N901EV

Service difficulty reports · 167

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 = 'N901EV' 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 ASOA2014042910419Skin · crackedLOWER WING PLANK AT RT BOOST PUMP LANDING FOR PANEL 610CB HAS MULTIPLE INDICATIONS. NOTED ON HORIZONTAL AND VERTICAL SURFACES GREATER THAN 50 PERCENT FSH AROUND ENTIRE CIRCUMERENCE. FAILED NDT INSP. COMPLIED WITH EA 26-2014-038. PERFORMED ROTO PEEN IAW SRM 5Mar 29, 2014 · N901EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014042910418Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE IS CRACKED NEAR DOOR ASSIST PULLEY. REPAIRED IAW REO 601R-52-11-513 & EC/TC 601R-52-11-513 WITH PN 601R31772-5, MATERIAL.Mar 29, 2014 · N901EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2013121809659Windshield · failedDURING APPROACH, CAPTAIN`S SIDE WINDSCREEN BEGAN BURNING. SELECTED LT WINDSHIELD HEAT OFF BURNING STOPPED. R & R WINDSHIELD IAW AMM 56-11-01.Dec 9, 2013 · N901EV · Cndair CL6002B19 · Flight Compartment WindowsSDR ASOA2013110809373Lamp · burned outNR 1 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-21, OPS CHECKED GOOD.Nov 4, 2013 · N901EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2013102509247Lamp · inoperativeCABIN AFT MOST CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP. OPS CHECKED GOOD IAW AMM 33-51-00.Oct 23, 2013 · N901EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2013072408770Lens · brokenEMERGENCY EXIT LIGHT COVER AT MAIN CABIN DOOR BROKEN. RESECURED EMERGENCY LIGHT COVER AT CABIN DOOR IAW AMM 33-51-10. NO FURTHER DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE.Jul 22, 2013 · N901EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2012110902458Engine · malfunctionedLOST ABOUT 5 PERCENT POWER IN LT ENGINE EVERY FEW SECONDS ON CLIMBOUT. ACFT RETURNED TO DEPARTURE AFTER T/O. EMERGENCY DECLARED AS A PRECAUTION. PERFORMED ACCELERATION CHECK ON LT ENGINE, OPS CHECKED GOOD IAW AMM 71-00-00-710-802. ACFT OK FOR SERVICE.Nov 8, 2012 · N901EV · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA2012070901877Floor Support · corrodedSEVERAL AREAS OF CORROSION ALONG RT CARGO FLOOR SUPPORT FROM FS 559+80 TO 559+112 AROUND FASTENER HOLES. FOUND DAMAGE DEPTH TO BE APPROX 0.30 WHICH EXCEEDS 10 PERCENT OF LOCAL THICKNESS OF 0.063. REMOVED FLOOR SUPPORT IAW SRM 51-42-06. FABRICATED A NEW FLOJun 28, 2012 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012070201847Seat Track · corrodedFOUND THE RT FLOOR SILL TO HAVE ONE AREA OF CORROSION AT 559+30 TO 559+84 .4" X 1" X .015" DEEP. FOUND DAMAGE BEYOND REPAIRABLE LIMITS. REPAIRED IAW REO 601R-53-51-194.Jun 28, 2012 · N901EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012062901842Stiffener · crackedFS 409+128 BULKHEAD VERTICAL POST AT LBL 27 INBD SIDE IS CRACKED IN RADIUS ON BOTTOM EDGE OF POST. COMPLIED WITH STEPS 1 AND 2 OF REO 601R-53-41-056. STEPS 3-17 OF REO 601R-53-41-056, REQUIRE COMPLIANCE. COMPLIED WITH STEP 3 OF REO 601R-53-41-056, REV F. PEJun 19, 2012 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012062501821Post · crackedBULKHEAD VERTICAL POST AT LBL 18 OTBD SIDE IS CRACKED IN RADIUS ON BOTTOM EDGE OF POST. REMOVED AIR FILTER FOR ACCESS IAW AMM 21-24-01-000-801. INSTALLED AIR FILTER IAW AMM 21-24-01-400-801. REMOVED AIR FILTER HSG BY REMOVING BOLTS, 8 EA FROM SUPPORT STRUCTJun 19, 2012 · N901EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2012070901876Frame · corrodedFRAME AT FS 364.00 IS HEAVILY CORRODED. REMOVED FS 364.00 FRAME IAW SRM 51-42-06 AND 51-42-21. DRILLED UP NEW FRAME IAW SRM 51-40-11. INSTALLED NEW FRAME IAW SRM 51-42-06 & 51-41-21.Jun 18, 2012 · N901EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2012070901875Angle · corrodedCORROSION ON SERVICE DOOR LOWER SILL ANGLE FWD EDGE. REMOVED SERVICE DOOR LOWER SILL ANGLE, FOUND TO BE OUT OF LIMITS IAW SRM 51-42-06 & 51-42-21, 53-00-00. S DRILLED, LOCATED AND INSTALLED NEW SILL ANGLE, IAW SRM 51-40-11.Jun 18, 2012 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012070201849Frame · corrodedFRAME AT FS 33.00 HEAVILY CORRODED. REMOVED AND REPLACED FRAME SECTION IAW SRM 51-42-06 & 51-42-21.Jun 18, 2012 · N901EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2012070201848Post · corrodedFS 349 BULKHEAD POST HEAVILY CORRODED. REMOVED AND REPLACED POST IAW SRM 51-42-21 & 51-42-06.Jun 18, 2012 · N901EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2012062901841Floor Support · corrodedCORROSION ON FLOOR SUPPORT, RBL27 FROM FS 559+112 TO FS 621.0. REMOVED FLOOR SUPPORT IAW SRM 51-41-02. LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-11.Jun 18, 2012 · N901EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012062901839Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT RBL 9 FROM FS 310.00 TO FS 333.00. REMOVED CORROSION ON FLOOR SUPPORT, FOUND TO BE WITHIN LIMITS IAW REO 601R-53-00-005. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-06 & REO 601R38778. STEP 2 OF REO 601R-53-00-005.Jun 18, 2012 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012062901838Angle · corrodedCORROSION ON PAX DOOR LOWER SEAL ANGLE UPPER HALF AFT EDGE AND LOWER SEAL ANGLE AROUND FASTENER HOLES. PAX DOOR SILL CORROSION BEYOND LIMITS IAW SRM 51-21-06. REMOVED & LOCATED NEW PAX DOOR SILL PLATE IAW SRM 51-40-16.Jun 18, 2012 · N901EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012062701828Angle · corrodedSERVICE DOOR ANGLE AT FS 319 IS CORRODED. R & R SVC DOOR ANGLE WITH A NEW SERVICEABLE ANGLE IAW SRM 51-42-06 AND 51-41-02 .Jun 18, 2012 · N901EV · Cndair CL6002B19 · Service DoorsSDR ASOA2012062501820Seat Track · corrodedSEAT TRACK AFT OF FS 559, RBL 9 CORRODED IN AND AROUND SCREW HOLES. R & R DAMAGED FLOOR SEAT TRACK FROM FS 559+4 TO 559+88, RBL 9 IAW MM TASKS 53-01-11-000-802 AND 53-01-11-400-802. (SDR CLOSED)Jun 18, 2012 · N901EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012062501819Seat Track · corrodedSEAT TRACK AT LBL 9 JUST AFT OF 559 CORRODED IN AND AROUND SCREW HOLE. R & R DAMAGED FLOOR SEAT TRACK FROM FS 559+4 TO 559+88, LBL 9, IAW MM TASKS 53-01-11-000-802 AND 53-01-11-400-802. (SDR CLOSED)Jun 18, 2012 · N901EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012062001815Seat Track · corrodedCORROSION ON CARGO SEAT TRACK AT FS 559+80 AT RBL9. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-61-49-01. REMOVED AND INSTALLED CORRODED SEAT TRACK IAW 52-41-02-00 SRM .Jun 18, 2012 · N901EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012062001814Seat Track · corrodedCORROSION ON SEAT TRACK FROM FS 364 TO 409. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.Jun 18, 2012 · N901EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012070601863Angle · crackedVERTICAL ANGLE ON LT SIDE OF NLG WHEEL WELL INTERNAL BOX STRUCTURE BETWEEN FS 202.75 AND 235.00 IS CRACKED AT THE TOP BETWEEN (2) RIVETS. DAMAGE IS APPROX 1 INCH LONG. REMOVED CRACKED ANGLE IAW SRM 51-42-06 & 51-42-21. DRILLED NEW SERVICEABLE ANGLE IAW SRM 5Jun 15, 2012 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012061801805Angle · crackedRT FS 621-625 OBLIQUE ANGLE IS CRACKED. REMOVED CRACKED RT FS 621-625 OBLIQUE ANGLE AND REPLACED WITH NEW PARTS IAW SRM 51-40-11 AND 51-42-21.Jun 15, 2012 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012062901837Web · crackedPASSENGER DOOR AFT STAIR WEB CRACKED AT 3RD STEP FROM TOP JUST INBD OF GAS STRUT SUPPORT BRACKET. INSTALLED GAS STRUT SUPPORT BRACKET ASSY ONTO AFT WEB ASSY ONTO PAX DOOR IAW SRM 51-42-06. REMOVED HANDRAIL STOP CUP FROM AFT WEB TO GAIN ACCESS FOR REPAIR. INJun 14, 2012 · N901EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012062501825Attach Fitting · crackedCLIP CRACKED AT FS 280.00, RBL 9. R & R CLIP AT FS 280.00, RBL 9 IAW SRM 5J1-42-21.Jun 14, 2012 · N901EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2012062501818Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE CRACKED APPROX 2" LONG, JUST ABOVE PWR ASSIST PULLEY BRACKET. REMOVED PAX DOOR AFT DRAG ANGLE, LOCATED AND DRILLED UP NEW ANGLE PN 601R31772-5S AND INSTALLED IAW SRM 51-42-06 AND SRM 51-40-11. THIS REPAIR REQUIRES MAJOR/MINOR CLAJun 14, 2012 · N901EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012061801804Angle · crackedANGLE CRACKED AT FS 280.00, RBL 9. R & R ANGLE AT FS 280.00, RBL 9 IAW IAW SRM 5J1-42-21. TJun 14, 2012 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2012070601862Glowstrip · missingRT AFT PHOTOLUMINESCENT AISLE PATH MARKER IS MISSING THE CHEVRON MARKER. INSTALLED NEW SERVICEABLE CHEVRON MARKER IAW AMM 33-51-01-400-806. (SDR CLOSED)Jun 11, 2012 · N901EV · Cndair CL6002B19 · Emergency EquipmentSDR ASOA201200902Flashlight · inoperativeF/O FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM 25-61-04.Mar 15, 2012 · N901EV · Cndair CL6002B19 · Emergency EquipmentSDR ASOA201200321Lamp · burned outNR 4 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.Jan 25, 2012 · N901EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201101690Lens · missingDURING POST FLIGHT, FOUND COVER TO FWD RT WING EMERGENCY LIGHT MISSING. REPLACED RT SIDE OVER WING FWD EMERGENCY LIGHT LENS COVER IAW AMM 33-51-21.Sep 9, 2011 · N901EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201101689Lamp · burned outFWD RT WING EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-21. OPS CHECKED GOOD.Sep 9, 2011 · N901EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201101373Sign · crackedF/A TRIPPED INTO GALLEY SERVICE DOOR, KNOCKING OFF EXIT SIGN. SIGN FELL AND CRACKED, WILL NOT STAY IN PLACE. (LIGHT LENS/ COVERS (INCLUDING EMERGENCY LIGHT) (INCLUDING EMERGENCY LIGHT) ) R & R EMER EXIT SIGN LENS COVER, CHECKS GOODS. AMM 33-51-13. DEFEJul 24, 2011 · N901EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201101372Lens · brokenEXIT SIGN BROKEN. R & R EMERGENCY EXIT SIGN LENS COVER, CHECKS GOODS. AMM 33-51-13. DEFER CLEARED, MX NOTIFIED.Jul 24, 2011 · N901EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201101065Battery Pack · failedNR1 & NR2 EXTERIOR AND NR1 INTERIOR CEILING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04, OP'S CHECK GOOD. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04, OP'S CHECK GOOD.May 26, 2011 · N901EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201100625Fire Bottle · inoperativeCARGO BRL LO MSG INFLIGHT. (NOTE THIS IS THE 2ND TIME THIS ACFT HAS HAD THIS DISCREPENCY IN 2 DAYS) QRH COMPLIED WITH, LANDED AT NEAREST SUITABLE AIPORT. (ENROUTE, ACFT DIVERTED, DUE TO MX -- EMERGENCY DECLARED) REMOVED BOTH CARGO BOTTLES AND INSTALLED SERVIMar 21, 2011 · N901EV · Cndair CL6002B19 · Extinguishing SystemSDR ASOA201001985Control Unit · failedREPEAT WRITE-UP ENROTE FO'S PFD , MFD FLIGHT DIRECTOR, NAV2 AUTOPILOT WERE ALL LOST AND WENT BLANK MULTIPLE TIMES ALSO, CAPTAINS FLIGHT DIRECTOR WAS LOST DC TIE 1 CLOSED AT ONE POINT. NOTICED A DC BUS 2 MSG ALSO, BUT IT EXTINGUISHED ITSELF (ENROUTE, ACFT DIVEDec 16, 2010 · N901EV · Cndair CL6002B19 · Central DisplaySDR ASOA201001046Cover · missingGALLEY SERVICE DOOR FLOOR EMERGENCY EXIT SIGN LIGHT COVER MISSING. (RESOLVED ON W/O: 168315/ TASKCARD: N/R-00004) REPLACED GALLEY SERVICE DOOR FLOOR EMERGENCY FLOOD LIGHT COVER IAW CMM 33-21-58. REPLACED GALLEY SERVICE DOOR FLOOR EMERGENCY FLOOD LIGHT COVER IJul 28, 2010 · N901EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201000260Lamp · inoperativeLT NR 1 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.Feb 15, 2010 · N901EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201000259Light · inoperativeNR 4 CEILING EMERGENCY FLOOD LIGHT INOP.Feb 15, 2010 · N901EV · Cndair CL6002B19 · Emergency LightingSDR ASOA200901465Floor Support · corrodedCARGO FLOOR SUPPORT AT LBL 45 HAS CORROSION FS 574 TO FS 621 AND SEVERAL GOUGES AT FS 589 LARGEST .700"L X .300"W X .018" DEEP APPROX.Dec 28, 2009 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200901464Floor Support · corrodedFLOORBEAM CAP HAS CORROSION AROUND NUTPLATE HOLES FS 589 TO FS 621 LBL 27.Dec 28, 2009 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200901444Wire · looseWIRE PULLED OUT OF EMERGENCY EXIT LIGHT ELECTRICAL CONNECTOR ON WARDROBE.Dec 21, 2009 · N901EV · Cndair CL6002B19 · Light System WiringSDR ASOA200901421Intercostal · crackedINTERCOSTAL AT RBL 18 CRACKED IN RADIUS ON LWR AFT FLANGE AT FS 640 BETWEEN WL 119.12 AND WL 111.09.Dec 15, 2009 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200901438Skin · crackedINDICATIONS NOTED AT LWR WING PLANK ACCESS HOLE, 640DB AT INBD ON PAINTED AREA OF HOLE APPROX 50 PERCENT FULLSCREEN HEIGHT ARE MARKED ON WING. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G.Dec 10, 2009 · N901EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA200901373Post · crackedFOUND FS 409.0+128 VERTICAL POST BL 0.0 LT SIDE HAS INDICATION NOTED AT WL 69 AFT FLANGE RADIUS APPROX .2" IN LENGTH 605 FSH FAILED NDT INSP. REMOVED POST ASSY IAW SRM 51-42-06 AND 51-42-21. POST ASSY INSTALLED AND NEW STIFFNERS IAW REO 601R-53-41-1125 COMDec 9, 2009 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200901372Post · crackedFOUND FS 409.0+128 VERTICAL POST RBL 18 OTBD SIDE HAS INDICATION NOTED AT WL 69.0 AFT FLANGE RADIUS APPROX .2" IN LENGTH 60 PERCENT FSH FAILED NDT INSP. REMOVED POST IAW SRM 51-42-06. LOCATED AND ASSEMBLED NEW SERVICEABLE OTBD STIFFNEER IAW SRM 51-40-11 & 5Dec 9, 2009 · N901EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200901371Bulkhead · crackedFOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .3" IN LENGTH 80 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETED AND THE REPAIR C/W THE REQUIREMENTS OF ECDec 9, 2009 · N901EV · Cndair CL6002B19 · Fuselage Main, Bulkhead
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