N905EV
Service difficulty reports · 293
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 = 'N905EV' 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 = 'N905EV' 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 SWIA2020031049140Support · damagedANGLE SUPPORT AT FS349.00 COMMON TO CROSSBEAM FRAME SUPPORT BETWEEN LBL 27 AND L/H FLOOR SILL IS EXFOLIATED. (C CHECK) RO 3/7/2020 REMOVED AND REPLACED ANGLE SUPPORT LOCATED BETWEEN LBL27 AND LH FLOOR SILL ON FS349 CROSSBEAM, REFERENCE CRJ200 SRM AND BOMBASDR SWIA2020031049222Seat Track · corroded*LH SEAT FLOOR TRACK (LBL 9), CORROSION AROUND NUMEROUS FASTENERS FS409.00+128 €“ 559.00 (MARKED) (C CHECK) RO 3/7/2020 REMOVED CORROSION ON RH SEAT TRACK LBL 9 BETWEEN FS409.00+12 TO FS559.00 REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS REF BSDR SWIA2020031049219Floorbeam · corroded*FLOORBEAM UPPER CAP LONGITUDIAL BL9 LH FS409.00 TRU FS409.0+128 HAS MULTIBLE AREAS OF CORROSION. MARKED (C CHECK) RO 3/7/2020 BLENDED CORROSION ON FLOORBEAM UPPER CAP BL9 LH AT FS409.0 - FS409.0+128 REF CRJ 200 SRM EVALUATED AND FOUND TO BE OUT OF LIMITSSDR SWIA2020031049216Floor Support · corroded*THE WARDROBE FLOOR SUPPORT FITTING HAS CORROSION BETWEEN FS295.00 AND FS310.00 BETWEEN LBL27.00 AND THE LH FLOOR SILL. (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED THE WARDROBE FLOOR SUPPORT FITTIING PLATE BETWEEN FS295.00 AND FS310.00 BETWEEN LBLSDR SWIA2020031049215Floor Support · corroded*THE WARDROBE FLOOR SUPPORT FITTIING HAS CORROSION BETWEEN FS295.00 AND FS310.00 BETWEEN LBL27.00 AND LBL9.00. (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED THE WARDROBE FLOOR SUPPORT FITTIING PLATE BETWEEN FS295.00 AND FS310.00 BETWEEN LBL27.00 AND SDR SWIA2020031049214Frame · corroded*FS605.00 FRAME IS CORRODED FROM LH STGR25 TO RH STGR24. FAGGED & CIRCLED WITH GREASE PENCIL. (C CHECK) RO 3/7/2020 BLENDED OUT CORROSION ON FS 605 LOWER FRAME AS MARKED BETWEEN STRINGER 25L TO 24R REF CRJ 200 SRM. ORIGINAL THICKNESS OF FS 605 LOWER FRAMSDR SWIA2020031049135Seat Track · corroded*RH SEAT FLOOR TRACK (RBL 9), CORROSION AROUND NUMEROUS FASTENERS FS409.00+128 €“ 559.00 (MARKED (C CHECK) RO 3/7/2020 REMOVED CORROSION ON RH SEAT TRACK RBL 9 BETWEEN FS409.00+12 TO FS559.00 REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS REF CRSDR SWIA2020031049133Intercostal · corroded*BETWEEN FS364.00 AND FS349.00 THE LH INTER-COSTAL IS CORRODED (C CHECK) RO 3/7/2020 LH INTER-COSTAL BETWEEN FS364.00 AND FS349.00 HAS CORROSION ON MORE THAN 2 ELEMENTS AND OVER FASTENER HOLES. INTERCOSTAL IS OUT OF LIMITS REF CRJ200 SRM. REMOVED INTERCOSTSDR SWIA2020031049132Floor Support · corroded* THE FLOOR SUPPORT CROSSBEAM AT FS349.00 AT THE LH FLOOR SILL HAS CORROSION. (MARKED) (C CHECK) RO 3/7/2020 REMOVED CORROSION FROM FLOOR SUPPORT CROSSBEAM REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS. FFLOOR