N758EV

Service difficulty reports · 295

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 = 'N758EV' 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 SWIA202055593Seat Track · corrodedRT SIDE SEAT TRACK FS 573-663 HAS CORROSION, AS MARKED. C-CHECK RO 1/17/2021. REMOVED AND REPLACED RT SIDE SEAT TRACK FS 573.00-FS 663.00, PER CRJ700 AMM 53-00-49-400-801-A17.Nov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202055592Seat Track · corrodedRT SIDE SEAT TRACK FS 378-483 HAS CORROSION, AS MARKED. C-CHECK RO 1/17/2021. INSTALLED NEW RT SIDE SEAT TRACK FS 378-483, REF CRJ700 AMM 53-00-49-400-801. CONFIG A17.Nov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202055591Seat Track · corrodedLT SIDE SEAT TRACK FS 483-573 HAS CORROSION, AS MARKED. C-CHECK RO 1/17/2021. LT SIDE SEAT TRACK FS 483 TO FS 573 IS OUT OF LIMITS, REF CRJ 700 SRM 53-31-49-101-001-A01. REMOVED AND INSTALLED NEW SEAT TRACK LT FS 483-573, REF CRJ700 AMM 53-00-49-400-801-A1Nov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202055590Seat Track · corrodedLT SIDE SEAT TRACK FS 378-483 HAS CORROSION, AS MARKED. C-CHECK RO 1/17/2021. REMOVED AND INSTALLED FABRICATED SEAT SIDE TRACK LT FS 378-FS 483, REF CRJ700 AMM 53-00-49-400-801-A17.Nov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202055589Mount · corrodedFWD INBOARD ENTRANCE STORAGE MOUNT ON THE FLOOR STRUCTURE HAS CORROSION AROUND AND IN THE BOLT HOLE, MARKED. C-CHECK RO 1/17/2021. REMOVED AND REPLACED THE 100% CORRODED FWD INBOARD ENTRANCE STORAGE MOUNT, REF CRJ700 SRM 51-42-21-001-001-A01. RESTORED FINISNov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SWIA202055588Attach Angle · corrodedRIGHT SIDE FLOOR SILL ATTACH ANGLE AT THE FS 319 FRAME HAS CORROSION, MARKED. C-CHECK RO 1/17/2021. REMOVED AND INSTALLED NEW RIGHT SIDE FLOOR SILL ATTACH ANGLE AT THE FS 319 FRAME, REF CRJ 700 SRM 51-42-06-001-001-A01 & CRJ 700 SRM 51-42-21-001-001-A01.Nov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SWIA202055587Fitting · corrodedPAX DOOR SURROUND STRUCTURE, THE FORWARD CLOSING FITTING IS CORRODED, MARKED. C-CHECK RO 1/17/2021. BLENDED CORROSION ON THE PAX DOOR FWD CLOSING FITTING "OUT OF LIMITS", REF CRJ700 SRM 51-21-06-001-001-A01, SRM 53-21-23-101-001-A01. ORIGINAL: .080, REMAININov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202055586Angle · corrodedPAX DOOR SURROUND STRUCTURE, MIDDLE CAP ANGLE IS CORRODED, MARKED. C-CHECK RO 1/17/2021. PAX DOOR SURROUND STRUCTURE, MIDDLE CAP ANGLE CORROSION IS EXFOLIATED THROUGH PART THICKNESS, 100% MATERIAL LOSS. REMOVED AND REPLACED CAP ANGLE WITH NEW PART PER CRJ70Nov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202055585Support Angle · corrodedAVIONICS COMPARTMENT CRAWLWAY SUPPORT ANGLE AT FS 280 HAS CORROSION, MARKED. C-CHECK RO 1/17/2021. REMOVED CORROSION FROM AVIONICS COMPARTMENT CRAWLWAY SUPPORT ANGLE AT FS 280 REF CRJ 700 SRM 51-21-06-001-001-A01. ORIGINAL MATERIAL THICKNESS .050" MATERIAL