N914EV
Service difficulty reports · 200
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 = 'N914EV' 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 = 'N914EV' 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 SWIA2025060900003Skin · dentedFOUND 1 INWARD DENT/GOUGE ON THE OUTER FUSELAGE SKIN APPROX. FS 785.00 IN BETWEEN STR 5R & STR 6R. (FILED CLOSED)COMPLIED WITH REO 601R-53-71-235 DATED: 2025-06-07 REV:-- REPAIR TO FUSELAGE SKIN BETWEEN V-STAB 43.75% - 55.625%(FS 780.00- FS 785.00) & BETWEEN SDR SWI202405200415Apu · overtempD: APU OVERTEMP WARNING IN FLIGHT. RAN QRH AND MESSAGE CLEARED.C: MEL 49-10-1ACAT C DUE 5/27/24APU OVERTEMP WARNING IN FLIGHT. RAN QRH AND MESSAGE CLEARED.MAY 17, 2024 STATION: FAR--DEFERRED APU PER CRJ 200 MEL 49-10-1A. MX ACTION COMPLIED WITH AND PLACARD INSDR SWIA202310250024Unknown · warning messageL 10TH DUCT WARNING MESSAGE ON CLIMB AT 15000FT. DID THE QRH PROCEDURE, DIRECTED TO GET LEFT ENGINE TO IDLE. DECLARED EMERGENCY AND DID A SINGLE ENGINE LANDING WITH RIGHT ENGINE. (FLIGHT 5541 FILED OPEN)FOUND LEAK COMING FROM LH 10TH STAGE PRSOV FLANGE CRACK FSDR SWIA20231023Unknown · warning messageREPEAT L 10TH DUCT WARNING MESSAGE ON CLIMB OUT. PLEASE REVIEW HISTORY AND T/S NEXT OVERNIGHTMCI TYPE: TROUBLESHOOTING PRIORITY 1 (FLIGHT 5452 FILED CLOSED)OCT 24, 2023 STATION: RDD--REMOVED AND REPLACED HEATING ELEMENT SENSOR AT A17WK PER CRJ-200 AMM 36-21SDR SWIA202305220017Landing Gear · warning messageGEAR DISAGREE WARNING MESSAGE WHILE SELECTING GEAR DOWN. NOSE GEAR SHOWED DOWN POSITION WHILE MAIN GEAR REMAINED IN UP POSITION. MESSAGE CLEARED DURING GO AROUND. ALL THREE SHOWED DOWN. COMPLIED WITH QRH. (FLT 5135, FILED CLOSED)UPON ARRIVAL TO A/C FOUND PSEUSDR SWIA2023051800017Landing Gear · warning messageGEAR DISAGREE WARNING MESSAGE WHILE SELECTING GEAR DOWN. NOSE GEAR SHOWED DOWN POSITION WHILE MAIN GEAR REMAINED IN UP POSITION. MESSAGE CLEARED DURING GO AROUND. ALL THREE SHOWED DOWN. COMPLIED WITH QRH. (FLT 5135, FILED OPEN)THIS IS CURRENTLY A WORK IN PROGSDR SWIA20230117None · corrodedDURING CORRODED FASTENERS REMOVAL FOUND CORROSION ON RBL 9.0 SEAT RAIL SECTION FS 409.0 TO FS 409+16. (C-CHECK RO 2/18/2023) SEAT RAIL AT RBL 9.0 FROM FS409.0 TO FS409+128 WAS REMOVED,FABRICATED AND INSTALLED NEW REF REO 601R-53-00-485 REV. D 2018-01-2SDR SWIA202301107None · corroded*LH CABIN PRESSURE FLOOR SILL CORROSION AROUND SCREW HOLES (2EA) BETWEEN FS529.00 & FS540.25 (C-CHECK RO 2/18/2023) REMOVED CORROSION ON THE LEFT-HAND CABIN PRESSURE FLOOR SILL PANEL AROUND 2 EA. SCREW HOLES BETWEEN FS529.00 AND FS540.25, AND EVALUATEDSDR SWIA2023011007None · corrodedCORROSION ON FRAME FS 589.00, BETWEEN STGR 19R - 20R. MARKED. (C-CHECK RO 