# Service difficulty reports: N133EV

A list on [N133EV](https://openairdocs.org/aircraft/N133EV.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 4 · 197 reports

- [SDR REXA2025100200899](https://openairdocs.org/sdr/REXA2025100200899.md): Drag Angle · cracked · Jul 7, 2025 · N133EV · Cndair CL6002D24 · Fuselage, Stabilizer Attach Fittings
  > R/H AFT DRAG ANGLE IS CRACKED. REMOVED UNSERVICEABLE RH AFT DRAG ANGLE P/N:AV670-21186-004. IAW CRJ900 SRM 51-42-13-001-001-A01,SRM 51-42-21-001-001-A01 AND SRM 51-42-22-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE RH AFT DRAG ANGLE PN# AV670-21186-004 I
- [SDR REXA2024103001245](https://openairdocs.org/sdr/REXA2024103001245.md): Seat Track · corroded · Jun 13, 2024 · N133EV · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL9 LOCATED BETWEEN FS 677 AND FS 847+16 IS CORRODED. REPLACED SEAT TRACK IAW CRJ-900 SRM 53-00-49-201-002-A01 AND 51-40-11-001-001-A01.
- [SDR REXA2024103001244](https://openairdocs.org/sdr/REXA2024103001244.md): Seat Track · corroded · Jun 13, 2024 · N133EV · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL9 LOCATED BETWEEN FS 677 AND FS 847+16 IS CORRODED. REPLACED SEAT TRACK IAW CRJ-900 SRM 53-00-49-201-002-A01 AND 51-40-11-001-001-A01.
- [SDR REXA2024103001212](https://openairdocs.org/sdr/REXA2024103001212.md): Pressure Deck · damaged · May 28, 2024 · N133EV · Cndair CL6002D24 · Fuselage Main, Structure
  > WHILE COMPLYING WITH SB 670BA-53-043 WE HAVE DISCOVERED THE EXISTING HOLE @ FS 792 COMMON TO THE LBL36, PRESSURE FLOOR SKIN AND LOWER STRAP TO HAVE LOW EDGE DISTANCE ON THE BEAM AND BOTTOM STRAP IF TRANSFERRED FROM A/C TO NEW PRESSURE FLOOR ASSY. REPAIRED IAW
- [SDR REXA2024061100416](https://openairdocs.org/sdr/REXA2024061100416.md): Door · cracked · May 17, 2024 · N133EV · Cndair CL6002D24 · Emergency Exits
  > FOUND THE LH AFT OVERWING EMERGENCY EXIT TO HAVE A CRACK JUST BELOW THE UPPER AFT LUG. DOOR PN# SH670-36600, SN# SB0923. REPAIRED IAW ENDEAVOR AIR EA CRJ952-16732 REV IR DATED 5-26-2024.
- [SDR REXA2024061100415](https://openairdocs.org/sdr/REXA2024061100415.md): Door · cracked · May 17, 2024 · N133EV · Cndair CL6002D24 · Emergency Exits
  > FOUND THE LH FWD OVERWING EMERGENCY EXIT TO HAVE A CRACK JUST BELOW THE UPPER AFT LUG. DOOR PN# SH670-36600, SN# SB0924. REPAIRED IAW ENDEAVOR AIR EA CRJ952-16731 REV IR DATED 5-26-2024.
- [SDR REXA2024061100414](https://openairdocs.org/sdr/REXA2024061100414.md): Door · cracked · May 17, 2024 · N133EV · Cndair CL6002D24 · Emergency Exits
  > FOUND THE RH AFT OVERWING EMERGENCY EXIT TO HAVE A CRACK JUST BELOW THE UPPER AFT LUG. DOOR PN# SH670-36600, SN# SB0921. REPAIRED IAW ENDEAVOR AIR EA CRJ952-16733 REV IR DATED 5-26-2024.
- [SDR REXA2024061100413](https://openairdocs.org/sdr/REXA2024061100413.md): Door · cracked · May 17, 2024 · N133EV · Cndair CL6002D24 · Emergency Exits
  > FOUND THE RH FWD OVERWING EMERGENCY EXIT TO HAVE A CRACK JUST BELOW THE UPPER AFT LUG. DOOR PN# SH670-36600, SN# SB0922. REPAIRED IAW ENDEAVOR AIR EA CRJ952-16734 REV IR DATED 5-26-2024.
