# Service difficulty reports: N131EV

A list on [N131EV](https://openairdocs.org/aircraft/N131EV.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 5 · 205 reports

- [SDR REXA2026091101796](https://openairdocs.org/sdr/REXA2026091101796.md): Door · inoperative · Sep 10, 2026 · N131EV · Cndair CL6002D24 · Passenger/Crew Doors
  > ALL EXTERIOR DOORS WOULD NOT OPEN. CONTACTED MAINTENANCE AND CONTRACT MAINTENANCE. PERFORMED OPS CHECK OF PAX DOOR,SERVICE DOOR & AFT CARGO DOOR, REF AMM 52-11-00,& 52-41-00& 52-31-00.
- [SDR REXA2026090801781](https://openairdocs.org/sdr/REXA2026090801781.md): Door · lack of lube · Aug 27, 2026 · N131EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR AND GALLEY SERVICE DOOR WILL NOT OPEN FROM OUTSIDE LUBED DOORS IAW AMM 12-20-52 OPS TEST GOOD. IAW AMM 52-11-08.
- [SDR REXA2025101400947](https://openairdocs.org/sdr/REXA2025101400947.md): Rib · cracked · Sep 21, 2025 · N131EV · Cndair CL6002D24 · Wing, Rib/Bulkhead
  > AFTER REMOVAL OF WING ACCESS PANEL 521BL AT LEFT WING TO PERFORM LUBRICATION OF SLAT TORQUE TUBES, CRACK ON MACHINED RIB LEADING EDGE SS57.16 AT LEFT WING MACHINED RIB LEADING EDGE SS57.16 AT LEFT WING WAS REPAIRED PER REO 690-57-41-549 REV.--
- [SDR REXA2025101400945](https://openairdocs.org/sdr/REXA2025101400945.md): Web · cracked · Sep 9, 2025 · N131EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB LEFT SIDE (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00. ELECTRICAL BAY FLOOR WEB LEFT SIDE (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER EA CRJ953-20131 REV.A.
- [SDR REXA2025101400944](https://openairdocs.org/sdr/REXA2025101400944.md): Web · cracked · Sep 9, 2025 · N131EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. CRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPAIRED IAW EA CRJ953-20206 REV.IR
- [SDR REXA2025101400940](https://openairdocs.org/sdr/REXA2025101400940.md): Frame · damaged · Sep 7, 2025 · N131EV · Cndair CL6002D24 · Fuselage Main, Frame
  > AFTER EXTERNAL RECEPTACLE SUPPORT REMOVAL, ELONGATED HOLES ON FRAME LOCATED IN FS202.75. WERE FOUND. FRAME LOCATED IN FS202.75. REPAIRED PER REO 690-53-11-2063 REV.--
- [SDR REXA2025101400939](https://openairdocs.org/sdr/REXA2025101400939.md): Angle · chafed · Sep 7, 2025 · N131EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION: WEAR ON ANGLE AT AFT FUSELAGE LOWER STRUCTURE BTW 55.63%/67.50%REAR SPAR DATUM AND STGR26R/26L. WEAR ON ANGLE AT AFT FUSELAGE LOWER STRUCTURE BTW 55.63%/67.50%REAR SPAR DATUM AND STGR26R/26L WAS FOUND DUE EXCESIVE DAMAGE THEREFORE WAS FABRI
- [SDR REXA2025101400937](https://openairdocs.org/sdr/REXA2025101400937.md): Skin · corroded · Sep 7, 2025 · N131EV · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION AT SETTLEMENT STRAPS OF BODY FAIGINS 193AR & 193AL CORROSION AT SETTLEMENT STRAPS OF BODY FAIGINS 193AL WAS REMOVED AND EVALUATED WITHIN LIMITS PER CRJ/900 SRM 51-21-06-001-001-A01 AND SRM 53-00-00-101-001-A01 AND STRAPS OF BODY FAIGINS 193AR WAS