Nov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202055557Floorbeam · corrodedCABIN, FS 549 FLOOR CROSS BEAM BETWEEN RBL 9 AND RBL 27 CORRODED, AS MARKED. C-CHECK RO 1/17/2021. COMPLIED WITH ALL STEPS OF REO 670-53-31-579 REV - DATED 2020-12-03 FOR CORROSION ON FLOOR CROSS BEAM AT FS 549 BETWEEN RBL 9 AND RBL 27.Nov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA202055556Seat Track · corrodedCABIN RBL 9 SEATRAIL AT FS 565 CORRODED AT NUTPLATE, AS MARKED. C-CHECK RO 1/17/2021. REMOVED CORROSION ON RBL 9.0 FS 476.0 TO FS 571.0, REF CRJ 700 SRM 51-21-06-001-001-A01, OUT OF LIMITS. REPAIRED THE FLOOR BEAM BETWEEN FS 476.0 TO FS 571.0 RBL 9.0, REF CNov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202055555Floor Support · corrodedCABIN RT FLOOR SILL FS 517/533 DECOMPRESSION PANEL AND HARDWARE CORRODED. C-CHECK RO 1/17/2021. REMOVED AND REPLACED RT FLOOR SILL FS 517/533 DECOMPRESSION PANEL AND HARDWARE, IAW CRJ 700 AMM 21-35-01-000-801-A01 AND 21-35-01-400-801-A01.Nov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202055554Door Sill · corrodedAFT BAGGAGE BAY DOOR SILL HAS AREAS OF CORROSION, FRETTING, A DENT, AND SOME GOUGES, MARKED. C-CHECK RO 1/17/2021. BLENDED DAMAGE ON THE AFT BAGGAGE BAY DOOR SILL "OUT OF LIMITS", REF CRJ700 SRM 51-21-06-001-001-A01, SRM 53-61-23-001-001-A01. REMOVED AND RENov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202055553Floor Support · corrodedRIGHT SIDE FLOOR SILL BETWEEN FS 280 AND FS 319 HAS CORROSION, SCRATCHES, AND A CRACK, MARKED. C-CHECK RO 1/17/2021. REMOVED CORROSION ON THE RT FLOOR SILL FS 280-FS 319, "OUT OF LIMITS." REMOVED AND REPLACED THE RT FLOOR SILL BETWEEN FS 280-FS 319, REF DRANov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202055552Stringer · corrodedSTRINGER, STGR 21R, HAS CORROSION BETWEEN APPROXIMATELY FS 349 TO FS 364, MARKED. C-CHECK RO 1/17/2021. INSTALLED 1 EA STGR CLEAT ONTO STGR 21R AT FS 364.00, REF CRJ700 SRM 51-42-06-001-001 A01, CRJ700 SRM 51-42-21-001-001-A01 AND DWG SH670-31350 REV A. SEENov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202055551Stringer · corrodedSTRINGER, STGR 19R, HAS CORROSION BETWEEN APPROXIMATELY FS 364 TO FS 374, MARKED. C-CHECK RO 1/17/2021. REMOVED CORROSION ON STR 19R FS 364-FS 374 "OUT OF LIMITS" REF CRJ700 SRM 53-21-03-101-007-A01. REMOVED AND REPLACED THE STRINGER AT 19R FS 364-FS 374, RNov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202055550Stringer · corrodedSTRINGER, STGR 20R, HAS CORROSION BETWEEN APPROXIMATELY FS 364 TO FS 394 AND FS 421 TO FS 437, MARKED. C-CHECK RO 1/17/2021. REMOVED CORROSION ON STRINGER 20R FS 364 - 394 "OUT OF LIMITS", REF CRJ700 SRM 51-21-06-001-001-A01, SRM 51-21-03-101-007-A01. REMOVNov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202055549Door Frame · corrodedPAX DOOR SURROUND STRUCTURE, BACK-UP SILL AT STGR 21L IS CORRODED BETWEEN FS 310 TO FS 333. C-CHECK RO 1/17/2021. REMOVED AND REPLACED CORRODED BACK UP SILL WITH NEW PART (P/N SH670-31822-1) ON STGR 21L BETWEEN FS 310.00 AND FS 333.00 USING ALL NEW FASTENERSNov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202055548Stringer · corrodedSTRINGER, STGR 19L, IS CORRODED BETWEEN FS 319 TO FS 349, MARKED. C-CHECK RO 1/17/2021. REMOVED CORRODED STRINGER 19L BETWEEN FS 310.00 AND 349.00, REF CRJ700 SRM 51-42-06-001-001 A01 AND 51-42-21-001-001 A01. INSTALLED NEW STRINGER (P/N SH670-31936-1) AT 1Nov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202055547Angle · corrodedPAX DOOR SURROUND STRUCTURE, LOWER KICKPLATE ANGLE IS CORRODED AROUND THE NUTPLATE ON THE INBOARD SIDE, MARKED. C-CHECK RO 1/17/2021. FOUND PAX DOOR SURROUND KICKPLATE TO BE 100% EXFOLIATED "OUT OF LIMITS." REMOVED AND REPLACED THE PAX DOOR SURROUND STRUCTUNov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202055546Stringer · corrodedSTRINGER, STGR 27, IS CORRODED BETWEEN FS 310 TO FS 319, MARKED. C-CHECK RO 1/17/2021. BLENDED CORROSION ON STRINGER 27 AT FS 310-FS 319 "OUT OF LIMITS", REF CRJ700 SRM 53-21-03-101-002-A01. REMOVED AND REPLACED THE STRINGER 27 AT FS 310 - FS 319, REF DRAWINov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202055545Stringer · corrodedSTRINGER, STGR 26R, IS CORRODED BETWEEN FS 295 TO FS 319, MARKED. C-CHECK RO 1/17/2021 BLENDED CORROSION ON STRINGER AT 26R FS 295-FS 319 "OUT OF LIMITS", REF CRJ700 STM 53-21-03-101-002-A01, SRM 51-21-06-001-001-A01. REMOVED AND REPLACED STRINGER 26R AT FNov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202055544Intercostal · corrodedINTERCOSTAL STGR 20R BETWEEN FS 319 TO FS 333 IS CORRODED, MARKED. C-CHECK RO 1/17/2021. REMOVED AND INSTALLED NEW INTERCOSTAL P/N SH670-32004-3, REF CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01 AND DRAWING SH670-31950 REV Y. COMPLIEDNov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202055543Doubler · corrodedTCAS OMNIDIRECTIONAL ANTENNA DOUBLER IS CORRODED AROUND THE CONNECTOR PENETRATION, LOCATED AT STGR 27, BETWEEN FS 295 TO FS 310. C-CHECK RO 1/17/2021. REMOVED CORROSION FROM THE TCAS ANTENNA DOUBLER "OUT OF LIMITS". REMOVED AND REPLACED THE TCAS ANTENNA AT Nov 21, 2020 · N758EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA202055542Support · crackedLEFT SIDE FUSELAGE BODY FAIRING SUPPORT STRUCTURE JUST AFT OF FS 909.0 STRAP HAS CRACK. C-CHECK RO 1/17/2021. REPAIRED THE LT SIDE FUSELAGE BODY SUPPORT FAIRING STRUCTURE AFT OF FS909 BY CUTTING AWAY DAMAGED AREA AND INSTALLING A REPAIR DOUBLER REF REO 670-5Nov 21, 2020 · N758EV · Cndair CL6002C10 · Aerodynamic FairingsSDR SWIA202055541Floorbeam · corrodedCOCKPIT AFT FLOOR SUPPORT ANGLE ON FWD SIDE OF 280 BEAM LBL 9-RBL 9 IS CORRODED. C-CHECK RO 1/17/2021. BLENDED CORROSION ON THE COCKPIT AFT FLOOR SUPPORT "OUT OF LIMITS", REF CRJ700 SRM 53-00-00-101-001-A01, SRM 51-21-06-001-001-A01 ORIGINAL: .063; REMAININGNov 20, 2020 · N758EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA202055621Track · brokenAFT CARGO DOOR, AFT TRACK UPPER STOP IS BROKEN. C-CHECK RO 1/17/2021. REMOVED AFT CARGO