N137EV

Service difficulty reports · 147

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N137EV' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR REXA2026080701531Lamp · inoperative2 EMERGENCY FLOODLIGHT LAMPS INOP R+R 2 EMERGENCY FLOODLIGHT LAMPS P/N 3071BPE/GPL REF AMM 33-51-05. OPS CHECK GOOD.Aug 5, 2026 · N137EV · Cndair CL6002D24 · Emergency LightingSDR REXA2026060400898Door · malfunctionedPAX DOOR WONT OPEN RIGGED PAX DOOR IAW AMM 52-11-02. OPS CHECK GOOD AT THIS TIME.May 29, 2026 · N137EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026051500589Door Sill · crackedCRACK 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 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-13-001-001-A01.Apr 27, 2026 · N137EV · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026051500593Angle · brokenRTN FINDING: BROKEN ANGLE CLIP, LOCATED ON FS364.00 AND LBL27.00 OF CPAX FLOOR STRUCTURE. CLIP LOCATED ON FS364.00 AND LBL27.00 OF CPAX FLOOR STRUCTURE WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01Apr 24, 2026 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026051500596Fitting · damagedSECONDARY NRC FROM RC 900-32-710-902: AFTER BUSHING REMOVAL WERE FOUND ELONGATE FITTINGS LH/RH AT AFT NLG DOOR. FITTINGS LH/RH AT AFT NLG DOOR WERE REPLACED PER CRJ 900 SRM 51-41-02-001-001-A01 AND PER CRJ-900 AMM 20-21-00-910-801 (A01)Apr 22, 2026 · N137EV · Cndair CL6002D24 · Landing Gear DoorsSDR REXA2026051500595Fitting · damagedSECONDARY NRC FROM RC 900-32-710-902: AFTER BUSHING REMOVAL WERE FOUND ELONGATE FITTINGS LH/RH AT AFT NLG DOOR. FITTINGS LH/RH AT AFT NLG DOOR WERE REPLACED PER CRJ 900 SRM 51-41-02-001-001-A01 AND PER CRJ-900 AMM 20-21-00-910-801 (A01)Apr 22, 2026 · N137EV · Cndair CL6002D24 · Landing Gear DoorsSDR REXA2026051500600Fitting · corrodedCORROSION FLOOR FITING IN FWD ACCESS 107 AND AFT ACCESS 108 (2EAS) ON GALLEY 1 SUMMARY OF NRC 00151: FLOOR FITINGS IN FWD ACCESS 107 AND AFT ACCESS 108 (2EAS) ON GALLEY 1 WERE REPLACED PER SAFRAN CMM 25-33-67 REV.NO 10Apr 17, 2026 · N137EV · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026051500599Fitting · corrodedCORROSION FLOOR FITING IN FWD ACCESS 107 AND AFT ACCESS 108 (2EAS) ON GALLEY 1 SUMMARY OF NRC 00151: FLOOR FITINGS IN FWD ACCESS 107 AND AFT ACCESS 108 (2EAS) ON GALLEY 1 WERE REPLACED PER SAFRAN CMM 25-33-67 REV.NO 10Apr 17, 2026 · N137EV · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026051500598Fitting · corrodedCORROSION FLOOR FITING IN FWD ACCESS 306 AND ACCESS 305 (2EAS) ON GALLEY 3 SUMMARY OF NRC 00150: FLOOR FITINGS IN FWD ACCESS 306 AND 305 (2EAS) ON GALLEY 3 WERE REPLACED PER ZODIAC AEROSPACE CMM 25-33-18 REV.NO 5Apr 17, 2026 · N137EV · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026051500597Fitting · corrodedCORROSION FLOOR FITING IN FWD ACCESS 306 AND ACCESS 305 (2EAS) ON GALLEY 3 SUMMARY OF NRC 00150: FLOOR FITINGS IN FWD ACCESS 306 AND 305 (2EAS) ON GALLEY 3 WERE REPLACED PER ZODIAC AEROSPACE CMM 25-33-18 REV.NO 5Apr 17, 2026 · N137EV · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026051500588Fitting · corrodedCORROSION WAS FOUND ON LUGS BORES L2, L5 AND L6 AT LH AILERON CENTER FITTING AND SCRATCH ON HINGE 4 LOWER BORE CORROSION ON LUGS BORES L2, L5 AND L6 AND SCRATCH ON HINGE 4 LOWER BORE WERE