# Service difficulty reports: N908EV

A list on [N908EV](https://openairdocs.org/aircraft/N908EV.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 · 280 reports

- [SDR SWIA2026062176249](https://openairdocs.org/sdr/SWIA2026062176249.md): Diaphragm · dented · Jun 21, 2026 · N908EV · Cndair CL6002B19 · Passenger/Crew Doors
  > DENTED DAMAGE TO PASSENGER DOOR FWD DIAPHRAGM UNDER UPPER CORNER COVER. REMOVED AND REPLACED PAX DOOR FWD DIAPHRAGM UNDER UPPER CORNER COVER WITH REFERENCE TO REO 601R-52-11-3108 REV -A. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1, 51-20-
- [SDR SWIA2026062176248](https://openairdocs.org/sdr/SWIA2026062176248.md): Skin · dented · Jun 21, 2026 · N908EV · Cndair CL6002B19 · Passenger/Crew Doors
  > DENT DAMAGE TOP PASSENGER DOOR AFT DIAPHRAGM UNDER UPPER CORNER COVER. REMOVED AND REPLACED PAX DOOR AFT DIAPHRAGM UNDER UPPER CORNER COVER WITH REFERENCE TO REO 601R-52-11-3108 REV-A. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1, 51-20-06
- [SDR SWIA2026062076247](https://openairdocs.org/sdr/SWIA2026062076247.md): Skin · dented · Jun 20, 2026 · N908EV · Cndair CL6002B19 · Passenger/Crew Doors
  > DENT DAMAGE TO INTERNAL SURFACE OF PASSENGER DOOR AFT, UPPER CORNER COVER. REMOVED AND REPLACED PAX DOOR AFT UPPER CORNER COVER WITH REFERENCE TO REO 601R-52-11-3108 REV -A. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1, 51-20-06 AND NDTM P
- [SDR SWIA2026062076246](https://openairdocs.org/sdr/SWIA2026062076246.md): Skin · dented · Jun 20, 2026 · N908EV · Cndair CL6002B19 · Passenger/Crew Doors
  > DENT DAMAGE TO INTERNAL SURFACE OF PASSENGER DOOR FWD, UPPER CORNER COVER. REMOVED AND REPLACED PAX DOOR FWD UPPER CORNER COVER WITH REFERENCE TO REO 601R-52-11-3108 REV -A. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1, 51-20-06 AND NDTM P
- [SDR SWIA202601140001](https://openairdocs.org/sdr/SWIA202601140001.md): Stop Fitting · cracked · Jan 11, 2026 · N908EV · Cndair CL6002B19 · Passenger/Crew Doors
  > MCD UPPER FORWARD STOP BRACKET AT THE 11 O'CLOCK POSITION IS CRACKED. REMOVED AND REPLACED MCD UPPER FORWARD STOP BRACKET AT THE 11 O'CLOCK POSITION IN REFERENCE TO CRJ200 SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY AND COMPLETED M-337.