- [SDR REXA2025101400936](https://openairdocs.org/sdr/REXA2025101400936.md): Skin · corroded · Sep 7, 2025 · N131EV · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > CORROSION AT EXTERNAL FUSELAGE SKIN, SETTLEMENT AREA OF AFT BODY FAIRING, 195DL, 196DR, 196AR & 195AL AREA OF AFT BODY FAIRING, 195DL, 196DR, 196AR & 195A OF CORROSION REMOVED AND EVALUATED WITHIN LIMITS ON SETTLEMENT AREA OF AFT BODY FAIRING (LT SIDE) FS847
- [SDR REXA2025101400935](https://openairdocs.org/sdr/REXA2025101400935.md): Angle · corroded · Sep 7, 2025 · N131EV · Cndair CL6002D24 · Aerodynamic Fairings
  > CORROSION AT UNION ANGLE BTW AT AFT BODY FAIRING FRAME FS 881.00 CORROSION ON UNION ANGLE BTW AT AFT BODY FAIRING FRAME FS 881.00 WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-82-55-101-002-A02 AND WAS FABRIC
- [SDR REXA2025101400934](https://openairdocs.org/sdr/REXA2025101400934.md): Support Bracket · cracked · Sep 7, 2025 · N131EV · Cndair CL6002D24 · Wing Miscellaneous Structure
  > CRACKED LH WING BRAKET SUPPORT ANGLE SS 15.50 LH WING BRAKET SUPPORT ANGLE SS 15.50 WAS REPLACED PER EA CRJ957-20250 REV. IR AND PER CRJ900 SRM 51-42-06-001-001-A01
- [SDR REXA2025101400932](https://openairdocs.org/sdr/REXA2025101400932.md): Hinge · corroded · Sep 3, 2025 · N131EV · Cndair CL6002D24 · Fuselage, Door Hinge
  > AFTER TO REMOVAL NLG AFT DOOR, WAS FOUND CORROSION ON NLG AFT DOOR HINGE FITTINGS BORE. (FUSELAGE AREA). NLG AFT DOOR HINGE FITTINGS BORE WAS FOUND DUE TO EXCESSIVE ALLOWABLE DAMAGE AND WERE REPLACED PER CRJ900 SRM 53-00-00-101-001-A01 AND SRM 51-42-21-001-001
- [SDR REXA2025101400931](https://openairdocs.org/sdr/REXA2025101400931.md): Fitting · corroded · Sep 3, 2025 · N131EV · Cndair CL6002D24 · Landing Gear Doors
  > AFTER TO REMOVAL NLG AFT DOOR, WAS FOUND CORROSION ON NLG AFT DOOR HINGE FITINGS BORE. CORROSION ON NLG AFT DOOR HINGE FIITINGS BORE WAS FOUND WITH EXCESIVE DAMAGE THEREFORE FITTINGS WERE REPLACED PER CRJ-900 SRM 53-00-00-101-001-A01 AND SRM 51-41-02-001-001
- [SDR REXA2025101400930](https://openairdocs.org/sdr/REXA2025101400930.md): Plate · cracked · Sep 3, 2025 · N131EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INITIAL INSPECTION:CRACK ON DIAPHRAGM BTW FS= 797 TO FS= 807 LBL 35 ON FWD AREA W/W AT MLG. DIAPHRAGM BTW FS= 797 TO FS= 807 LBL 35 ON FWD AREA W/W AT MLG WAS REPLACED PER CRJ900 SRM 51-41-02-001-001-A01
- [SDR REXA2025101400928](https://openairdocs.org/sdr/REXA2025101400928.md): Hinge · cracked · Sep 3, 2025 · N131EV · Cndair CL6002D24 · Fuselage, Door Hinge
  > CRACK ON AFT HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT. AFT HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WAS REPLACED PER SRM 51-42-06-001-001-A01
- [SDR REXA2025101400927](https://openairdocs.org/sdr/REXA2025101400927.md): Fitting · chafed · Sep 3, 2025 · N131EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION': WEAR ON FLAP FITTING OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE FLAP FITTING OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE WAS FOUND DUE TO EXCESSIVE ALLOWABLE DAMAGE AND WERE REPLACED PER
- [SDR REXA2025101400926](https://openairdocs.org/sdr/REXA2025101400926.md): Plate · chafed · Sep 3, 2025 · N131EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "INITIAL INSPECTION': WEAR ON PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH WING TRAILING EDGE WAS FOUND DUE TO EXCESSIVE ALLOWABLE DAMAGE AND WERE REPLACED P
