# Service difficulty reports: N900EV

A list on [N900EV](https://openairdocs.org/aircraft/N900EV.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 · 259 reports

- [SDR SWIA2023041000322](https://openairdocs.org/sdr/SWIA2023041000322.md): Unknown · corroded · Mar 22, 2023 · N900EV · Cndair CL6002B19 · Fuselage, Powerplant Attach Fittings
  > SEAT TRACK BEAM AT LBL9 UNDER FLOOR PANEL 251BLF HAS CORROSION AND MISSING NUT PLATE AT SAME LOCATION FLAGGED WITH RED STREAMER (C-CHECK RO 4/5/2023) REMOVED AND INSTALLED NEW SEAT TRACK BEAM LBL9 FS409+5 - FS409+118 REF REO NO. 601R-53-31-1266 REV -- D
- [SDR SWIA2023041000309](https://openairdocs.org/sdr/SWIA2023041000309.md): Unknown · corroded · Mar 9, 2023 · N900EV · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURRING INVESTIGATION OF DENT AT FS394 STR23L FOUND FRAME AT FS394 SKIN ATTACH FLANGE BETWEEN STR22L-23L CORRODED (C-CHECK RO 4/5/2023) REMOVED CORROSION ON FRAME FS394 SKIN AT STR 22L - 23L. REF CRJ200 SRM 51-21-06. INSTALLED REPAIR SEGMENT FOR FRAME A
- [SDR SWIA2023041000308](https://openairdocs.org/sdr/SWIA2023041000308.md): Unknown · corroded · Mar 8, 2023 · N900EV · Cndair CL6002B19 · Fuselage Floor Panel
  > FLOOR BEAM AT LBL9 HAS CORROSION ON FLOOR PANEL ATTACH FLANGES FROM F.S. 409+128 TO F.S. 559.00 (MARKED) (C-CHECK RO 4/5/2023) BLENDED OUT CORROSION ON FLOORBEAM LBL9 FROM FS409+128 TO FS559.00 PER CRJ-200 SRM 51-21-06 AND REO 601R-53-41-3136 REV -- DA
- [SDR SWIA2023041000305](https://openairdocs.org/sdr/SWIA2023041000305.md): Unknown · damaged · Mar 5, 2023 · N900EV · Cndair CL6002B19 · Fuselage Floor Panel
  > WHILE REPLACING FLOOR BEAM CAP AT RBL 9 FROM FS 409+128 TO FS 559, FOUND MISSED CUT ON FLOOR BEAM VERTICAL "C" CHANNEL OUTBOARD WEB FROM FS 439 TO FS 471. (C-CHECK RO 4/5/2023) COMPLIED WITH REPAIR TO FLOOR BEAM AT RBL9, FS409+112 - FS484 REF REO 60
- [SDR SWIA2023041000304](https://openairdocs.org/sdr/SWIA2023041000304.md): Unknown · corroded · Mar 4, 2023 · N900EV · Cndair CL6002B19 · Fuselage Floor Panel
  > DURING TRIMMING OF HAT CHANNEL FLANGES OF FLOOR BEAM SUPPORT @ FS 409+128 TO 559.0, NOTICED HEAVY CORROSION ON SUPPORT FITTING PN 600-31068-19. @ FS 460.00 RBL 9.0 (C-CHECK RO 4/5/2023) BLENDED CORROSION ON FLOOR BEAM SUPPORT FITTING. REF CRJ200 SRM 5
- [SDR SWIA2023041000227](https://openairdocs.org/sdr/SWIA2023041000227.md): Unknown · corroded · Feb 27, 2023 · N900EV · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > MULTIPLE AREAS OF CORROSION ON RH PRESSURE FLOOR SILL PANEL. AREAS MARKED. (C-CHECK RO 4/5/2023) BLENDED MULTIPLE AREAS OF CORROSION ON RH PRESSURE FLOOR SILL FROM FS409+128 - FS559. REF CRJ200 SRM 51-21-06. PERFORMED REPAIR ON FLOOR SILL AT FS516.85+5.