- [SDR SWIA2026011200001](https://openairdocs.org/sdr/SWIA2026011200001.md): Stop Fitting · cracked · Jan 11, 2026 · N908EV · Cndair CL6002B19 · Passenger/Crew Doors
  > MCD UPPER FORWARD STOP BRACKET AT THE 11 O'CLOCK POSITION IS CRACKED. OPEN
- [SDR SWIA202504070329](https://openairdocs.org/sdr/SWIA202504070329.md): Bracket · bent · Mar 29, 2025 · N908EV · Cndair CL6002B19 · Main Landing Gear
  > AFTER TAKEOFF, DURING LANDING GEAR RETRACTION, RECEIVED A GEAR DISAGREE WARNING MESSAGE. WITH THE GEAR HANDLE SELECTED IN THE UP POSITION. NOSE GEAR INDICATOR WAS INDICATING UP, BUT €ŒRED€?. MAIN GEAR WERE BOTH INDICATING WHITE DASHED MARKS. COMPLIED QRH PRO
- [SDR SWI2025F00403](https://openairdocs.org/sdr/SWI2025F00403.md): Warning Message · illuminated · Mar 29, 2025 · N908EV · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, DURING LANDING GEAR RETRACTION, RECEIVED A GEAR DISAGREE WARNING MESSAGE. WITH THE GEAR HANDLE SELECTED IN THE UP POSITION. NOSE GEAR INDICATOR WAS INDICATING UP, BUT €ŒRED€?. MAIN GEAR WERE BOTH INDICATING WHITE DASHED MARKS. COMPLIED QRH PRO
- [SDR J6BA20241106](https://openairdocs.org/sdr/J6BA20241106.md): Floor Support · corroded · Nov 6, 2024 · N908EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION DAMMAGE ON LEFT SIDE PRESSURE FLOOR ASSEBLY APPROX LBL 36.00 - LBL 45.00 AND FS 449.85 AND FS 473.15. (FILED CLOSED) REPAIRED LEFT SIDE PRESSURE FLOOR ASSEMBLY APPROX LBL 36.00 - LBL 45.00 AND FS 449.85 FS 473.15 WITH REFERENCE TO REO 601R-53-4
- [SDR J6BA20241029](https://openairdocs.org/sdr/J6BA20241029.md): Floor Support · corroded · Oct 29, 2024 · N908EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION DAMAGE ON RIGHT SIDE PRESSURE FLOOR SILL ASSY APPROX RBL 45.00 AT F449.85, FS461.50, FS513.00 AND FS559.00. (FILED CLOSED) REPAIRED RIGHT SIDE PRESSURE FLOOR ASSEMBLY APPROX RBL 45.00 AND FS449.85, FS461.50, FS513.00 AND FS559.00 WITH REFERENCE
- [SDR J6BA2024112200923](https://openairdocs.org/sdr/J6BA2024112200923.md): Floor Support · corroded · Sep 23, 2024 · N908EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION DAMAGE ON RIGHT SIDE PRESSURE FLOOR SILL ASSY APPROX RBL 36.00 AND FS409+128, FS424, FS439, FS449, FS461, FS473.15, FS499, FS513, FS529, FS544,AND FS559.. (FILED CLOSED) BLENDED CORROSION ON THE RH PRESSURE FLOOR SILL ASSY APPROX RBL 36.00 AND
- [SDR SWIA2023062300002](https://openairdocs.org/sdr/SWIA2023062300002.md): Unknown · damaged · Jun 22, 2023 · N908EV · Cndair CL6002B19 · Empennage Structure
  > FOUND DAMAGED AREA MEASURING 0.76" LENGTH X 0.184" WIDTH TO LHS ELEVATOR UPPER SKIN (DWG: 601R24028, 0.050" NOMINAL THK, REF), AT TRAILING EDGE, BTW RS NO. 8 & RS NO. 9. WITH 1 DAMAGED FASTENER. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. FORM M-337 WILL BE
- [SDR SWIA202157478](https://openairdocs.org/sdr/SWIA202157478.md): Bracket · cracked · Apr 7, 2021 · N908EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR FWD BALANCE SPRING BRACKET CRACKED (C-CHECK RO 4/12/2021) REMOVED, LOCATED, AND DRILLED NEW CARGO DOOR FWD BALANCE SPRING BRACKET IAW CRJ 200 SRM 51-42-06 AND 51-40-11. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202157516](https://openairdocs.org/sdr/SWIA202157516.md): Skin · damaged · Mar 31, 2021 · N908EV · Cndair CL6002B19 · Wing, Plate/Skin
  > UPON INCORPRATION PF SB 601R-57-054 REV B (MODIFICATION AND COLD WORK OF THE HOLES FOR THE DRAIN FITTINGS ON THE WING LOWER PLANK) A FREZZE PLUG WAS FOUND TO BE INSTALLED THRUOUGH THE LH LOWER CENTER PLANK AT THE AFT SATELLITE HOLE FOR THE DRAIN AT WS 85.50 TH
- [SDR SWIA202157564](https://openairdocs.org/sdr/SWIA202157564.md): Bolt · corroded · Mar 29, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > 9G BULKHEAD HARDWARE IS CORRODED AND REQUIRES REPLACEMENT. (C-CHECK RO 4/12/2021) RECIEVED NEW SERVICABLE HARDWARE. REFERENCE CAMP 22170328 FOR INSTALLATION.