2/18/2023) REMOVED CORROSION ON FRAME FS589.00, BETWEEN STGR 19R-20R REF. CRJ-200 SRM, 51-21-06. PARTS FABBED AND INSTALLED REPAIR PARTS FRAME SECTION -1 AND FRAME SPLICE -2 ON FRSDR SWIA20230116None · crackedPRESSURE FLOOR SUPPORT BEAM AT FS 460.0 RBL 9.0 CASTING HAS CRACK AT UPPER RADIUS. (C-CHECK RO 2/18/2023) REMOVED CRACKED FITTING AT FS460.00, RBL 9.0, AND INSTALLED NEW FITTING, PN: 600-31068-19. REF. DWG 601R31146 REV. J, DWG 601R31118 REV. L, CRJ200 SDR SWIA2023011006None · crackedFS 280. BOTH AT LBL 9.0 AND RBL 9.0 (2 EA) INBOARD CLIPS HAS SUSPECT CRACKS AT UPPER RADIUS. (C-CHECK RO 2/18/2023) REMOVED AND INSTALLED 1 EA NEW INBOARD ATTACH CLIP AT LBL 9.0 AT FS 280.0 P/N 601R31113-57 AND 1 EA ATTACH CLIP AT RBL 9.0 P/N 601R31113-SDR SWIA202301106None · damagedEXISTING PASSENGER DOOR SEAL STRIKER DAMAGE JUST ABOVE FORWARD UPPER PIN STOP FITTING ON FORWARD SIDE OF DOOR CUTOUT (C-CHECK RO 2/18/2023) REMOVED AND REPLACED PASSENGER DOOR SEAL STRIKER JUST ABOVE FORWARD UPPER PIN STOP FITTING ON FORWARD SIDE OF DOOSDR SWIA20230114None · dentedGROUND AIR CONDITIONING DOOR SURROUND (LANDING PLATE) IS PUSHED IN (DENTED) AND DAMAGED. (C-CHECK RO 2/18/2023) REMOVED AND REPLACED FWD ANGLE AT GROUND AIR CONDITIONING DOOR SURROUND REF. CRJ-200 SRM, 51-42-06 AND DWG 601R35226 REV-P. COMPLIED WITH TASSDR SWIA202301007None · dentedDENT NEAR FS409+16 STGR 26L (C-CHECK RO 2/18/2023) PERFORMED PERMANENT REPAIR TO DENT AREA OF FUSELAGE STATION FS409.00 AT STGR26L. REF. MHIRJ REO 601R-53-31-1258 REV -- DATED 2023-01-26. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY STRUCTURAL MAJORSDR SWIA202301006None · dented*MULTIPLE DENTS NOTED ON L/H FLIGHT SPOILER UPPER SURFACE (MARKED) (C-CHECK RO 2/18/2023) REMOVED THE PAINT & EVALUATED THE MULTIPLE DENTS ON THE LH FLIGHT SPOILER REF CRJ-200 SRM 57-73-00 AND COMPLIED WITH ALL THE STEPS OF THE REO 601R-57-73-401 REV--SDR SWIA202301004None · chafed*CHAFFING NOTED AT R/H AILERON L/E LOWER SKIN (MARKED) (C-CHECK RO 2/18/2023) BLENDED OUT DAMAGE ON SKIN PANEL @ AIL STA.370.664 FOUND TO BE WITHIN LIMITS REF REO 670-57-61-194 REV -C DATED 2019-01-07. REMOVED AND REPLACED SKIN PANEL @ AIL STA.324.459SDR SWIA202301002None · chafed* AFT CARGO DOOR, EXTERIOR SKIN REPAIR DOUBLER ( PREVIOUS REPAIR ) HAS CHAFFED AREAS ( 2 EACH ). (C-CHECK RO 2/18/2023) REMOVED & INSTALLED NEW REPAIR DOUBLER (-1) P/N 2024T-3 0.080 PO: T-58292 REF REO NO. 601R-52-31-310 REV -B DATED 2019-06-13, CRJ200 SDR SWIA202212300None · dentedTHE UPPER SURFACE OF THE LH AILERON HAS MULTIPLE DENTS. PLEASE PLOT, MAP AND EVALUATED THE DAMAGE/AREA. IF THE DAMAGE IS FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICES/PROCEDURES. (C-CHECK RO 2/18/2023) DENTS ON SDR