N917EV
Service difficulty reports · 231
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 = 'N917EV' 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.
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 = 'N917EV' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWIA2020090252177Floorbeam · crackedLT F.S. 484.00 ANGLES AT LBL 36 AND LBL 27 ARE CRACKED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED CRACKED ANGLE AT F.S. 484 LBL27 IAW CRJ 200 SRM. REFERENCE CAMP #21306170 FOR REPAIR OF LBL 36 ANGLE AT F.S. #84.SDR SWIA2020090252176Stiffener · crackedRT MAIN LANDING GEAR WHEEL WELL UPPER I/B BATT RIB ANGLE IS CRACKED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED BATT RIBB ANGLE PN: 600-10389-2 IAW CRJ-200 SRM.SDR SWIA2020090252159Seat Track · corrodedRT SIDE SEAT RAIL BETWEEN F.S. 449.85 AND F.S. 499.00 IS CORRODED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED RT SIDE SEAT RAIL BETWEEN F.S. 449.85 AND F.S. 499.00 IAW CRJ 200 AMM.SDR SWIA2020090252157Angle · crackedLT MAIN LANDING GEAR WHEELWELL UPPER I/B BATT RIB ANGLE IS CRACKED. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED SERVICEABLE LT MAIN LANDING GEAR WHEEL WELL UPPER I/B BATT RIB ANGLE IAW CRJ 200 SRM AND MHIRJ REO. COMPLIED WITH SKYWEST TASK CARD, SCANNED M-33SDR SWIA2020090252156Floor Support · corrodedLT CABIN FLOOR SILL IS CORRODED IN SEVERAL AREAS BETWEEN F.S. 409.00+128 AND F.S. 559.00. C-CHECK RO 8/29/2020. REPAIRED LT SILL PANEL FROM FS 409.00+128 TO FS 559.00 IAW BOMBARDIER REO. TASK CARD COMPLIED WITH, FORM M-337 ATTACHED. WEIGHT AND BALANCE NOT EFSDR SWIA2020090252154Seat Track · corrodedRT SIDE SEAT RAIL BETWEEN F.S. 544.00 AND F.S. 559.00 +96 IS CORRODED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED RT SIDE SEAT RAIL BETWEEN F.S. 544.00 - F.S. 559.00+96 IAW CRJ-200 AMM.SDR SWIA2020090252153Seat Track · corrodedRT SIDE SEAT RAIL BETWEEN F.S. 499.00 AND F.S. 544.00 IS CORRODED. C-CHECK RO 8/29/2020. REMOVED CORRODED SEAT RAIL AND INSTALLED NEWLY FABRICATED SEAT RAIL (REFERENCE CAMP #21262560 FOR FABRICATION) BETWEEN F.S. 499.00 AND F.S 544.00 IAW CRJ 200 AMM.SDR SWIA2020090252151Floorbeam · crackedF.S. 280 RBL9 SUPPORT CLIP IS CRACKED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED CRACKED SUPPORT CLIP AT FS.280 RBL9 OUTBOARD IAW CRJ 200SRM.SDR SWIA2020090252192Bracket · corrodedFWD AND AFT PASSENGER DOOR BRACKET ASSEMBLIES ARE CORRODED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED FWD AND AFT PASSENGER DOOR BRACKET ASSEMBLIES PT# 601R31527-217 IAW CRJ 200 SRM.SDR SWIA2020090252168Attach Angle · corrodedON AIRCRAFT PASSENGER DOOR FRAME WHILE REMOVING ANGLE 601R31527-205 FOUND THAT ATTACHING ANGLE 601R31527-179 IS HEAVILY CORRODED AND NEEDS REPLACED. C-CHECK RO 8/29/2020. REMOVED ANGLE 601R31527-205, FOUND ATTACHING ANGLE 601R31527-179 IS HEAVILY CORRODED ASDR SWIA202090252194Bracket · chafedRT WING INBOARD TRAILING EDGE, I/B FLAP STUB FAIRING MOUNTING BRACKET CHAFED APPOX. 0.025 DEEP. C-CHECK RO 8/29/2020. REMOVED DAMAGED RT WING I/B TRAILING EDGE FLAP STUB FAIRING MOUNTING BRACKET AND INSTALLED NEW SERVICEABLE MOUNT BRACKET IAW CRJ 200 SRM.SDR SWIA2020090252184Gusset · corrodedPASSENGER DOOR GUSSET AT FS310.00 AND BETWEEN STRINGER 15L AND STRINGER16L CORRODED AND REQUIRES EVALUATION. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED NEW GUSSET IAW CRJ 200. SEE CONTINUATION CARD FOR DETAILS OF WORK PREFORMED.SDR SWIA2020090252160Intercostal · corrodedINTERCOSTAL LOWER CORRODED BETWEEN FS 295.00 AND FS310.00 AND BETWEEN STRINGER 16L AND STRINGER 17L. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED NEW INTERCOSTAL IAW CRJ 200 SRM AND DRAWING. COMPLIED WITH SKYCARD AND FORM M-337. WEIGHT AND BALANCE NOT AFFECSDR SWIA2020090252179Fitting · crackedWINDSHIELD CENTER POST LOWER FITTING IS CRACKED THRU THE LOWER FASTENER LOCATIONS ON THE AFT SIDE OF FITTING. C-CHECK RO 8/29/2020. REMOVED UNSERVICEABLE POST FITTING AND INSTALLED SERVICEABLE POST FITTING IAW CRJ 200 SRM.SDR SWIA2020090252191Intercostal · corrodedFWD AVIONICS BAY DOOR INTERCOSTAL IS CORRODED AT F.S. 364 BETWEEN STRINGER 27 TO 26L IS CORRODED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED INTERCOSTAL AT FS 364 BETWEEN STRINGER 27.0 TO 26L IAW CRJ-200 SRM.SDR SWIA2020090252190Intercostal · corrodedFWD AVIONICS BAY DOOR INTERCOSTAL IS CORRODED AT F.S. 364 BETWEEN STRINGER 27 TO STRINGER 26R. C-CHECK RO 8/29/2020. REMOVED AND REPLACED FS364 BETWEEN STRINGER 27 AND STRINGER 26R CRJ-200 SRM.SDR SWIA2020090252182Support Plate · corrodedRT CABIN FLOOR SUPPORT PLATE FOR GALLEY 1 IS CORRODED AT RBL 36 BETWEEN FS310 AND FS 319. C-CHECK RO 8/29/2020. REMOVED AND REPLACED RT CABIN FLOOR SUPPORT IAW CRJ-200 SRM.SDR SWIA2020090252178Floorbeam · crackedFS 484 ANGLE CLIP ON OB SIDE OF RBL 27 FLOOR BEAM IS CRACKED. C-CHECK RO 8/29/2020. R & R ANGLE CLIP ON OB SIDE OF RBL 27 IAW CRJ-200 SRM. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.SDR SWIA2020090252167Bulkhead · chafedFS 280 BULKHEAD IS CHAFED ON AFT FACE BETWEEN RBL 11.00 AND RBL 18.80 APPROXIMATELY 16 INCHES ABOVE FLOOR LEVEL. C-CHECK RO 8/29/2020. PERFORMED A MAJOR REPAIR TO FS 280 BULKHEAD CHAFE IAW REO. COMPLETED SKYWEST TASK CARD. COMPLETED FORM M-337 IS ATTACHED.SDR SWIA2020090252166Floor Support · corrodedRT CABIN PRESSURE FLOOR SILL HAS CORROSION FROM FS409+128 TO FS 559.00 ON BOTH THE FLOOR SILL PANEL AND FLOOR ANGLES. C-CHECK RO 8/29/2020. REPAIRED RT CABIN FLOOR SILL IAW MHIRJ REO AND CRJ 200 SRM. COMPLIED WITH SKYCARD AND FORM M-337. SEE CONTINUATION CSDR SWIA2020090252165Frame · corrodedF.S. 319 FRAME IS CORRODED BETWEEN STRINGER 27 TO 26L. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED NEW FRAME SECTION AND SPLICES IAW CRJ 200 SRM AND SKYWEST CARD. COMPLETED FORM M-337 AND M-131. WEIGHT REMOVED .35 WEIGHT INSTALLED .6 TOTAL WEIGHT INSTALLEDSDR SWIA2020090252164Frame · corrodedF.S.333 FRAME IS CORRODED BETWEEN STRINGER 27 TO STRINGER 26L AND 23L TO 22L. C-CHECK RO 8/29/2020. REMOVED AND INSTALLED NEW FRAME SECTORS AT FS 333 STRINGER 18L-23R IAW CRJ 200 SRM, AND DWG. COMPLIED WITH SKY CARD FORM M-337 COMPLETED. WEIGHT AND BALANCSDR SWIA2020090252152Floor Support · corrodedLT CARGO FLOOR SILL IS CRACKED AT FS 589 AND CORRODED AROUND SEVERAL NUTPLATE HOLES. C-CHECK RO 8/29/2020. REMOVED DAMAGED LT SILL AND