- [SDR SWIA202157491](https://openairdocs.org/sdr/SWIA202157491.md): Plug · misinstalled · Mar 16, 2021 · N908EV · Cndair CL6002B19 · Wing Main, Frame Structure
  > DURING NDT REINSPECT (REF RA36481-601R-57-21-2553 ON CP 21955500) IT WAS DISCOVERED THAT THERE IS A FREEZE PLUG INSTALLED ON THE AFT ATTACHMENT HOLE FOR THE FUEL WATER DRAIN AT W.S 85.50 IN THE RH LOWER WING PLANK. NEITHER SKYWEST NOR MHIRJ ENGINEERING (THD) H
- [SDR SWIA202157515](https://openairdocs.org/sdr/SWIA202157515.md): Pan · blocked · Mar 13, 2021 · N908EV · Cndair CL6002B19 · Powerplant System
  > LH ENGINE INLET PANDOWN IS INSTALLED PER SB CF34-NAC-71-039 AND NDT TASK 54-430-602 CAN NOT BE PERFORMED. (C-CHECK RO 4/12/2021) REMOVED AND INSTALLED LH ENGINE INLET PANDOWN TO PERFORM NDT TASK 54-430-602 IAW MHIRJ REO 601R-54-11-3752 REV -- DATED 20
- [SDR SWIA202157561](https://openairdocs.org/sdr/SWIA202157561.md): Seat Track · corroded · Mar 12, 2021 · N908EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RBL 9 STA. 559 + 4 TO STA 559 + 85 FOUND TO BE CORRODED. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM 53-01-11-400-802. REFER TO CP 22462583 FOR FAB OF SEAT TRACK
- [SDR SWIA202157560](https://openairdocs.org/sdr/SWIA202157560.md): Seat Track · corroded · Mar 12, 2021 · N908EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RBL 9 STA 409.00 + 126 TO STA 559+4 FOUND TO BE CORRODED. (C-CHECK RO 4/12/2021) SEAT TRACK RBL 9 STA 409.00 + 126 TO STA 559+4 WAS REMOVED AND REPLACED AS REQUIRED IAW CRJ 200 SRM 53-01-11-400-802. SEE ATTACHED CONTINUATION CARD FOR DETAILS
- [SDR SWIA202157514](https://openairdocs.org/sdr/SWIA202157514.md): Hinge Arm · gouged · Mar 10, 2021 · N908EV · Cndair CL6002B19 · Trailing Edge Flaps
  > R/H INBOARD FLAP, OUTBOARD HINGE ARM, OUTBOARD FORWARD LUG HAS GOUGE DAMAGE. (C-CHECK RO 4/12/2021) REPAIRED RH INBD FLAP, OUTBD HINGE ARM, OUTBD FWD LUG IAW MHIRJ REO# 601R-57-54-322 REV-- DATE 2021-03-14. REFERENCE CONTINUATION CARD FOR WORK PERFORMED
- [SDR SWIA202157559](https://openairdocs.org/sdr/SWIA202157559.md): Seat Track · corroded · Mar 7, 2021 · N908EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 FLOOR SEAT TRACK IS CORRODED AT F.S. 449.85 AND BETWEEN F.S. 529 TO F.S. 531. REQUIRES FABRICATION. (C-CHECK RO 4/12/2021) FABRICATED NEW SERVICEABLE LBL 9 FLOOR SEAT TRACK BETWEEN FS 409+126 AND 559+4 IAW REO 601R-53-00-485 REV -D DATED 2018
- [SDR SWIA202157513](https://openairdocs.org/sdr/SWIA202157513.md): Bulkhead · cracked · Mar 6, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > WHILE COMPLYING WITH FS 621 BULKHEAD REO 601R-53-61-1240 REV-D DATED 2016-10-31 FOUND BALANCE SPRING BRACKET CRACKED AT UPPER OUTBOARD CORNER (C-CHECK RO 4/12/2021) LOCATED, DRILLED, INSTALLED, AND PAINTED NEW BALANCE SPRING BRACKET IAW CRJ 200 SRM 51-4
