N741EV
Service difficulty reports · 325
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 = 'N741EV' 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 = 'N741EV' 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 SWIA202008252018Splice · corrodedA BAY - FS 280 LONGITUDINAL SPLICE CORRODED MULTIPLE PLACES FROM 26L TO 19R. REMOVED CORROSION FROM FS280 LOWER BUTTSTRAP AND FOUND REWORKED AREA TO BE ACCEPTABLE AS IS REF REO. PRESSURE LEAK CHECK GOOD.SDR SWIA202008252017Floorbeam · corroded* A BAY - FS 280 - FLOORBOARD BRKT ON 280 FACING AFT CORRODED @ MULTIPLE LOCATIONS AS MARKED (C-CHCECK 8/23/2020) / REPLACED A BAY - FS 280 - FLOORBOARD BRKT ON 280 FACING AFT REF CRJ700SRM.SDR SWIA202008252016Insulation · degradedFWD FUSELAGE - BELOW FLOOR - BETWEEN FS 280 & 265 - STGR 25R - POLYFAB BAG DEGRADED BEYOND USE AND CONTAMINATING ABAY - WASN'T ABLE TO REMOVE. REPLACED FWD FUSELAGE BELOW FLOOR BETWEEN FS280-265 STGR 25R INSULATION WITH NEW. IAW AMM.SDR SWIA202008252015Frame · corroded* FWD FUSELAGE - BELOW FLOOR - FS 250 FRAME CORRODED @ STGR 26R. REPAIRED DAMAGE REF REO.SDR SWIA20200252014Bushing · out of toleranceNLG APEX BUSHINGS OUT OF LIMITS. REPLACED WITH NEW NLG APEX BUSHINGS IAW CMM 32-21-06. MAXIMUM GAP 0.012", MEASURED GAP 0.005", GAP IS WITHIN LIMITSSDR SWIA202008252013Floor Support · corrodedR/H FLOOR SILL @ STR 17R FUS 985 - 1000 HAS CORRSOIN. REPAIRED CORRODED FLOOR SILL AT STR 17R FS 985-1000 AS PER CRJ 700 SRM.SDR SWIA202008252012Floorbeam · crackedLEFT FS274 CRACKED LEFT OF LBL9.00. REPAIRED CRACKED LEFT FLOORBEAM LBL9.00 AT FS280.00 TO FS265.00 REF CRJ700 SRM.COMPLIED WITH STRUCTURAL MAJOR REPAIR AND FORM M-337 ATTACHED.SDR SWIA202008252011Support · cracked*CRACK BETWEEN FRAME AND DIAPHRAGM AT FS909 BELOW WL97.50 ON WING-TO-BODY SUPPORT STRUCTURE. REPAIRED CRACK BETWEEN FRAME AND DIAPHRAGM AT FS909 BELOW WL97.50 REFERENCING REO.SDR SWIA202008252010Seat Track · corrodedLEFT HAND SIDE SEAT RAIL HAS CORROSION AND CORROSION ON FASTENERS AT MULTIPLE AREAS, FS785.00 - 854.00. REPLACED R/H SIDE SEAT RAIL BETWEEN F.S. 784.00 TO F.S. 861.00 REF. AMM. FABRICATED SEAT TRACK IAW SRM.SDR SWIA202008252009Seat Track · corrodedLEFT HAND SIDE SEAT RAIL HAS CORROSION AND DAMAGE AT MULTIPLE AREAS, FS869.00 961.00. REPLACED L/H SIDE SEAT TRACK BETWEEN F.S. 861.00 TO F.S. 961.00 IAW AMM. FABRICATED SEAT TRACK IAW SRM.SDR SWIA202008252008Seat Track · corrodedRIGHT HAND SIDE SEAT RAIL HAS CORROSION AND DAMAGE AT MULTIPLE AREAS, FS869.00 961.00. REPLACED R/H SIDE SEAT RAIL BETWEEN F.S. 861.00 TO F.S. 961.00 REF. CRJ 700 AMM. FABRICATED SEAT TRACK IAW SRM.SDR SWIA202008252007Seat Track · corrodedRIGHT HAND SIDE SEAT RAIL HAS CORROSION AT MULTIPLE AREAS, FS854.00 869.00. REPLACED R/H SIDE SEAT TRACK BETWEEN F.S. 855.00 TO F.S. 861.00 REF. CRJ 700 AMM. FABRICATED SEAT TRACK IAW SRM.SDR SWIA202008252006Seat Track · corrodedLEFT HAND SIDE SEAT RAIL HAS