N916EV

Service difficulty reports · 214

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 = 'N916EV' 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 SWIA2020091652516Frame · corrodedFRAME HAS CORROSION AT APPROX FS 513 AND APPROX STGR 5R. C-CHECK RO 9/12/2020. REMOVED CORROSION FROM FS 513.00 FRAME NEAR STRINGER 5R. REMAINING MATERIAL WITHIN LIMITS, REF REO BOMBARDIER DWG & CRJ200 SRM. COMPLIED WITH TASK CARD.Aug 3, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020091652515Retainer · crackedLT OVERWING EMERGENCY EXIT DOOR SEAL RETAINER IS CRACKED, MARKED. C-CHECK RO 9/12/2020. REMOVED AND REPLACED THE LT EMERGENCY EXIT DOOR SEAL RETAINER, REF CRJ200 SRM DRAWING. RESTORED ACCESS. COMPLIED WITH ST, ALL CHECKS GOOD.Aug 3, 2020 · N916EV · Cndair CL6002B19 · Emergency ExitsSDR SWIA2020091652514Skin · dentedDENT ON EXTERNAL SKIN BETWEEN FS 589.00 AND FS 605.00 STGR 25R AND 26R, MARKED. C-CHECK RO 9/12/2020. COMPLIED WITH PERMANENT REPAIR DENT ON EXTERNAL SKIN BETWEEN FS 589.00 AND FS 605.00 STGR 25R AND 26R, REF REO. VERIFIED ALL APPLICABLE STEPS COMPLIED WITHAug 3, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2020091652513Skin · gougedPREVIOUS REPAIR AT FS 605.00 AND WL 73.50, BELOW CARGO DOOR, HAS MULTIPLE GOUGES, MARKED. C-CHECK RO 9/12/2020. GOUGES AT PREVIOUS REPAIR "OUT OF LIMITS," NO DAMAGE ALLOWED. REMOVED AND REPLACED DOUBLER AT FS 605 WL 73.5 BELOW CARGO DOOR, REF CRJ200 SRM REOAug 3, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2020091652512Floorbeam · corrodedSERVICE DOOR SURROUND STRUCTURE FS 319 FLOOR SUPPORT BRACKET AT AND ABOVE FLOOR LEVEL IS CORRODED, MARKED. C-CHECK RO 9/12/2020. REPLACED PART, EVALUATED 100% MATERIAL LOSS. REMOVED AND REPLACED WITH NEW PART, REF CRJ200 SRM BOMBARDIER DRAWING. COMPLIED WIAug 2, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020091652511Frame · crackedFUSELAGE FRAME AT APPROX FS 333 BETWEEN STGR 0 AND STGR 3L IS CRACKED AT A TOOLING HOLE, FLAGGED. C-CHECK RO 9/12/2020. REMOVED AND RELPLACED THE FUSELAGE FRAME AT FS 333.00 BETWEEN STGR 0 AND STGR 3L WITH NEW PART AND HARDWARE, REF BOMBARDIER DRAWING CRJ200Aug 2, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020091652510Striker · gougedPASSENGER DOOR CUTOUT AFT SEAL STRIKER IS GOUGED, MARKED. C-CHECK RO 9/12/2020. COMPLIED WITH REPAIR OF PASSENGER DOOR CUTOUT AFT SEAL STRIKER, REF BOMBARDIER REO. TYPE 1 ALL CHECKS GOOD.Aug 2, 2020 · N916EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020091652509Floorbeam · corrodedRT 559.00+10 TO 559.00+80 RBL 9 FLOOR BEAM HAS CORROSION AS MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW RBL 9.0 FLOOR BEAM CAP. SEE CONTINUE CARD FOR FURTHER DETAILS, REF REO CRJ200 SRM, DWG. COMPLIED WITH TASK CARD.Aug 1, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2020091652508Floor Support · corrodedRT FS 409.00+128 TO 559 UPPER FLOOR SILL HAVE NUMEROUS AREAS OF CORROSION AS MARKED. C-CHECK RO 9/12/2020. BLENDED 18 EA LOCATIONS ON THE RT FS 409+128-FS 559 UPPER FLOOR SILL WITHIN LIMITS, REF CRJ200 SRM REO. RESTORED FINISH, NO DEFECTS NOTED. COMPLIED WAug 1, 2020 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020091652507Floor Support · corrodedLT FS 409.00+128 TO 559 UPPER FLOOR SILL ANGLES HAVE NUMEROUS AREAS OF CORROSION AS MARKED. C-CHECK RO 9/12/2020. REPAIRED CORROSION ON LT FS 409.00+128 TO 559 UPPER FLOOR SILL ANGLE, REF REO. COMPLIED WITH TASK CARDAug 1, 2020 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020091652506Fitting · crackedRT WINDSHIELD SIDE POST LOWER AFT CLIP IS CRACKED. C-CHECK RO 9/12/2020. REMOVED