SUPPORT CROSSBEAM AT FS349.00 AT TSDR SWIA2020031049131Seat Track · corroded*THE SEAT TRACK AT LBL9.00 FROM FS364.00 TO FS394.00 HAS MULTIPLE LOCATIONS OF PITTED CORROSION. (MARKED) (C CHECK) RO 3/7/2020 BLENDED SEAT TRACK CORROSION AT LBL9.0 FROM FS364.00 TO FS394.00. EVALUATED AS OUT-OF-LIMITS. REPLACED SEAT TRACK WITH NEW SEATSDR SWIA2020031049129Door Sill · corroded* THE RH FLOOR SILL AT FS 319.00 HAS CORROSION. (MARKED) (C CHECK) RO 3/7/2020 REMOVED CORROSION TO THE R/H FLOOR SILL AT FS 319.00 PER REF: CRJ200 SRM. GALLEY SUPPORT ANGLE ORIGINAL THICKNESS IS .090", AMOUNT REMAINING IS .087" REF NDT, REMOVED .003" ANDSDR SWIA2020031049127Floor Support · corroded* LBL 9.0 AT FS 559.0 TO FS 559.0+80 UPPER CAP HAS AREAS OF CORROSION. (C CHECK) RO 3/7/2020 BLENDED CORROSION FROM FLOOR SUPPORT BEAM CAP AT FS559.00 - FS559.00+80 REF CRJ 200 SRM. ELAUATED AND FOUNF TO BE OUT OF LIMITS. PERFORMED SPLICE REPAIR ON FLOOR SDR SWIA2020031049126Floor Support · corroded* RBL 9.0 FS 559.0 TO FS 559.0+80 UPPER CAP FLOOR SUPPORT HAS AREAS OF CORROSION.(MARKED) (C CHECK) RO 3/7/2020 REMOVED CORROSION FORM RBL 9.0 FS559.0+80 UPPER FLOOR CAP. NDTD FOR THICKNESS, AND EVALUATED AS OUT-OF-LIMITS. INSTALLED NEW UPPER FLOOR SUPPORSDR SWIA2020031049124Angle · damagedF.S 409.0+128 BL 0.0 RH AFT VERTICAL POST RADIUS DEFECT NOTED. (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED NEW LH AND RH ANGLE AT FS 409+128 BL 0 VERTICAL POST. REF CRJ-200 SRM, BOMBARDIER REO AND BOMBARDIER DWG. COMPLIED WITH SKYWEST TASK CARD. ALL ASSOCISDR SWIA2020031049121Angle · corroded*AFT PRESSURE BULKHEAD (FS621) LOWER FLOOR ANGLE IS CHAFED AND CORRODED AROUND SCREW HOLES FROM LH TO RH MARKED WITH GREASE PENCIL & FLAGGED (C CHECK) RO 3/7/2020 REMOVED CORROSION AND CHAFFING ON AFT PRESSURE BULKHEAD (FS621.00) LOWER FLANGE ANGLE REF CRJSDR SWIA2020031049118Channel · corroded*PRESSURE FLOOR BEAM CHANNEL CORROSION FS409.00+128 €“ 559.00 RBL 9(L) (MARKED) (C CHECK) RO 3/7/2020 REMOVED CORROSION FROM PRESSURE FLOOR BEAM CHANNEL BETWEEN FS409.00+128 AND FS559.00 RBL9 REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS, REFSDR SWIA2020031049116Channel · corroded*PRESSURE FLOOR BEAM CHANNEL CORROSION FS409.00+128 €“ 559.00 LBL 9(R) (MARKED) (C CHECK) RO 3/7/2020 REMOVED CORROSION ON PRESSURE FLOOR BEAM CHANNEL FS409.00+128 THRU FS559.00 LBL 9(R). REF. CRJ200 SRM. ORIGINAL MATERIAL THICKNESS IN AREA IS .050" REF.SDR SWIA2020031049114Strap · corroded*PRESSURE FLOOR BEAM STRAP CORROSION FS559.00 RBL 27 AND OUTBD (MARKED) (C CHECK) RO 3/7/2020 REMOVED CORROSION FROM PRESSURE FLOOR BEAM STRAP FS559.00 RBL 27 AND OUTBD. IAW CRJ 200 SRM. STRAP ORIGINAL MATERIAL THICKNESS =.050 IN., MATERIAL LEFT AFTER BLENSDR SWIA2020031049112Strap · corroded*PRESSURE FLOOR BEAM STRAP CORROSION FS559.00 LBL 27 AND OUTBD (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED NEW PRESSURE FLOOR BEAM STRAP AT FS 559.00 & LBL 27.00. REF. BOMBARDIER CRJ200 SRM AND DWG. PRESSURE LEAK CHECKS GOOD.SDR SWIA2020031049111Strap · corroded*PRESSURE FLOOR BEAM STRAP CORROSION FS424.00 RBL 27 AND OUTBD (MARKED) (C CHECK) RO 3/7/2020 REMOVED CORROSION FROM PRESSURE FLOOR BEAM STRAP FS424.00 RBL27 AND OUTBD. CRJ200 SRM. STRAP ORIGINAL MATERIAL THICKNESS = 0.050", MATERIAL LEFT AFTER BLENDING =SDR SWIA2020031049109Strap · corroded*PRESSURE FLOOR BEAM STRAP CORROSION FS424.00 RBL 0 €“ RBL 9 (MARKED) (C CHECK) RO 3/7/2020 REMOVED CORROSION FROM PRESSURE FLOOR BEAM STRAP AT FS424.00 RBL 0 -RBL 9 REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS, REMOVED AND INSTALLED NEW FLOOSDR SWIA2020031049108Strap · corroded*PRESSURE FLOOR BEAM STRAP CORROSION FS424.00 LBL 0 €“ LBL 9 (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED PRESSURE FLOOR BEAM STRAP FS424.00 LBL 0 €“ LBL 9. REF: CRJ-200 AND BOMBARDIER. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA2020031049106Door Sill · corroded*RH PRESSURE FLOOR SILL ANGLE HAS CORROSION FROM FS409.00+128 TO FS559.00 (MARKED) (C CHECK) RO 3/7/2020 REPAIRED RH FLOOR PRESSURE SILL ANGLE REF REO. ALL STEPS COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS. WEIGHT CHANGE NEGLIGIBLE DUE TO BLENDS ONLYSDR SWIA2020031049105Door Sill · corroded*RH PRESSURE FLOOR SILL HAS CORROSION FROM FS409.00+128 TO FS559.00 (MARKED). (C CHECK) RO 3/7/2020 REPAIRED RH FLOOR PRESSURE SILL REF REO. ALL STEPS COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS. NO WEIGHT CHANGE AS THESE WERE MINIMAL BLENDS.SDR SWIA2020031049103Door Sill · corroded*LH PRESSURE FLOOR SILL HAS CORROSION FROM FS409.00+128 TO FS559.00 (MARKED) (C CHECK) RO 3/7/2020 REPAIRED LH FLOOR PRESSURE SILL. ALL STEPS COMPLIED WITH. SEE CONTINUATION CARD FOR DETAILS. NO WEIGHT CHANGE AS THESE WERE MINIMAL BLENDS. PRESSURE CHECKS GSDR SWIA2020031049207Plate · corroded*PAX DOOR FWD ANCHOR SERATED PLATE IS CORRODED (C CHECK) RO 3/7/2020 REMOVED AND REPLACED PAX DOOR FWD ANCHOR FITTING SERRATED PLATE, REF CRJ200 SRM AND CRJ200 AMM. PAX DOOR COUNTER BALANCE ADJUSTMENT CHECK IS GOOD.SDR SWIA2020031049171Rib · cracked*RH WING BATT RIB AT APPROXIMATELY WS48.00 IN GEAR WELL AREA IS CRACKED (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED RH WING BATT RIB AT APPOXIMATELY WS48.00 IN GEAR WELL AREA. REF: CRJ200 SRM.SDR SWIA2020031049170Rib · cracked*LH WING BATT RIB AT APPOXIMATELY WS48.00 IN GEAR WELL AREA IS CRACKED (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED LH WING BATT RIB AT APPOXIMATELY WS48.00 IN GEAR WELL AREA. REF: CRJ200 SRM.SDR SWIA2020031049169Anchor Fitting · cracked*PAX DOOR AFT ANCHOR IS CRACKED. FLAGGED (C CHECK) RO 3/7/2020 ORDERED AND RECEIVED NEW SERVICEABLE PAX DOOR AFT ANCHOR FITTING P/N 601R38074-7 QTY.1 AND HAS BEEN INSTALLED WITH NEW ATTACHING