INSTALLED NEW SERVICEABLE FLOOR SILL IAW CRJ 200 SRM AND BOMBARDIER REO. WEIGHT AND BALANCE NOT EFFECTED. COMPLIED WITH M-SDR SWIA2020090252150Floor Support · corrodedCARGO FLOOR BEAM LBL 27 HAS CORROSION AROUND 3EA NUTPLATES ON OB FLANGE BETWEEN FS 589 AND FS 612. C-CHECK RO 8/29/2020. PERFORMED A MAJOR REPAIR BY REPLACING THE CARGO FLOOR BEAM AT LBL 27 BETWEEN FS 589 AND FS 612 IAW CRJ 200 SRM COMPLETED SDR AND CPCP. SDR SWIA2020090252149Channel · crackedCARGO DOOR CUTOUT SURROUND HAT CHANNEL FS 574 IS CRACKED IN TWO LOCATIONS. (C-CHECK) RO 8/29/2020. REMOVED OLD PART AND INSTALLED SERVICABLE PART IAW CRJ 200 SRM. CALIBRATED TOOL USED 204368 CAL DUE 10-31-20.SDR SWIA2020090252163Skin · damagedAFTER DETAILED INSPECTION ON THE FUSELAGE SKIN SURROUND FOR ATTACHING PNL. 131 AL, FOUND ONE EACH REPAIRED HOLE'S FREEZE PLUG NOT SEATED. REQUIRES REPAIR. C-CHECK RO 8/29/2020. PANEL 131AL HAD A DAMAGED/LOOSE FREEZE PLUG AND REPAIRED IAW BOMBARDIER REO. COMSDR SWIA2020090252183Control Unit · corrodedRT WING AILERON OUBOARD PCU ATTACHMENT LUG APPEARS CORRODED. REMOVED AND REPLACED RT O/B AILERON PCU IAW CRJ 200 MIP.SDR SWIA2020090252186Stop Fitting · corrodedMAIN AVIONICS COMPARTMENT DOOR SIDE FITTINGS ON FUSELAGE HAVE CORRODED STOPS. C-CHECK RO 8/29/2020. REMOVED AND REPLACED CORRODED STOPS (PADS) WITH NEW/SERVICEABLE ONES.SDR SWIA2020090252162Skin · dentedRIGHT INBOARD FLAP HAS FOUR SHARP DENTS ON THE LOWER SKIN. FIRST DENT .015" DEEP .250" LONG, 14.625" FROM TRAILING EDGE 5.25" FROM INBOARD RIB. SECOND DENT .008" DEEP .375" LONG, 15.375" FROM TRAILING EDGE 19.5" FROM INBOARD RIB. THIRD DENT .008" DEEP .375"SDR SWIA2020090252188Mount · corrodedLEFT WING INBOARD AND OUTBOARD GROUND SPOILER PCU MOUNTING HARDWARE CORRODED. C-CHECK RO 8/29/2020. INSTALLED SERVICEABLE MOUNTING AND ATTACHING HARDWARE TO LT WING INBOARD AND OUTBOARD GROUND SPOILERS PCU IAW CRJ 200 AMM. OPERATIONAL TEST CHECKS GOOD IAW CSDR SWIA2020090252187Nut · corrodedLEFT WING SPOILERON AND FLIGHT SPOILER INBOARD AND OUTBOARD PCU MOUNTING HARDWARE (NUTS) ARE CORRODED. C-CHECK RO 8/29/2020. REMOVED AND REPLACED CORRODED NUTS IAW CRJ-200-AMM.SDR SWIA2020090252181Bolt · corrodedRIGHT WING INBOARD AND OUTBOARD GROUND SPOILER PCU MOUNTING HARDWARE CORRODED. REPLACED THE RT INBOARD AND OUTBOARD GROUND SPOILER ACTUATOR MOUNTING HARDWARE WITH NEW SERVICABLE HARDWARE IAW CRJ 200 AMM. OPERATIONAL TEST CHECKS GOOD IAW CRJ 200 AMM.SDR SWIA202052180Nut · corrodedRIGHT WING SPOILERON AND FLIGHT SPOILER INBOARD AND OUTBOARD PCU MOUNTING HARDWARE (NUTS) ARE CORRODED. C-CHECK RO 8/29/2020. REPLACED CORRODED NUTS ON THE RT WING SPOILERON AND FLIGHT SPOILER INBOARD AND OUTBOARD PCU TO WING ATTACHMENT POINT WITH NEW SERVICSDR SWIA2020090252161Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: DENT FOUND RT FWD FUSELAGE BETWEEN STRINGERS R25 & R24. REINSPECT NEEDED EVERY 600 HOURS PER REO. PERMANENT REPAIR DUE IN 5300 FLIGHT HOURS BY 38018.2 TAT., PART NUMBER: - , SERIAL NUMBER: 7769, POSITION: C-CHECK ROSDR SWIA2020090252158Skin · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: REPAIRED 2 ELONGATED FASTENER HOLES ON FWD FUSE SKIN USED FOR ATTACHING PANEL 