REPAIRED PER REO 670-57-61-237 REV:--, REO 690-57-61-513 REV:-- & CLEANEApr 17, 2026 · N137EV · Cndair CL6002D24 · Wing, Control Surface Attach FittingsSDR REXA2026051500585Bracket · crackedCRACKED UPPER SUPPORT BRACKET OF PYLON TIE-BAR, THROUGH ACCESS PANEL 443BT AT RH PYLON UPPER SUPPORT BRACKET OF PYLON TIE-BAR, THROUGH ACCESS PANEL 443BT AT RH PYLON WAS REPLACED PER SRM 51-42-06-001-001-A01Apr 16, 2026 · N137EV · Cndair CL6002D24 · Engine Thrust ReverserSDR REXA2026051500594Bracket · corrodedCORROSION ON PRESS-TO-TEST INDICATOR LIGHT BRAKET BTW FS881 TO FS897.70 AND STGR 23RH TO 24RH AT AFT WASTE SERVICE PANEL CORROSION ON PRESS-TO-TEST INDICATOR LIGHT BRAKET BTW FS881 TO FS897.70 & STGR 23RH TO 24RH AT AFT WASTE SERVICE PANEL WAS REMOVED PER CRJ9Apr 15, 2026 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026051500584Door Sill · corrodedCORROSION ON LOWER SILL BTS FS 1009 AND FS 1035 (APPROX) AT AFT CARGO COMPT DOOR CUTOUT. LOWER SILL BTS FS 1009 AND FS 1035 (APPROX) AT AFT CARGO COMPT DOOR CUTOUT WAS REPAIRED PER CRJ-900 SRM 53-61-23-201-001-A01.Apr 15, 2026 · N137EV · Cndair CL6002D24 · Fuselage Main, StructureSDR REXA2026051500583Angle · crackedCRACK ON MAIN LANDING GEAR BINS SUPPORT STRUCTURE RETAINER ANGLE FS 797.00 AND RBL 34 AT RH WHEEL WELL AREA MAIN LANDING GEAR BINS SUPPORT STRUCTURE RETAINER ANGLE FS 797.00 AND RBL 34 AT RH WHEEL WELL AREA WAS REPLACED PER SRM 51-41-02-001-001-A01.Apr 15, 2026 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026051500592Duct · crackedCRACK ON APU EXHAUST DUCT (INTERNAL AREA). CRACK ON APU EXHAUST DUCT (INTERNAL AREA) WAS WELDED PER HONEYWELL CMM REPAIR 1-1.Apr 13, 2026 · N137EV · Cndair CL6002D24 · APU Cowling/ContainmentSDR REXA2024100400837Bracket · unknownWHILE INCORPORATING SB 670SH-53-043 REV C, R/H VOLUMETRIC FUSE BRACKET P/N: SH698-75355-1 FOUND TO NOT WORK WITH EXISTING A/C FASTENER HOLES (LOW ED). COMPLIED WITH MHIRJ EO SH698-75355 SNIEO S10 ALL STEPS 1-5. STEP #3 IS NOT REQUIRED DUE TO THE PART BEING FASep 17, 2024 · N137EV · Cndair CL6002D24 · Standard Practices/StructuresSDR REXA2024100400836Fitting · noneWHILE PERFORMING SB 670BA-53-044 REVISION G, DATED JUL 05/2022 FOUND FITTINGS AT STR12A LH AND RH SIDES PN CC670-33562-001SB AND CC670-33563-001SB CAN NOT BE INSTALLED IAW SERVICE BULLETIN INSTRUCTIONS DUE TO EXISTING FASTENER PITCH ON THE AIRCRAFT. REPAIRED Sep 13, 2024 · N137EV · Cndair CL6002D24 · Standard Practices/StructuresSDR REXA2024060500410Sensor · inoperativeBRAKE OVHT WARNING MESSAGE IN FIGHT. RAN QRH BUT MESSAGE APPEARED AGAIN. DEFERRING EICAS BRAKE TEMPERATURE MONTORING SENSOR FOR LHOB BREAK IAW MEL 32-46-1D. MMO2 UPDATED. PLACARD INSTALLED. MOC #102931 NOTIFIED. R/R LH OB BRAKE TEMP. SENSOR IAW CRJ 900 AMM 3May 23, 2024 · N137EV · Cndair CL6002D24 · Landing Gear Brake SystemSDR REXA2022062401385Beam · corrodedFLOOR BEAM AT LBL9.00 HAS CORROSION BETWEEN FS661+24 AND 661+90. REPAIRED FLOOR BEAM PER CRJ900 SRM 53-00-43-201-001-A03 AND REO 690-53-31-651 REV -- DATED 2022-06-20Jun 21, 2022 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022062401383Angle · corrodedCORROSION ON LOWER SILL ANGLE (BELOW LH FWD EMER DOOR) BETWEEN FS720-744. REMOVED CORROSION AND APPLIED REPAIR ANGLE REF EA:CRJ953-13834 REV IR 6/11/2022.Jun 15, 