HARDWARE REF CRJ 200 AMM AND CRJ 200 SRM. PAX DOOR COUNTER BALSDR SWIA2020031049101Skin · cracked*THE EXTERNAL FUSELAGE ON THE LOWER RH SIDE JUST AFT OF AFT NOSE LANDING GEAR DOOR IS CRACKED. (MARKED). (C CHECK) RO 3/7/2020 REPAIRED THE EXTERNAL FUSELAGE ON THE LOWER RH SIDE JUST AFT OF AFT NOSE LANDING GEAR DOOR. REF BOMBARDIER REO. PRESSURE CHECKS SDR SWIA2020031049240Attach Angle · chafed*THE VERITCAL STABILIZER LEADING EDGE PANEL LOWER FAIRING SUPPORT RIB'S RH UPPER ATTACH ANGLE IS CHAFED. (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED A NEW ANGLE, ON THE VERTICAL STABILIZER LEADING EDGE, THE LOWER FAIRING SUPPORT RIB R-H UPPER ATTACH ANGLE SDR SWIA2020031049239Attach Angle · chafed*THE VERITCAL STABILIZER LEADING EDGE PANEL LOWER FAIRING SUPPORT RIB'S LH UPPER ATTACH ANGLE IS CHAFED. (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED A NEW ANGLE, ON THE VERTICAL STABILIZER LEADING EDGE, THE LOWER FAIRING SUPPORT RIB L-H UPPER ATTACH ANGLE SDR SWIA2020031049202Fastener · corroded*RH OUTBD GROUND SPOILER, CORROSION ON BOTH HINGE ATTACH HARDWARE (C CHECK) RO 3/7/2020 REPLACED RH OUTBD GROUND SPOILER BOTH HINGE ATTACHING HARDWARE REF CRJ200 AMM. OPS CHECK GOOD.SDR SWIA2020031049200Fastener · corroded*LH SPOILERON, CORROSION ON THE INBD HINGE ATTACH HARDWARE (C CHECK) RO 3/7/2020 REPLACED LH SPOILERON INBD HINGE ATTACHING HARDWARE REF CRJ200 AMM. CHECKS GOOD.SDR SWIA2020031049193Fastener · corroded*LH INBD GROUND SPOILER CORROSION ON BOTH HINGE ATTACH HARDWARE (C CHECK) RO 3/7/2020 REPLACED LH INBD GROUND SPOILER BOTH HINGE ATTACHING HARDWARE REF CRJ200 AMM. OPS CHECK GOOD.SDR SWIA2020031049100Frame · cracked*FRAME BELOW THE LEFT WINDSHIELD SIDE POST SUPPORT IS CRACKED. (C CHECK) RO 3/7/2020 REMOVED FRAME BELOW LEFT WINDSHIELD SIDE POST SUPPORT REF CRJ 200 SRM. INSTALLED NEW FRAME BELOW LEFT WINDSHIELD SIDE POST SUPPORT WITH NEW REF CRJ 200 SRM. PRESSURE LEASDR SWIA2020031049098Intercostal · cracked* THE INTERCOSTAL BETWEEN FS 621 AND FS 625, AT STRINGER LOCATION 15R, HAS A SUSPECTED CRACK ON ITS OUTBOARD FLANGE THAT ATTACHES TO THE FUSELAGE SKIN. (C CHECK) RO 3/7/2020 REMOVED CRACKED INTERCOSTAL CLIP REF. CRJ200 SRM. LOCATED AND DRILLED FULL SIZE ALSDR SWIA2020031049097Intercostal · cracked* THE INTERCOSTAL BETWEEN FS 621 AND FS 625, AT STRINGER LOCATION 14L, HAS A SUSPECTED CRACK ON ITS OUTBOARD FLANGE THAT ATTACHES TO THE FUSELAGE SKIN. (C CHECK) RO 3/7/2020 VERIFIED THE CRACK. REMOVED THE CRACKED INTERCOSTAL / BRACKET AT STRINGER 14L BETSDR SWIA2020031049096Intercostal · cracked* THE INTERCOSTAL ADJACENT TO STRINGER 14R, THAT SPANS BETWEEN FS 621 AND FS 625, IS CRACKED. (C CHECK) RO 3/7/2020 REMOVED AND REPLACED CLIP P/N: 601-35012-52 BETWEEN FS 621 AND FS 625, STRINGER 14R REF. CRJ-200 SRM AND BOMBARDIER. COMPLIED WITH SKYWEST TSDR SWIA2020031049095Intercostal · cracked* THE INTERCOSTAL