SWIA20221209None · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA67724-601R-52-11-2861 N914EV MXCODEID55300-PR - DUE TO DENT IN MCD ABOUT 3/4 WAY UP DENT MEASURES 1 1/4 WIDE BY 1 3/4 LONG AND 1/32 DEPTH, COMPLIED WITH TEMPORARY DISPOSITION PER REO 601R-52-11-2861 STEPS 1 -4. PERMANESDR SWIA202265390Unknown · odorSTRONG SMELL OF FUEL IN CABIN (FLIGHT 5682 - FILED CLOSED) UPON FURTHER INSPECTION, FUEL LEAK FOUND INSIDE THE APU BOX AT THE FUEL SHUTOFF SOLENOID VALVE FITTING GOING INTO FUEL CONTROL. REMOVED AND REPLACED THE PACKING ON THE FUEL SHUTOFF SOLENOID VALVE SDR SWIA2019120946855Support Angle · cracked* SUPPORT ANGLE CRACKED ON AFT SIDE OF FS 621 LEFT SIDE AT APROX STRG14L MARKED (C-CHECK) RO 12/6/2019 REMOVED AND REPLACED CRACKED SUPPORT ANGLE WITH NEW ANGLE ON AFT SIDE OF FS 621 LEFT SIDE AT APROX STRG14L IAW SRM.SDR SWIA2019120946854Support Angle · cracked* SUPPORT ANGLE CRACKED ON FS 621 RIGHT SIDE AT APROX STRG14R MARKED (C-CHECK) RO 12/6/2019 REPLACED ANGLE AT AFT SIDE OF FS621 RHS AT APPROX STGR14R IAW SRM. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**)SDR SWIA2019120946853Floor Support · corroded* L/H PRESSURE FLOOR SILL PANEL HAS SEVERAL AREAS OF CORROSION FROM FS 409+128 TO FS 559.0 (C-CHECK) RO 12/6/2019 LH PRESSURE FLOOR SILL PANEL BLENDED FROM FS 409+128 TO FS 559.0, FOUND TO BE WITHIN LIMITS AND RESTORED TO ORIGINAL IAW REO. COMPLIED WITH SKYSDR SWIA2019120946852Floor Support · corroded* L/H PRESSURE FLOOR SILL ANGLE HAS SEVERAL AREAS OF CORROSION FROM FS 409+128 TO FS 559.0 (C-CHECK) RO 12/6/2019 LH PRESSURE FLOOR SILL ANGLE IS BLENDED, FOUND TO BE WITHIN LIMITS AND RESTORED TO ORIGINAL IAW REO.SDR SWIA2019120946851Floor Support · corroded* R/H PRESURE FLOOR SILL PANEL HAS SEVERAL AREAS OF CORROSION FS 409+128 TO FS 559.0 (C-CHECK) RO 12/6/2019 REMOVED CORROSION AND EVALUATED REPAIRS AT 9 LOCATION ON R/H PRESSURE FLOOR SILL PANEL . REPAIRS FOUND TO BE WITHIN LIMITS. IAW REO. NO FASTENERS REMOVSDR SWIA2019120946850Floor Support · corroded* R/H PRESSURE FLOOR SILL ANGLE HAS SEVERAL AREAS OF CORROSION FROM FS 409+128 TO FS 559.0 (C-CHECK) RO 12/6/2019 BLENDED DAMAGE ON RH FLOOR SILL AT ALL LOCATIONS FS409.128 - FS559.0. IAW SRM. ALL WITHIN LIMITS IAW REO. RESTORED THE CIC AND TOP COAT FINISH. SDR SWIA2019120946849Floor Support · corroded* FLOOR BEAM CAP @ FS 559+16 TO FS 559+80 RBL 9 HAS CORROSION (C-CHECK) RO 12/6/2019 FABRICATED AND INSTALLED NEW FLOOR BEAM CAP IAW REO. SEE CONTINUE CARD FOR ALL DETAILS.SDR SWIA2019120946848Floor Support · corroded* L/H SILL FROM FS 559.0 TO FS 559+80 HAS CORROSION SEVERAL AREAS (C-CHECK) RO 12/6/2019 REMOVED CORROSION ON L/H FLOOR SILL FROM FS559.00 TO FS559.00+80 AND EVALUATED REPAIR. REPAIR FOUND TO BE WITHIN LIMITS AND RESTORED SILL TO ORIG. CONFIGURATION. IAW REOSDR SWIA2019120946847Floor Support · corroded* R/H SILL FROM FS 559.0 TO FS 559+80 HAS CORROSION SEVERAL AREAS (C-CHECK) RO 12/6/2019 COMPLIED WITH ALL THE STEPS IAW REO. REMOVED CORROSION ON R/H FLOOR SILL BETWEEN FS559.0 AND FS559.