- [SDR REXA2024032900316](https://openairdocs.org/sdr/REXA2024032900316.md): Lamp · inoperative · Mar 21, 2024 · N133EV · Cndair CL6002D24 · Emergency Lighting
  > UPON WALK AROUND FOUND RH AFT EMERGENCY LIGHT INOP. RELAMPED RH AFT EMERGENCY LIGHT IAW CMM 33-52-07 OPS TEST GOOD A/C OK FOR SVC.
- [SDR REXA2022072801706](https://openairdocs.org/sdr/REXA2022072801706.md): Light · inoperative · Jul 22, 2022 · N133EV · Cndair CL6002D24 · Emergency Lighting
  > LEFT SIDE AFT EMERGENCY LIGHT INOP REMOVED AND REPLACED THE LH AFT OVERWING EMER LT DS102 PER AMM 33-51-15. REPAIRED DAMAGED WIRING PER ESPM 20-44-00. ALL CHECKS GOOD.
- [SDR REXA2022031000435](https://openairdocs.org/sdr/REXA2022031000435.md): Retainer · damaged · Mar 3, 2022 · N133EV · Cndair CL6002D24 · Horizontal Stabilizer Structure
  > PNL 331AL HAS A BLOWN SCREW HOLE. MARKED W/ GREEN TAPE. - REMOVED UNSERVICEABLE RETAINER ON 331AL IAW CRJ900 AMM 55-12-05-000-801-A01, SRM 51-77-00-001-001-A01. LOCATED, DRILLED & INSTALLED NEW SERVICEABLE RETAINER ON 331AL IAW CRJ900 SRM 51-40-11-001-001-A01
- [SDR REXA2022031000383](https://openairdocs.org/sdr/REXA2022031000383.md): Joint · corroded · Mar 3, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 27 FOUND CORRODED BETWEEN FS 280-FS 349 - RECEIVED & CW ENDEAVOR AIR EA CRJ 953-12750 & CRJ 953-12758 ON STGR 27 AT FS 310-FS 333 & FS 333-349, REF JOB 81522261 OP 504 FOR EDGE SEAL, PAINT & CIC. WVAC EMP STAMP # 796 MTC. REMOVED AND REPLACED STR 27 JOINT
- [SDR REXA2022031000382](https://openairdocs.org/sdr/REXA2022031000382.md): Stringer · corroded · Mar 3, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 27 FOUND CORRODED BETWEEN FS 280-FS 349 - RECEIVED & CW ENDEAVOR AIR EA CRJ 953-12750 & CRJ 953-12758 ON STGR 27 AT FS 310-FS 333 & FS 333-349, REF JOB 81522261 OP 504 FOR EDGE SEAL, PAINT & CIC. WVAC EMP STAMP # 796 MTC. REMOVED AND REPLACED STR 27 JOINT
- [SDR REXA2022031000373](https://openairdocs.org/sdr/REXA2022031000373.md): Coaming · cracked · Mar 3, 2022 · N133EV · Cndair CL6002D24 · Engine Cowling System
  > R-H-S UPPER TRANSCOWL LATCH SEAL FOUND BROKEN. - REPLACED PLACARD IAW CRJ900 AMM 20-60-04-400-801(A0)
- [SDR REXA2022031000438](https://openairdocs.org/sdr/REXA2022031000438.md): Yoke · chafed · Mar 2, 2022 · N133EV · Cndair CL6002D24 · Engine Mount Section
  > RH ENGINE YOKE LOWER SIDE IS CHAFED (MARKED WITH TAPE). - REPLACED RH ENGINE YOKE ASSY REF 81522265 OP 15 FOR WORK PERFORMED.
