N135EV

Service difficulty reports · 134

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 = 'N135EV' 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 REXA2025011401094Bulkhead Web · corrodedCORROSION FOUND ON BS 280 RT BULKHEAD LOWER WEB. REPAIRED FS 280.00 R/H LOWER WEB IAW SRM 53-11-10-201-004-A01.Jan 13, 2026 · N135EV · Cndair CL6002D24 · Fuselage Main, BulkheadSDR REXA2025011401093Bulkhead Web · corrodedCORROSION FOUND ON BS 280 LT BULKHEAD LOWER WEB. INSTALLED BS 280 LT CAP ANGLE IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, AND SRM 51-42-22-001-001-A01. FABRICATED, LOCATED AND DRILLED NEW REPAIR PARTS, LHS LOWER WEB, AND LT BUTTSTRAP, IAW SRM 53Jan 13, 2026 · N135EV · Cndair CL6002D24 · Fuselage Main, BulkheadSDR REXA2025011101087Floorbeam · crackedTHE LH LOWER CORROSION CAP ANGLE PN CC670-34096-2 ON THE RH FS 280 BULKHEAD IS CRACKED. REMOVED FS 280.00 BULKHEAD LH CAP ANGLE IAW CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01. LOCATED AND DRILLED NEW FS 280.00 LH CAP ANGLE P/N: CC670-34096-2S, Jan 3, 2026 · N135EV · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026011500002Floorbeam · corrodedTHE RT FS 280 FLOORBEAM HAS DEEP CORROSION AND REQUIRES REPLACEMENT. REMOVED BS 280 RT FLOORBEAM IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01, INSTALLED A NEW RT BS 280 FLOORBEAM, IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-Dec 28, 2025 · N135EV · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026012000007Floorbeam · corrodedTHE LH FS 280 FLOOR BEAM HAS DEEP CORROSION AND REQUIRES REPLACEMENT REMOVED FS280.00 LH CROSSBEAM IAW CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01 INSTALLED NEW LH FS 280 CROSSBEAM PN CC670-34094JP-1S IAW SRM 51-42-06-0Dec 26, 2025 · N135EV · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026012000006Angle · corrodedBS 280 FWD J ANGLE IS CORRODED. REMOVED THE J ANGLE IAW SRM 51-42-06-001-001-A01, & 51-42-21-001-001-A01. LOCATED AND DRILLED NEW J-ANGLE AT FS280, P/N: CC670-34095-1S, IAW CRJ-900 SRM 51-40-11-001-001-A01. INSTALLED NEW J-ANGLE AT FS280, P/N: CC670-34095-1SDec 26, 2025 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026011500001Diaphragm · corrodedLAVATORY STRUCTURAL LANDING BELOW FWD LAV SERVICE PORT IS CORRODED. LAVATORY DIAPHRAGM IS OUT OF LIMITS IAW SRM 53-21-23-101-005-A02, DUE TO MORE THAN 30 PERCENT OF THE LENGTH OF A MEMBER IS CORRODED. LOCATED AND DRILLED A NEW SERVICEABLE FWD LAVATORY DIADec 26, 2025 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2025011101085Floorbeam · corrodedF.S. 280 FWD J ANGLE IS CORRODED. REMOVED 280 J ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW J-ANGLE AT FS280, P/N: CC670-34095-1S, IAW CRJ-900 SRM 51-40-11-001-001-A01. INSTALLED NEW J-ANGLE AT FS280, P/N: CC6Dec 26, 2025 · N135EV · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2024123001619Door · crackedLH AFT EE DOOR FWD LUG IS SUSPECTED TO BE CRACKED. REQUIRES EVAL COMPLIED WITH ENDEAVOR AIR EA CRJ952-17932 REV IR 12/10/2024Dec 29, 2024 · N135EV · Cndair CL6002D24 · Emergency ExitsSDR REXA2024123001618Door · crackedLH FWD EE DOOR FWD LUG IS SUSPECTED TO BE CRACKED. REQUIRES EVAL COMPLIED WITH ENDEAVOR AIR EA CRJ952-17934 REV IR 12/10/2024.Dec 29, 2024 · N135EV · Cndair CL6002D24 · Emergency ExitsSDR REXA2024123001617Door · crackedR/H AFT EMERGENCY EXIT DOOR AFT