N922EV
Service difficulty reports · 159
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 = 'N922EV' 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 = 'N922EV' 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 SWIA202055255Skin · dentedTRANSFER FROM EAML 550059. DENT BETWEEN FS 640 AND 672.2 HAS LARGE DENT APPROXIMATELY 6.4 X 6.3 INCHES WITH HOLE IN CENTER APPROXIMATELY 2.6 X 1.8 INCHES. LT FUSELAGE STRUCTURE DAMAGE BETWEEN FS 640.00 AND FS 672.20, STR 13L AND 16L WAS REPAIRED BY BOMBARDISDR SWIA202053519Bulkhead · damagedEVALUATE RT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIV NUT LOCATIONS, REFERENCE RIL 5378. REPAIR IF NEEDED, IAW ENGINEERING INSTRUCTIONS. C-CHECK RO 10/18/2020. COMPLIED WITH MHIRJ EO IN REPAIR OF TOOOLING DAMAGE TO RT 9G BULKHEAD AFT WALL. REPAIR DOUBLER MSDR SWIA202053518Bulkhead · damagedEVALUATE CENTER 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIV NUT LOCATIONS, REFERENCE RIL 5378. REPAIR IF NEEDED, IAW ENGINEERING INSTRUCTIONS. C-CHECK RO 10/18/2020. COMPLIED WITH MHIRJ EO IN REPAIR OF TOOLING DAMAGE TO CENTER 9G BULKHEAD AFT WALL. REPAIR DOSDR SWIA202053517Bulkhead · damagedEVALUATE LT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIV NUT LOCATIONS, REFERENCE RIL NR 5378. REPAIR IF NEEDED, IAW ENGINEERING INSTRUCTIONS. C-CHECK RO 10/18/2020. COMPLIED WITH MHIRJ EO IN REPAIR OF TOOLING DAMAGE TO LT 9G BULKHEAD AFT WALL. REPAIR DOUBLERSDR SWIA202053513Floorbeam · corrodedFLOOR SUPPORT PLATE AT FS 559+48 BETWEEN RBL 9 AND RBL 27 IS CORRODED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED FLOOR SUPPORT PLATE AT FS 559+48 BETWEEN RBL 9 AND RBL 27, IAW CRJ 200 SRM. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.SDR SWIA202053512Control Rod · corrodedRT ELEVATOR SYSTEM MECHANICAL CONTROL PATH INPUT ROD BEARING AND HARDWARE LOCATED AFT END OF VERTICAL STABILIZER CANTED RIB APPEARS TO HAVE CORROSION (RUST). C-CHECK RO 10/18/2020. REMOVED AND REPLACED LT ELEVATOR CONTROL PATH INPUT ROD AND FWD AND AFT HARDWSDR SWIA202053511Control Rod · corrodedLT ELEVATOR SYSTEM MECHANICAL CONTROL PATH INPUT ROD BEARING AND HARDWARE LOCATED AFT END OF VERTICAL STABILIZER CANTED RIB APPEARS TO HAVE CORROSION (RUST). C-CHECK RO 10/18/2020. REMOVED AND REPLACED LT ELEVATOR CONTROL PATH INPUT ROD AND FWD AND AFT HARDWSDR SWIA202053498Window Post · crackedRT WINDSHIELD SIDE POST LOWER AFT FITTING IS CRACKED. C-CHECK RO 10/18/2020. REMOVED DAMAGED RT WINDSHIELD SIDE POST LOWER AFT FITTING. LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE FITTING, IAW CRJ200-SRM.SDR SWIA202053497Window Post · chafedSTRAP ON WINDSHIELD CENTER POST, ATTACHING CENTER POST TO CENTER SUPPORT CLIPS FOUND TO BE CHAFED. CAUSED BY CRACKED LT