- [SDR REXA2025101400925](https://openairdocs.org/sdr/REXA2025101400925.md): Door Frame · cracked · Sep 3, 2025 · N131EV · Cndair CL6002D24 · Fuselage Main, Structure
  > CRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR). AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01
- [SDR REXA2025101400924](https://openairdocs.org/sdr/REXA2025101400924.md): Striker · corroded · Sep 3, 2025 · N131EV · Cndair CL6002D24 · Service Doors
  > INITIAL INSPECTION:CORROSION ON STRIKER SEAL OF LOWER SEAL AT GALLEY SERVICE DOOR. CORROSION ON STRIKER SEAL OF LOWER SEAL AT GALLEY SERVICE DOOR WAS REMOVED, AND WAS EVALUATED OUT LIMITS THEREFORE WAS REPLACED PER CRJ-900 SRM 51-21-06-001-001-A01, SRM 53-21-
- [SDR REXA2025101400922](https://openairdocs.org/sdr/REXA2025101400922.md): Retainer · cracked · Sep 3, 2025 · N131EV · Cndair CL6002D24 · Cargo/Baggage Doors
  > CRACK ON SEAL RETAINER, AFT SIDE AT CTR BAGGAGE BAY DOOR. SEAL RETAINER AFT SIDE AT CTR BAGGAGE BAY DOOR WAS REPLACED PER CRJ900 SRM 51-40-11-001-001-A01 AND WILL BE ATTENDED IN NRC 181
- [SDR REXA2025042900527](https://openairdocs.org/sdr/REXA2025042900527.md): Printer · inoperative · Apr 23, 2025 · N131EV · Cndair CL6002D24 · Flight Compartment Equipment
  > AFTER SENDING PDC TO THE PRINTER IT STARTING SMOKING AND PRINTED BURNT PAPER. REPLACED ACARS PRINTER PER AMM 23-22-05. OPS TEST GOOD.
- [SDR REXA2024120601556](https://openairdocs.org/sdr/REXA2024120601556.md): Hydraulic Line · leaking · Dec 2, 2024 · N131EV · Cndair CL6002D24 · Hydraulic System, Main
  > HYD SYSTEM 3 QUANTITY ZERO ON FINAL. PER QRH PULLED MANUAL GEAR EXTENSION. FOUND LEAK AT HYDRAULIC #3 GEAR DOWN LINE AT F.S. 355.00 AND REPAIRED LINE PER AMM 20-30-00. SERVICED HYDRAULIC #3 IAW AMM 12-12-29. LEAK CHECK GOOD. DUE TO LEAK REMOVED AND REPLACED
- [SDR REXA2024102500960](https://openairdocs.org/sdr/REXA2024102500960.md): Light · inoperative · Oct 25, 2024 · N131EV · Cndair CL6002D24 · Emergency Lighting
  > EMERG EXTERNAL LIGHT INOP REMOVED AND REPLACED EMERG EXTERNAL LIGHT IAW CRJ 900 AMM 33-51-15 OPS CHECK GOOD AT THIS TIME P/N ON/OFF 2LA006954-00
- [SDR REXA2024090500682](https://openairdocs.org/sdr/REXA2024090500682.md): Lamp · inoperative · Sep 3, 2024 · N131EV · Cndair CL6002D24 · Emergency Lighting
  > DURING WALK AROUND FOUND RH EXTERNAL EMERGENCY LIGHT INOP R/R RH EXTERNAL EMERGENCY LIGHT BULB IAW CMM 33-51-02 OPS CHECK GOOD
- [SDR REXA2024103001210](https://openairdocs.org/sdr/REXA2024103001210.md): Lug · cracked · Aug 5, 2024 · N131EV · Cndair CL6002D24 · Emergency Exits
  > R/H AFT EMERGENCY EXIT DOOR 845, P/N SH670-36600, S/N SB 0901 AFT LUG IS CRACKED. REPAIRED DAMAGE I.A.W. ENDEAVOR EA# CRJ952-16979 REV.IR, DATED 07/25/2024.
- [SDR REXA2024103001168](https://openairdocs.org/sdr/REXA2024103001168.md): Lug · cracked · Aug 5, 2024 · N131EV · Cndair CL6002D24 · Emergency Exits
  > L/H FORWARD EMERGENCY EXIT DOOR 835, P/N SH670-36600, S/N SB 0904 AFT LUG IS CRACKED. REPAIRED DAMAGE I.A.W. ENDEAVOR EA# CRJ952-16977 REV.IR, DATED 07/25/2024.