DOOR, AFT TRACK UPPER STOP, REF CRJ 700 AMM 52-31-23-000-801 (A01) AND INSTALLED WITH NEW FROM STOCK, REF CRJ 700 AMM 52-31-23-400-801 (A01).Nov 16, 2020 · N758EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWIA202055584Shaft · corrodedFORWARD CARGO DOOR OUTER HANDLE SHAFT HARDWARE IS CORRODED. C-CHECK RO 1/17/2021. CLEANED FWD CARGO DOOR OUTER HANDLE SHAFT HARDWARE. FOUND NO CORROSION PRESENT, REF CRJ700 SRM 51-26-00-001-001-A01. REPLACED ONE STRIPPED NUT, REF CRJ700 SRM 51-41-02-001-00Nov 16, 2020 · N758EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWIA202055540Screw · brokenSCREW SHANK STUCKED ON RT WING PANEL 684FB. C-CHECK RO 1/17/2021. REMOVED SCREW SHANK AND COMPLIED WITH NECESSARY REPAIRS, IAW REO 670-57-52-477 REV- DATED 2020-12-17. SEE CONTINUATION CARD FOR DETAILS.Nov 14, 2020 · N758EV · Cndair CL6002C10 · Wing, Plate/SkinSDR SWIA202055539Bracket · broken1 EACH BRACKET BROKEN ON PANEL 433BB. C-CHECK RO 1/17/2021. REMOVED AND REPLACED 1 EACH BRACKET BROKEN ON PANEL 433BB, IAW CRJ 700 SRM 51-42-06-001-001-A01.Nov 11, 2020 · N758EV · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202055538Skin · damagedFS 1031.00-FS 1051.00 STRG 23-24RT EXTERIOR SKIN PITTING DAMAGE, MARKED. C-CHECK RO 1/17/2021. REPAIRED AREA ON FUSELAGE SKIN BETWEEN FS 1031.00 TO FS 1051.00 BETWEEN STRINGER 23R TO STRINGER 24R TO COMPLY WITH REO 670-53-61-1778 REV- DATE 2020-12-02. SEE CNov 10, 2020 · N758EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA202055537Panel · erodedLEADING EDGE OF PANEL 341BR ERODED ENTIRE LENGTH. C-CHECK RO 1/17/2021. BLENDED LEADING EDGE PANEL 341BR, IAW CRJ700 SRM 51-12-00-001-001-A01 AND REO 670-55-12-175 REV -- DATE 2020-12-01.Nov 10, 2020 · N758EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA202055536Panel · erodedLEADING EDGE OF PANEL 331BL ERODED ENTIRE LENGTH. C-CHECK RO 1/17/2021. BLENDED LEADING EDGE PANEL 331BL, IAW CRJ700 SRM 51-12-00-001-001-A01 AND REO 670-55-12-175 REV DATE 2020-12-01.Nov 10, 2020 · N758EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA202055535Bearing · damagedROUTE LT AILERON TO BACK SHOP TO REMOVE AND REPLACE SWEDGED BEARINGS AND BUSHINGS AT HINGE POINTS (INBOARD, MID, OUTBOARD) ON LT AILERON, PER AMM. C-CHECK RO 1/17/2021. REMOVED AND REPLACED WORN BUSHINGS AND BEARINGS, REF CRJ 700 AMM 20-31-00-400-804-A01 FORNov 3, 2020 · N758EV · Cndair CL6002C10 · AileronsSDR SWIA2019030145586Bolt · brokenBROKEN TIE BOLTS. (INSP)MSO M2397945 SN DEC10-2409, 2 BOLTS. LAST SHOP VISIT FAT M2382446 TIRE CHANGE, 3RD CYCLE ON BOLTS SINCE OVERHAUL. MS21250-08034 BOLTS USED ON THE WHEELS.Mar 1, 2019 · N758EV · Cndair CL6002C10 · Wheel/Ski/FloatSDR SWIA2018092445093Not Reported · dentedDENT AFT OF FS 409.00 BETWEEN STR 16L AND 15L. (C-CHECK) RO: 09/21/2018. REPAIRED DENT AFT OF FS 409.00 BETWWEN STR 16L AND 15L IAW SRM.Aug 10, 2018 · N758EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2018092445094Frame · crackedFOUND LT FS220 FRAME HAS CRACK INDICATION FROM FASTENER