- [SDR SWIA202157489](https://openairdocs.org/sdr/SWIA202157489.md): Frame · cracked · Mar 3, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FS605 FRAME OUTER FLANGES CRACKED IMMEDIATELY ABOVE & BELOW STGR9L. (C-CHECK RO 4/12/2021) REPAIRED DAMAGE BY CUTTING OUT CRACK IAW REO 601R-53-61-5214 REV -A DATED 2016-11-04. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. WEIGHT
- [SDR SWIA202157488](https://openairdocs.org/sdr/SWIA202157488.md): Beam · cracked · Mar 3, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Structure
  > CARGO DOOR BEAM MEMBER LOWER ANGLE AT FS621 CRACKED IN THE RADIUS. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED THE CARGO DOOR BEAM MEMBER LOWER ANGLE AT FS 621 IAW CRJ 200 SRM 51-42-21, 51-40-11 AND SKY CARD 51-900-1003 NO WEIGHT CHANGE FORM 337 IS ATTA
- [SDR SWIA202157481](https://openairdocs.org/sdr/SWIA202157481.md): Lug · gouged · Feb 25, 2021 · N908EV · Cndair CL6002B19 · Horizontal Stabilizer, Attach Fittings
  > HORIZONTAL STAB PIVOT LH OTBD LUG OTBD SIDE AND RH OTBD LUG OTBD SIDE HAVE GOUGES (C-CHECK RO 4/12/2021) REPAIRED H-STAB PIVOT LH OUTBD LUG, OUTBD SIDE AND RH OUTBD LUG, OUTBD SIDE IAW MHIRJ REO#601R-55-11-682 REV-- DATE 2021-02-27. FORM 337 AND MAJOR
- [SDR SWIA202157487](https://openairdocs.org/sdr/SWIA202157487.md): Floorbeam · cracked · Feb 21, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FOUND FLOOR SUPPORT ANGLE TO BE CRACKED AT F.S 621 BETWEEN LBL27 AND LBL 36. (C-CHECK RO 4/12/2021) REPAIRED DAMAGE BY REMOVING AND INSTALLING NEW REPAIR ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMP
- [SDR SWIA202157475](https://openairdocs.org/sdr/SWIA202157475.md): Floorbeam · cracked · Feb 20, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 484 INTERCOSTAL BETWEEN LBL27 AND LBL36 IS CRACKED ON THE OUTBARD SIDE. (C-CHECK RO 4/12/2021) REPAIRED F.S.484 INTERCOSTAL BETWEEN LBL 27 AND LBL36 IAW CRJ 200 MHIRJ REO 601R-53-41-2872 REV. --, DATED 2021-03-09. / MAJOR REPAIR FORM M-337 IS COMPLE
- [SDR SWIA202157512](https://openairdocs.org/sdr/SWIA202157512.md): Doubler · gouged · Feb 18, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DOUBLER AND ATTACHING HARDWARE GOUGED ON F.S. 280.00 BULKHEAD AFT FACE AT RBL9 APPROX 18 INCHES ABOVE FLOOR LEVEL. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED THE FS 280 BULKHEAD DOUBLER AT RBL 9 IAW CRJ-200 SRM 51-40-11 AND 51-42-06, REFERENCING REO 60
- [SDR SWIA202157511](https://openairdocs.org/sdr/SWIA202157511.md): Stringer · cracked · Feb 17, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L AT FS282 ANGLE APPEARS TO BE CRACKED AT THE 4TH HOLE. (C-CHECK RO 4/12/2021) REPAIRED STRINGER 3L ANGLE AND ELONGATED HOLES IN THE UPPER SILL FITTING AND STRINGER SPLICING AT FS 282 IAW MHIRJ REO 601R-53-21-3400 REV-- DATED 2021-03-24 AND
