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 REXA201806113487Light · inoperativeRIGHT SIDE MIDDLE EMERGENCY LIGHT WAS OUT. REMOVED AND REPLACED RIGHT SIDE MIDDLE EMERGENCY LIGHT, LIGHT REMAINS INOPERATIVE. R & R THE EMERGENCY LIGHT IAW AMM 33-51-15, OPS CHECKED GOOD.Jun 10, 2018 · N137EV · Cndair CL6002D24 · Emergency LightingSDR REXA201806050444Charger · inoperativeCABIN EMERGENCY LIGHTS DS154, DS156, AND S342 WERE INOPERATIVE. REMOVED AND REPAIRED THE NR 1 EMERGENCY LIGHT BATTERY CHARGER IAW AMM 33-21-17, OPS TESTED GOOD IAW AMM 33-51-17-710-801.May 22, 2018 · N137EV · Cndair CL6002D24 · Emergency LightingSDR REXA2018060500438Former · corrodedMAIN DOOR HAD CORROSION AROUND FWD LOWER TENSION LATCH. REMOVED AND REPLACED THE FWD FORMER ON THE PAX DOOR IAW SRM 51-42-06, AND SRM 51-42-21.May 20, 2018 · N137EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA201806050443Angle · corrodedMAIN DOOR, FWD SIDE ANGLE BRACKET BELOW THE HINGED STEP WAS CORRODED. REMOVED & REPLACED THE TOP WEB PANEL IAW SRM 51-42-06, AND 51-42-13.May 19, 2018 · N137EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA201806050442Web · corrodedMAIN ENTRANCE DOOR, FWD SIDE LOWER STAIR ACCESS PANEL FRAME AREA WAS CORRODED. REMOVED & REPLACED THE FWD SIDE RISER WEB IAW SRM 51-42-06, AND 51-42-13.May 19, 2018 · N137EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA201806050441Handle · crackedTHE PAX DOOR INNER HANDLE WAS CRACKED AT THE MOUNT POINT. LOCATED & DRILLED A NEW HANDLE IAW SRM 51-40-11, INSTALLED THE HANDLE IAW WC 6273079, 1015659 8000-0074.May 19, 2018 · N137EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2018006050437Skin · corrodedMAIN DOOR FWD SIDE LOWER ACCESS DOOR CORRODED AROUND EDGE. REMOVED & REPLACED THE INNER DOOR SKIN WITH NEW FABRICATED SKIN IAW SRM 51-42-06, AND 51-42-13.May 19, 2018 · N137EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA201806050440Bracket · crackedJB-6 SUPPORT BRACKET WAS CRACKED AT THE NUTPLATE. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-42-06, AND 51-40-11.May 18, 2018 · N137EV · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR REXA201806050439Web · crackedWEB AT BS 192, WL 79.5, RT SIDE AT ADG PUMP WAS CRACKED. REPAIRED THE WEB IAW SRM 53-11-43-201-001-A01.May 15, 2018 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2018040400250Unknown · odorDURING DESCENT STRONG MILDEW ODOR THRU PACKS WITH LOW PSI 20. RAN PACK BOTH HOT AND COLD NO ODOR NOTICED IAW AMM 21-50-00.Apr 4, 2018 · N137EV · Cndair CL6002D24 · Air Distribution SystemSDR REXA2018020600101Unknown · odorA/C PACKS HAVE A FOUL ODOR. PERFORMED AN OPS TEST OF AIR CONDITIONING SYS WITH APU AND ENGINES IAW AMM 21-51-00. OPS CHECK GOOD. RAN THE LT & RT PACKS FOR OVER 1 HOUR. SUSPECT DE ICE FLUID INGESTION. ODOR IN COCKPIT DISAPPATED.Feb 6, 2018 · N137EV · Cndair CL6002D24 · Air Distribution SystemSDR REXA2018012500049Sign · detachedEXIT SIGN DETACHED. INSTALLED THE SIGN, NO DEFECTS NOTED IAW AMM 33-51-07.Jan 25, 2018 · N137EV · Cndair CL6002D24 · Emergency LightingSDR REXA2017122801296Smoke Detector · false activationDURING APPROACH, APPROX 12,000 FT, RECEIVED AN EICAS FOR THE FWD LAVATORY SMOKE WARNING, FOLLOWED ABOUT 15 SECONDS LATER BY AN AFT LAV SMOKE WARNING. . COMPLETED EMERGENCY CHECKLIST & QRH. NO VISIBLE SMOKE OR ODOR WAS DETECTED. ALARM CEASED ON OPENING THE Dec 28, 2017 · N137EV · Cndair CL6002D24 · Smoke DetectionSDR REXA2017121901270Smoke Detector · activatedSMOKE FWD LAVATORY WARNING MESSAGE. FOUND THE CIRCUIT BREAKER OPEN FOR THE LAVATORY FAN, RESET AND CLOSED BREAKER FOR THE LAVATORY FAN. PERFORMED TEST OF THE LAV SMOKE DETECTOR IAW AMM 26-16-00. OPS CHECKED GOOD. OK FOR SERVICEDec 19, 2017 · N137EV · Cndair CL6002D24 · Smoke DetectionSDR REXA2017121101244Bulb · burned outAFT FACE OF CREW STORAGE FLOOD LIGHT BULBS BURNT OUT. CONNECTED P337 TO J337 BEHIND GALLEY G2, RELAMPED D85515 AND D5159 FLOOR LEVEL EMERGANCY FLOOD LIGHTS. OPERATIONAL TEST OF THE FLOOR LEVEL EMERGANCY FLOODLIGHTS CHECKS GOOD IAW CRJ900 AMM 33-51-11Dec 11, 2017 · N137EV · Cndair CL6002D24 · Emergency LightingSDR REXA2017121001269Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED PASSENGER DOOR AFT DRAG ANGLE IAW SRM 52-11-04-201-002-A01 TYPE II.Dec 10, 2017 · N137EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR ASOA201704151449Angle · damagedHI-PRESSURE CONNECTION BOX INVOLVED IN PULL AWAY INCIDENT. REMOVED, FABRICATED AND INSTALLED STRINGER 17L RE-INFORCEMENT ANGLE IAW EC/TC EO 900-53-00-00001 REV O AND DRAWING NR CC670-35171 REV C.Apr 15, 2017 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA201704034017Bulb · burned outDURING MAINTENANCE INSPECTION, THE EXTERIOR EMERGENCY LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICApr 3, 2017 · N137EV · Cndair CL6002D24 · Emergency LightingSDR ASOA201703313069Lamp · inoperativeTHE CREW REPORTED EMERGENCY LIGHT ON RIGHT SIDE OF SERVICE DOOR NEAR THE FLOOR WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE LAMP AND OPERATIONAL CHECKED GOOD.Mar 31, 2017 · N137EV · Cndair CL6002D24 · Emergency LightingSDR ASOA201702111304Fan · failedAFT LAV SMOKE WARNING FLIGHT FL 240. REMOVED AND REPLACED LAV EXHAUST FAN IAW AMM 21-23-93 IPC 21-23-93 ITEM 5 . OPS CK GOOD.Feb 11, 2017 · N137EV · Cndair CL6002D24 · Air Distribution FanSDR ASOA2016040414687Glowstrip · missing2 SMALL AREAS OF EMERGENCY GLOW IN THE DARK STRIPS ARE MISSING IN FRONT. REPLACED MISSING EMERGENCY FLOOR PATH MARKING, PHOTOLUMINESCENT IN THE FRONT GALLEY IAW AMM 33-51-01, ACFT GOOD TO RETURN TO SERVICE.Apr 4, 2016 · N137EV · Cndair CL6002D24 · Emergency EquipmentSDR ASOA2015121014182Sign · missingOVERHEAD EXIT SIGN AT ROW 13 MISSING. REINSTALLED OVERHEAD EXIT SIGN AT CENTER AISLE SEAT ROW 13, REF AMM 25-61-00.Dec 10, 2015 · N137EV · Cndair CL6002D24 · Emergency LightingSDR ASOA2015100813872Light · missingEMERGENCY LIGHT FRONT OF CLOSED F/A REPORT MISSING. INSTALLED NEW FLOOR LIGHTING STRIP ON FLOOR IAW AMM 25-25-00. ACFT OK FOR SERVICE.Oct 8, 2015 · N137EV · Cndair CL6002D24 · Emergency LightingSDR ASOA2015082713591Lens · brokenEMERGENCY LIGHT LENS BROKEN. REPLACED THE LENS IAW AMM 33-51-11.Aug 27, 2015 · N137EV · Cndair CL6002D24 · Emergency LightingSDR ASOA2015070713265Megaphone · not reportedCABIN MEGAPHONE REQUIRES REPLACEMENT. R & R MEGAPHONE IAW AMM 25-61-14 AND AIPC REF. 25-61-14, FIG 1, ITEM 5.Jul 3, 2015 · N137EV · Cndair CL6002D24 · Emergency EquipmentSDR ASOA2015033012502Wire · disconnectedAFT EMERGENCY LIGHT ON THE RT OVERWING IS INOPERATIVE. REMOVED RT OVERWING EXT EMERGENCY LIGHT DS101 FOUND WIRE PULLED FROM PIN. REPINNED WIRE IAW ESPM 20-16 REINSTALLED LIGHT ASSY WIRE. T/S SYSTEM AND FOUND POSITIVE WIRE PULLED OUT OF THE BACK OF THE LIGHTMar 23, 2015 · N137EV · Cndair CL6002D24 · Light System WiringSDR ASOA2015033012501Spring · malfunctionedPASSENGER DOOR FAILED FUNCTIONAL CHECK. R & R FWD GAS SPRING OF THE FWD COUNTER BALANCE SYSTEM IAW AMM 52-11-17-000-801 AND 52-11-17-400-801-A01. OPS AND FUNCTIONAL TEST GOOD.Mar 22, 2015 · N137EV · Cndair CL6002D24 · Passenger/Crew DoorsSDR ASOA2015033012500Battery Pack · failedOPS TEST OF THE EMERGENCY LIGHT FAILED. FOUND NR 1 EMERGENCY BATTERY PACK TO BE UNSERVICABLE REF-AMM 33-51-17-000-801, A01 AND 33-51-17-400-801, A01. REMOVED BATTERY PACK IAW AMM 33-51-17-000-801, A02, AJPC 33-51-17-ITEM 6 INSTALLED A SERVICEABLE BATTERY PACMar 21, 2015 · N137EV · Cndair CL6002D24 · Emergency LightingSDR ASOA2015033012499Stringer · corrodedFOUND CORROSION ON STR 19R 2" AFT OF FS 437.00. REMOVED CORROSION STR 19R, 2" AFT OF FS437.00, REF: SRM 51-21-06-001-001-A01. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-03-101-007-A02. COMPLIED WITH EA 32-201-096. RECEIVED ECTC EA 32-2015-096 VERIFIMar 13, 2015 · N137EV · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR ASOA2015033012498Angle · corrodedCORROSION ON LOWER SILL ANGLE AT SERVICE DOOR FS 314. LWR SILL ANGLE CORRODED OUT OF LIMITS IAW SRM 51-21-06-001-001-A01. R & R LWR SILL ANGLE IAW SRM 51-42-06-001-001-A01. REMOVED ATTACH ANGLE FROM WEB CORRODED BEYOND LIMITS REQUIRE REPLACEMENT IAW SRM 5Mar 9, 2015 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2015032712495Angle · corrodedCORROSION AROUND ALL NUTPLATE LOCATIONS ON AFT CARGO DOOR SILL PLATE FROM FS 1000 TO FS 1047. DAMAGE ON AFT CARGO DOOR SILL PALTE FOUND TO BE OUT OF LIMITS IAW SRM 53-61-23-101-001-A01. REMOVED AFT CARGO DOOR SILL PLATE IAW SRM 51-42-06-001-001-A01, 51-42-21Mar 9, 2015 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2015032712494Attach Fitting · corrodedMID CARGO BAY CARGO ATTACH POINT CORRODED AT FS629 AND APPROXIMATELY STR 23L. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. VERIFIED ALL STEPS OF EA 32-2015-094 ARE COMPLETE. COMPLIED WITH ECTC EA 32-2016-094.Mar 9, 2015 · N137EV · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR ASOA2015032712493Attach Fitting · corrodedFWD CARGO BAY CARGO ATTACH POINT CORRODED AT FS 565 AND AT APPROXIMATELY STR 24L. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH STS EA 32-2015-093.Mar 9, 2015 · N137EV · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR ASOA2015032712492Attach Fitting · corrodedFWD CARGO BAY CARGO ATTACH POINT CORRODED AT STR 27 AND FS 565. DAMAGE WAS FOUND TO BE FAR OUT OF LIMITS. REMOVED BRACKET IAW SRM 51-42-22-001-001-A01 AND 51-42-20-001-001-A01. STARTED LOCATING FASTENER HOLES IN NEW BRACKET IAW SRM 51-40-11-001-001-A01. CMar 9, 2015 · N137EV · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR ASOA2015032712491Attach Fitting · corrodedFWD CARGO BAY CARGO ATTACH POINT CORRODED AT STR 27 AND LBL 3.4, FS 557. BEGAN REMOVING CORRISION ON FWD CARGO BAY ATTACH POINT AT STRINGS 27 BETWEEN FS 533+549 IAW SRM 51-21-06-001-001-A01. REMOVED REMAINING CORROSION FROM ATTACH POINT IAW SRM 51-21-00-001-Mar 9, 2015 · N137EV · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR ASOA2015032712490Bulkhead Web · corrodedCORROSION FOUND ON THE LT WEB AT FS280.00. REMOVED CORROSION FROM WEB AT LBL 11, FS 280 IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-11-10-201-003-A01, FIG 53-11-10-994-804. RECEIVED AND COMPLIED WITH EA 32-201-085 AS PERMANEMar 9, 2015 · N137EV · Cndair CL6002D24 · Fuselage Main, BulkheadSDR ASOA2015032712489Seat Track · corrodedSEAT TRACK SEGMENT FROM FS5661+32 TO FS677 AND AT RBL9 IS CORRODED OUT OF LIMITS. RECEIVED EC/TC REO 670-53-00-343. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN. REMOVED SEAT TRACK SEGMENT FROM FS 661+32 - FS 677 AT RBL 9 IMar 9, 2015 · N137EV · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015032712488Seat Track · corrodedSEAT TRACK SEGMENT FROM FS5661+32 TO FS677 AND AT LBL9 IS CORRODED OUT OF LIMITS. RECEIVED ECTC REO 670-53-00-343. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343 REV J AS WRITTEN. REMOVED SENT TRACK SEGMENT FROM FS 661+32- FS.677 AT LBL 9 IAWMar 9, 2015 · N137EV · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015032712487Seat Track · corrodedSEAT TRACK SEGMENT FROM FS581 TO FS661+32 AND AT RBL9 CORRODED IN SEVERAL PLACES. RECEIVED AND COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN. R & R SEAT RAIL SEGMENT AT FS581, RBL9 IAW AMM 53-00-49-000-801, CONFIG A11 AND 53-0Mar 9, 2015 · N137EV · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015032712486Seat Track · corrodedSEAT TRACK SEGMENT FROM BS 581 TO 661+32 AND AT LBL9 CORRODED OUT OF LIMITS RECEIVED & COMPLIED WITH EC/TC REO 670-53-00-343 & GREO 670-53-00-343, REV J AS WRITTEN. R & R SEAT RAIL SEGMENT FS 581, LBL9 IAW AMM 53-00-49-000-801, CONFIG A11 & 53-00-49-400-801 Mar 9, 2015 · N137EV · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015032712485Seat Track · corrodedSEAT TRACK SEGMENT CORRODED BETWEEN FS 485 AND FS 581 AT RBL 9. RECEIVED EC/TC REO 670-53-00-343. REMOVED SEAT TRACK AT RBL BETWEEN FS 485- FS 581 IAW AMM 53-00-49-000-801-A01-A11. INSTALLED NEW SEAT TRACK SEGMENT BETWEEN FS 485 AND FS 581 AT RBL 9 IAW AMM Mar 9, 2015 · N137EV · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015032712484Floor