2022 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022062401379None · corrodedRH FLOOR SILL BETWEEN FS280-295 HAS AREAS OF CORROSION ON TOP AND BOTTOM SURFACES. REPLACED FLOOR SILL.Jun 15, 2022 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022062401369Frame · crackedFRAME/SH670-36600-1/CRACKED/FRAME/SH670-36600-1 FRAME/SH670-36600-1/CRACKEDJun 10, 2022 · N137EV · Cndair CL6002D24 · Emergency ExitsSDR REXA2022062301293Frame · crackedRH FWD EMERGENCY EXIT DOOR CRACK AT UPPER TANGS. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER.Jun 7, 2022 · N137EV · Cndair CL6002D24 · Emergency ExitsSDR REXA2022062301292Frame · crackedLH SIDE FWD EMERGENCY EXIT HAS CRACKS AT UPPER TANGS. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER.Jun 7, 2022 · N137EV · Cndair CL6002D24 · Emergency ExitsSDR REXA2022062301291Frame · crackedLH SIDE AFT EMERGENCY EXIT DOOR HAS CRACK AT UPPER TANGS. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER.Jun 7, 2022 · N137EV · Cndair CL6002D24 · Emergency ExitsSDR REXA2022062301290Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED, REPLACED AFT DRAG ANGLE.Jun 7, 2022 · N137EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022062401384Angle · corrodedCORROSION ON PAX DOOR FORWARD CAP ANGLE REPLACED PAX DOOR FWD CAP ANGLE.Jun 5, 2022 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022062401371None · corrodedLH SIDEWALL SEAT RAIL HAS CORROSION. FS667-FS720. REPLACED SEAT RAIL.Jun 3, 2022 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022062401382Frame · corrodedIN THE AVIONICS BAY THE FS319 LOWER FRAME SECTOR HAS CORROSION NOTED ON ITS ATTACH FLANGE AND WEB BETWEEN STGR25L AND STGR27. PERFORMED FRAME SPLICE REPAIR REF CRJ900 SRM 53-00-06-201-006-A01.Jun 2, 2022 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022062401381Intercostal · corrodedAVIONICS DOOR FWD LH LATCH PIN INTERCOSTAL CORRODED.Jun 2, 2022 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022070101452Stringer · corrodedCORROSION FOUND ON STGR 26L BETWEEN FS954 AND FS969. PERFORMED SPLICE REPAIR OF STRINGER REF EA: CRJ953.13833 REV A 6/24/2022..Jun 1, 2022 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022062401386Frame · corrodedCORROSION FOUND ON WEB AND ATTACH FLANGE AT FS847+32 BETWEEN STGR25L AND 26R. PERFORMED FRAME SPLICE REPAIR REF CRJ900 SRM 53-00-06-201-001-A03.Jun 1, 2022 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022062401378Seat Track · corrodedFLOOR SEAT TRACK LBL9 HAS FRETTING AND CORROSION FS661+32-FS677.00. REPLACED SEAT TRACK.Jun 1, 2022 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022062401375None · corrodedRH SIDEWALL SEAT RAIL HAS FRETTING AND CORROSION AT FS847+32-FS865. REPLACED SEAT RAIL.May 31, 2022 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022062401376None · corrodedRH SIDEWALL SEAT RAIL HAS FRETTING AND CORROSION FS865-FS969. REPLACED SEAT RAIL.May 31, 2022 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022062401380Intercostal · corrodedIN THE AVIONICS BAY THE INTERCOSTAL TO THE RH SIDE OF STGR 27 BETWEEN FS349 AND FS364 COMMONLY REFERED TO AS STGR 27R HAS CORROSION NOTED ON ATTACH FLANGE . REPLACED INTERCOSTAL.May 29, 2022 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022062401377Seat Track · corrodedSEAT