- [SDR REXA2024080600622](https://openairdocs.org/sdr/REXA2024080600622.md): Lug · cracked · Aug 5, 2024 · N131EV · Cndair CL6002D24 · Emergency Exits
  > R/H FORWARD EMERGENCY EXIT DOOR 843, P/N SH670-36600, S/N SB 0903 AFT LUG IS CRACKED. REPAIRED DAMAGE I.A.W. ENDEAVOR EA# CRJ952-16978 REV.IR, DATED 07/25/2024.
- [SDR REXA2022042700713](https://openairdocs.org/sdr/REXA2022042700713.md): None · corroded · Apr 21, 2022 · N131EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR BEAM IS CORRODED AT FS 661+32 - REPAIRED FLOOR BEAM AT LBL9 BETWEEN FS. 661+32 & FS. 693 IAW SNIEO SH670-33413-501 & MHIRJ REO: 690-53-31-647 & SNIEO: SH690-3340-501 REMOVED & REINSTALLED SPOT TRACK IAW CRJ900 AMM 53-00-49- 000/400-801-A07 FOR ACCE
- [SDR REXA2022042700707](https://openairdocs.org/sdr/REXA2022042700707.md): Frame · corroded · Apr 21, 2022 · N131EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FRAME AT FS 847+32 HAS MULTIPLE SPOTS OF CORROSION FROM STGR 26L TO 26R. - CORROSION REPAIRED IAW EA'S CRJ953-13109 REV IR DATED 3/24/2022, CRJ 953-13110 REV IR DATED 3/15/2022, AMM 21-23-38-000/400-804-A01, 21-23-00-790-801-A01, SRM 51-42-21-001-001-A01, 51-4
- [SDR REXA2022042700734](https://openairdocs.org/sdr/REXA2022042700734.md): Intercostal · corroded · Apr 19, 2022 · N131EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > 2 INTERCOSTALS BETWEEN FS 333.00 & FS 364.00 AT STR. 20R ARE CORRODED - REMOVED AND INSTALLED WATER HOSE F.S. 333-349, CLEATS AND CANNON PLUG BRACKET, REPLACED INTERCOSTALS AND INSTALLED MOUNTING BRACKET AND APPLIED CIC IAW CRJ 900 AMM 38-32-01-400-801-A02, SR
- [SDR REXA2022042700733](https://openairdocs.org/sdr/REXA2022042700733.md): Intercostal · corroded · Apr 19, 2022 · N131EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CONTINUATION OF JOB 81521761 OP 531; 2 INTERCOSTALS BETWEEN FS 333 AND FS 364 AT STR 20R ARE CORRODED. - REMOVED AND INSTALLED WATER HOSE F.S. 333-349, CLEATS AND CANNON PLUG BRACKET, REPLACED INTERCOSTALS AND INSTALLED MOUNTING BRACKET AND APPLIED CIC IAW CRJ
- [SDR REXA2022042700754](https://openairdocs.org/sdr/REXA2022042700754.md): Splice · corroded · Apr 17, 2022 · N131EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > 22R STRINGER SPLICE AT FS 333 IS CORRODED. TCI#: 53-20-304. - REPLACED 22R STRINGER SPLICE IAW CRJ900 SRMS 51-42-06-001-001-A01 & 51-40-11-001-001-A01. REMOVED & REINSTALLED #2 DME TRANSCEIVER IAW CRJ900 AMMS 34-53-01-000/400-801-A01. OPS CHECK GOOD. REMOVED &
- [SDR REXA2022042700755](https://openairdocs.org/sdr/REXA2022042700755.md): Cleat · corroded · Apr 12, 2022 · N131EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STRINGER 22R BETWEEN FS 319.70 TO FS 333 HAS 2 STRINGER CLIPS CORRODED. - FABBED CLEATS FOR 22R 319 - 333 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 53-00-06-001-001-A01, 51-40-11-001-001-A01, & DRAWINGS SH670-35625 & SH670-31253.
- [SDR REXA2022042700730](https://openairdocs.org/sdr/REXA2022042700730.md): None · corroded · Apr 12, 2022 · N131EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 20L ATTACHMENT CLIP TO FS 295 FRAME IS CORRODED. - REPLACED CLIP AT FS 295 20L IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01.