- [SDR REXA2022031000436](https://openairdocs.org/sdr/REXA2022031000436.md): Skin · none · Mar 2, 2022 · N133EV · Cndair CL6002D24 · Vertical Stabilizer
  > WHILE ACCOMPLISHING RAPAIR ON L/H V.STAB FWD DRAG ANGLE, TECH DRILLED INTO SKIN. - REMOVED & REINSTALLED PANEL 325AL IAW CRJ 900 AMM 55-32-32-000/400-806(A01) REPAIRED L/H VERTICLE DRAG ANGLE (FWD) IAW REO 690-55-31-064. RESTORED SURFACE & SEALED IAW SRM 51-23
- [SDR REXA2022031000396](https://openairdocs.org/sdr/REXA2022031000396.md): Intercostal · corroded · Mar 2, 2022 · N133EV · Cndair CL6002D24 · Fuselage Main, Structure
  > FORWARD JACK FITTING LEFT INTERCOSTAL CORRODED BETWEEN FS 265.00 TO FS 28.00, LBL 2.0. - REMOVED AND REPLACED L/H INTERCOSTAL AT FS 280 LBL 2.0 AND ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01 AND EA CRJ953-12903 R
- [SDR REXA2022031000388](https://openairdocs.org/sdr/REXA2022031000388.md): Channel · corroded · Mar 1, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > ANTENNA DOUBLER PLATE FOUND CORRODED BETWEEN FS 295-FS 310. BETWEEN STGRS. - REMOVED & REINSTALLED TCAS ANTENNA IAW CRJ 900 AMM 34-43-07-000/400-801(A03) REMOVED & REPLACED LOWER TCAS CHANNEL IAW SRM 51-42-06/21-001-001-A01, 51-40-11-001-001-A01. PERFORMED BON
- [SDR REXA2022031000434](https://openairdocs.org/sdr/REXA2022031000434.md): Angle · corroded · Feb 28, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER SILL PLATE CORRODED - REMOVED AND REINSTALLED CAP ANGLE ON TOP OF PAX DOOR LOWER SILL PLATE IAW CRJ900 SRM 51-41-02-001-001-A01. REMOVED AND REINSTALLED PROX SENSOR PX25 IAW CRJ900 AMM 51-70-04-000/400-802-A02. PERFORMED HEALTH CHECK OF PROX SEN
- [SDR REXA2022031000429](https://openairdocs.org/sdr/REXA2022031000429.md): Cleat · corroded · Feb 28, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORRODED STRINGER 21R FROM FS 333 TO FS 379. - REMOVED AND REINSTALLED FUEL QUANITY GAUGING COMPUTER IAW CRJ 900 AMM 28-41-22-000/400-801-A01. REMOVED INTERCOSTAL RBL 39 BETWEEN FS 349 AND 364 IAW CRJ 900 SRM 51-42-21-001-001-A01. REMOVED CLEAT P/N:SH670-32681
- [SDR REXA2022031000428](https://openairdocs.org/sdr/REXA2022031000428.md): Stringer · corroded · Feb 28, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORRODED STRINGER 21R FROM FS 333 TO FS 379. - REMOVED AND REINSTALLED FUEL QUANITY GAUGING COMPUTER IAW CRJ 900 AMM 28-41-22-000/400-801-A01. REMOVED INTERCOSTAL RBL 39 BETWEEN FS 349 AND 364 IAW CRJ 900 SRM 51-42-21-001-001-A01. REMOVED CLEAT P/N:SH670-32681
- [SDR REXA2022031000422](https://openairdocs.org/sdr/REXA2022031000422.md): Frame · corroded · Feb 28, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 364 FRAME IS CORRODED ON LOWER FLANGE AT ATTACHMENT FLANGE FOR LONGERON AT 25R - REPAIRED FRAME 364 BETWEEN STR 24L TO 24R IAW ENDEAVOR AIR EA CRJ953-12814
- [SDR REXA2022031000421](https://openairdocs.org/sdr/REXA2022031000421.md): Frame · corroded · Feb 28, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON FS319.70 AT STR 20R INTERCOSTAL ATTACH FLANGE, FWD SIDE. - RECEIVED & CW ENDEAVOR AIR EA CRJ953-12754 REV A DATED 2-11-22
- [SDR REXA2022031000404](https://openairdocs.org/sdr/REXA2022031000404.md): Splice · corroded · Feb 28, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH AVI DOOR LONGERON BETWEEN FS 364 - FS 333 IS CORRODED STR. 25R - REMOVED & REINSTALLED AVI DOOR RAILS, 2 GUSSETTS & 2 BRACKETS IAW CRJ 900 AMM 53-21-23-000/400-805(A01) & SRM 51-42-21-001-001-A01. RE-MOVED & REPLACED GUSSETT, GUIDE RAIL, & LONGERON AT STR 2