- [SDR SWIA2023041000226](https://openairdocs.org/sdr/SWIA2023041000226.md): Unknown · corroded · Feb 26, 2023 · N900EV · Cndair CL6002B19 · Fuselage Internal Mounting Structure
  > LH SILL HAS 5 SPOTS OF CORROSION BETWEEN FS 450.85 AND 491.00 (C-CHECK RO 4/5/2023) REPAIRED CORROSION ON LH SILL BETWEEN F.S. 450.85 AND F.S. 491.00, REF BOMBARDIER REO 601R-53-41-666 REV -C DATED 2012-11-06, SEE CONTINUE CARD FOR DETAILS.COMPLIED WIT
- [SDR SWIA2023041000224](https://openairdocs.org/sdr/SWIA2023041000224.md): Unknown · corroded · Feb 24, 2023 · N900EV · Cndair CL6002B19 · Fuselage Floor Panel
  > * FLOOR BEAM AT LBL27 HAS CORROSION ON FLOOR PANEL ATTACH FLANGE AT FS559, MARKED (C-CHECK RO 4/5/2023) REPAIRED CORRODED FLOOR PANEL ATTACH FLANGE ON FLOOR BEAM AT LBL27 AT FS559 WITH REPAIR ANGLE AND JOGGLE STRAP PER REO 601R-53-41-3138 REV -- 2023-0
- [SDR SWIA20230223](https://openairdocs.org/sdr/SWIA20230223.md): Unknown · cracked · Feb 23, 2023 · N900EV · Cndair CL6002B19 · Master Cylinder/Brake Valve
  > IN RH W/W, BRAKE PRESSURE TRANDUCER'S FWD HYD LINE MOUNTING BRACKET IS CRACKED (MARKED). (C-CHECK RO 4/5/2023) REPLACED RH MLG UPPER W/W BRAKE PRESSURE TRANSDUCERS FWD HYD MOUNTING BRACKET. REF CRJ200 SRM 51-42-06 AND REF DWG 601R75261 REV -N. PRESSURE
- [SDR SWIA2023041000223](https://openairdocs.org/sdr/SWIA2023041000223.md): Unknown · damaged · Feb 23, 2023 · N900EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR HINGE (FUSELAGE SIDE) HAS NUMEROUS LUGS OUT OF LIMITS. CHECKED WITH PAX DOOR GO/NO GO GAUGE TUC8495 (C-CHECK RO 4/5/2023) REMOVED AND REPLACED THE PAX DOOR HINGE (FUSELAGE SIDE) REF CRJ 200 SRM 53-21-23 REPAIR -01, REV 39 DATED MAR 10, 2022. C
- [SDR SWIA2023041000221](https://openairdocs.org/sdr/SWIA2023041000221.md): Unknown · corroded · Feb 21, 2023 · N900EV · Cndair CL6002B19 · Fuselage Floor Panel
  > CORROSION FOUND AT NUTPLATE LOCATIONS THROUGHOUT FLOOR BEAM RBL9 BETWEEN FS409 - FS409+128 (C-CHECK RO 4/5/2023) REMOVED AND REPLACED FLOOR BEAM CAP RBL9 BETWEEN FS409 - FS409+128 REF REO NO. 601R-53-31-1269 REV -- DATED 2023-03-15 CRJ200 SRM51-42-21, S