- [SDR REXA2022042700706](https://openairdocs.org/sdr/REXA2022042700706.md): Frame · corroded · Apr 12, 2022 · N131EV · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FRAME AT FS1000 HAS MULTIPLE SPOTS OF CORROSION FROM STGR 24L TO 24R. - REMOVED AND INSTALLED DISTRIBUTION DUCT, REPAIRED FRAME FS 1000 24L-24R IAW CRJ 900 AMM 21-23-44-400-801-A01, CRJ 900 SRM 51-42-06-001-001-A01 AND EA CRJ 953-13089 REV A DATED 3/13/22.
- [SDR REXA2022042700702](https://openairdocs.org/sdr/REXA2022042700702.md): Frame · corroded · Apr 12, 2022 · N131EV · Cndair CL6002D24 · Fuselage Main, Frame
  > FS 364 LOWER FRAME SEGMENT CORRODED BETWEEN STGR 25L AND 25R. TCI: 53-20-305 - REPAIRED FS 364 FRAME, INSTALLED AVI BAY PROX SWTICH, HYDRAULIC TUBE COVERS, INSTALLED LONGERON AT STGR 25R (FS 364-394), INSTALLED FITTINGS, AND PERFORMED EDDY CURRENT INSPECTION I
- [SDR REXA2022042700720](https://openairdocs.org/sdr/REXA2022042700720.md): Stringer · corroded · Apr 11, 2022 · N131EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > STGR 21R IS CORRODED BETWEEN FS 485 AND FS 501. - DISPLAYED AND REINSTALLED WIRE BUNDLE BETWEEN STGR 20R AND 22R AND BETWEEN FS 485 AND FS 501. REMOVED AND REPLACED AC CIC AND AC DCUT AND WIRING BETWEEN STGR 20R AND 21R AND FS 485 TO 51 REMOVED CORRODED SECTIO
- [SDR REXA2022042700691](https://openairdocs.org/sdr/REXA2022042700691.md): Door Sill · corroded · Apr 11, 2022 · N131EV · Cndair CL6002D24 · Cargo/Baggage Doors
  > AFT BAGGAGE BAY DOOR SILL IS CORRODED BETWEEN FS 1000 TP FS 1047.00. - REPLCED SILL INSTALLED LOWER COAMING, TIEDOWN BRACKETS AND RELATED NUTPLATES AND BRACKETS AT AFT CARGO DOOR SILL IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 54-42-20-001-001
- [SDR REXA2022042700732](https://openairdocs.org/sdr/REXA2022042700732.md): Intercostal · corroded · Apr 10, 2022 · N131EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > 2 INTERCOSTALS BETWEEN FS 310.00 AND FS 333.00 AT STRINGER 20R ARE CORRODED. - REMOVED/LOCATED/DRILLED AND INSTALLED 2 SERVICEABLE INTERCOSTALS BETWEEN FS 310-333 STR 20R, ATTACHED BRACKET,WIRE BUNDLE,JB-10 MOUNTING TRAY AND CIC IAW CRJ 900 SRM 53-21-23-101-00
- [SDR REXA2022042700704](https://openairdocs.org/sdr/REXA2022042700704.md): Floorbeam · corroded · Apr 10, 2022 · N131EV · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FLOOR BEAM AT RBL27 HAS MULTIPLE SPOTS OF CORROSION FROM FS 1000 TO FS 1088. - REPAIRED FLOOR BEAM RBL 27 FS 1000-FS 1088 IAW CRJ 900 SRM 51-25-01-001-001-A01, 51-41-02-001-001-A01, 53-00-41-201-001-A03, AMM 53-00-49-400 801-A07, AND EA CRJ 953-13075 REV IR 03
- [SDR REXA2022042700703](https://openairdocs.org/sdr/REXA2022042700703.md): Floor Panel · corroded · Apr 10, 2022 · N131EV · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RH FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM FS 988 TO FS 1088. - REPAIRED FLOOR SILL IAW EA CRJ 953-13092 REV IR, SRM 51-42-10-001-001-A01 AND SRM 51-25-10-001-002-A01.