- [SDR REXA2022031000403](https://openairdocs.org/sdr/REXA2022031000403.md): Longeron · corroded · Feb 28, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH AVI DOOR LONGERON BETWEEN FS 364 - FS 333 IS CORRODED STR. 25R - REMOVED & REINSTALLED AVI DOOR RAILS, 2 GUSSETTS & 2 BRACKETS IAW CRJ 900 AMM 53-21-23-000/400-805(A01) & SRM 51-42-21-001-001-A01. RE-MOVED & REPLACED GUSSETT, GUIDE RAIL, & LONGERON AT STR 2
- [SDR REXA2022031000381](https://openairdocs.org/sdr/REXA2022031000381.md): Stringer Splice · corroded · Feb 28, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 26L BETWEEN FS 280-FS 349 FOUND CORRODED. - REPAIRED STGR 26L BETWEEN FS 280 - FS 333 IAW ENDEAVOR EA#CRJ953-12934 REV IR AND REPLACED STRINGER 26L FROM FS 364-333 IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01
- [SDR REXA2022031000380](https://openairdocs.org/sdr/REXA2022031000380.md): Stringer · corroded · Feb 28, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 26L BETWEEN FS 280-FS 349 FOUND CORRODED. - REPAIRED STGR 26L BETWEEN FS 280 - FS 333 IAW ENDEAVOR EA#CRJ953-12934 REV IR AND REPLACED STRINGER 26L FROM FS 364-333 IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01
- [SDR REXA2022031000365](https://openairdocs.org/sdr/REXA2022031000365.md): Bracket · corroded · Feb 28, 2022 · N133EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR STOP SCREW AND ANGLE ASSY CORRODED AT FS 338.963 AND BETWEEN DD5 AND DD6 - REMOVED CORROSION ON BRACKET ASSY PN 601R38921-9. BEYOND ALL ALLOWABLE DAMAGE. REQUIRES REPLACEMENT IAW CRJ 900 SRM 51-21-06-001-001-A01. INSTALLED NEW BRACKET P/N:601R38921-9
- [SDR REXA2022031000431](https://openairdocs.org/sdr/REXA2022031000431.md): Joint · corroded · Feb 26, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORRODED STRINGER 21R FROM FS 280 TO FS 333. - REMOVED CLEATS AT STR 21R FROM FS 310, FS 319, AND FS 333 IAW CRJ 900 SRM 51-42-06-001-001-A01. REMOVED UNION SPLICE FROM STR 21R AT FS 333 IAW CRJ 900 SRM 51-42-06-001-001-A01 PART CORRODED BEYOND ALLOWABLE LIMIT
- [SDR REXA2022031000430](https://openairdocs.org/sdr/REXA2022031000430.md): Stringer · corroded · Feb 26, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORRODED STRINGER 21R FROM FS 280 TO FS 333. - REMOVED CLEATS AT STR 21R FROM FS 310, FS 319, AND FS 333 IAW CRJ 900 SRM 51-42-06-001-001-A01. REMOVED UNION SPLICE FROM STR 21R AT FS 333 IAW CRJ 900 SRM 51-42-06-001-001-A01 PART CORRODED BEYOND ALLOWABLE LIMIT
- [SDR REXA2022031000427](https://openairdocs.org/sdr/REXA2022031000427.md): Drag Angle · cracked · Feb 23, 2022 · N133EV · Cndair CL6002D24 · Vertical Stabilizer
  > L/H AFT DRAG ANGLE IS CRACKED - REMOVED AND REPLACED LH AFT DRAG ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-13-001-001-A01
- [SDR REXA2022031000399](https://openairdocs.org/sdr/REXA2022031000399.md): Seat Track · corroded · Feb 22, 2022 · N133EV · Cndair CL6002D24 · Fuselage Main, Structure
  > FWD FUSELAGE L/H FLOOR SEAT TRACK #2 FS477-581 RBL9 CORRODED. - REMOVED SEAT RAIL AT RBL 9 BETWEEN FS 477 AND 581 IAW CRJ900 AMM53-00-49-000-801-A01. FABBED, LOCATED, DRILLED AND INSTALLED SEAT RAIL AT RBL 9 FS 477-581 IAW CRJ900 SRM 53-00-49-201-002-A01, 51-
- [SDR REXA2022031000395](https://openairdocs.org/sdr/REXA2022031000395.md): Intercostal · corroded · Feb 22, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STGR 20R CORRODED BETWEEN FS 310 AND FS 364. - REMOVED AND REPLACED FWD INTERCOSTAL AT STRG 20R IAW CRJ 900 SRM 51-42-06-001-001-A01. REMOVED, LOCATED, DRILLED NEW FWD AND CENTER INTERCOSTALS AT STRG 20R BETWEEN FS 310-364 IAW CRJ 900 SRM 51-40