LUG CRACKED. COMPLIED WITH ENDEAVOR AIR EA CRJ952-17933 REV IR 12/10/2024.Dec 29, 2024 · N135EV · Cndair CL6002D24 · Emergency ExitsSDR REXA2024121601593Floor Support · corrodedCORROSION FOUND ON FLOOR SILL LEFT HAND SIDE AT FS 792 AND FS 801 ON THE OUTBOARD HOLES. COMPLIED WITH MHIRJ REO 690-53-41-506 REV-- DATED 2024-12--09Dec 7, 2024 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2024121001570None · noneWHILE PERFORMING SERVICE BULLETIN 670BA-53-044 REVISION G, DATED JUL05/2022 FOUND FITTINGS AT STR12A LH AND RH SIDES PN CC670-33563-001SB AND CC670-33562-001SB CANNOT BE INSTALLED AS DESCRIBED IN SERVICE BULLETIN DUE TO AIRCRAFT EXISTING FASTENER PITCH COMPLIEDec 4, 2024 · N135EV · Cndair CL6002D24 · Standard Practices/StructuresSDR REXA2023012600158Terminal Block · burnedAT 3500 MSL COCKPIT CREW NOTED METALLIC BURNING SMELL AND SMOKE FROM LOWER LEFT CORNER OF CAPTAINS WINDSHIELD NEAR VENT/POWER ELEMENT. CLEANED AND RESECURED LOOSE WIRES TO THE TERMINAL BLOCK REF AMM 56-11-01. PERFORMED OPS CHECK OF THE WINDOW TEMP CONTROLLER Jan 20, 2023 · N135EV · Cndair CL6002D24 · Ice/Rain Protection System WiringSDR REXA2022100402177Lamp · inoperativeR/H AFT EXTERIOR EMERG LIGHT INOP REMOVED AND REPLACED R/H AFT EXTERIOR EMERG LIGHT BULB IAW AMM 33-51-15. OPS CHECK GOOD. P/N: 8GH002473-08Sep 28, 2022 · N135EV · Cndair CL6002D24 · Emergency LightingSDR REXA2022060201044Fairing · crackedRH ENGINE UPPER COWL HINGE LINE FAIRING 443BT CRACKED PERFORMED REPAIR ON RH ENGINE UPPER COWL HINGE LINE FAIRING PER EA CRJ954-12492 REV D DATED 05/24/2022May 27, 2022 · N135EV · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2022060201045Hinge · corrodedPAX DOOR STEP 832ET, UPPER HINGE HAS AREAS OF CORROSION CA REMOVED CORRODED UPPER HINGE AND REPLACED WITH NEW HINGE PER CRJ900 SRM 51-42-06-001-001-A01May 25, 2022 · N135EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022060201043Stringer · corrodedSTGR 21R AT FS 364.00 TO FS 379.00 CORROSION PERFORMED REPAIR ON STGR 21R AT FS 364.00 TO FS 379.00 PER EA CRJ953-13542 REV IR DATED 05/05/2022May 24, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022060201049Stringer · corrodedSTGR 20R AT FS 394.00 TO 409.00 CORROSION PERFORMED REPAIR ON STGR 20R AT FS 394.00 TO 409.00 PER EA CRJ953-13497 REV IR DATED 05/03/2022May 23, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022060201048Stringer · corrodedSTGR 19R AT FS 364.00 TO FS 379.00 HAS SIGNS OF CORROSION ON UPPER SURFACE PERFORMED REPAIR ON STGR 19R AT FS 364.00 TO FS 379.00 PER EA CRJ953-13544 REV IR DATED 05/06/2022May 23, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022060201047Stringer · corrodedSTGR 21R AT FS 394.00 TO FS 409.00 CORROSION PERFORMED REPAIR ON STGR 21R AT FS 394.00 TO FS 409.00 PER EA CRJ953-13543 REV IR DATED 05/09/2022May 23, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022060201046Stringer · corrodedSTGR 20R AT FS 437.00 TO FS 453.00 CORROSION PERFORMED REPAIR ON STGR 20R FS 437.00 TO FS 453.00 PER EA CRJ953-13568May 23, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022051900954Stringer · corrodedSTGR 25R FS280.00 TO FS364.00 CORROSION PERFORMED REPAIR ON STGR 25R FROM FS 280.00 TO FS 364.00 PER EA CRJ953-12932 REV IR DATED 2/16/2022 AND CRJ953-12933 REV IR DATED 2/16/2022May 10, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022051900955Splice · corrodedSTGR 20R AT FS 477.00 CORRODED. REMOVED CORRODED JOINT SPLICE ON STGR 20R AT FS 477.00 AND REPLACED WITH NEW JOINT SPLICE ER CRJ900 SRM 51-21-06 AND 51-42-21May 4, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022050900816Stringer · corroded"STGR 24R FS 280.00 TO FS 349.00 HAS SEVERAL PITS AROUND FASTENER TAILS. " PERFORMED REPAIR ON STGR 24R FROM FS 280.00 TO FS 364.00 PER EA CRJ953-13023 REV IR DATED 3/3/2022 AND EA CRJ953-12015 REV IR DATED 3/2/2022.Apr 29, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022050900818Web · crackedSUSPECTED CRACK ON PAX DOOR AFT WEB SKIN DRAG ANGLE PERFORMED REPAIR ON PAX DOOR AFT WEB SKIN DRAG ANGLE PER CRJ900 SRM 52-11-04-201-002-A01.Apr 22, 2022 · N135EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022050900825Seal · tornCREW ESCAPE HATCH HAS TORN SEAL REMOVED, REPLACED, AND LUBRICATED CREW ESCAPE HATCH IAW CRJ900 AMM 52-22-07, AMM 12-20-52, AMM 52-22-00Apr 18, 2022 · N135EV · Cndair CL6002D24 · Emergency ExitsSDR REXA2022050900823Stringer · corrodedREPAIR REQUIRED ON STRINGER 21R FROM FS 333.00 TO FS 349.00 DUE TO CORROSION. PERFORMED REPAIR ON STRINGER 21R FROM FS 333.00 TO FS 349.00 PER EA CRJ953-13183 REV IR DATED: 4/9/2022Apr 16, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022050900822Stringer · corrodedSTGR 21R FROM FS 310.00 TO FS 333.00 CORRODED PERFORMED REPAIR ON STRINGER 21R FROM FS 310.00 TO FS 333.00 PER EA CRJ953-13182 REV IR DATED: 4/9/2022Apr 15, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022050900821Beam · crackedPAX DOOR AFT GAS SPRING SUPPORT BEAM CRACKED REMOVED CRACKED PAX DOOR GAS SPRING SUPPORT BEAM AND REPLACED WITH NEW BEAM. REF. CRJ900 SRM 51-42-06-001-001-A01Apr 14, 2022 · N135EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022050900817Plate · wornEXCESSIVE WEAR ON PAX DOOR FWD AND AFT GUIDE PLATE BLENDED OUT LIGHT WEAR ON PAX DOOR FWD AND AFT GUIDE PLATES PER CRJ900 SRM 52-11-06-201-001-A01Apr 12, 2022 · N135EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2022050900820None · wornRH ENGINE LOWER CORE COWL RUB STRIP HAS HEAVY WEAR REMOVED WORN RH ENG. LOWER CORE COWL RUB STRIP AND REPLACED WITH NEW RUB STRIP PER EA CRJ954-13184 REV A DATED: 4/5/2022.Apr 8, 2022 · N135EV · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2022050900824Stringer · corrodedSTRINGER 22R AT FS 333.00 CORRODED REMOVED AND REPLACED DAMAGED STRINGER 22R AT FS 333.00 PER CRJ900 SRM 51-42-21-001-001-A01.Apr 6, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022050900819Stringer · corrodedSTRINGER 26L BETWEEN FS 280.00 TO FS 364.00 CORRODED PERFORMED REPAIR ON STRINGER 26L BETWEEN FS 280.00 TO FS 364.00 PER EA CRJ953-12941 REV IR DATED 2/17/2022Apr 6, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2022050600815Channel · crackedAFT CARGO DOOR AFT TRACK LOWER U-CHANNEL SUPPORT BRACKET CRACKED REMOVED CRACKED U-CHANNEL BRACKET ON AFT CARGO DOOR AFT LOWER TRACK AND REPLACED WITH NEW BRACKET PER CRJ900 SRM 51-42-06-001-001-A01Apr 6, 2022 · N135EV · Cndair CL6002D24 · Cargo/Baggage DoorsSDR REXA2022050500814Stringer · corrodedSTRINGER 26R BETWEEN FS 280.00 TO FS 364.00 HAS CORROSION AROUND SEVERAL FASTENER TAILS. PERFORMED REPAIR ON STRINGER 26R BETWEEN FS 280.00 TO FS 364.00 PER ENGINEERING AUTHORIZATION CRJ953-12934 REV IR DATED 2/16/2022.Mar 31, 2022 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA201808150698Bulb · inoperativePAX DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-51-15. OPS TESTED GOOD IAW AMM 33-51-15-710-801.Aug 10, 2018 · N135EV · Cndair CL6002D24 · Emergency LightingSDR REXA201808150697Light · wornSEVERAL EMERGENCY LIGHT STRIPS WERE WORN THROGHOUT THE CABIN. REPLACED IAW AMM 33-51-01-400-801, STEP A.Aug 10, 2018 · N135EV · Cndair CL6002D24 · Emergency LightingSDR REXA2018081520696Intercostal · crackedAFTER REMOVAL OF PAX DOOR INNER SKIN FOUND AFT UPPER INTERCOSTAL DENTED AND CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11, 51-42-06, AND 51-42-21.Aug 2, 2018 · N135EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2018081520695Intercostal · crackedAFTER REMOVAL OF PAX DOOR INNER SKIN FOUND AFT LOWER INTERCOSTAL DENTED AND CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-11, 51-42-06, AND 51-42-21.Aug 2, 2018 · N135EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2018081502693Fitting · crackedPASSENGER DOOR MACHINED LINTLE CRACKED AT BS 282. REPAIRED LINTLE IAW REO 670-53-21-493, REV D.Aug 2, 2018 · N135EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2018081530691Frame · corrodedFRAME AT BS 333, STRINGER 27 WAS FOUND CORRODED. RPAIRED THE FRAME IAW SRM 53-00-06.Jul 30, 2018 · N135EV · Cndair CL6002D24 · Fuselage Main, FrameSDR REXA2018081520690Intercostal · crackedAFTER REMOVAL OF THE PAX DOOR INNER SKIN, FOUND FWD, UPPER INTERCOSTAL WAS DENTED AND CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND 51-42-21.Jul 29, 2018 · N135EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2018081528688Floor Support · corrodedAFT CARGO, LBL 27 FLOOR SUPPORT WAS CORRODED, BS 1031 - 1015. REMOVED THE CORRODED SECTION OF THE FLOOR SUPPORT AND INSTALLED A REPAIR IAW REO 670-53-00-029.Jul 28, 2018 · N135EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2018081527687Hinge · crackedPAX DOOR TOP STEP 832ET INBD HINGE WAS CRACKED AND CORRODED. REMOVED & REPLACED THE DOOR STEP HINGE IAW AMM 53-11-04.Jul 27, 2018 · N135EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2018081526692Step · crackedPAX DOOR MID STEP WAS CRACKED, LT SIDE. REMOVED THE CRACK AND FOUND WITHIN LIMITS IAW SRM 52-11-04.Jul 26, 2018 · N135EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2018081560689Attach Bracket · crackedNOSE HYDRAULIC COMPARTMENT, UPPER ACCUMULATOR, FWD ATACHMENT BRACKET CRACKED. REPLACED THE ATTACH BRACKET IAW SRM 51-42-21.Jul 26, 2018 · N135EV · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR REXA2018021400125Oxygen Mask · leakingOBSERVER`S OXYGEN MASK LEAKING. R & R THE OBSERVER`S OXYGEN MASK IAW AMM 35-11-12, OPS CHECKED GOOD.Feb 14, 2018 · N135EV · Cndair CL6002D24 · Crew Oxygen SystemSDR REXA2018012900068Connector · defectiveL BLEED DUCT WARNING CAME ON IN CRUISE FLIGHT, FOLLOWED BY RAPID DECENT TO 10000' FOLLOWED QRH CHECKLIST SUCCESSFULLY. AIRCRAFT LANDED UNEVENTFULLY. REPLACED ELBOW CONNECTIONS LT BLEED LOOP A, MT137P2, MT202P2, AND LOOP B MT203P1 IAW AMM 36-21-01 OPS TEST GOODJan 29, 2018 · N135EV · Cndair CL6002D24 · Pneumatic Indicating SystemSDR REXA2018010200008Bulb · inoperativeEMERGENCY LIGHTS IN GALLEY RT SIDE FWD & AFT HAVE BULBS OUT. REPLACED THE BULBS, OP TESTED GOOD IAW AMM 33-51-00. PJan 2, 2018 · N135EV · Cndair CL6002D24 · Emergency Lighting
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