- [SDR SWIA202157566](https://openairdocs.org/sdr/SWIA202157566.md): Seat Track · gouged · Feb 15, 2021 · N908EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > R/H SIDE SEAT RAIL AT FS 449.00 TO FS 544.00 GOUGED AND PITTED IN TWO PLACES. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED RH SIDE SEAT RAIL AT FS 449.00 TO FS 544.00 IAW CRJ 200 AMM 53-01-11-400-802 REF CONTINUATION CARD FOR DETAILS OF WORK PERFORMED RE
- [SDR SWIA202157565](https://openairdocs.org/sdr/SWIA202157565.md): Seat Track · corroded · Feb 15, 2021 · N908EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > R/H SIDE SEAT RAIL CHANNEL CORRODED AT FS 370.00 TO FS 409.00 ON LOWER EDGE. (C-CHECK RO 4/12/2021) REMOVED LLIGHT SURFACE CORROSION FROM THE R/H SEAT RAIL CHANNEL BETWEEN FS 379.00 AND FS 409.00 IAW CRJ-200 SRM 51-21-06 AND FOUND TO BE WITHIN ALLOWABLE
- [SDR SWIA202157558](https://openairdocs.org/sdr/SWIA202157558.md): Seat Track · corroded · Feb 15, 2021 · N908EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > L/H SIDE SEAT RAIL AT FS 409.00+112 TO FS 424.00 CORRODED ON LOWER INSIDE EDGE. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED L/H SIDE SEAT RAIL AT FS 409.00+112 TO FS424.00 IAW CRJ 200 AMM 53-01-11-000/400-802. REFERENCE CAMP# 22401229 FOR FABRICATION
- [SDR SWIA202157557](https://openairdocs.org/sdr/SWIA202157557.md): Seat Track · corroded · Feb 15, 2021 · N908EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > L/H SIDE SEAT RAIL CORRODED AND GOUGED FROM FS 364.00 TO FS 409.00+16. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED LH SIDE SEAT RAIL FROM FS 364.00 TO FS 409.00+16 IAW CRJ 200 AMM 53-00-11-000/400-802 AND BOMBARDIER REO 601R-53-00-055 REV C DATED 2017-0
- [SDR SWIA202157556](https://openairdocs.org/sdr/SWIA202157556.md): Seat Track · corroded · Feb 15, 2021 · N908EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > R/H SIDE SEAT RAIL HAS SURFACE CORROSION FROM FS 409.00 +112 TO FS 437.00 (C-CHECK RO 4/12/2021) REMOVED AND REPLACED RH SIDE SEAT RAIL BETWEEN FS409+112 AND FS437 IAW CRJ200 AMM 53-01-11-000/400-802. FOUND TO BE OUT OF LIMITS IAW CRJ200 SRM 53-21-49. R
- [SDR SWIA202157555](https://openairdocs.org/sdr/SWIA202157555.md): Seat Track · corroded · Feb 15, 2021 · N908EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > R/H SIDE SEAT RAIL HAS LGHT SURFACE CORROSION FROM FS 409.00 TO FS 409.00 +112. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED RH SIDE SEAT RAIL FROM FS 409.00 TO FS 409.00+112 IAW CRJ 200 53-01-11-000-400-802 REF CAMP # 22401311 FOR FABRICATION OF THE NEW
- [SDR SWIA202157486](https://openairdocs.org/sdr/SWIA202157486.md): Attach Angle · cracked · Feb 15, 2021 · N908EV · Cndair CL6002B19 · Wing, Attach Fittings
  > BAT RIB AT W.S. 48.30, UPPER ATTACH ANGLE CRACKED (C-CHECK RO 4/12/2021) REPAIRED LH BAT RIB AT W.S. 48.30 UPPER ATTACH ANGLE BY REMOVING AND INSTALLING NEW SERVICABLE ANGLE IAW CRJ 200 SRM 51-42-21 AND REO 601R-57-21-3432 REV -- DATED 2021-02-25. COMPL