SUPPORT CLIP, P/N 601R34012-25. C-CHECK RO 10/18/2020. REMOVED DAMAGED WINDSHIELD CENTER POST STRAP AND INSTALLED NEW SERVICEABLE STRAP, SDR SWIA202053496Angle · crackedUPPER ANGLE COMMON TO THE LT INBOARD BATTERY RIB AT WS 48.30 IS CRACKED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED ANGLE, IAW CRJ 200 SRMS. REFER TO CONTINUE CARD FOR WORK PERFORMED.SDR SWIA202053489Fitting · crackedWINDSHIELD CENTER SUPPORT CLIPS ON THE LT AND RT SIDE ARE CRACKED. C-CHECK RO 10/18/2020. REMOVED DAMAGED WINDSHIELD CENTER SUPPORT CLIPS ON THE LT AND RT SIDE AND INSTALLED NEW SERVICEABLE CLIPS, IAW CRJ200.SDR SWIA202053510Floorbeam · corrodedFS 559.0+80 CROSS BEAM RBL 9 TO RBL 27 IS CORRODED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED FLOOR SUPPORT PLATE AT FS 559.0+80 ON TOP OF CROSS BEAM RBL 9 TO RBL 27, IAW CRJ 200 SRM.SDR SWIA202053495Counterbalance · crackedAFT ANCHOR FITTING FOR PASSENGER DOOR COUNTERBALANCE IS CRACKED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED PAX DOOR ANCHOR FITTING, IAW CRJ 200 AMM.SDR SWIA202053509Seat Track · corrodedRBL 27 SEAT TRACK IS CORRODED FROM FS 559.0+80 TO FS 559.0+96. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SEAT TRACK FROM FS 559.0+80 TO FS 559.0+96 AT RBL 27, IAW CRJ 200.SDR SWIA202053508Floor Support · corrodedRBL 9 FLOOR BEAM IS CORRODED BETWEEN FS 559.0+96 TO FS 559.0+112. C-CHECK RO 10/18/2020. REMOVED FABRICATED OUT OF N126-1577 EXTRUSION AND INSTALLED NEW RBL 9 FLOOR BEAM CAP BETWEEN FS 559.0+96 TO FS 559+112, IAW CRJ 200 SRM & IAW MHIRJ REO. REF ATTACHED COSDR SWIA202053507Seat Track · corrodedFLOOR SEAT TRACK ON RBL 9 BETWEEN FS 559.0+80 TO FS 559.0+96 IS CORRODED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SEAT TRACK ON RBL 9 BETWEEN FS 559.0+80 TO FS 559.0+96, IAW CRJ 200 AMM.SDR SWIA202053506Seat Track · corrodedRBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN FS 574 TO FS 559.0+112. C-CHECK RO 10/18/2020. REMOVED AND REPLACED CORRODED SEAT TRACK, IAW CRJ200 AMM. USED TOOL WVACT 6025 CAL DUE 31 MAR 2021.SDR SWIA202053505Seat Track · corrodedLBL 27 FLOOR SEAT RAIL IS CORRODED BETWEEN FS 559.0+80 TO 559.0+96. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SEAT RAIL BETWEEN LBL 27 BETWEEN FS 559.0+80 TO 559.0+96, IAW CRJ 200 AMM.SDR SWIA202053504Seat Track · corrodedLBL 9 CARGO SEAT TRACK IS CORRODED BETWEEN FS 559.00+112 TO FS 574. C-CHECK RO 10/18/2020. REMOVED AND REPLACED LBL 9 CARGO SEAT TRACK, IAW AMM.SDR SWIA202053494Attach Angle · crackedINBOARD AND OUTBOARD ANGLE ATTACHING TO FS 484 INTERCOSTAL BETWEEN PRESSURE FLOOR BEAM RBL 27 AND RBL 36 ARE CRACKED AT UPPER EDGE AT FASTENER HOLE. C-CHECK RO 10/18/2020. REMOVED AND REPLACED ANGLES, IAW CRJ 200 SRM. REFER TO CONTINUE