TRACK AT LBL9, FS581-FS661+32 HAS OUT OF LIMITS CORROSION DAMAGE. REPLACED SEAT TRACK.May 29, 2022 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022062401374Seat Track · corrodedLEFT SIDE SEAT TRACK IS CORRODED FS913.00-969.00. REPLACED SEAT TRACK.May 29, 2022 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022062401373None · corrodedLH SIDEWALL SEAT RAIL HAS FRETTING AND CORROSION FS847+16-FS913 REPLACED SEAT RAIL.May 29, 2022 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022062401372None · corrodedLH SIDEWALL SEAT RAIL HAS FRETTING AND CORROSION FS744.15-FS761.85. REPLACED SEAT RAIL.May 29, 2022 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022062401370None · corrodedLH SIDEWALL SEAT RAIL FS661+16-FS 667.00 IS CORRODED. REPLACED SIDEWALL SEAT RAIL AT FS661+6-FS667.00May 17, 2022 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022062301289Panel · chafedPANEL 684AB IS CHAFED. PANEL REPLACED.May 15, 2022 · N137EV · Cndair CL6002D24 · Wing, Control SurfacesSDR REXA2022062301288Panel · chafedLEFT INBOARD FLAP LEADING EDGE PANEL 584GB IS CHAFFED. LOCATED, DRILLED, AND INSTALLED NEW PANEL 584GB PER CRJ SRM 51-40-11-001-001-A01May 12, 2022 · N137EV · Cndair CL6002D24 · Wing, Control SurfacesSDR REXA2020100500676Charger · failedMID-CABIN OVERHEAD EXIT LIT WITH BOTH EMERGENCY LIGHT SWITCHS IN OFF POSITION. R & R BATTERY CHARGER ASSY, IAW AMM 33-51-17 P/N ON/OFF 11-0049 S/N OFF 23668 S/N ON 26709. OPERATIONS CHECK GOOD.Sep 28, 2020 · N137EV · Cndair CL6002D24 · Emergency LightingSDR REXA2018092400887Smoke Detector · false activationINTEMITENT FWD LAV SMOKE MASTER WARNING IN FLIGHT. FLIGHT ATTENDENT VERIFIED NO SMOKE IN LAV IN FLIGHT. R&R FWD LAV SMOKE DETECTION IAW AMM 26-16-01, OPS CK GOOD P/N OFF ON 474560-46 S/N OFF TJA0563 S/N ON TJA0529.Sep 20, 2018 · N137EV · Cndair CL6002D24 · Smoke DetectionSDR REXA2018091000812Oxygen Mask · looseAFTER CHANGING O2 UNIT ON PREVIOUS WRITE UP, AIRCRAFT SHOWED APPROX 174. DURING FLIGHT NOTICED O2 AT 1040 AND DROPS APPROX 10 PSI EVERY COUPLE MIN. OXY LOW PRESS CAUTION ON FAIL AT GATE 880PSI. FOUND FO'S BOX AND MASK LOOSE REINSTALLED FO'S BOX AND MASK REF MSep 6, 2018 · N137EV · Cndair CL6002D24 · Crew Oxygen SystemSDR REXA2018090700808Stowage Box · inoperativeFO SIDE O2 MASK PUSH TO TEST BUTTON INOP. REMOVED AND REPLACED THE FO STOWAGE BOX IAW TECHNICAL SUPPLEMENT 001820. OPS CHECK GOOD, NO DEFECTS NOTED AT THIS TIME. A/C OKAY FOR SERVICE.Sep 6, 2018 · N137EV · Cndair CL6002D24 · Crew Oxygen SystemSDR REXA201806210523Unknown · odorDURING DESENT, A STRONG OIL ODOR WAS COMING FROM THE VENTS, THROUGHOUT CABIN & FLIGHT DECK. BLEEDS NORMAL & OOF OF ENGINES. ODOR DISSIPATED AFTER BLEEDS TRANSFERED TO APU. PERFORMED AN OPS CHECK OF THE LT AND RT PACKS WITH ENGINES AS BLEED SOURCE IAW AMJun 20, 2018 · N137EV · Cndair CL6002D24 · Air Distribution SystemSDR REXA201806210522Nacelle · contaminatedAFTER ENGINE START AND DURING FLIGHT, A STRONG OIL ODOR FROM THE A/C PACKS, ODOR IN THE COCKPIT & AFT ROWS. RAN ENGINES IAW AMM 71-00-00. RAN PACKS IAW 21-51-00. OPENED THE ENGINE COWLS AND FOUND RESIDUAL OIL. CLEANED IAW SRM 51-26-00. NO DEFECTS FOUND. Jun 20, 2018 · N137EV · Cndair CL6002D24 · Nacelle/Pylon, Main Frame
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