AND REPLACED RT WINDSHIELD SIDE POST LOWER AFT CLIP, REF CRJ 200 SRM & BOMBARDIER DRAWING. REMOVED 0.12 POUNDS THEN INSTALLED 0.12 POUNDS, NO WEIGHT CHANGE. TUC1755 CAL DUE: 3Jul 31, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020091652505Fitting · crackedLT WINDSHIELD SIDE POST LOWER AFT CLIP IS CRACKED. C-CHECK RO 9/12/2020. REMOVED AND REPLACED LT WINDSHIELD SIDE POST LOWER AFT CLIP, REF CRJ 200 SRM & BOMBARDIER DRAWING. COMPLIED WITH TASK CARD.Jul 31, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020091652555Vane · chafedTHE LT INBOARD FLAP VANE IS CHAFED OUTBOARD OF THE NR 3 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW SACRIFICIAL DOUBLER ON LT INBOARD FLAP AT WS 141.00, REF CRJ200 SRM. OPS CHECKS GOOD.Jul 30, 2020 · N916EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020091652554Vane · chafedTHE LT INBOARD FLAP VANE IS CHAFED OUTBOARD OF THE NR 2 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW SACRIFICIAL DOUBLER ON LT INBOARD FLAP AT WS 105.02, REF CRJ200 SRM. OPS CHECKS GOOD.Jul 30, 2020 · N916EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020091652553Vane · chafedTHE LT INBOARD FLAP VANE IS CHAFED INBOARD OF THE NR 1 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW SACRIFICIAL DOUBLER ON LT INBOARD FLAP AT WS 56.55, REF CRJ200 SRM. OPS CHECKS GOOD.Jul 30, 2020 · N916EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020091652552Vane · chafedTHE RT INBOARD FLAP VANE IS CHAFED OUTBOARD OF THE NR 3 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW SACRIFICIAL DOUBLER ON RT INBOARD FLAP AT WS 141.00 (PN K601R41302-7), REF CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.Jul 30, 2020 · N916EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020091652551Vane · chafedTHE RT INBOARD FLAP VANE IS CHAFED OUTBOARD OF THE NR 2 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW SACRIFICIAL DOUBLER ON RT INBOARD FLAP AT WS 105.02 (PN K601R41302-7), REF CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.Jul 30, 2020 · N916EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020091652550Vane · chafedTHE RT INBOARD FLAP VANE IS CHAFED INBOARD OF THE NR 1 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW SACRIFICIAL DOUBLER ON RT INBOARD FLAP AT WS 56.55 (P/N K601R41302-10), REF CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.Jul 30, 2020 · N916EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020091652504Structure · gougedSERVICE DOOR BACKUP STRUCTURE HAS MULTIPLE GOUGES/CHAFES AROUND PERIMETER. C-CHECK RO 9/12/2020. REPLACED/INSTALLED THE LOWER SECTION OF THE SERVICE DOOR SEAL STRIKER, REF BOMBARDIER DRAWING CRJ200 SRM. COMPLIED WITH SKYWEST TASK CARD.Jul 30, 2020 · N916EV · Cndair CL6002B19 · Galley DoorsSDR SWIA2020091652503Vane · chafedTHE RT INBOARD FLAP VANE IS CHAFED ON TRAILING EDGE UPPER SIDE OF THE NR 1 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. BLENDED CHAFE ON THE RT INBD FLAP VANE TRAILING EDGE UPPER SIDE OF THE NR 1 ACTUATOR, REF CRJ-200 SRM. NDT COMPLIED WITH (SEE NDT REPORT FOR MJul 30, 2020 · N916EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020091652502Skin · dentedCREASE NOTED IN AIRCRAFT SKIN BETWEEN FS 718.00 AND FS 755.00 NEAR STGR 19L AND STGR 27L. C-CHECK RO 9/12/2020. REPAIRED DENTS TO LT FUSELAGE SKIN BETWEEN FS 718-FS 755 STR 19L-STR 26L, REF REO AND CRJ200 SRM.Jul 29, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2020091652501Skin · chafedCENTER WING SKIN MATING SURFACE FOR PANEL 193AB AT FORWARD WING SPAR AND LBL 45 IS CHAFED, MARKED. C-CHECK RO 9/12/2020. BLENDED CHAFE DAMAGE TO A SMOOTH CONTOUR. REMAINING MATERIAL WITHIN LIMITS, REF REO. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH Jul 28, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2020091652500Hinge · chafedSERVICE DOOR HINGE IS CHAFED AND GOUGED IN X3 AREA'S. C-CHECK RO 9/12/2020. REPAIRED SERVICE DOOR HINGE CHAFED AND GOUGED AREAS, REF REO AND CRJ-200 SRM. SEE CONTINUATION FOR DETAILS.Jul 27, 2020 · N916EV · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA2020091652499Stop Fitting · chafedAVIONICS BAY DOOR ACCESS FWD LT AND RT DOOR STOP FITTINGS ON FUSELAGE ARE CHAFED. C-CHECK RO 9/12/2020. REMOVED AND REPLACED STOP FITTINGS AT AVIONICS BAY DOOR ACCESS FWD LT AND RT DOOR STOP FITTINGS, REF CRJ 200 SRM. ALL CHECKS GOOD.Jul 26, 2020 · N916EV · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA2020091652541Skin · crackedELEVATOR TRAILING EDGE PANEL 334AB IS CRACKED. C-CHECK RO 9/12/2020. RECEIVED NEW ELEVATOR TRAILING EDGE PANEL NR 601R24029-5. LOCATED, DRILLED MOUNTING HOLES, COMPLIED WITH CRJ-200 SRM PANEL READY FOR INSTALL.Jul 25, 2020 · N916EV · Cndair CL6002B19 · Elevator, Plate/SkinSDR SWIA2020091652561Fairing · chafedRT FLAP STUB FAIRING IS CHAFED. C-CHECK RO 9/12/2020. FOUND RT FLAP STUB FAIRING OUT OF LIMIT, PER CRJ 200 SRM. TRANSFERRED PARTS (SEALS AND RETAINERS) FROM DAMAGED FAIRING TO NEW AND COMPLETE ASSEMBLED NEW RT STUB FAIRING ASSY FOR REPLACING, REF BOMBARDIERJul 24, 2020 · N916EV · Cndair CL6002B19 · Leading Edge DevicesSDR SWIA2020091652560Fairing · chafedLT FLAP STUB FAIRING IS CHAFED. C-CHECK RO 9/12/2020. FOUND LT FLAP STUB FAIRING OUT OF LIMIT, NO ALLOWABLE DAMAGE APPLIED. TRANSFERRED PARTS (SEALS AND RETAINERS) FROM DAMAGED FAIRING TO NEW AND COMPLETE ASSEMBLED NEW LT STUB FAIRING ASSY 601R31199-91 PO# Jul 24, 2020 · N916EV · Cndair CL6002B19 · Leading Edge DevicesSDR SWIA2020091652498Structure · crackedLT FWD EQUIPTMENT BAY FLOOR AT FRAME 193.00 POSSIBLE CRACK. C-CHECK RO 9/12/2020. COMPLIED WITH PERMANENT REPAIR RT FWD EQUIPMENT BAY FLOOR, REF REO. ALL APPLICABLE STEPS COMPLIED WITH, ALL CHECKS OKAY, COMPLETED TASK CARD.Jul 23, 2020 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020091652497Cap · damagedCOMPLY WITH REO 601R-53-41-1116 REPAIR & REINFORCEMENT FOR FS 559.00 LOWER CAP ANGLES BL 9.00 & 18.00 LHS & RHS. C-CHECK RO 9/12/2020. COMPLIED WITH REO REPAIR & REINFORCEMENT FOR FS 559.00 LOWER CAP ANGLES BL 9.00 & 18.00 LHS & RHS. COMPLIED WITH ST, LEAK Jul 13, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020091652496Skin · dentedCOMPLIED WITH SCHEDULED MAINTENANCE CODE: RA, DENT ON RT FWD FUSELAGE SKIN BETWEEN FS 202.75 AND FS 220.00 AND BETWEEN STR 16R AND STR 17R. COMPLIED WITH TEMPORARY REPAIR PER REO. PERMANENT REPAIR WITHIN 2600 FLIGHT HOURS DUE BY TAT 34476.7, PART NUMBER: - ,Jul 13, 2020 · N916EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA201743201Vertical Support · crackedBS 409+128, RBL 18 VERTICAL POST INBD AND OTBD CRACKED. REMOVED AND REPLACED THE POST IAW REO.Apr 11, 2017 · N916EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA201743200Floorbeam · corrodedFUSELAGE FLOORBEAM AT LBL 27 CORRODED. (REMOVED AND REPLACED FLOORBEAM IAW SRM.Apr 11, 2017 · N916EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201743199Bulkhead Web · crackedREAR PRESSURE BULKHEAD WEB CRACKED. REPAIRED REAR PRESSURE BULKHEAD IAW REO.Apr 11, 2017 · N916EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201743198Fitting · crackedWINDSHIELD CENTER POST LOWER LT FITTING CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM.Apr 11, 2017 · N916EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA201743197Fitting · crackedWINDSHIELD CENTER POST RT FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM.Apr 11, 2017 · N916EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA201743196Frame · corrodedBS 605 FRAME CORRODED. REMOVED AND REPLACED THE FRAME IAW SRM.Apr 11, 2017 · N916EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA201743195Frame · corrodedFRAME BS 349 CORRODED. REMOVED AND REPLACED THE FRAME IAW SRM.Apr 11, 2017 · N916EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA201743194Vertical Support · crackedBS 409+128, LBL 18 VERTICAL POST INBD AND OTBD CRACKED. REMOVED AND REPLACED VERTICAL POST IAW SRM AND REO.Apr 11, 2017 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201743193Stringer · corrodedCORROSION FOUND ON STRINGER 27, BETWEEN BS 333 AND 349. REPAIRED THE STRINGER IAW SRM.Apr 11, 2017 · N916EV · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR ASOA2015072813397Handle · lack of lubePAX DOOR HANDLE DIFFICULT TO OPEN. CLEANED AND LUBRICATED THE PAX DOOR HANDLES AND PERFORMED AN OPS CHECK IAW AMM 52-11-00. OPS CHECKED GOOD.Jul 28, 2015 · N916EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2015070213247Light · inoperativeSERVICE DOOR FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE. REPLACED SERVICE DOOR FLOOR LEVEL EMERGENCY LIGHT ASSY IAW AMM 33-51-10. OPS CHECK GOOD.Jun 30, 2015 · N916EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2015032012437Door · unknownPAX DOOR HARD TO OPEN. ACCOMPLISHED VISUAL INSPECTION OF PASSENGER DOOR, NO DEFECTS FOUND. ACCOMPLISHED OPS TEST OF PAX DOOR OPEN AND CLOSE 6 CYCLES OPS TEST GOOD. REF AMM 52-11-00-710-802.Mar 16, 2015 · N916EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2015032012436Door · unknownPASSENGER DOOR VERY DIFFICULT TO OPEN. CYCLED PAX DOOR SEVERAL TIMES, OPS CHECK GOOD IAW AMM 52-11-00.Mar 16, 2015 · N916EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2014100311378Attach Fitting · damagedRT MLG UPLOCK ATTACH FITTING DAMAGED. REMOVED AND REPLACED THE ATTACH FITTING IAW SRM 51-42-06, 51-42-21, AND DWG 601R31092.Sep 17, 2014 · N916EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2014100311377Frame · damagedLT MLG UPLOCK AFT FRAME ASSY DAMAGED. REMOVED AND REPLACED THE LT MLG UPLOCK AFT FRAME ASSY IAW SRM 51-42-06, SRM 51-42-21, SRM 51-40-06, SRM 51-40-11, AND DWG 601R31092.Sep 17, 2014 · N916EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2014100311376Floorbeam · crackedRBL 9 OTBD ANGLE AT BS 280 FLOORBEAM CRACKED. R & R ANGLE IAW REO 600-53-0725.Sep 14, 2014 · N916EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2014100311375Seat Track · corrodedLEFT FLOOR SEAT TRACK FROM BS 364 - 400 HAS CORROSION. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802 & AMM 53-01-11-400-802.Sep 10, 2014 · N916EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014100311374Seat Track · corrodedRT FLOOR SEAT TRACK FROM BS 364 400 HAS CORROSION. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.Sep 10, 2014 · N916EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014100311373Intercostal · crackedINTERCOSTAL AT BS 625.30, WL 92.00 IS CRACKED. REPAIRED IAW ECTC REO 601R-53-61-5265 AND GREO 601R-53-61-5265, REV.Sep 10, 2014 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014100311372Intercostal · crackedINTERCOSTAL BS 625.30, WL 100 IS CRACKED. REPAIRED IAW ECTC REO 601R-53-61-5265 AND GREO 601R-53-61-526S REV.Sep 10, 2014 · N916EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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