- [SDR SWIA2023041000220](https://openairdocs.org/sdr/SWIA2023041000220.md): Unknown · cracked · Feb 20, 2023 · N900EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > CARGO DOOR'S AFT BALANCE SPRING BRACKET IS CRACKED (C-CHECK RO 4/5/2023) INSTALLED 1EA NEW CARGO DOOR'S AFT BALANCE SPRING BRACKET REF CRJ200 SRM 51-42-06 AND DWG# 601R35055 REV TCOMPLIED WITH 51-900-1003-SKY
- [SDR SWIA2023041000218](https://openairdocs.org/sdr/SWIA2023041000218.md): Unknown · cracked · Feb 18, 2023 · N900EV · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR. SUSPECTED CRACK ON AFT DRAG ANGLE BY THE MOTOR ASSSIST PULLEY. (C-CHECK RO 4/5/2023) VERIFIED CRACK, REMOVED, LOCATED, AND INSTALLED NEW DRAG ANGLE P/N 601R31772-5. REF: CRJ-200 SRM 51-42-06, CRJ-200 SRM 51-42-13, AND DRAWING 601R31707
- [SDR SWIA2023041000206](https://openairdocs.org/sdr/SWIA2023041000206.md): Unknown · cracked · Feb 6, 2023 · N900EV · Cndair CL6002B19 · Wing, Longeron/Stringer
  > FOUND CRACKING AT RIGHT HAND WING LOWER WING PLANK AT APPROX WS 148.019, FWD OF REAR SPAR (C-CHECK RO 4/5/2023) COMPLIED WITH PARAGRAPH (B) OF AD 2002-03-14 BY REPAIRING CRACK ON THE RIGHT SIDE LOWER WING PLANK BEFORE FURTHER FLIGHT PER A METHOD APPROVE
- [SDR SWIA2023041000131](https://openairdocs.org/sdr/SWIA2023041000131.md): Unknown · damaged · Jan 31, 2023 · N900EV · Cndair CL6002B19 · Engine Thrust Reverser
  > ADM# N900EV-7616THERE WAS DAMAGE NOTED ON THE LH ENGINE UPPER TRANSLATING COWL AT THE 9 O€™CLOCK POSITION, APPROX. 2€? X 1.75€? X.0310. PLEASE PLOT, MAP, AND EVALUATE DAMAGE. IF FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD
- [SDR SWIA202265906](https://openairdocs.org/sdr/SWIA202265906.md): None · failed · Jun 8, 2022 · N900EV · Cndair CL6002B19 · Landing Gear Door Actuator
  > DEPARTING ACV, CREW REPORTS DURING GEAR RETRACTION RECEIVED GEAR DISAGREE WARNING. NLG DID NOT RETRACT. (FLIGHT 5341 - FILED CLOSED) FOUND NLG SELECTOR VALVE CONNECTOR DISCONNECTED. RESECURED CONNECTOR AND VERIFIED TO BE LOCKED AND SECURED IN REF TO CRJ200
- [SDR SWIA202161979](https://openairdocs.org/sdr/SWIA202161979.md): None · cracked · Oct 30, 2021 · N900EV · Cndair CL6002B19 · Window/Windshield System
  > CRACK FORMING IN UPPER LEFT HAND CORNER OF CA SIDE WINDSHIELD. (FLIGHT 4688 - FILED CLOSED) REMOVED CA SIDE WINDSHIELD AND WINDSHIELD WIPER DRIVE ARM REF AMM 56-11-01 / PLEASE REFERENCE AML 769130 FOR INSTALL.