Support · corrodedCORROSION ON SERVICE DOOR FLOOR SUPPORT ANGLE AT FS 314. CORRODED BEYOND LIMITS IAW SRM 51-21-06-001-001-A01. REMOVED SERVICE DOOR FLOOR SUPPORT ANGLE AT SERVICE DOOR 51-42-06-001-001-A01. INSTALLED SERVICE DOOR FLOOR SUPPORT ANGLE AT SERVICE DOOR FLOOR SILMar 9, 2015 · N137EV · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR ASOA2015032712483Skin · damagedBLEND ON COUNTER SINK AT FS 913.00 AND 2.7" BELOW STRINGER 16L REF W/O 299955, N/R 00042 FOUND UPON TEMP FASTENER REMOVAL. MEASURED BLEND AT RIVET COUNTERSINK BLEND MEASURES 0.029", DEEP X 0.350", WIDE X 0.200 LONG DANAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-Mar 9, 2015 · N137EV · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR ASOA2015032712482Skin · damagedLIGHTNING STRIKE TEMP FASTENER AT FS 847+16 BETWEEN STRS 14L + 15L. TEMP FASTENER AT FS 847+16 BETWEEN STRS 14L AND 15L. REMOVED FINISH AT TEMP FASTENER IAW SRM 51-26-00-001-001-A01 REMOVED TEMP FASTENER IAW SRM 51-42-13-001-001-A01. INSTALLED RIVETS IAW SMar 9, 2015 · N137EV · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR ASOA2015032712481Skin · damagedLIGHTING STRIKE TEMP FASTENER AT FS 661+62 BETWEEN STRS 12L + 13L. TEMP FASTENER AT FS661 BETWEEN STR 12L + 13L REMOVED FINISH AT TEMP FASTENER IAW SRM 51-26-00-001-001-A01 REMOVED TEMP FASTENER IAW SRM 51-42-13-001-001-A01. INSTALLED RIVETS IAW SRM TEMPORARMar 9, 2015 · N137EV · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR ASOA2015032612475Floorbeam · corroded2EA FLOORBEAM PACKERS CORRODED AT RBL9 AND FS 333. R & R 2 EA PACKERS WITH NEW PACKERS IAW SRM 51-42-00-001-001-A01.Mar 8, 2015 · N137EV · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR ASOA2015032612474Floorbeam · corroded1 EACH FLOORBEAM PACKER CORRODED AT RBL9 AND FS 349. REMOVED CORRODED PACKER AND REPLACED WITH NEW PACKER IAW SRM 51-42-06-001-001-A01.Mar 8, 2015 · N137EV · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR ASOA2015032612473Seat Track · corrodedGALLEY 2 FLOOR TIE DOWN CORRODED ON RBL9 SEAT TRACK. REMOVED CORRODED FITTING AND INSTALLED NEW SERVICABLE FITTING GALLEY NR 2 LOCATION RBL9 IAW SRM 51-41-02-001-001.Mar 8, 2015 · N137EV · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015032612472Door Frame · corrodedRIGHT COCKPIT DOOR POST CORRODED AT FS 280 BEAM. BOTTOM OF DOOR POST CORRODED 100 PERCENT MATERIAL LOSS, RBL11, FS280 IAW SRM 51-21-06-001-001-A01. COMPLIED WITH EA 32-2015-087 P1, STEPS 1 (A-I). RECEIVED ECTC EA 32-2015-087 AND EA 32-2015-087 FINAL. VERIMar 8, 2015 · N137EV · Cndair CL6002D24 · Fuselage Main, StructureSDR ASOA2015032612471Door Frame · corrodedLT COCKPIT DOOR POST CORRODED AT FS 280 BEAM. BOTTOM OF DOOR POST CORRODED 100 PERCENT MATERIAL LOSS, RBL11, FS280 IAW SRM 51-21-06-001-001-A01. COMPLIED WITH STS EA 32-2015-086 P1, STEPS 1 (A-I). RECEIVED EA 32-2015-086 FINAL. VERIFIED ALL STEPS PREVIOUSMar 8, 2015 · N137EV · Cndair CL6002D24 · Fuselage Main, Structure
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