+80. REPLACED BLIND FASTENERS. SILL ORIGINAL THICKNESS IS 0.063 IAW SRMSDR SWIA2019120946846Seat Track · corroded* SEAT TRACK FS 559+112 TO JUST AFT OF FS 574.0 LBL 9 HAS CORROSION (C-CHECK) RO 12/6/2019 BLENDED OUT CORROSION IS OUT OF LIMITS, REMOVED, REPLACED AND INSTALLED NEW CARGO TIE-DOWN TRACK P/N 601R38779-5 AT FS559+112 TO FS568 LBL9.IAW AMM.SDR SWIA2019120946845Seat Track · corroded* SEAT TRACK FS 559+112 TO JUST AFT OF FS 574.0 RBL 9 HAS CORROSION (C-CHECK) RO 12/6/2019 REPLACED CARGO SEAT TRACK BETWEEN FS559+112 AND FS574.00 RBL 9 IAW AMM. SEE CONTINUE CARD FOR DETAILSSDR SWIA2019120946844Seat Track · corroded* SMALL SECTION OF SEAT TRACK JUST AFT OF FS 559+80 TO FS 559+96 LBL 27 HAS CORROSION (C-CHECK) RO 12/6/2019 REMOVED CORROSION ON THE AFFECTED SEAT TRACK. REF CRJ200 SRM 51-21-06. SEE CONTINUATION CARD FOR ADDITIONAL DETAILSSDR SWIA2019120946843Seat Track · corroded* SMALL SECTION OF SEAT TRACK JUST AFT OF FS 559+80 TO FS 559+96 LBL 9 HAS CORROSION (C-CHECK) RO 12/6/2019 REMOVED AND BLENDED OUT CORROSION IS WITHIN LIMITS ON SEAT TRACK AT FS559+80 TO FS559+96 LBL9. IAW SRM.SDR SWIA2019120946842Seat Track · corroded* SMALL SECTION OF SEAT TRACK JUST AFT OF FS 559+80 TO FS 559+96 RBL 27 HAS CORROSION (C-CHECK) RO 12/6/2019 REMOVED CORROSION ON THE AFFECTED SEAT TRACK. IAW SRM. REFER TO CONTINUE CARD FOR ADDITIONAL DETAILS.SDR SWIA2019120946841Seat Track · corroded* SMALL SECTION OF SEAT TRACK JUST AFT OF FS 559+80 TO FS 559+96 RBL 9 HAS CORROSION (C-CHECK) RO 12/6/2019 BLENDED OUT DAMAGE AND RESTORED FINISH TO SEAT TRACK AFT OF FS559+80 TO FS559+96. IAW SRM.SDR SWIA2019120946840Floorbeam · corroded* CROSS BEAM TOP CAP FS 559+112 LBL 27 TO SILL HAS CORROSION (C-CHECK) RO 12/6/2019 REMOVED CORROSION AND EVALUATED REPAIRS. REPAIRS FOUND TO BE WITHIN LIMITS AND RESTORED REPAIR TO ORIG. FINISH. IAW SRM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.SDR SWIA2019120946839Floorbeam · corroded* CROSS BEAM TOP CAP FS 559+80 RBL 27 TO THE SILL HAS CORROSION (C-CHECK) RO 12/6/2019 BLENDED CORROSION FROM CROSS BEAM TOP CAP FS 559+80 RBL 27 TO THE SILL. THE AREA IS FOUND TO BE WITHIN LIMITS AND RESTORED TO ORIGINAL IAW SRM.SDR SWIA2019120946838Floorbeam · corroded* CROSS BEAM TOP CAP FS 559+80 RBL 9 TO RBL 27 HAS CORROSION (C-CHECK) RO 12/6/2019 CROSS BEAM TOP CAP FS 559+80 RBL 9 TO RBL 27 IS BLENDED, FOUND TO BE WITHIN LIMITS AND RESTORED TO