- [SDR SWIA202054171](https://openairdocs.org/sdr/SWIA202054171.md): Window · cracked · Nov 24, 2020 · N900EV · Cndair CL6002B19 · Flight Compartment Windows
  > CRACK IN LEFT WINDOW. FLIGHT 5889-FILED CLOSED. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 21870767 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED LT WINDOW ASSEMBLY, IAW CRJ200 AMM AND TASK CARD. OPERATIONS AND LEAK CHECKS GOOD AT THIS TIME
- [SDR SWIA2020020348097](https://openairdocs.org/sdr/SWIA2020020348097.md): Support · corroded · Dec 29, 2019 · N900EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH SILL HAS CORROSION AT FS 559+4 (C-CHECK) RO 1/28/2020 EVALUATED FOUND TO BE OUT OF LIMITS IAW BOMBA REO. WORK TO BE ACCOMPLISHED ON SN 7507203 AAR WO 1018024 1000 0117 CAMP 20064949
- [SDR SWIA2020061851087](https://openairdocs.org/sdr/SWIA2020061851087.md): Fitting · damaged · Dec 23, 2019 · N900EV · Cndair CL6002B19 · Vertical Stabilizer Miscellaneous Structure
  > STEADY FITTING HAS 6 LOOSE BOLTS, WASHERS ON RIGHT HAND OUTBOARD BOLT CAN BE TURNED BY HAND. REPAIRED V/STAB STEADY FITTING ELONGATED HOLES AND LOOSE HDWR IAW REO. THIS SDR FOR T/STEADY FITTING IS BEING SUBMITTED AS A PART OF VDR_2020NM064006.
- [SDR SWIA2019020348042](https://openairdocs.org/sdr/SWIA2019020348042.md): Floor Support · damaged · Dec 23, 2019 · N900EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REPAIR FLOOR SUPPORT STRUCTURE RBL9 FS 559+80 - 559+96 (C-CHECK) RO 1/28/2020 REPAIRED FLOOR SUPPORT STRUCTURE RBL 9, F.S. 559+80 - 559+96 IAW REO.
- [SDR SWIA2020020348060](https://openairdocs.org/sdr/SWIA2020020348060.md): Bracket · cracked · Dec 21, 2019 · N900EV · Cndair CL6002B19 · Cargo/Baggage Doors
  > FOUND CARGO DOOR BRACKET FOR SPRING BOX ATTACHED TO 621 BULKHEAD CRACKED AFTER REMOVAL (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED SPRING BOX ATTACHMENT BRACKET IAW CRJ 200SRM.
- [SDR SWIA2020020348096](https://openairdocs.org/sdr/SWIA2020020348096.md): Floor Support · corroded · Dec 17, 2019 · N900EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT STRUCTURE RBL 9 HAS CORROSION BTWEEN FS 559.00+80 AND FS 559.00+96 (C-CHECK) RO 1/28/2020 REMOVED CORROSION IAW CRJ200 SRM 51-21-06. OUT OF LIMITS IAW CRJ200 SRM. WORK TO BE ACCOMPLISHED ON W/O 1018024 1000/0184 SN 7507374
- [SDR SWIA2019020348041](https://openairdocs.org/sdr/SWIA2019020348041.md): Frame · corroded · Dec 15, 2019 · N900EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 589 HAS CORROSION SPOTS ON THE FWD AND AFT SIDE BETWEEN STGR 22R AND 20R IN THE CARGO BAY BELOW THE FLOOR (C-CHECK) RO 1/28/2020 TRIMED OUT OUTER FLANGE FRAME AND PERFORMED REPAIR IAW CRJ200 SRM T.063 7075-T6 TAG B33959 S1710-1 TAG B13723 MS20420AD5-
- [SDR SWIA2020020348101](https://openairdocs.org/sdr/SWIA2020020348101.md): Attach Bracket · damaged · Dec 14, 2019 · N900EV · Cndair CL6002B19 · Wing, Attach Fittings
  > R/H STUB FAIRING FWD ATTAC BRACKET IS DAMAGED (C-CHECK) RO 1/28/2020 AFTER FUTHER EVALUATION STUB FAIRING AND BRACKET FOUND TO BE OUT OF LIMITS. RECEAVED, LOCATED, DRILLED AND ASSEMBLED NEW FAIRING AND BRACKET IAW CRJ 200 SRM.