CARD FOR WORK PERFORMSDR SWIA202053493Attach Angle · crackedINBOARD AND OUTBOARD ANGLE ATTACHING TO FS 484 INTERCOSTAL BETWEEN PRESSURE FLOOR BEAM LBL 27 AND LBL 36 ARE CRACKED AT UPPER EDGE AT FASTENER HOLE. C-CHECK RO 10/18/2020. REMOVED AND REPLACED ANGLES, IAW CRJ 200 SRM. REFER TO CONTINUE CARD FOR WORK PERFORMSDR SWIA202053488Seat Track · corrodedSEAT TRACK SEGMENT AT RBL 9 BETWEEN FS 409+128 TO FS 559 IS CORRODED AT MULTIPLE LOCATIONS. C-CHECK RO 10/18/2020. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK, IAW CRJ 200 AMM & REO. REFER TO CONTINUE CARD FOR WORK PERFORMED.SDR SWIA202053487Seat Track · corrodedSEAT TRACK SEGMENT AT LBL 9 BETWEEN FS 409+128 TO FS 559 IS CORRODED MULTIPLE LOCATIONS. C-CHECK RO 10/18/2020. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK, IAW CRJ 200 AMM & REO. REFER TO CONTINUATION CARD FOR WORK PERFORMED.SDR SWIA202053486Seat Track · corrodedSEAT TRACK SEGMENT AT LBL 9 BETWEEN FS 364 TO FS 400 IS CORRODED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SEAT TRACK SEGMENT AT LBL 9 BETWEEN FS 364 AND FS 400, IAW CRJ 200 AMM. REFERENCE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.SDR SWIA202053485Seat Track · corrodedSEAT TRACK SEGMENT AT RBL 9 BETWEEN FS 364 TO FS 400 IS CORRODED. C-CHECK RO 10/18/2020. REMOVED, FABRICATED, AND REPLACED SEAT TRACK, IAW CRJ 200 SRM & REO. REFER TO CONTINUE CARD FOR WORK PERFORMED.SDR SWIA202053484Floorbeam · crackedINBOARD AND OUTBORD ANGLES ATTACHING THE LBL 9 FLOOR BEAM AT FS 280 CROSSBEAM ARE CRACKED IN UPPER RADIUS. C-CHECK RO 10/18/2020. REMOVED AND REPLACED CRACKED CLIPS 2 EA AT STA 280 LBL 9, IAW CRJ200 SRM.SDR SWIA202053480Floor Support · corrodedFLOOR BEAM AT LBL 9 UPPER INBOARD FLANGE IS CORRODED AT MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559. C-CHECK RO 10/18/2020. REPAIRED FLOORBEAM, IAW REO. WEIGHT CHANGE +1.55 LB. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. REFER TO CONTINUE CASDR SWIA202053476Frame · corrodedFRAME SECTOR FS 349 IS CORRODED BETWEEN STRINGERS 25L TO 26R. C-CHECK RO 10/18/2020. REMOVED AND REPLACED FRAME SECTOR FS 349 BETWEEN STRINGERS 25L AND 26R, IAW CRJ 200 SRM. REFERENCE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.SDR SWIA202053474Floor Support · corrodedRIGHT SIDE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION BETWEEN FS 409+128 TO FS 559. C-CHECK RO 10/18/2020. REPAIRED RT SIDE PRESSURE FLOOR SILL CORROSION AT MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559, IAW REO. MAJOR REPAIR TASK CARD & FORM M337 COMPLSDR SWIA202053473Floor Support · corrodedFLOOR BEAM AT RBL 9 UPPER INBOARD FLANGE IS CORRODED AT MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559 AND OUTBOARD FLANGE IS CORRODED AT 1 