N903EV

Service difficulty reports · 265

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 = 'N903EV' 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 SWIA2020040749998Support Strap · corroded* THE FLOOR SUPPORT STRAP FROM LH FLOOR SILL TO LBL27.00 HAS CORROSION AT FS559.00. (MARKED) (C-CHECK) RO 4/4/2020 REPLACED FLOOR SUPPORT STRAP AT LH FLOOR SILL TO LBL27.00 AT FS559 REF CRJ200 SRM. AND DWG. NO LEAKS. SEE ATTACHED TASK. SEE CONTINUE CARD FFeb 14, 2020 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020040749997Floor Support · corroded* THE FLOOR BEAM AT RBL9.00 FROM FS409.00+128 TO FS559.00 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK) RO 4/4/2020 REPAIRED FLOOR BEAM AT RBL9 FROM FS409+128 TO FS559 PER REO. COMPLETED SKYWEST TASK CARD.Feb 14, 2020 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020040749996Floor Support · corroded* THE FLOOR BEAM AT LBL27.00 FROM FS424.00 TO FS559.00 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK) RO 4/4/2020 REPAIRED THE FLOOR BEAM CORROSION AT LBL27.00 FROM FS424.00 TO FS559.00 REF REO. COMPLETED M-337Feb 14, 2020 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020040749995Rib · cracked* R/H BATT RIB CAP AT WS 48.30 IS CRACKED (C-CHECK) RO 4/4/2020 INSTALLED NEW R/H BATT RIB CAP AT WS 48.30 REF CRJ200 SRM, BOMBARDIER DWG AND BOMBARDIER DWG. COMPLETED SKYWEST TASK CARD.Feb 13, 2020 · N903EV · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA2020040749994Rib · cracked* R/H BATT RIB WEB AT WS 53.60 IS CRACKED (C-CHECK) RO 4/4/2020 REPLACED R/H BATT RIB WEB AT WS 53.60 REF CRJ200 SRM AND BOMBARDIER DWG. SEE ATTACHED TASK. NO LEAKS NOTED. SEE CONTINUE CARD FOR DETAILS.Feb 13, 2020 · N903EV · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA2020040749993Rib · cracked* L/H BATT RIB ANGLE AT WS 48.30 IS CRACKED (C-CHECK) RO 4/4/2020 REPLACED LH BATT RIB ANGLE AT WS 48.30. REF CRJ200SRM AND BOMBARDIER REO .BOMBARDIER DWG. COMPLETED SKYWEST TASK CARD.Feb 13, 2020 · N903EV · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA2020040750049Skin · dentedDENT DAMAGE WAS FOUND TO L/H FLIGHT SPOILER TOP SKIN SURFACE. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO 4/4/2020 L/H FLIGHT SPOILER DENTS OUT OF LIMITS REPLACED WFeb 12, 2020 · N903EV · Cndair CL6002B19 · SpoilersSDR SWIA2020040749992Fitting · crackedLEFT WINDSHIELD SIDE POST BOTTOM OUTBD CLIP CRACKED (C-CHECK) RO 4/4/2020 INSTALLED NEW LEFT WINDSHIELD SIDE POST BOTTOM OUTBOARD CLIP REF BOMBARDIER DWG AND CRJ-200 SRM, COMPLIED WITH SKYWEST TASK CARD, SEE CONTINUATION CARD FOR DETAILS,Feb 12, 2020 · N903EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020040749991Skin · dentedDENT FOUND BELOW CARGO DOOR 6.8" AFT OF F.S. 605.0 AND BETWEEN STGR 18L AND 19L. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO 4/4/2020 REPAIRED DENT PER REO. COMPLEFeb 12, 2020 · N903EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2020040750031Fastener · corrodedR/H FLIGHT SPOILER BONDING WIRE ATTACH HARDWARE HAS CORROSION (C-CHECK) RO 4/4/2020 REMOVED AND INSTALED NEW HARDWARE FOR R/H WING FLIGHT SPOILER INBOARD AND OUTBOARD BONDING WIRES REF CRJ200 SRM. PERFORMED ELECTRICAL BONDING TEST FOR R/H WING FLIGHT SPOILFeb 11, 2020 · N903EV · Cndair CL6002B19 · SpoilersSDR SWIA2020040750030Fastener · corrodedR/H INBD GROUND SPOILER PCU ATTACH LINK HARDWARE HAS CORROSION (C-CHECK) RO 4/4/2020 REMOVED AND REPLACED HARDWARE FOR R/H INBD GRND