N933EV

Service difficulty reports · 186

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 = 'N933EV' 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 SWIA202265850None · corrodedRH PRESSURE FLOOR SILL PANEL HAS SPOTS OF CORROSION AT FS.409.00. + 128 TO FS.559.00. (MARKED) (C-CHECK RO 6/1/2022) REMOVED CORROSION ON RH PRESSURE FLOOR SILL PANEL HAS 8 SPOTS AT. FS. 409.00+128 TO FS559.00 REF. REO #601R-53-41-666 REV.-C DATED 2012Apr 7, 2022 · N933EV · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265849None · corroded* LH PRESSURE FLOOR SILL HAS SPOTS OF CORROSION AT LBL36 AND APPOX. FS. 484.00 (MARKED). (C-CHECK RO 6/1/2022) REMOVED CORROSION ON LH PRESSURE FLOOR SILL FROM 2 SPOTS AT LBL36 AND APPOX. FS. 484.00 REF CRJ200 SRM 51-21-06. EVALUATED AND FOUND TO BE WIApr 6, 2022 · N933EV · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265848None · corroded* FLOOR BOARD SUPPORT ANGLE AT FS.621.00 BETWEEN RBL9 AND RBL27 HAS A SPOTS OF CORRSIOIN (MARKED). (C-CHECK RO 6/1/2022) INSTALLED NEW FLOOR BOARD SUPPORT ANGLE AT FS.621.00 BETWEEN RBL9 AND RBL27.REF REO 601R-53-61-3780 REV -A DATE 2011-07-15, REO 601RApr 6, 2022 · N933EV · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202265847None · corroded* THE RH WING LOWER SKIN'S EXTERNAL SURFACE HAS A SMALL SPOT OF SURFACE CORROSION AT RBL 45, WHERE ACCESS PANEL 193AB MEETS THE WING'S TRAILING EDGE. (C-CHECK RO 6/1/2022) REMOVED THE CORROSION WHERE PANEL 193AB MEETS THE R/H WING TRAILING EDGE AT RBL 4Apr 5, 2022 · N933EV · Cndair CL6002B19 · Wing StructureSDR SWIA202265846None · cracked* R/H WINDSHIELD SIDE POST SUPPORT CRACKED. (C-CHECK RO 6/1/2022) REMOVED AND REPLACED CRACKED R/H WINDSHIELD SIDE POST SUPPORT FITTING WITH NEW REF. CRJ 200 SRM 51-42-21 AND DWG #601R33007 REV -U. COMPLIED SKYWEST CARD 51-900-1003-SKY AND FORM M-337.Apr 4, 2022 · N933EV · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202265845None · cracked* L/H WINDSHIELD SIDE POST SUPPORT CRACKED. (C-CHECK RO 6/1/2022) REMOVED AND REPLACED L/H WINDSHIELD SIDE POST SUPPORT REF. CRJ200 SRM 51-42-21 AND DWG 601R33007 REV -U. COMPLIED WITH TASK CARD 51-900-1003-SKY.Apr 4, 2022 · N933EV · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202265844None · gougedL/H WING - FWD FACE OF FWD SPAR HAS A GOUGE TO BARE METAL - WS 389L (C-CHECK RO 6/1/2022) REPAIRED L/H WING - FWD FACE OF FWD SPAR REF REO 601R-57-21-3586 REV -- DATED 2022-04-15. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.Apr 2, 2022 · N933EV · Cndair CL6002B19 · Wing StructureSDR SWIA202265843None · chafed*LH AILERON ASSY UPPER LEADING-EDGE SKIN CHAFFED MULTIPLE AREAS ALONG ENTIRE WIDTH (MARKED) (C-CHECK RO 6/1/2022) REMOVED AND REPLACED LH AILERON ASSY UPPER LEADING-EDGE SKIN REF DWG CC670-13000 REV-D, CRJ200 SRM 51-42-21, CRJ200 SRM 51-42-22, AND CRJ20Apr 1, 2022 · N933EV · Cndair CL6002B19 · Aileron TabsSDR SWIA202265842None · gouged* THE MAIN AVIONICS COMPARTMENT DOOR'S HANDLE HOUSING HAS GOUGES FROM CONTACT WITH THE HANDLE ASSY, AND SURFACE CORROSION NEAR ITS MID POINT ON THE RH SIDE OF THE HANDLE CUTOUT. (C-CHECK RO 6/1/2022) INSTALLED NEW AVNX COMPARTMENT DOOR HANDLE ASSY REF CMar 28, 2022 · N933EV · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA202265841None · gouged* THE CARGO DOOR'S EXTERNAL HANDLE HOUSING HAS SMALL GOUGES FROM CONTACT WITH THE HANDLE ASSY. (C-CHECK RO 6/1/2022) REMOVED AND INSTALLED NEW CARGO DOOR HANDLE HOUSING REF CRJ200 SRM 51-42-21 AND DWG 601R35027 REV-AY. COMPLIED WITH TASK CARD 51-900-100Mar 28, 2022 · N933EV · Cndair CL6002B19 · DoorsSDR SWIA202265840None · chafed* THE CARGO DOOR'S EXTERNAL SKIN HAS CHAFES AND