- [SDR REXA2022042700751](https://openairdocs.org/sdr/REXA2022042700751.md): Frame · corroded · Apr 9, 2022 · N131EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 333 BETWEEN STR 18R AND 20R CORRODED. - WORK SUMMARY STATEMENT REQUIRED. WVAC 712 MTC 4/7/22 C/A: 9. REMOVED AND REPLACED FRAME SECTION AT FS 333 BETWEEN STGR 18R AND 20R IAW ENDEAVOR AIR EA CRJ 953-13229 REV IR DATE 4/4/2022 AND LOCATED AND DRILLED NEW GUS
- [SDR REXA2022042700745](https://openairdocs.org/sdr/REXA2022042700745.md): Angle · corroded · Apr 7, 2022 · N131EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FWD WATER WASTE SERVICE DOOR SURROUND DIAPHRAGM CORRODED JUST AFT OF FS 379.00, STR 23R. - REPLACED ANGLE P/N: SH670-32310-1 IAW CRJ-900 SRMS 51-40-11-001-001-A01 & 51-42-06-001-001-A01. REPAIRED DISCREPANT AREA IAW ENDEAVOR EA CRJ953-13159 REV IR DATED 3-24-2
- [SDR REXA2022042700744](https://openairdocs.org/sdr/REXA2022042700744.md): Rib · cracked · Apr 7, 2022 · N131EV · Cndair CL6002D24 · Wing, Attach Fittings
  > LEADING EDGE SKIN PANEL 522BL IS BENT NEAR FS 249.04 MARKED WITH RED TAPE - REPAIRED PROTRUDING DENT IAW ENDEAVOR EA CRJ 957-13243 REV IR & REPAIRED BROKEN RIB IAW ENDEAVOR EA CRJ 957-13204 REV IR & REMOVED TAPE
- [SDR REXA2022042700715](https://openairdocs.org/sdr/REXA2022042700715.md): None · corroded · Apr 7, 2022 · N131EV · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RBL 9 FLOOR BEAM IS CORRODED AT FS 685. - REPAIRED IAW ENDEAVOR EA CRJ 953-13208 RV IR & RECEIVED, LOCATED, DRILLED, DEBURRED AND REPLACED FACTORY SPLICE IAW CRJ900 SRM'S 51-40-11-001-001-A01 & 51-42-21-001-001-A01.
- [SDR REXA2022042700690](https://openairdocs.org/sdr/REXA2022042700690.md): None · cracked · Apr 7, 2022 · N131EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PASSENGER DOOR FWD AND AFT UPPER CORNERS ARE DENTED. - OUT OF LIMITS PER CRJ900 SRM 52-11-01-201-004-A01 FOR VISUAL CRACK. DRILLED & LOCATED SERVICEABLE CORNER COVER IAW CRJ900 SRM 51-401-11-001-001-A01. REF MWC JOB 81521761 OP: 561 FOR INSTALL OF FWD & AFT CO
- [SDR REXA2022042700746](https://openairdocs.org/sdr/REXA2022042700746.md): Fitting · none · Apr 5, 2022 · N131EV · Cndair CL6002D24 · Wing Structure
  > RH AILERON LUG MARKED "G" HAS OS BORE, REQUIRES FABRICATION OF BUSHING. - COMPLIED WITH BOMBARDIER REO 670-57-61-237 REV -- DATED 2017-07-25.
- [SDR REXA2022042700743](https://openairdocs.org/sdr/REXA2022042700743.md): Bracket · cracked · Apr 5, 2022 · N131EV · Cndair CL6002D24 · Passenger/Crew Doors
  > CABLE SUPPORT BRACKET ON FWD WEB OF PAX DOOR IS CRACKED WITH MATERIAL MISSING ON CORNER. (P/N B0816005-17359) - REMOVED AND REPLACED CABLE SUPPORT BRACKET ON FWD WEB, P/N B0816005-17359, IAW CRJ 900 SRM 51-42-13-001-001-A01.
- [SDR REXA2022042700753](https://openairdocs.org/sdr/REXA2022042700753.md): Drag Angle · none · Apr 4, 2022 · N131EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE HAS ELONGATED FASTENER HOLES WHERE POWER ASSIST PULLEY BRACKET ATTACHES. - REMOVED AND REPLACED AFT DRAG ANGLE P/N 601R31772-5 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-13-001-001-A01
- [SDR REXA2022042700752](https://openairdocs.org/sdr/REXA2022042700752.md): Web · corroded · Apr 4, 2022 · N131EV · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT WEB HAS CORROSION AT LOWER STEP AREA. - REMOVED AND REPLACED AFT WEB P/N 601R317071-11 IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-02-001-001-A01.

Next page: https://openairdocs.org/aircraft/N131EV/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 = 'N131EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N131EV/reports

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