SPOLIER ATTACHING LINK WITH NEW HARDWARE P/N: NAS6205-12D, MS17826-5 (2EA), NAS6305419D REF CRJ-200 AMMFeb 11, 2020 · N903EV · Cndair CL6002B19 · SpoilersSDR SWIA2020040750029Fastener · corrodedR/H OUTBD GROUND SPOILER PCU ATTACH LINK HARDWARE HAS CORROSION (C-CHECK) RO 4/4/2020 REPLACED HARDWARE FOR RH OTBD GRND SPOILER PCU ATTACMENT LINK REF CRJ-200 AMM, OPS CHECK GOOD.Feb 11, 2020 · N903EV · Cndair CL6002B19 · SpoilersSDR SWIA2020040750028Fastener · corroded* L/H OUTBD GROUND SPOILER HAS CORROSION ON PCU LINK HARDWARE (C-CHECK) RO 4/4/2020 REMOVED AND REPLACED HARDWARE AT L/H OTBD GRND SPOILER PCU LINK REF CRJ-200 AMM ,OPS CHECK GOODFeb 11, 2020 · N903EV · Cndair CL6002B19 · SpoilersSDR SWIA2020040749990Bulkhead · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWLOF BOMBARDIER. (J)(2) MODIFYIFeb 4, 2020 · N903EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020040749989Angle · weakCOMPLY 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 4/4/2020 COMPLIED WITH REO REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS COMPLETED SKYWEST TASK CARD.Feb 4, 2020 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020040750027Bearing · corrodedREMOVE & REINSTALL RH AILERON TO PERFORM REPLACMENT OF AILERON BEARINGS, BUSHINGS, AND HARDWARE PER AMM. USE NEW BOLTS WHEN REINSTALLING AILERON IAW AMM. COMPLY WITH TASK CARD (C-CHECK) RO 4/4/2020 REMOVED AND INSTALLED RH AILERON REF AMM. OPS TEST GOOD, RDec 31, 2019 · N903EV · Cndair CL6002B19 · AileronsSDR SWIA2020040750026Bearing · corrodedREMOVE & REINSTALL LH AILERON TO PERFORM REPLACMENT OF AILERON BEARINGS, BUSHINGS, AND HARDWARE PER AMM. USE NEW BOLTS WHEN REINSTALLING AILERON IAW AMM. COMPLY WITH TASK CARD (C-CHECK) RO 4/4/2020 REMOVED AND INSTALLED LH AILERON REF AMM. OPS TEST GOOD, RDec 31, 2019 · N903EV · Cndair CL6002B19 · AileronsSDR ASOA2018092075212Cargo Track · corrodedAFT CARGO BAY SEAT RAIL BEAM AT LBL9 HAS CORROSION BETWEEN FS589.0 AND 605.0. REMOVED AND REPLACED BEAM IAW SRM 51-42-21, 51-42-22, AND EC/TC REO 601R-53-61-3780 REV A DATED 2011-07-15.Sep 17, 2018 · N903EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2018092075211Stringer · crackedSTRINGER 3L IS CRACKED AROSS FASTENERS AT FS 379. REPAIRED IAW SRM 53-00-03 AND SRM SUPPLEMENT 53-00-03.Sep 17, 2018 · N903EV · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR ASOA2018092055206Bulkhead · chafedEVALUATE OR REPAIR RT 9G LAVATORY BULKHEAD AFT SIDE DAMAGE AT INSERT/RIVNUT LOCATIONS. COMPLIED WITH EC/TC EO CL-600-2B19-53-L05832 REV 0 DATED 2018-09-13.Sep 15, 2018 · N903EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2018092055205Bulkhead · chafedEVALUATE OR REPAIR CENTER 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIVNUT LOCATIONS. COMPLIED WITH EC/TC EO CL-600-2B19-53-L05831 REV 0 DATED 2018-09-13.Sep 15, 2018 · N903EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2018092055204Bulkhead · chafed, EVALUATE OR REPAIR LT 9G BULKHEAD AFT SIDE DAMAGE AT INSERT/RIVNUT LOCATIONS. COMPLIED WITH EC/TC EO CL-600-2B19-53-L05830 REV 0 DATED 2018-09-13.Sep 15, 2018 · N903EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2018091355191Seat Track · corrodedTRACK SEGMENT BETWEEN FS 612 AND FS 617 CORRODED. REMOVED AND REPLACED SEGMENT IAW AMM 53-00-49-400-801.Sep 5, 2018 · N903EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2018091325190Intercostal · corrodedPAX DOOR INTERCOSTAL LOCATED 18" FROM HINGE BETWEEN FS 320 