SCRATCHES ALONG THE TOP EDGE NEAR IT'S CENTERLINE. (C-CHECK RO 6/1/2022) REPAIRED THE CARGO DOOR'S EXTERNAL SKIN CHAFES AND SCRATCHES ALONG THE TOP EDGE NEAR IT'S CENTERLINE REF REO 601R-52-31-396 REV -- DMar 28, 2022 · N933EV · Cndair CL6002B19 · DoorsSDR SWIA202165839None · damagedCOMPLY WITH REO 601R-53-41-1116 REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS (C-CHECK RO 6/1/2022) COMPLIED WITH REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS REF REO 601R-53-41-1116 REV CDec 23, 2021 · N933EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202165838None · 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 WITHDec 23, 2021 · N933EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2021091561079Selector Valve · failedRECEIVED GEAR DISAGREE WARNING MESSAGE AFTER SELECTING GEAR DOWN FOR LANDING. RAN QRH, LANDING GEAR EXTENDED WITH MANUAL RELEASE. (FLIGHT 5325 - FILED CLOSED) TROUBLESHOT GEAR DISAGREE WARNING MESSAGE PER CRJ200 FIM 32-60-00. REMOVED AND REPLACED MLG SELSep 14, 2021 · N933EV · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA202159001Windshield · crackedTRANSFER FROM EAML 667907 : RIGHT WINDSHIELD CRACKED UPON PARKING AT GATE (FLIGHT 5076 - FILED CLOSED) REMOVED AND REPLACED RH WINDSHIELD IAW AMM 56-11-01 AND COMPLIED WITH TASK CARD 56-220-1000-SKY. OPS AND LEAK CHECK GOOD.Jun 25, 2021 · N933EV · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA201904195770Warning Message · false activationHIT SEVERE TURBULENCE. RECEIVED R/L ENG OIL WARNING MESSAGES AND AP PITCH TRIM, STAB TRIM, MACH TRIM CAUTION MESSAGES. (FLT#5975) PER AMM FOR SEVERE TURBULENCE EVENT PERFORMED FDR DOWNLOAD REFERENCE. DATA ANALYSIS SHOWED AN AIRCRAFT INSPECTION REQUIRED. COMPLApr 17, 2019 · N933EV · Cndair CL6002B19 · Central WarningSDR SWIA2019021445527Frame · corrodedFS 559.00 + 96 FRAME CORRODED ON FWD SIDE NEAR STR 27. (C-CHECK) RO: 02/12/2019 PERFORMED REPAIR AT FS559.00+96 FRAME IAW SRM. PERFORMED LEAK CHECK IAW AMM, NO LEAKS NOTED.Jan 21, 2019 · N933EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2019021445522Skin · corrodedLANDING AT LT WING PLANK CUTOUT FOR ACCESS PANEL 550HB HAS PITTING CORROSION. (C-CHECK) RO: 02/12/2019 COMPLIED WITH PERMANENT REPAIR LT WING PLANK CUTOUT FOR ACCESS PANEL 550HB IAW REO. ALL CHECKS OKAY.Jan 16, 2019 · N933EV · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2019021445526Door Sill · gougedCARGO DOOR LOWER SILL HAS SEVERAL GOUGES BETWEEN FS 574.00 AND FS 621.00. (C-CHECK) RO: 02/12/2019 REMOVED AND REPLACED CARGO SILL IAW SRM AND REO.Jan 15, 2019 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019021445525Panel · corrodedR/H PRESSURE FLOOR SILL PANEL HAS CORROSION AT MULTIPLE PLACES BETWEEN FS 409.00 + 128 AND FS 559.00. (C-CHECK) RO: 02/12/2019 REMOVED CORROSION ON MULTIPLE AREAS OF RT PRESSURE FLOOR SILL PANEL IAW SRM. COMPLIED WITH ALL STEPS IAW REO. PRESSURE CHECK GOOD.Jan 15, 2019 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019021445524Strap · corrodedRT FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN RBL 27.0 AND RBL 42.0 CORRODED. (C-CHECK) RO: 02/12/2019 REMOVED AND REPLACED FLOOR STRAP AT FS559 RBL27-42, REF SRM. ALL CHECKS OKAY.Jan 15, 2019 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019021445523Strap · corrodedLT FLOOR SUPPORT STRAP AT FS 559.00 BETWEEN LBL 27.0 AND LBL 42.0 CORRODED. (C-CHECK) RO: 02/12/2019 REMOVED AND REPLACED DAMAGED LT FLOOR SUPPORT STRAP P/N 601R31025-29 AT FS 559.00 BETWEEN LBL 27.0 AND LBL 42.0 IAW REO.Jan 15, 2019 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019021445521Frame · corrodedFS 605.00 FRAME CORRODED FWD SIDE BETWEEN STR 27 AND 21L.