- [SDR REXA2022031000394](https://openairdocs.org/sdr/REXA2022031000394.md): Intercostal · corroded · Feb 22, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STGR 20R CORRODED BETWEEN FS 310 AND FS 364. - "REMOVED AND REPLACED FWD INTERCOSTAL AT STRG 20R IAW CRJ 900 SRM 51-42-06-001-001-A01. REMOVED, LOCATED, DRILLED NEW FWD AND CENTER INTERCOSTALS AT STRG 20R BETWEEN FS 310-364 IAW CRJ 900 SRM 51-4
- [SDR REXA2022031000356](https://openairdocs.org/sdr/REXA2022031000356.md): Skin · corroded · Feb 22, 2022 · N133EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR INNER SKIN CORRODED IN MULTIPLE LOCATIONS ON BOTH SIDES OF SKIN. - REPLACED INNER SKIN IAW CRJ900 SRM 51-42-10-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-40-11-001-001-A01.
- [SDR REXA2022031000355](https://openairdocs.org/sdr/REXA2022031000355.md): Cover · cracked · Feb 22, 2022 · N133EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR FWD AND AFT UPPER CORNER COVERS DENTED. P/N 600-31902-287 AND 600-31902-288 - REPLACED PAX DOOR CORNER COVERS IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-10-001-001-A01, 51-42-06-001-001-A01.
- [SDR REXA2022031000432](https://openairdocs.org/sdr/REXA2022031000432.md): Angle · corroded · Feb 21, 2022 · N133EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR BOTTOM STAIR ANGLE DENTED AND CORRODED P/N: 601R317726-3 - REPLACED DAMAGED ANGLE WITH NEW PN 601R317726-3 IAW CRJ 900 SRM TASKS 51-40-11-001-001-A01, 51-42-06-001-001-A01, & 51-42-15-001-001-A01 ALSO IAW CRJ 900 SRM 51-42-13-001-001-A01.
- [SDR REXA2022031000376](https://openairdocs.org/sdr/REXA2022031000376.md): Frame · corroded · Feb 21, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME AT FS 295 CORRODED BETWEEN SGR 24R AND STGR 24L. - REPAIRED FS 295 FRAME SECTOR FROM STR 25L TO 19R PER ENDEAVOR EA CRJ953-12551, DATED 01/25/2022
- [SDR REXA2022031000437](https://openairdocs.org/sdr/REXA2022031000437.md): Yoke · chafed · Feb 18, 2022 · N133EV · Cndair CL6002D24 · Engine Mount Section
  > ON LH FWD ENGINE MOUNT YOKE FITTING, THE UPR & LWR SIDE ARE CHAFFED FROM HINGE FAIRING. - REPAIRED L/H ENGINE MOUNT YOKE IAW BOMBARDIER REO 670-71-21-057 AND MHIRJ REO 690-71-21-033
- [SDR REXA2022031000392](https://openairdocs.org/sdr/REXA2022031000392.md): Stringer · corroded · Feb 18, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 19R CORRODED BETWEEN FS 295 AND FS 310 - REMOVED AND REPLACED STR 19R BETWEEN FS 280 AND FS 310 IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR REXA2022031000390](https://openairdocs.org/sdr/REXA2022031000390.md): Intercostal · corroded · Feb 17, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL 26L FOUND CORRODED BETWEEN FS 349-FS 364. - LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTAL P/N SH670- 32077-3S PER CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2022031000389](https://openairdocs.org/sdr/REXA2022031000389.md): Angle · corroded · Feb 17, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > IN AVIONIC BAY AT FS 280 FLOOR BOARD PANEL NOT STRIP FOUND CORRODED. - REMOVED AND REPLACE AVI BAY FLOOR ANGLE AT FS 280 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2022031000386](https://openairdocs.org/sdr/REXA2022031000386.md): Joint · corroded · Feb 15, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 26R FOUND CORRODED BETWEEN FS 280-FS 349. - REPLACED STR 26R SPLICE AND STRINGER AT FS 280-333 IAW CRJ900 SRM 51- 40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01. REF 81522261 OP 504 FOR FS 333-349- PAINT DAMAGE ONLY.