AND FS 338 (ABOVE OUTER HANDLE) IS CORRODED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21.Sep 4, 2018 · N903EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201809025198Door Sill · corrodedRT PRESSURE FLOOR SILL ANGLE CORRODED BETWEEN AT FS 513.00. REO 601R-53-41-2366 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666 REV C DATED 11/Sep 2, 2018 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201809025197Door Sill · corrodedLT PRESSURE FLOOR SILL ANGLES ARE CORRODED BETWEEN FS 513.00 TO FS 559.00. REO 601R-53-41-2367 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666 Sep 2, 2018 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201809025196Door Sill · corrodedLT PRESSURE FLOOR SILL ANGLES ARE CORRODED BETWEEN FS 473.15 TO FS 484.00. REO 601R-53-41-2367 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666 Sep 2, 2018 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201809025195Door Sill · corrodedLT PRESSURE FLOOR SILL ANGLES BETWEEN FS 424.00 AND FS 461.00 ARE CORRODED. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666 REV C DATED 11/06/2012 AS WRITTEN.Sep 2, 2018 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201809025193Door Sill · corrodedLT PRESSURE FLOOR SILL ANGLES ARE CORRODED BETWEEN FS 513.00 TO FS 559.00. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666 REV C DATED 11/06/2012 AS WRITTEN.Sep 2, 2018 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201809025192Door Sill · corrodedLT PRESSURE FLOOR SILL IS CORRODED AROUND NUTPLATE HOLES BETWEEN FS 424.00 AND FS 461.00. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666 REV C DATED 11/06/2012 AS WRITTEN.Sep 2, 2018 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2018091325186Door Sill · corrodedRT PRESSURE FLOOR SILL ANGLES ARE CORRODED BETWEEN FS 529.00 TO FS 544.00. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666 REV C DATED 11/06/2012 AS WRITTEN.Sep 2, 2018 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2018091025185Door Sill · corrodedRT PRESSURE FLOOR SILL IS CORRODED AROUND NUTPLATE HOLES FS 529.00 TO FS 544.00. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666 REV C DATED 11/06/2012 AS WRITTEN.Sep 2, 2018 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2018091025184Roll Pin · migratedPAX DOOR HINGE IS GOUGED ON FUSELAGE SIDE OF HINGE AFT LANDING FROM MIGRATED ROLL PIN. COMPLIED WITH EC/TC REO 601R-53-21-814 AS WRITTEN.Sep 2, 2018 · N903EV · Cndair CL6002B19 · Fuselage, Door HingeSDR ASOA2018090725183Stiffener · chafedPASSENGER DOOR PRESSURE VENT FLAP HAS TWO CHAFED STIFFENERS. REPAIR TO THE NICK/GOUGE ON THE VENT FLAP ON THE PAX DOOR IS COMPLETED IAW REO 601R-52-11-1040. THE REPAIR MEETS ALL REQUIREMENTS FOR REO 601R-52-11-1040.Sep 2, 2018 · N903EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2018090615182Skin · dentedDENT FUSELAGE LOWER SKIN BETWEEN FS409+16 AND FS409-32 AND STRINGER 21 LEFT TO STRINGER 22 LEFT. COMPLIED WITH TEMPORARY REPAIR PER REO 601R-53-31-906. REPAIRED DAMAGE IAW SRM 53-00-31 REPAIR 1.Aug 31, 2018 · N903EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2018080344875Door Sill · crackedCRACK ON DOOR SILL OF PAX DOOR. (100 FH INSPECTION 200) FO: 7/12/2018 CLOSED REPAIR COMPLETED IAW REO.Jul 10, 2018 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018071244875Door Sill · crackedCRACK ON DOOR SILL OF PAX DOOR. FO: 7/12/2018. WORK IN PROGRESS.Jul 10, 2018 