- [SDR SWIA202157477](https://openairdocs.org/sdr/SWIA202157477.md): Skin · corroded · Feb 14, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE LOWER SKIN HAS CORROSION BETWEEN FS 559.00+80 AND FS 589, STR 23L AND STR 24R. (C-CHECK RO 4/12/2021) REPAIRED EXTERNAL FUSELAGE LOWER SKIN CORROSION BETWEEN FS 559.00+80 AND FS 589 STR 23L AND 24 R IAW BOMBARDIER REO 601R-53-00-834 RE
- [SDR SWIA202157554](https://openairdocs.org/sdr/SWIA202157554.md): Skin · corroded · Feb 12, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN IS CORRODED BETWEEN STGR20L AND 20R UNDER FAIRING 195BB CONTOURING SEALANT BED. (C-CHECK RO 4/12/2021) UPON FURTHER INVESTIGATION FOUND THE CORROSION TO BE ON THE LOWEER SKIN BETWEEN STR 23L AND STR 24R COMMON TO BELLY FAIRING 195
- [SDR SWIA202157553](https://openairdocs.org/sdr/SWIA202157553.md): Skin · corroded · Feb 12, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN IS CORRODED IN MULTIPLE PLACES BETWEEN FS559+80 AND FS574 FROM STGR 26L TO STGR 26R. (C-CHECK RO 4/12/2021) REMOVED CORROSION FROM THE EXTERNAL FUSELAGE SKIN BETWEEN FS 559.00+80 AND FS 574, STR 26L AND STR 26R IAW CRJ-200 SRM 51-
- [SDR SWIA202157552](https://openairdocs.org/sdr/SWIA202157552.md): Skin · corroded · Feb 12, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN IS CORRODED ALONG FS559+112 CIRRCUMFERENTIAL JOINT FROM STGR 25L TO 25R. (C-CHECK RO 4/12/2021) REMOVED CORROSION FROM THE EXTERNAL FUSELAGE SKIN AT FS 559.00+112 IAW CRJ-200 SRM 51-21-06 AND FOUND TO BE OUT OF LLOWABLE LIITS IAW
- [SDR SWIA202157510](https://openairdocs.org/sdr/SWIA202157510.md): Floor Support · damaged · Feb 12, 2021 · N908EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TRANSFERED FROM PARENT CAMP # 22280420 PN: 601R35280-3 REQUIRES REPLACEMENT AT LBL 9.0 BETWEEN F.S 605.0 - 621.0. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED LBL 9 BEAM FLOOR FITTING ASSY 601R35280-1 BETWEEN FS 605.0 TO FS 621.0 IAW CRJ CRJ 200 SRM 51-4
- [SDR SWIA202157509](https://openairdocs.org/sdr/SWIA202157509.md): Skin · corroded · Feb 12, 2021 · N908EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LH WING LOWER WING PLANK CUTOUT FOR FUEL PANEL 510AB LANDING HAS CORROSION ON THE IB, OB, AND FWD LOCATIONS FWD EDGE IS IN THE CRITICAL ZONE (C-CHECK RO 4/12/2021) REPAIRED THE LH WING LOWER WING PLANK CUTOUT FOR FUEL PANEL 510AB LANDING HAS CORROSIO
- [SDR SWIA202157492](https://openairdocs.org/sdr/SWIA202157492.md): Skin · corroded · Feb 12, 2021 · N908EV · Cndair CL6002B19 · Wing, Plate/Skin
  > LH WING LOWER WING PLANK CUTOUR FOR FUEL PANEL 540BB HAS CORROSION ON THE IB.OB, AND FWD EDGES IN THE CRITICAL ZONE (C-CHECK RO 4/12/2021) REPAIRED LH WING LOWER WING PLANK CUTOUR FOR FUEL PANEL 540BB HAS CORROSION ON THE IB.OB, AND FWD EDGES IN THE CRI