LOCATION AT FS 559. C-CHECK RO 10/18/2020. REPAIRED FLOOR BEAM AT RBL 9 UPPER INBOARD FLANGE CORROSION AT MULTIPLE LOSDR SWIA202053472Floor Support · corrodedLEFT SIDE PRESSURE FLOOR SILL HAS CORROSION AT MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559. C-CHECK RO 10/18/2020. REPAIRED LEFT SIDE PRESSURE FLOOR SILL CORROSION AT MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559, IAW REO. COMPLETED AND ATTACHED TASSDR SWIA202053471Floor Support · corrodedFLOOR BEAM LBL 9 UPPER INBOARD FLANGE IS CORRODED AT APPROXIMATELY FS 409+30, FS 409+60 AND FS 409+118. C-CHECK RO 10/18/2020. REMOVED, FABRICATED, AND REPLACED/INSTALLED FLOORBEAM CAP, IAW REO CRJ 200 SRMS. MAJOR REPAIR TASK & FORM 337 COMPLETED AND ATTACHSDR SWIA202053492Bracket · crackedOBLIQUE ANGLE IS CRACKED IN RADIUS AT STRINGER 14R AFT SIDE OF FS 621 BULKHEAD. C-CHECK RO 10/18/2020. REMOVED AND REPLACED OBLIQUE ANGLE AT STRINGER 14R ON AFT SIDE OF FS 621 BULKHEAD, IAW BOMBARDIER REO.SDR SWIA202053491Angle · crackedOBLIQUE ANGLE IS CRACKED IN RADIUS AT STRINGER 14L AFT SIDE OF FS 621 BULKHEAD. C-CHECK RO 10/18/2020. REMOVED AND REPLACED OBLIQUE ANGLE AT STRINGER 14L AFT SIDE OF FS 621 BULKHEAD, IAW BOMBARDIER REO.SDR SWIA202053503Gusset · corrodedPAX DOOR SURROUND STRUCTURE GUSSET CORRODED AT FS 349 AT STGR 15L. C-CHECK RO 10/18/2020. REMOVE AND REPLACED PAX DOOR SURROUND STRUCTURE GUSSET AT FS 349 AT STR 15L, IAW CRJ SRM.SDR SWIA202053502Gusset · corrodedPAX DOOR SURROUND STRUCTURE GUSSET CORRODED BETWEEN STGR 15L AND STGR 16L AT FS 310. C-CHECK RO 10/18/2020. REMOVED AND REPLACED GUSSET, IAW CRJ 200 SRM. REFER TO CONTINUE CARD FOR WORK PERFORMED.SDR SWIA202053501Hinge · corrodedPAX DOOR FWD AND AFT HINGE CUPS CORRODED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED FWD AND AFT HINGE CUPS AT PAX DOOR LOWER SILL, IAW CRJ 200 SRM.SDR SWIA202053475Floorbeam · corrodedSERVICE DOOR FLOOR BEAM ANGLE CORRODED AT STGR 18 AND AT FS 349. C-CHECK RO 10/18/2020. REPAIRED SERVICE DOOR FLOOR BEAM ANGLE AT STGR 18 AT FS 349, IAW REO. SEE ATTACHED STRUCTURAL MAJOR REPAIR TASK CARD AND CONTINUE CARD FOR DETAILS OF WORK PERFORMED. NOSDR SWIA202053500Intercostal · corrodedPAX DOOR INTERCOSTAL DD6 CORRODED. C-CHECK RO 10/18/2020. REPAIRED IAW REO. MAJOR REPAIR TASK CARD AND FORM M337 ATTACHED. NO MEASURABLE WEIGHT CHANGE REQUIRED. REFER TO CONTINUE CARD FOR WORK PERFORMED.SDR SWIA202053483Bracket · crackedRT MLG WHEEL WELL FWD HYDRAULIC FUSE BRACKET IS CRACKED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED BRACKET AT RT MLG WHEEL WELL FWD HYDRAULIC FUSE, IAW CRJ200 SRM.SDR SWIA202053482Bracket · crackedLT MLG WHEEL WELL FWD HYDRAULIC FUSE BRACKET IS CRACKED. C-CHECK RO 10/18/2020. REMOVED AND REPLACED HYD FUSE BRACKET, IAW CRJ200 SRM. REFER TO CONTINUE CARD FOR WORK PERFORMED.SDR SWIA202053490Support · crackedLEFT WINDSHIELD SIDE POST SUPPORT P/N 601R34032-21 IS CRACKED AT THE RADIUS ABOVE STRINGER. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SUPPORT, IAW CRJ 200 SRM. MAJOR REPAIR TASK AND FORM M337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE, WAS A PART FOR PART SDR SWIA202053470Support · crackedRIGHT WINDSHIELD SIDE POST SUPPORT P/N 601R34032-22 IS CRACKED IN THE RADIUS ABOVE THE STRINGER. C-CHECK RO 10/18/2020. REMOVED AND REPLACED SUPPORT, IAW CRJ 200 SRM. MAJOR REPAIR TASK AND FORM M337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE, WAS A PART FOR SDR SWIA202053499Skin · corrodedFOUND MINOR EXTERNAL SKIN CORROSION ON BELLY SKIN PANEL FS 559.00+92 TO FS 559.00+112 BETWEEN STGR 26L AND 26R. C-CHECK RO 10/18/2020. REPAIRED IAW REO. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. NO MEASURABLE WEIGHT CHANGE. REFER TO CONTINUE SDR SWIA202053481Angle · crackedRT WHEEL WELL AT WS 50.54 THERE IS A CRACKED ANGLE. C-CHECK RO 10/18/2020. REMOVED DAMAGED ANGLE IN RT WHEEL WELL AT WS 50.54. LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE ANGLE, IAW CRJ200-SRM.SDR SWIA202053479Access Panel · corrodedRT WING LOWER SKIN FUEL PANEL ACCESS PANEL CUT OUT 640BB IS CORRODED AROUND CIRFUMFERENCE. C-CHECK RO 10/18/2020. REPAIRED RT WING LOWER SKIN FUEL PANEL ACCESS PANEL CUT OUT 640BB IS CORRODED AROUND CIRFUMFERENCE. BOMBARDIER REO IT WAS IN THE CRITICAL AREA.SDR SWIA202053477Access Panel · corrodedLT WING LOWER WING PLANK ACCESS PANEL CUTOUT AT 510AB IS CORRODED AROUND THE CIRCUMFERENCE. C-CHECK RO 10/18/2020. REPAIRED LT WING PLANK ACCESS PANEL CUTOUT AT 510AB CORROSION, IAW MHIRJ REO AND BOMARDIER REO. SPECIAL INSPECTION PER NDTM IS DUE AT 62883 FLSDR SWIA202053469Skin · chafedLOWER WING PLANK HAS MINOR CHAFING DAMAGE FROM FUSELAGE FAIRING AT AT BOTH LBL 45 AND RBL 45 AT APPROXIMATELY FS 513. C-CHECK RO 10/18/2020. REPAIRED IAW REO. NO MEASUREABLE WEIGHT CHANGES. MAJOR REPAIR TASK CARD & FORM M337 COMPLETED AND ATTACHED. REFER SDR SWIA202053516Bulkhead · chafedRT ENGINE NOSE INLET AFT BULKHEAD INSPECTION HOLES AT 7, 10, AND 12 O`CLOCK POSITIONS ARE CHAFED AND HAVE BENT/MISSING INSPECTION DOORS. C-CHECK RO 10/18/2020. REPAIRED RT ENGINE NOSE INLET AFT BULKHEAD INSPECTION HOLES AT 7, 10, AND 12 O`CLOCK POSITIONS ARESDR SWIA202053478Skin · dentedADM NR N922EV-6861. THE DENT IS ON THE LT SIDE OF THE FUSELAGE AT FS 262.00 AND APPROXIMATELY 35 INCHES DOWN FROM WL 73.50. THE DAMAGE IS A DENT WITH A LENGTH OF 0.975 INCHES AND A WIDTH OF 0.446 INCHES. THE DEPTH OF THE DENT IS 0.012 INCHES. PLOT, MAP, AN
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