- [SDR SWIA2020020348100](https://openairdocs.org/sdr/SWIA2020020348100.md): Cargo Track · corroded · Dec 14, 2019 · N900EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 CARGO FLOOR SEAT TRACK HAS CORROSION AT FF 559.0+94 (C-CHECK) RO 1/28/2020 REMOVED CORROSION IAW CRJ 200 SRM FOUND TO BE OUT OF LIMITS IAW CRJ 200 SRM REMOVED AND REPLACED IAW CRJ 200 AMM. N126-2075 B17426
- [SDR SWIA2020020348095](https://openairdocs.org/sdr/SWIA2020020348095.md): Seat Track · corroded · Dec 14, 2019 · N900EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 FLOOR SEAT TRACK BETWEEN FS 409.0+128 AND FS 559.0 HAS CORROSION (C-CHECK) RO 1/28/2020 SEAT TRACK FOUND TO BE OUT OF LIMITS IAW CRJ 200 SRM 53-21-49. REMOVED AND REPLACED IAW BOMBA REO.
- [SDR SWIA2020020348059](https://openairdocs.org/sdr/SWIA2020020348059.md): Floor Support · cracked · Dec 14, 2019 · N900EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AF FS 513.0 BETWEEN OTBD SILL NAD LBL 27 IS CRACKED AT INBD CLIP (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED INBD CLIP AT FS513 LBL27 REF CRJ200 SRM.
- [SDR SWIA2020020348058](https://openairdocs.org/sdr/SWIA2020020348058.md): Floor Support · cracked · Dec 14, 2019 · N900EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT FS 513.0 BETWEEN LBL 9 AND LBL 27 IS CRACKED AT INBD CLIP (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED INBD CLIP AT FS513 BETWEEN LBL9 AND LBL27 REF CRJ200 SRM.
- [SDR SWIA2020020348057](https://openairdocs.org/sdr/SWIA2020020348057.md): Floor Support · cracked · Dec 14, 2019 · N900EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT FS 513.0 BETWEEN LH OTBD PRESS SILL AND LBL 27 IS CRACKED OTBD CLIP (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED OTBD CLIP AT FS513 LH OTBD PRESSURE SILL AND LBL27 REF CRJ200 SRM
- [SDR SWIA2020020348056](https://openairdocs.org/sdr/SWIA2020020348056.md): Floor Support · cracked · Dec 14, 2019 · N900EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 513.0 INTERCOSTAL BETWEEN RH PRESSURE SILL AND RBL 27 IS CRACKED ON INBD CLIP (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED INBD CLIP AT FS513 BETWEEN RH PRESSURE SILL AND RBL27 REF CRJ200 SRM.
- [SDR SWIA2020020348055](https://openairdocs.org/sdr/SWIA2020020348055.md): Floor Support · cracked · Dec 14, 2019 · N900EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 513.0 INTERCOSTAL BETWEEN RH PRESSURE SILL AND RBL 27 HAS CRACKED CLIP ON OTBD END (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED ANGLE AT FS513 BETWEEN RH PRESSURE SILL AND RBL 27 REF CRJ 200 SRM.
- [SDR SWIA2020020348053](https://openairdocs.org/sdr/SWIA2020020348053.md): Support Bracket · cracked · Dec 14, 2019 · N900EV · Cndair CL6002B19 · Wing Main, Frame Structure
  > LH OVERWING ACCESS PNL SUPPORT BRACKET AT FS 449.85 IS CRACKEDREMOVED CRACKED BRACKET AND INSTALLED NEW BRACKET IAW CRJ 200 SRM.
- [SDR SWIA2020020348052](https://openairdocs.org/sdr/SWIA2020020348052.md): Support Bracket · cracked · Dec 14, 2019 · N900EV · Cndair CL6002B19 · Wing Main, Frame Structure
  > LH WING OVERWING ACCESS PNL SUPPORT BRACKET AT FS 461.0 IS CRACKED (C-CHECK) RO 1/28/2020 REMOVED CRACKED BRACKET AND INSTALLED NEW BRACKET IAW CRJ 200 SRM.