(C-CHECK) RO: 02/12/2019 REMOVED AND INSTALLED NEW FRAME SEGMENT AT FS 605 FROM STRINGER 20 L TO 20R IAW SRM AND REO.Jan 15, 2019 · N933EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2019021445520Bulkhead · chafedFORWARD FACE 621 BULKHEAD SEVERAL CHAFES ON Z ANGLE AT LBL 18 AND RBL 18, 27. (C-CHECK) RO: 02/12/2019 COMPLIED WITH PERMANENT REPAIR 621 Z ANGLE, IAW REO.Jan 14, 2019 · N933EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2019021445519Bulkhead · chafedFORWARD FACE 621 BULKHEAD HAS MULTIPLE CHAFES AT LBL 9 18 27 35 AND RBL 9 18 27 35. (C-CHECK) RO: 02/12/2019 COMPLIED WITH PERMANENT REPAIR 621 CHAFES IAW REO.Jan 14, 2019 · N933EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2019021445516Attach Fitting · chafedTHE FLOORBEAM ATTACHMENT TO THE REAR PRESSURE BULKHEAD FOR RBL 9.0 HAS A CHAFED SPOT ON ITS UPPER OUTBOARD FLANGE AT APPROX FS 619. (C-CHECK) RO: 02/12/2019 COMPLIED WITH REO.Jan 14, 2019 · N933EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2019021445515Skin · dentedDENT IN FUSELAGE SKIN BETWEEN STGR23L & STGR24L JUST FORWARD OF FRAME FS265.00. (C-CHECK) RO: 02/12/2019 COMPLIED WITH ALL STEPS OF REPAIR IAW REO.Jan 12, 2019 · N933EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2019021445518Support · corrodedSUPPORT ANGLE AT FS349 FOR WINDSCREEN SUPPORT STRUCTURE FOUND CORRODED. (C-CHECK) RO: 02/12/2019. REMOVED AND INSTALLED NEW ANGLE P/N 601R38783-13, IAW SRM.Jan 10, 2019 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019021445517Structure · corrodedFLOOR FRAME, FS349.00, AT THE SERVICE DOOR LOWER SILL IS CORRODED. (C-CHECK) RO: 02/12/2019 REPAIRED CORRODED FLOOR FRAME AT SERVICE DOOR, FS349.00 IAW REO.Jan 10, 2019 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018070944863Warning System · false activationRECEIVED A GEAR DISAGREE WARNING MESSAGE WHEN WE LOWERED GEAR AT 210 KNOTS WITH FLAPS UP. IT CLEARED ON ITS OWN WHILE THE GEAR WAS COMING DOWN. (FLT 5073) CLOSED PERFORMED A DETAILED INSPECTION OF THE LANDING GEAR HARNESSES. NO DEFECTS NOTED AT THIS TIME. PERJul 9, 2018 · N933EV · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA2018052944735Floorbeam · gougedTWO GOUGES ON THE FLOORBEAM AT LBL 27 AND BS 618 ON INBD AND OTBD FLANGES. PERFORMED A TEMPORARY REPAIR IAW REO.May 25, 2018 · N933EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201744111Strut · dischargedGEAR DISAGREE AFTER TAKE OFF. NLG DID NOT COME UP. SERVICED THE NOSE LANDING GEAR STRUT AND REPLACED THE SCHRADER VALVE IAW AMM.Dec 28, 2017 · N933EV · Cndair CL6002B19 · Nose/Tail Landing GearSDR SWIA201744039Angle · crackedLOWER ANGLE OF CARGO DOOR SUPPORT BEAM THAT ATTACHES TO REAR PRESSURE BULKHEAD IS CRACKED APPROX .500 LONG. (C-CHECK) REMOVED AND REPLACED ANGLE IAW SRM.Nov 14, 2017 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201744038Bulkhead · chafedREAR PRESSURE BULKHEAD WEB FWD FACE HAS 7 CHAFED AREAS .200 LONG BY .200 WIDE APPROX .003 DEEP WL105 AT LBL27.50, LBL18, I/B OF LBL9.50, I/B OF RBL9.50 RBL18, RBL27.50 & RBL36.20. (C-CHECK) REPAIRED DAMAGE IAW REO.Nov 14, 2017 · N933EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201701181076Lamp · burned outPAX CALL INDICATOR LIGHT ON CABIN OVERHEAD EXIT SIGN INOPERATIVE. REMOVED AND REPLACED THE EXIT SIGN INDICATION LIGHTS IAW AMM 33-51-14. OPS CHECKED GOOD.Jan 18, 2017 · N933EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2016050514796Skin · crackedPAX DOOR SKIN IS CRACKED BEHIND AFT COUNTER BALANCE PULLY MOUNT. COMPLIED WITH EC/TC REO 601R-52-11-702 AND MET ALL REQUIREMENTS OF REO 601R-52-11-702, REV C, MCO CLEARED. COMPLIED WITH ECTC REO 