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018011844141Unknown · failedGEAR DISAGREE IN FLIGHT. RETURN TO FIELD. FLT (5016). FO: 1/15/2018. CLOSED. REPLACED NLG.Jan 12, 2018 · N903EV · Cndair CL6002B19 · Nose/Tail Landing GearSDR SWIA2017080743613Proximity Sensor · failedGEAR DISAGREE EICAS MESSAGE WITH A RED NOSE GEAR INDICATION. REMOVED AND REPLACED THE NLG DOWNLOCK PROXIMITY SENSOR PS2GA IAW AMM. OPS CHECKED GOOD. PERFORMED TESTS OF MLG EXTENSION & RETRACTION SYSTEM IAW AMM. OPS CHECKED GOOD.Aug 6, 2017 · N903EV · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA2017041843215Wire Harness · failedGEAR DISAGREE FOR NOSE GEAR. DIVERTED. REMOVED AND REPLACED THE DOWNLOCK NR 2 SENSOR HARNESS IAW AMM. OPS CHECKED GOOD.Apr 18, 2017 · N903EV · Cndair CL6002B19 · Landing Gear System WiringSDR ASOA201611086152Frame · corrodedFRAME CORRODED AT BS 364 BETWEEN STRINGERS 26L AND 26R. REPAIRED THE FRAME IAW EC/TC EA 20-2016-324. AIRCRAFT APPROVED FOR RETURN TO SERVICE.Nov 8, 2016 · N903EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA201611086151Intercostal · corrodedINTERCOSTAL CORRODED FORWARD OF AVIONICS DOOR BETWEEN BS 349 AND 364, STRINGERS 27L AND 27R. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06. AIRCRAFT APPROVED FOR RETURN TO SERVICE.Nov 8, 2016 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201611086150Floorbeam · corrodedFLOORBEAM CORRODED AT BS 559+112, LBL 27. REPAIRED THE FLOORBEAM IAW EC/TC EO 600-53-0780. AIRCRAFT APPROVED FOR RETURN TO SERVICE.Nov 8, 2016 · N903EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201611086149Drag Angle · crackedPAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED THE DRAG ANGLE IAW EC/TC REO 601R-52-11-513. AIRCRAFT APPROVED FOR RETURN TO SERVICE.Nov 8, 2016 · N903EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA20161016112Drag Angle · crackedDURING C CHECK FOUND PAX DOOR AFT DRAG ANGLE CRACKED AT MOTOR ASSIST CABLE SUPPORT BRACKET. MTC REPAIRED CRACK IAW EC/TC REO 601R-52-11-513 AND REO 601R-52-11-513 REV B.Oct 16, 2016 · N903EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA20161004035Frame · corrodedDISCOVERED FRAME BS 364 CORRODED BETWEEN STRINGERS 26L AND 26R. REPAIRED IAW EA 20-2016-324 AND ECTC EA 20-2016-324. THIS IS CLASSIFIED AS A MAJOR REPAIR.Oct 4, 2016 · N903EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA20160930113Seat Track · corrodedDURING C CHECK FOUND SEAT TRACK CORRODED AT RBL9 FS364-394. MTC R & R SET TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802. C/W EC/TC REO 601R-53-00-485 AND RIL 4354.Sep 30, 2016 · N903EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA20160930111Door Sill · corrodedDURING C CHECK FOUND LT FLOOR SILL CORRODED AT FS559-559+32. MTC C/W EC/TC REO 601R-53-00-526 & GREO 601R-53-00-526.Sep 30, 2016 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA20160930110Seat Track · corrodedDURING C CHECK FOUND SEAT TRACK CORRODED AT LBL 9 BS 364-394. R & R SEAT TRACK IAW AMM 53-01-11-000-802 & 53-01-11-400-802.Sep 30, 2016 · N903EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA20161016087Drag Angle · crackedPAX DOOR DRAG AFT ANGLE CRACKED AT MOTOR ASSIST CABLE SUPPORT BRACKET. REPAIRED CRACKED PAX DOOR AFT DRAG ANGLE IAW ECTC REO 601R-52-11-513 AND REO 601R-52-11-513 REV B, TYPE II REPAIR. ALL DEFECTS CORRECTEDSep 30, 2016 · N903EV · Cndair CL6002B19 · Passenger/Crew Doors
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