- [SDR SWIA2019020348040](https://openairdocs.org/sdr/SWIA2019020348040.md): Floorbeam · damaged · Dec 13, 2019 · N900EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > PERFORM LOCAL REPAIR TO RBL 9 FLOORBEAM CAP AT FS 559+4 IAW S/N SPECIFIC REO. (C-CHECK) RO 1/28/2020 REPAIRED FLOOR BEAM CAP AT FS 559+4 IAW BOMBA REO. P/N-KFN587-3 TAG#A84011 P/N-HST11AG6-4 TAG#A80240 P/N-KFN587-3 TAG#A83571 P/N-HST11AG5-6 TAG#B99244
- [SDR SWIA2019020348039](https://openairdocs.org/sdr/SWIA2019020348039.md): Floor Support · damaged · Dec 12, 2019 · N900EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > REPAIR OR REPLACE RBL 27 FLOORBEAM CAP THAT HAS DAMAGE BETWEEN FS 559+80 AND FS 559+112 (C-CHECK) RO 1/28/2020 REPAIRED FLOORBEAM ON RBL 27 BETWEEN FS 559+80 AND FS 559+112 IAW CRJ 200 SRM.
- [SDR SWIA2020020348098](https://openairdocs.org/sdr/SWIA2020020348098.md): Bulkhead Web · cracked · Dec 11, 2019 · N900EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD WEB IS CRACKED AT BLO APPROX WL 112 (C-CHECK) RO 1/28/2020 REPAIRED AFT PRESSURE BULKEAD AT BL 0 WL 112 IAW BOMBARDIER REO. FILLER TO BE INSTALLED ON AND REO WILL BE SCANNED ON CAMP # 19794163
- [SDR SWIA2020020348063](https://openairdocs.org/sdr/SWIA2020020348063.md): Angle · cracked · Dec 11, 2019 · N900EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > I/B AND O/B ANGLE CLIPS ON STGR 3L JUST AFT OF FRAME 280 ARE CRACKED IN THE CABIN (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED I/B AND O/B ANGLE CLIPS IAW CRJ-200 SRM 51-42-06 AND SRM
- [SDR SWIA2020020348062](https://openairdocs.org/sdr/SWIA2020020348062.md): Window Post · cracked · Dec 11, 2019 · N900EV · Cndair CL6002B19 · Fuselage Main, Structure
  > R/H WINDSHIELD SIDE POST SUPPORT FITTING IS CRACKED (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED R/H WINDSHIELD SIDE POST SUPPORT FITTING IAW CRJ-200 SRM.
- [SDR SWIA2020020348051](https://openairdocs.org/sdr/SWIA2020020348051.md): Window Post · cracked · Dec 11, 2019 · N900EV · Cndair CL6002B19 · Fuselage Main, Structure
  > L/H WINDSHIELD SIDE POST SUPPORT FITTING IS CRACKED (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED L/H WINDSHIELD SIDE POST SUPPORT FITTING IAW CRJ-200 SRM 51-42-21.
- [SDR SWIA2020020348050](https://openairdocs.org/sdr/SWIA2020020348050.md): Window Post · cracked · Dec 11, 2019 · N900EV · Cndair CL6002B19 · Fuselage Main, Structure
  > L/H WINDSHIELD SIDE POST WEB IS CRACKED (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED L/H WINDSHIELD SIDE POST WEB IAW CRJ-200 SRM.
- [SDR SWIA2019020348038](https://openairdocs.org/sdr/SWIA2019020348038.md): Frame · cracked · Dec 11, 2019 · N900EV · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME 333 IS CRACKED AT TOOLING HOLE JUST I/B OF STGR 2L IN THE CABIN (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED FRAME SECTION IAW CRJ-200 SRM.