601R-52-11-702 AND NOT ALL THE REQUIREMENTS OF REO 601R-52-11-70May 5, 2016 · N933EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2016042114793Intercostal · crackedINTERCOSTAL AT STRINGER 15L AND BS 621-625 IS CRACKED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21, 51-42-22, AND DWG 601R-350121.Apr 21, 2016 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2016041314792Stiffener · crackedCRACK WAS DISCOVERED IN STIFFENER AT BS 185, RBL 13.7. WHEN DAMAGE SKIN PANEL WAS REMOVED. REMOVED 2 STIFFENER AT FS 185, RBL 13.7, I ORDERED NEW STIFFENER IAW SRM 51-42-06, SRM 51-42-21. DRILLED AND INSTALL NEW 2-STIFFNER AT FS 185, RBL 13.7 IAW SRM 51-42-Apr 13, 2016 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2016041314786Intercostal · crackedINTERCOSTAL CRACKED AT BS 623, STRINGER 15L, LBL51. INSTALLED A NEW INTERCOSTAL IAW SRM 51-42-21, 51-42-22, AND DWG 601R350121.Apr 13, 2016 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2016041314785Intercostal · crackedINTERCOSTAL CRACKED AT FS 623, STRINGER 14L, LBL 51. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-21 & 51-42-22.Apr 13, 2016 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2016041314784Angle · corrodedANGLE CRACKED AT BS 623, STRINGER 15R, RBL 51. R & R THE ANGLE IAW SRM 51-42-06.Apr 13, 2016 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2016041314783Angle · crackedANGLE CRACKED AT BS 625.30, STRINGER 14R, RBL 45. R & R THE ANGLE IAW SRM 51-42-06, AND DWG -601-35012.Apr 13, 2016 · N933EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2016041114782Seat Track · corrodedRT SIDE SEAT TRACK FROM BS 544-559+112 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.Apr 11, 2016 · N933EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2016041114781Seat Track · corrodedLEFT SIDE SEAT TRACK CORRODED FROM BS 544-559+112 CORRODED. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.Apr 11, 2016 · N933EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2016041114780Seat Track · corrodedRIGHT SIDE SEAT RAIL FROM FS 499-544 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.Apr 11, 2016 · N933EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2016041114779Seat Track · corrodedLEFT SIDE SEAT TRACK FROM BS 499-544 HAS CORROSION. R & R THE SEAT IAW AMM 53-01-11-000-802, 53-01-11-400-802.Apr 11, 2016 · N933EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2016041114778Seat Track · corrodedRT SIDE SEAT TRACK AT BS 449-499 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND 53-01-11-000-802.Apr 11, 2016 · N933EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2016041114777Seat Track · corrodedLEFT SIDE SEAT TRACK FROM BS 449-499 HAS CORROSION. R & R SEAT TRACK AT FS449-499 IAW AMM 53-01-11-000-802 AND 53-01-11-400-802. CApr 11, 2016 · N933EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2016041114776Seat Track · corrodedRIGHT SEAT TRACK FROM FS 559+112-574, RBL 18 HAS CORROSION. EVALUATED SEAT TRACK RT FLOOR FROM FS 559+112-574, RBL18 OUT OF LIMITS IAW SRM 53-61-49. REMOVED IAW SRM 53-00-49. INSTALLED NEW FABRICATED SEAT TRACK RT FLOOR FS 559+112-574, RBL18 IAW AMM 53-00-49Apr 11, 2016 · N933EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2016041114775Seat Track · corrodedRIGHT SEAT TRACK FROM 559+80-559+96, RBL 9 HAS CORROSION. COMPLIED WITH ECTC ROE 601R-53-00-485. FABRICATED SEAT RAILS IAW GREO 601R-53-00-485, REV A. REMOVED SEAT RAIL AT FS 559+80-559+96, RBL9 IAW AMM 53-01-11-000-802. INSTALLED NEW FABRICATED SEAT RAIL Apr 11, 2016 · N933EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
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