOR REPAIR TASK
- [SDR SWIA202052889](https://openairdocs.org/sdr/SWIA202052889.md): Floor Panel · cracked · Sep 17, 2020 · N744EV · Cndair CL6002C10 · Fuselage Floor Panel
  > COCKPIT PANEL 221KLW IS CRACKED. C-CHECK RO 9/27/2020. REMOVED & INSTALLED THE COCKPIT PANEL 221KLW, REF CRJ 700 AMM.
- [SDR SWIA202052888](https://openairdocs.org/sdr/SWIA202052888.md): Support · cracked · Sep 10, 2020 · N744EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LT MLG FAIRING DIAPHRAGM ASSY SUPPORT STRUCTURE CRACKED, MARKED. C-CHECK RO 9/27/2020. THE CRACKED LT MLG FAIRING DIAPHRAGM ASSY SUPPORT (P/N CC670-39205-5) HAS BEEN REPLACED WITH NEW AND INSTALLED WITH NEW HARDWARE, REF CRJ700 SRM.

Next page: https://openairdocs.org/aircraft/N744EV/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 = 'N744EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N744EV/reports

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