- [SDR SWIA202157479](https://openairdocs.org/sdr/SWIA202157479.md): Fitting · damaged · Feb 12, 2021 · N908EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DISCREANCY TRANSFERED FROM PARENT CAMP 22281732, PN: 601R35289-1 REQUIRES REPLACEMENT AT LBL 27 BETWEEN F.S 605.0 - 621.0. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED FITTING P/N 601R35289-1 AT LBL 27 BETWEEN FS 605.0 TO FS 621.00 IAW CRJ 200 SRM 51-42-
- [SDR SWIA202157551](https://openairdocs.org/sdr/SWIA202157551.md): Seat Track · corroded · Feb 11, 2021 · N908EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 FLOOR SEAT TRACK IS CORRODED AT F.S. 449.85 AND BETWEEN F.S. 529 TO F.S. 531. (C-CHECK RO 4/12/2021) FOUND THE LBL 9 SEAT TRACK FROM FS 409+126 TO FS 559+4 TO BE OUT OF ALOOWABLE LIMITS IAW CRJ-200 SRM 53-41-49. INSTALLED NEW SEAT TRACK AT LBL 9 F
- [SDR SWIA202157508](https://openairdocs.org/sdr/SWIA202157508.md): Bulkhead · damaged · Feb 11, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > F.S.621.00 REAR PRESSURE BULKHEAD HAS TOOLING DAMAGE LOCATED AT WL105, BUTT LINES LBL18, LBL27, RBL9, RBL27, AND RBL36. DAMAGE MEASURES APPROX. 0.125" DIA X 0.006" DEEP. (C-CHECK RO 4/12/2021) REPAIRED FS 621.00 REAR PRESSURE BULKHEAD TOOLING DAMAGE LOC
- [SDR SWIA202157507](https://openairdocs.org/sdr/SWIA202157507.md): Intercostal · corroded · Feb 11, 2021 · N908EV · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > AVIONICS BAY DOOR INTERCOSTAL BETWEEN STGR 27 TO STGR 26 L IS CORODED. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED AVIONICS BAY DOOR INTERCOSTAL BETWEEN STGR 27 TO STGR 26 L IAW CRJ200 SRM 51-40-11, 51-42-06 AND 51-42-21. FORM 337 AND MAJOR REPAIR TASK
- [SDR SWIA202157493](https://openairdocs.org/sdr/SWIA202157493.md): Skin · dented · Feb 11, 2021 · N908EV · Cndair CL6002B19 · Ailerons
  > RH AILERON LOWER SKIN IS DENTED ON THE OB END APROX 3 INCHES LONG 2 INCHES WIDE AND 3 INCHES FROM THE TE OF THE AILERON (C-CHECK RO 4/12/2021) REPAIRED DAMAGE IAW REO 670-57-61-001 REV -C DATED 2012-01-16. REFERENCE CONTINUATION CARD FOR WORK PERFORMED
- [SDR SWIA202157485](https://openairdocs.org/sdr/SWIA202157485.md): Floor Mat · corroded · Feb 11, 2021 · N908EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > STUB RAIL PN: 601R35289-4 AT RBL 27.0 FROM F.S. 605.0 TO F.S. 621.0 REQUIRES REPLACEMENT DUE TO CORROSION OUT OF LIMITS, REF: PARENT CAMP: 22280534. (C-CHECK RO 4/12/2021) INSTALLED NEW STUB RAIL FITTING PN: 601R35289-4 AT RBL 27 FROM F.S 605 TO F.S 621
- [SDR SWIA202157550](https://openairdocs.org/sdr/SWIA202157550.md): Plate · corroded · Feb 10, 2021 · N908EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT ANCHOR FITTING SERRATED PLATE IS CORRODED. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED PAX DOOR AFT ANCHOR FITTING SERRATED PLATE IAW CRJ 200 AMM 52-11-17-000/400-804.

Next page: https://openairdocs.org/aircraft/N908EV/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 = 'N908EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N908EV/reports

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