ADJACENT TO STRINGER 14L, THAT SPANS BETWEEN FS 621 AND FS 625, IS CRACKED. (C CHECK) RO 3/7/2020 REMOVED AND REPLACED CLIP P/N: 601-35012-51 BETWEEN FS 621 AND FS 625, STRINGER 14L REF. CRJ-200 SRM AND BOMBARDIER. COMPLIED WITH SKYWEST TSDR SWIA2020031049237Bracket · chafed*PASSENGER DOOR UPPER AFT ROLLER BRACKET ON SURROUND, CHAFFED (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED PAX DOOR UPPER AFT ROLLER BRACKET ON DOOR SURROUND, PN 600-31471-9 PO T-51948, REFERENCE CRJ200 SRM.SDR SWIA2020031049244Latch · broken*GROUND A/C DOOR 172BR AFT LATCH BULLNOSE BROKEN (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED NEW LATCH AND RIVETS IN PANEL 172BR, AFT GROUND A/C DOOR, REF CRJ200, SRM.SDR SWIA2020031049189Nut Plate · corroded*NUT PLATES ATTACHING HINGE FITTINGS IN BOTTOM OF R/H EMERGANCY-EXIT HAVE CORROSION. (C CHECK) RO 3/7/2020 REMOVED ATTACHING HINGE IN ORDER TO REMOVE NUTPLATES, REMOVED CORRODIED NUTPLATES AND RIVETS, INSTALLED NEW NUTPLATES AND RIVETS, INSTALLED ATTACHINGSDR SWIA2020031049168Mount Bracket · cracked*PAX DOOR ASSIST MOTOR MOUNT BRACKET IS CRACKED. (C CHECK) RO 3/7/2020 REMOVED DISCREPANT CRACKED MOTOR MOUNT BRACKET REF. CRJ200 SRM. LOCATED AND DRILLED FULL SIZE ALL HOLES COMMON TO REPLACEMENT PAX DOOR MOTOR MOUNT BRACKET, REF. CRJ200 SRM. INSTALLED RSDR SWIA2020031049233Panel · chafedCHAFFING ON THE RIGHT HAND WING AILERON PANEL 699BB. (C CHECK) RO 3/7/2020 ORDERED AND RECIEVED NEW RH AILERON PANEL 699BB. DRILLED AND COUNTERSUNK FASTENER HOLES ON NEW PANEL REF SRM.SDR SWIA2020031049232Guide · chafedCHAFFING ON THE GUIDES ON RIGHT HAND WING FLAP HINGE FAIRING 692BB. (C CHECK) RO 3/7/2020 REMOVED AND REPLACED GUIDES ON RIGHT HAND WING FLAP HINGE FAIRING 692BB REF CRJ-200 SRM.SDR SWIA2020031049094Skin · dentedADM#3845 - DENT FOUND ON RH SIDE OF FUSELAGE SKIN PANEL APPROXIMATELY FS 275.8 BETWEEN STGR 22R AND 23R. (C CHECK) RO 3/7/2020 HAND DRESSED TO REFORM TO ORIGINAL CONTOUR TO DISCREPANT SKIN, ENSURED NO OIL CANNING OCCURRED POST REWORK COMPLIED WITH REO. SESDR SWIA2020031049243Skin · dentedADM#3858 - L/H WING TRAILING EDGE WS 220.00 HAS 11 DENTS ON THE UPPER SKIN. (MARKED) (C CHECK) RO 3/7/2020 REMOVED AND REPLACED L/H WING TRAILING EDGE PANEL P/N 601R10226+5 PER REF: DWG, AD AND CRJ200 SRM. SEE CONTINUATION FOR DETAILSSDR SWIA2020031049242Skin · dentedADM#3861 - R/H WING TRAILING EDGE WS 220.00 HAS 6 DENTS ON UPPER SKIN. (MARKED (C CHECK) RO 3/7/2020 DENT AT APPROXIMATELY WS219.40 MEASURES .560" LONG BY .463" AND .004" DEEP WITH A W/D RATIO OF 115. DENT AT APPROXIMATELY WS221.80 MEASURES .450 LONG BYSDR SWIA2020031049204Skin · dentedADM#3863 - TOTAL OF 9 DENTS WERE FOUND ON THE R/H FLIGHT SPOILER UPPER SKIN(MARKED) (C CHECK) RO 3/7/2020 REMOVED AND INSTALLED NEW RH FLIGHT SPOILER REF. CRJ200 AMM RIG AND OP CHECKS GOOD.
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