131AL PER REO. PERFORM DETAILED VISUAL INSPECTION, PART NUMBER: - SERIAL NUMBER: 7769, POSITION: C-CHECK RO 8/29/2020. PERFORMED DETAILED VISSDR SWIA2019031945647Clamp · looseCARGO BTL LOW CAUTION MESSAGE IN CRUISE. RAN QRH AND LANDED AT NEAREST SUITABLE AIRPORT. (FLT#3500) CLOSED UPON INVESTIGATION OF RIGHT HAND CARGO FIRE BOTTLE BEING RELEASED, ALSO FOUND THE RIGHT HAND 14TH STAGE DUCT ASSY INSULATION WAS BLOWN APART DUE TO THE ASDR SWIA2018092845106Floorbeam · corrodedCORROSION ON FLOOR BEAM ON LBL9 BETWEEN FS559.0 - FS559+16 AROUND SCREW HOLES. (C-CHECK) RO: 09/27/2018 REPAIRED FLOOR BEAM BETWEEN FS559.0 - FS559+16 AROUND SCREW HOLES IAW REO.SDR SWIA2018092845104Seat Track · corrodedCORRODED SEAT RAIL BEAM ON LBL28.00 NEAR FS559.00+112. (C-CHECK) RO: 09/27/2018 REMOVED CORROSION AROUND SCREW HOLE ON SEAT RAIL BEAM AT LBL28, FS559.00+110 IAW SRM.SDR SWIA2018092845105Hinge Fitting · gougedFUSELAGE PASSENGER DOOR HINGE AFT LANDING HAS GOUGE FROM HINGE PIN ROLL PIN. (C-CHECK) RO: 09/27/2018 BLENDED FUSELAGE PAX DOOR HINGE AFT LANDING IAW REO.SDR SWIA2018092845103Floor Panel · corrodedTHERE IS AN AREA OF CORROSION ON THE L/H FLIGHT COMPARTMENT FLOOR PANEL AFT EDGE OUTBOARD OF THE PARKING BRAKE HANDLE. (C-CHECK) RO: 09/27/2018 REMOVED CORROSION ON THE L/H FLIGHT COMPARTMENT FLOOR PANEL AFT EDGE OUTBOARD OF THE PARKING BRAKE HANDLE IAW SRM.SDR SWIA2018092845102Anchor Fitting · gougedGALLEY UPPER ANCHOR FITTING ON FUSELAGE IS GOUGED AT APPROXIMATELY FS 300. (C-CHECK) RO: 09/27/2018REMOVED DAMAGE ON GALLEY UPPER ANCHOR FITTING ON FUSELAGE AT FS295.00 TO FS310.00 STGR 4R. IAW REO AND SRM.SDR SWIA2018092845101Bracket · corrodedSERVICE DOOR AFT SILL & BRACKET IS CORRODED. (C-CHECK) RO: 09/27/2018 REMOVED AND REPLACED SERVICE DOOR SILL AND BRACKET IAW SRM.SDR SWIA2018092845100Skin · dentedREAR FUSELAGE LH SIDE DENTED APPROX FS767 LOCATED AFT OF LH PAC HEAT EXCHANGER EXHAUST. (C-CHECK) RO: 09/27/2018 REPAIRED LH SIDE DENT APROX FS767 AFT OF LH PAC HEAT EXCHANGER EXHAUST IAW REO.SDR SWIA2017091543766Pump · failedAFTER TAKEOFF, SELECTING GEAR UP, HAD A GEAR DISAGREE, AND NOSE DOOR OPEN WARNING MESSAGE. REMOVED AND REPLACED 3B HYDRAULIC PUMP IAW AMM. OPS AND LEAK CHECKED GOOD. PERFORMED GEAR SWINGS IAW AMM. NO DEFECTS NOTED.SDR SWIA201743664Skin · dentedEXTERNAL FUSELAGE SKIN IS DENTED AT STRINGER 7L BETWEEN BS 424 AND 439. REPAIRED THE SKIN IAW REO.SDR SWIA201743667Skin · dentedLEFT WING INBD FLAP HAS TWO DENTD ON THE UPPER SURFACE. REPAIRED THE DAMAGE IAW REO.SDR SWIA201743666Skin · dentedLEFT WING OTBD FLAP HAS ONE DENT ON THE ON THE UPPER SURFACE. COMPLIED WITH REPAIR IAW SRM.SDR SWIA201743663Skin · dentedEXTERNAL FUSELAGE SKIN HAS ONE PROTRUDING DENT AT APPROX BS 658 BETWEEN STRINGERS 21L AND 22L. REPAIRED IAW REO.SDR SWIA201743665Crossbeam · crackedBS 280 CROSSBEAM IS CRACKED JUST OTBD OF LBL 9 AND RBL 9. REPAIRED THE CROSSBEAM IAW REO.SDR ASOA20161103102Floorbeam · corrodedFLOORBEAM RBL 9 CORRODED AT FS 409+130. REPAIRED RBL9 AT FS 409+130 PER REO 601R-53-41-2096 AND EC/TC REO 601R-53-41-2096. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
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