CORROSION ON MULTIPLE FASTENERS, FS573.00 669.00. REPLACED L/H SIDE SEAT RAIL BETWEEN F.S. 573.00 TO F.S.675.00 REF. CRJ 700 AMM. / FABRICATED NEW SEAT TRACK IAW SRM.SDR SWIA202008252005Seat Track · corrodedLEFT HAND SIDE SEAT RAIL HAS CORROSION AND CORROSION ON FASTENERS AT MULTIPLE AREAS, FS378.00 483.00. (MARKED) (C-CHECK 8/23/2020) / INSTALLED NEW SEAT RAIL ON L/H SIDE BETWEEN FS378.00 TO S483.00 REF CRJ700 AMM.SDR SWIA202008252004Seat Track · corrodedRIGHT HAND SIDE SEAT RAIL HAS CORROSION ON MULTIPLE FASTENERS, FS573.00 669.00. (MARKED) (C-CHECK 8/23/2020) INSTALLED NEW SEAT RAIL ON R/H SIDE BETWEEN FS573.00-FS669.00 / REF CRJ700 AMM.SDR SWIA202008252003Seat Track · corrodedRIGHT HAND SIDE SEAT RAIL HAS CORROSION AND DAMAGE AT MULTIPLE AREAS, FS483.00 FS573.00. REPLACED THE R/H SIDE SEAT RAIL BETWEEN F.S 483.00 TO F.S. 573.00 REF. CRJ 700 AMM. FABRICATED SEAT TRACK IAW SRM.SDR SWIA202008252002Seat Track · corrodedRIGHT HAND SIDE SEAT RAIL HAS CORROSION AND DAMAGE AT MULTIPLE AREAS, FS378.00 - 483.00. INSTALLED NEW SEAT RAIL ON R/H SIDE BETWEEN FS378.00-FS483.00 / REF CRJ700 AMM.SDR SWIA202008252001Seat Track · corrodedCORROSION MULTIPLE AREAS ON SEAT RAIL FS581.00 FS670.00, BL9R. (MARKED) (C-CHECK 8/23/2020) REMOVED CORROSION FROM RH FLOOR SEAT RAIL FS581 - FS670. FOUND REWORKED AREA OUT OF LIMITS. REPLACE SEAT RAIL REF CRJ-700 SRM.SDR SWIA202008252000Seat Track · corrodedCORROSION MULTIPLE AREAS ON SEAT RAIL FS581.00 FS670.00, BL9L. REPLACED SEAT TRACK BETWEEN F.S. 581.00 TO F.S. 677.00 AT LBL 9 REF. AMM. FABRICATED NEW SEAT TRACK FROM P/N 20276-288-0-0 IAW SRM.SDR SWIA2020082551999Seat Track · corrodedCORROSION MULTIPLE AREAS ON SEAT RAIL FS485.00 FS581.00, BL9R. INSTALLED NEW SEAT RAIL ON R/H SIDE RBL9.00 BETWEEN FS 485.00 - FS581.00 / REF CRJ700 AMM.SDR SWIA2020082551998Seat Track · corrodedCORROSION MULTIPLE AREAS ON SEAT RAIL FS349.00 FS485.00, BL9L. REPLACED SEAT TRACK BETWEEN F.S. 349.00 TO F.S.485.00 AT LBL 9 REF. CRJ 700 AMM. FABRICATED NEW SEAT TRACK FROM P/N 20276-228-0-0 PO#T55627 REF. CRJ 700 SRM.SDR SWIA2020082551997Seat Track · corrodedCORROSION MULTIPLE AREAS ON SEAT RAIL FS349.00 FS485.00, BL9R. (MARKED) (C-CHECK 8/23/2020) / REPLACED SEAT RAIL BETWEEN F.S. 374.00 TO F.S. 485.00 REF. CRJ 700 AMM. FABRICATED SEAT FROM P/N 20276-288-0-0 PO# T55037 REF. CRJ 700 SRM.SDR SWIA2020082551996Attach Angle · corrodedRIGHT WHEEL WELL - ATTACH ANGLE, ON THE RIGHT WING REAR SPAR, FOR TIRE BURST PANEL (642BZ) IS CORRODED. (MARKED) (C-CHECK 8/23/2020) / REMOVED CORROSION R/H WHEEL WELL ATTACH ANGLE ON THE RIGHT WING REAR SPAR FOR THE TIRE BURTS PANEL 642BZ FOUND TO BE WITHISDR SWIA2020082551995Attach Angle · corrodedLEFT WHEEL WELL - ATTACH ANGLE, ON THE LEFT WING REAR SPAR, FOR TIRE BURST PANEL (542BZ) IS CORRODED. REPLACED WITH NEW LH WHEEL WELL ATTACH ANGLE P/N CC670-10338-1 ON THE LEFT WING REAR SPAR FOR THE TIRE BURTS PANEL 542BZ REF SRM.SDR SWIA2020082551994Bracket · crackedAFT CARGO DOOR SURROUND STRUCTURE LOWER BRACKET IS CRACKED. FS1047. REPLACED AFT CARGO DOOR SURROUND BRACKET PN: MM670-35552-005 WITH NEW IAW SRM.SDR SWIA2020082551993Tube · corrodedPASSENGER STAIR WIRE HARNESS TUBE AT DOOR LOWER SILL HAS EVIDENCE OF CORROSION. REPLACED PAX DOOR HARNESS TUBE ASSY REF ESPM AND EM.SDR SWIA2020082551991Mount Bracket · corrodedCORROSION - BAGG DOOR - FWD UPPER ROLLER ASSY MOUNT BRACKET - LWR OTBD MOUNT BOLT CORRODED. REPLACED BOLT COMMON TO THE AFT BAGGAGE BAY FWD UPPER ROLLER ASSY MOUNT BRACKET. REF CRJ-700 SRM.SDR SWIA2020082551990Door Frame · corrodedPAX DOOR FRAME320 IS CORRODED, APPOX STGR 13. REPAIRED PASSENGER DOOR FRAME FS320.00. REF REO ALL STEPS COMPLIED WITHSDR SWIA2020082551989Floorbeam · corrodedCORROSION NOTED ON FS280 CROSSBEAM, RH SIDE. REMOVED AND REPLACED RH FS280.00 CROSSBEAM REF: SRM DRAWING AND WITH TASK CARD.SDR SWIA2020082551988Plate · corrodedLH OVERWING EMER EXIT STEP PLATE HAS CORROSION AROUND AFT SCREW ON TOP. REMOVED CORROSION ON LH OVERWING EMER EXIT STEP PLATE AS PER SRM. DAMAGE FOUND TO BE WITH IN ALLOWABLE LIMITS.SDR SWIA2020082551987Floor Support · corrodedCORROSION NOTED ON COCKPIT ENTRY FLOOR SUPPORT. REMOVED AND REPLACED COCKPIT FLOOR SUPPORT ANGLE SRM, AND DRAWING .SDR SWIA2020082551986Plate · corrodedRH OVERWING EMER EXIT STEP PLATE HAS CORROSION AROUND NUT CLIP HOLES AND ALONG INNER BOTTOM EDGE. REMOVED CORROSION ON RH OVERWING EMER EXIT STEP PLATE AS PER SRM. DAMAGE FOUND TO BE WITHIN LIMITSSDR SWIA2020082551985Skin · chafedRH ENGINE LOWER INNER CORE COWL INNER SKIN CHAFFED ON REPAIR. REMOVED AND FABRICATED NEW REPAIR DOUBLER PER CRJ 700 SRM, FABRICATED DOUBLER OUT OF AISI 321 CRES STAINLESS STEEL .010, LOCATED DRILLED AND INSTALLED WET WITH RED RTV -106 / AND RESTORED FINISH OSDR SWIA2020082551984Cascade · chafedRH ENGINE UPPER OUTB CASCADE IS CHAFED AT THE OUTBD ATTACH AREA. REPAIRED RH ENGINE UPPER OTBD CASCADE IS CHAFED AT THE OUTBD ATTACH AREA. REF REO.SDR SWIA2020082551983Rod End · corrodedL/H WING OUTBOARD AILERON PCU ROD END HAS EVIDENCE OF CORROSION. REPLACED WITH NEW L/H WING OUTBOARD AILERON PCU REF CRJ 700 AMM A02. OPS CHECK GOOD.SDR SWIA2020082551982Pcu · corrodedL/H WING INBOARD AILERON PCU ROD END HAS EVIDENCE OF CORROSION. REPLACED LH WING IB AILERON PCU REF CRJ 700 AMM. OPS CHECK GOOD.SDR SWIA2020082551981Actuator · corrodedL/H WING OUTBOARD FLAP, INBOARD HINGE ARM SPRING ACTUATOR IS CORRODED. (C-CHECK 8/23/2020) REMOVED CORRODED AND INSTALLED NEW LH WING OB FLAP IB HINGE ARM SPRING ACTUATOR REF CRJ700 AMM. / OPS TEST GOOD SEE CONTINUATION FOR WORK ACCOPLISHEDSDR SWIA2020082551980Skin · chafedTHE RH AILERON'S UPPER LEADING EDGE SHROUD IS CHAFED IN MULTIPLE AREAS. REMOVED AND REPLACED UPPER SKIN OF RH AILERON LEADING EDGE PN CC670-13052-4 ,DUE TO BEING OUT OF LIMITS PER SRM AND FASTENER INSTALLATION DRAWING