- [SDR REXA2022031000385](https://openairdocs.org/sdr/REXA2022031000385.md): Stringer · corroded · Feb 15, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 26R FOUND CORRODED BETWEEN FS 280-FS 349. - REPLACED STR 26R SPLICE AND STRINGER AT FS 280-333 IAW CRJ900 SRM 51- 40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01. REF 81522261 OP 504 FOR FS 333-349- PAINT DAMAGE ONLY.
- [SDR REXA2022031000384](https://openairdocs.org/sdr/REXA2022031000384.md): Stringer · corroded · Feb 15, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 25R FOUND CORRODED BETWEEN FS 280-FS 349. - REPAIRED STR 25R IAW EA CRJ953-12673 REV IR DATED 1/1/2022.
- [SDR REXA2022031000370](https://openairdocs.org/sdr/REXA2022031000370.md): Bracket · corroded · Feb 10, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PANEL 193AL FUSELAGE ATTACHMENT FITTING FACES ARE CORRODED. 2EA. - REPAIRED AND REPLACED 193AL ATTACH FITTINGS/BRACKETS IAW CRJ 900 SRM 51-42-21-001-001-A01 AND EA CRJ 953-12977 REV IR DATED 1/24/2022.
- [SDR REXA2022031000433](https://openairdocs.org/sdr/REXA2022031000433.md): Stringer · corroded · Feb 9, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 22R IS CORRODED BETWEEN FS 280 AND FS 295 - REPLACED STR 22R F.S.280-333 IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01.
- [SDR REXA2022031000405](https://openairdocs.org/sdr/REXA2022031000405.md): Crossbeam · corroded · Feb 7, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FOUND L/H CROSSBEAM AT FS. 280 TO BE CORRODED. - REMOVED, LOCATED, DRILLED, & INSTALLED NEW SERVICEABLE LH 280 CROSSBEAM, REMOVED & INSTALLED IB & OB SHEAR BOXES, INTERCOSTAL, STANDOFF, & LH & RH DRIP TRAYS & APPLIED CIC IAW CRJ 900 SRM 51-42-06-001-001-A01, 5
- [SDR REXA2022031000406](https://openairdocs.org/sdr/REXA2022031000406.md): Crossbeam · corroded · Feb 6, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FOUND R/H CROSSBEAM AT FS. 280 TO BE CORRODED. - REMOVED, LOCATED, DRILLED & INSTALLED NEW SERVICEABLE RH 280 CROSSBEAM IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, & 51-42-22-001-001-A01 REMOVED & INSTALLED IB & OB SHEAR BO
- [SDR REXA2022031000393](https://openairdocs.org/sdr/REXA2022031000393.md): Bulkhead · corroded · Feb 6, 2022 · N133EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > BULKHEAD AT FS 280 AND APPROX RBL9 CORRODED. - REMOVED & REINSTALLED LH & RH 280 CAP ANGLES & J ANGLE TO REPLACE UNSERVICEABLE LH & RH FS 280 LOWER WEB AND DOUBLER WITH SERVICEABLE LH & RH FS 280 LOWER WEB AND DOUBLER IAW CRJ900 SRM'S 51-42-13-001-001-A01, 51-

Next page: https://openairdocs.org/aircraft/N133EV/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 = 'N133EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N133EV/reports

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