HOLE TOWARDS LIGHTNING HOLE APPROX 1/8" LONG. (C-CHECK) RO: 09/21/2018. REMOVED AND INSTALLED NEW SERVICEABLE FRAME AT LT FS220 IAW SRM.Jul 24, 2018 · N758EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201711043316Stringer · corrodedSTRINGER 26R CORRODED BETWEEN BS 333 AND 349. MAINTENANCE REPLACED THE STRINGER.Nov 4, 2017 · N758EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201711033314Stringer · corrodedSTRINGER 25R HAS CORROSION BETWEEN BS 280 - 295 AND 295 - 310. REMOVED AND REPLACED THE STRINGER AND SPLICE IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-42-06-001-001-A01, AND DRAWING SH670-31630.Nov 3, 2017 · N758EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201711033315Tie Down · corrodedONE CARGO TRACK PAD CORRODED. REMOVED AND REPLACED THE CARGO TRACK PAD IAW SRM 51-42-21-001-001-A01.Nov 2, 2017 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201710283313Angle · corrodedPASSENGER DOOR OPENING UPPER MID CAP ANGLE BETWEEN FS 310-349 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED ANGLEOct 28, 2017 · N758EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201710283312Seat Track · corrodedFLOOR SEAT RAIL SEGMENT LBL9 FS581-677 HAS CORROSION. MAINTENANCE REPLACED FLOOR SEAT RAIL SEGMENT LBL9 FS581-677.Oct 28, 2017 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201710283311Seat Track · corrodedFLOOR SEAT RAIL SEGMENT RBL9 FS847-969 HAS CORROSION. MAINTENANCE REPLACED FLOOR SEAT RAIL SEGMENT AT RBL9 FS847-969.Oct 28, 2017 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201710283310Spline · corrodedSPLICE ANGLE AT FS939 ON AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE IS CORRODED. MAINTENANCE REMOVED AND INSTALLED SERVICEABLE SPLICE ANGLE.Oct 28, 2017 · N758EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201710273309Seat Track · corrodedLEFT SIDEWALL SEAT RAIL SEGMENT FS565-677 HAS CORROSION. MAINTENANCE REPLACED LEFT SIDEWALL SEAT RAIL SEGMENT AT FS565-677.Oct 27, 2017 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201710273308Seat Track · corrodedSEAT TRACK LBL 9, BS 379 - 581 CORRODED. MAINTENANCE REPLACED THE SEAT TRACK.Oct 27, 2017 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201710273306Seat Track · corrodedSEAT TRACK BS 830 - 969 HAS CORROSION. MAINTENANCE REPLACED THE SEAT TRACK.Oct 27, 2017 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201710273305Drag Angle · crackedLEFT VERTICAL AFT DRAG ANGLE CRACKED, FORWARD END. MAINTENANCE REPLACED THE AFT DRAG ANGLE.Oct 27, 2017 · N758EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201710273304Structure · corrodedLBL 9 PACKER CORRODED AT BS 533. MAINTENANCE REPLACED THE PACKER.Oct 27, 2017 · N758EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201710273303Seat Track · corrodedSEAT TRACK CORRODED AT RBL 9, BS 349 - 485. MAINTENANCE REPLACED THE SEAT TRACK.Oct 27, 2017 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
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