CC670-13000SDR SWIA2020082551979Skin · damagedTHE LH WING OUTBOARD FLAP'S UPPER SKIN PANEL HAS 3 "SMOKING RIVETS" ALONG ITS TRAILING EDGE, NEAR THE INBOARD END. REMOVED DAMAGED FASTENERS PER SRM. REQUESTED ENGINEERING TO REWORK FATENER HOLES, REO. WAS RECEIVED , OPENED HOLES TO 5/32, INSTALLED FASTENESDR SWIA2020082551978Skin · dentedTHE RH FUSELAGE SKIN HAS 3 DENTS BETWEEN FS 409 AND FS 421 AND BETWEEN STR 16R AND STR 17R. REPAIRED RH FUSELAGE SKIN 3 EA. DENTS BETWEEN FS 409 AND FS 421 AND BETWEEN STR 16R AND STR 17R AS PER REO.SDR SWIA2020082551977Skin · dented* THE RH FUSELAGE SKIN HAS 1 DENT BETWEEN FS 394 AND FS 409 AND BETWEEN STR 16R AND STR 17R. (MARKED WITH BLACK GREASE PENCIL) (C-CHECK 8/23/2020)REPAIRED DENT ON RH FUSELAGE SKIN BETWEEN FS 394 AND 409 AND BETWEEN STR 16R AND 17R AS PER MHIRJ REO.SDR SWIA2020082551976Skin · dentedTHE RH FUSELAGE SKIN HAS 1 DENT BETWEEN FS 409 AND FS 421 AND BETWEEN STR 15R AND STR 16R. REPAIRED RH FUSELAGE SKIN DENT BETWEEN FS 409 AND FS 421 AND BETWEEN STR 15R AND STR 16R AS PER REO.SDR SWIA2020082551975Skin · dentedTHE RH FUSELAGE SKIN HAS 1 DENT BETWEEN FS 394 AND FS 409 AND BETWEEN STR 15R AND STR 16R. REPAIRED DENT AREA REF COMPLIED WITH REOSDR SWIA2020082551974Skin · dentedTHE RH FUSELAGE SKIN HAS 1 DENT BETWEEN FS 349 AND FS 364 AND BETWEEN STR 15R AND STR 16R. COMPLIED WITH REO DISPOSITION FOR DENT DAMAGE TO FUSELAGE SKIN BETWEEN FS 349-364AND STR 15R-16R.SDR SWIA20208251973Skin · dented* THE LH SIDE FUSELAGE SKIN PANEL BETWEEN FS 169 AND FS 173, JUST FWD OF THE TRU ACCESS DOOR, HAS 2 DENTS NEXT TO ONE ANOTHER. REPAIRED DENT LOCATED AT LH SIDE FUSELAGE SKIN PANEL FS 169-FS 173 JUST FWD OF THE TRU ACCESS DOOR. REF REO.SDR SWIA2020082551972Skin · dentedOVAL SHAPED DENT THAT IS 2 IN LONG BY 1 INCH WIDE LOCATED AT APPROX. FS 1162, STRINGER 23L. MAP EVALUATE AND REPAIR AS REQUIRED. IF FOUND WITHIN LIMITS, ELIMINATE DENT USING AIRCRAFT STANDARD PRACTICES/PROCEDURES. REPAIRED OVAL SHAPED DENT AT APPROX FS1162 SSDR SWIA2018010345394Intercostal · corrodedPASSENGER DOOR DD6 INTERCOSTAL BETWEEN FS323.363 AND FS338.963 HAS CORROSION. (C-CHECK) RO: 12/31/2018 REPLACED PAX DOOR INTERCOSTAL DD6 BTW FS323.363 - FS338.963 WITH NEW IAW SRM AND REO.SDR SWIA2018010345392Canister · crackedLT WING €“ SLAT TRACK CANISTER FOR SLAT TRACK 1-3 €“ WELDED BRACKET CRACKED. (C-CHECK) RO: 12/31/2018 REPAIRED LT WING SLAT TRACK CANISTER FOR SLAT TRACK 1-3 IAW REO.SDR SWIA2018010345393Retainer · crackedFWD CARGO DOOR SEAL RETAINER BENT AND CRACKED ON I/B FWD SIDE. (C-CHECK) RO: 12/31/2018 REMOVED AND REPLACED FWD CARGO DOOR I/B LOWER SEAL RETAINER WITH NEW SEAL RETAINER P/N LE670-39644-1 IAW SRM AND AMM.SDR ASOA201704111446Conduit · damagedRT ENGINE IDG POWER LEAD CONDUIT DAMAGED. COMPLIED WITH EC/TC REO 670-24-21-001 AND REO 670-24-21-001 FOR REPAIR OF RT ENGINE IDG CONDUIT.
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