ORIGINAL FINISH IAW SRM.SDR SWIA2019120946837Floor Support · corroded* RH SILL FROM FS 559+80 TO FS 621.0 HAS SEVERAL AREAS OF CORROSION (C-CHECK) RO 12/6/2019 REMOVED CORROSION ON R/H FLOOR SILL FROM FS559.00+90 TO FS621.00 AND EVALUATED REPAIR. REPAIR WAS FOUND WITHIN LIMITS AND RESTORED TO ORIG. CONDITION. AIW REO. SEE COSDR SWIA2019120946836Bulkhead · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD 2019-08-04/02 40000 FC - COMPLY WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITHSDR SWIA2019091746314Warning System · activatedGEAR DISAGREE ON TAKE OFF. C/W QRH PROCEDURE ALL THREE GEAR CAME DOWN AND LOCKED. FLT DIVERTED TO MBS. (FLT#4303) CLOSED DEFERRED MLG RETRACTION SYSTEM PER.SDR SWIA2019082246196Engine · overtempRIGHT ENGINE HIGH TEMP, PEAKED 169; FOLLOWING QRH PROCEDURE ENGINE SHUTDOWN IN FLIGHT. EMERGENCY DECLARED. REMOVED AND REPLACED ENGINE OIL LEVEL SIGNAL CONDITIONER, ENGINE REPLENISHMENT SIGNAL CONDITIONER, RH ENGINE LOW-OIL LEVEL PROBE, RH ENGINE VIOLET HARNSDR SWIA2019080146107Sensor · out of adjustRECEIVED NWS STEERING INOP CAUTION MESSAGE FOLLOWED BY WOW INPUT CAUTION MESSAGE FOLLOWED BY WOW OUTPUT FAIL. NORMAL LANDING AND STEERING OPERATION. FLT 3959. COMPLIED WITH RE-RIG OF SENSOR-TO-TARGET GAP FOR NLG WOFFW PS13GA AND PS4GA IAW AMM, COMPLETED FULLSDR SWIA2019080246115Seal · failedAFTER TAKEOFF NOSE GEAR DISAGREE ACCOMPANIED BY NOSE DOOR OPEN AND STEERING INOP. PERFORMED QRH PROCEDURE AND LANDED WITHOUT INCIDENT. FLT 3742. REMOVED AND REPACKED BACKUP NLG SEALS AND INSTALLED NEW GUIDE PINS IAW AMM. PERFORMED MLG EXTENSION AND RETRACTIOSDR SWIA2018073044880Pump · failedHYD 3 LO PRESS CAUTION MESSAGE AFTER TAKE OFF. (FLT 3623) FO: 7/16/2018 CLOSED / REMOVED AND REPLACED ACMP 3A IAW AMM. SERVICED HYD SYSTEM 3, OPS CHECK GOOD.SDR SWIA201743729Bracket · brokenRECEIVED A GEAR DISAGREE WARNING MESSAGE. CREW COMPLIED WITH QRH & RETURNED TO FIELD. REPLACED THE NOSE GEAR UPLOCK BRACKET. SYSTEM OPS CHECKED GOOD.SDR SWIA201743519Skin · crackedLOWER WING PLANK HAS MULTIPLE INDICATIONS NOTED ON THE LANDING FOR ACCESS PANEL 550BB ON THE OTBD SIDE AND FWD SIDE. REPAIRED IAW REO.SDR SWIA201743518Skin · crackedLOWER WING PLANK HAS MULTIPLE INDICATIONS NOTED ON THE LANDING FOR ACCESS PANEL 540DB ON THE OTBD SIDE, BOTH .200 INCH . REPAIRED IAW REO.SDR SWIA201743515Skin · crackedLOWER RT WING PLANK HAS ONE INDICATION NOTED ON THE LANDING FOR ACCESS PANEL 650GB ON THE AFT SIDE. REPAIRED IAW REO.SDR SWIA201743517Skin · crackedMULTIPLE INDICATIONS NOTED IN LOWER WING PLANK AT RT BOOST PUMP ACCESS PANEL LANDING 610CB AROUND ENTIRE CIRCUMFERENCE HORIZONTAL AND VERTICAL SURFACES. REPAIRED IAW REO.
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