- [SDR SWIA2020020348099](https://openairdocs.org/sdr/SWIA2020020348099.md): Seat Track · corroded · Dec 9, 2019 · N900EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 #4 FLOOR SEAT TRACK BETWEEN FS559.0+4 AND FS559.0+80 HAS CORROSION (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 AMM. TOOL# AAR519954 CAL DUE: 05/09/20
- [SDR SWIA2020020348094](https://openairdocs.org/sdr/SWIA2020020348094.md): Door Frame · corroded · Dec 9, 2019 · N900EV · Cndair CL6002B19 · Fuselage Main, Structure
  > PASSENGER DOOR CUT-OUT HAS CORROSION AT LOWER AFT CORNER BY DRAIN HOLE (C-CHECK) RO 1/28/2020 REPAIRED LOWER AFT CORNER OF PASSENGER DOOR CUT-OUT IAW BOMBA REO.
- [SDR SWIA2020020348093](https://openairdocs.org/sdr/SWIA2020020348093.md): Not Reported · corroded · Dec 9, 2019 · N900EV · Cndair CL6002B19 · Fuselage Main, Structure
  > RBL27 HAS CORROSION BETWEEN FS589.0 TO FS621.0 (C-CHECK) RO 1/28/2020 EVALUATED AND FOUND TO BE OUT OF LIMITS IAW REO. WORK TO BE ACCOMPLISHED ON CP 20065025, AAR NON-ROUTINE 1018024/1000/0120 S/N: 7507206
- [SDR SWIA2020020348092](https://openairdocs.org/sdr/SWIA2020020348092.md): Cargo Track · corroded · Dec 9, 2019 · N900EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL27 CARGO TRACK HAS CORROSION BETWEEN FS559.0+80 TO FS559.0+96 (C-CHECK) RO 1/28/2020 REMOVED AND REPLACED RBL27 CARGO TRACK BETWEEN FS559.0+80 TO FS559.0+96 IAWCRJ200- AMM
- [SDR SWIA2020020348091](https://openairdocs.org/sdr/SWIA2020020348091.md): Not Reported · corroded · Dec 9, 2019 · N900EV · Cndair CL6002B19 · Fuselage Main, Structure
  > RBL27 HAS CORROSION BETWEEN FS559.0+80 TO FS559.0+112 (C-CHECK) RO 1/28/2020 EVALUATED AND FOUND TO BE OUT OF LIMITS IAW REO. WORK TO BE ACCOMPLISHED ON CP 20064968, AAR NON-ROUTINE 1018024/1000/0118 S/N: 7507204
- [SDR SWIA2020020348090](https://openairdocs.org/sdr/SWIA2020020348090.md): Floor Support · corroded · Dec 9, 2019 · N900EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LBL9 HAS CORROSION ON FLOOR SUPPORT BETWEEN FS589.0 TO FS621.0 (C-CHECK) RO 1/28/2020 EVALUATED AND FOUND TO BE OUT OF LIMITS IAW REO. WORK TO BE ACCOMPLISHED ON CP 20064973, AAR NON-ROUTINE 1018024/1000/0119 S/N: 7507205
- [SDR SWIA2020020348089](https://openairdocs.org/sdr/SWIA2020020348089.md): Seat Track · corroded · Dec 9, 2019 · N900EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 TRACK AT FS559.0+112 HAS CORROSION (C-CHECK) RO 1/28/2020 REMOVED CORRODED TRACK ( CORRODED BEYOND SRM LIMITS), FABRICATED AND INSTALLED NEW TRACK IAW BOMBARDIER REO.
- [SDR SWIA2020020348088](https://openairdocs.org/sdr/SWIA2020020348088.md): Cargo Track · corroded · Dec 9, 2019 · N900EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 CARGO TRACK HAS CORROSION AT FS559.0+94 (C-CHECK) RO 1/28/2020 REMOVED AND INSTALLED RBL9 CARGO TRACK AT FS559.0+94 IAW: CRJ200-AMM. TORQUE GUN: AAR531535 DATE:4/9/2020

Next page: https://openairdocs.org/aircraft/N900EV/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 = 'N900EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N900EV/reports

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