N927EV

Service difficulty reports · 208

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 = 'N927EV' 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 ASOA201001787Shear Tie · corrodedFS 349 FRAME HAS CORROSION ON SHEAR TIE AT STR 27. REO 601R-53-21-1199, HAS BEEN ACCOMPLISHED. ACFT RETURNED TO SERVICE.Nov 15, 2010 · N927EV · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR ASOA201001817Sill · corrodedPAX DOOR CUTOUT LOWER FLOOR SILL IS CORRODED AT PROX SENSOR. RESOLVED ON W/O: 180442 TASKCARD: N/R-00546 . UPON FURTHER INVESTIGATION FOUND PAX DOOR LOWER SILL ANGLE TO BE CORRODED BEYOND LIMITS. LOWER SILL ANGLE REQUIRES REPLACEMENT. LOWER PAX DOOR SILL ANov 9, 2010 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001771Anchor Fitting · crackedPASSENGER DOOR AFT ANCHOR FITTING IS CRACKED. REPAIRED ANCHOR FITTING SIDE PASSENGER DOOR IAW AMM 52-11-17-000-804 AND 52-11-17-400-804.Nov 9, 2010 · N927EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001756Drag Angle · crackedPAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED CRACKED ANGLE, INSTALLED NEW ANGLE IAW SRM 51-42-06/-13/-15/-22. REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.Nov 9, 2010 · N927EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001755Seat Track · corrodedSEAT TRACK ANCHOR POINTS (3EA) AT FS 559+96-574 ARE CORRODED LBL 27. SEAT TRACK ANCHOR POINTS AT F.S. 559+96-574 REPLACED IAW SRM 51-41-04.Nov 9, 2010 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001754Seat Track · corrodedSEAT TRACK AT FS 559+80-559+96 LBL 27 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-41-02. REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.Nov 9, 2010 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001753Seat Track · corrodedSEAT TRACK AT FS 559+86-559+96 LBL 9 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-41-02. J REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.Nov 9, 2010 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001752Seat Track · corrodedSEAT TRACK AT FS 559+112-568, LBL 9 HAS CORROSION. REMOVED DAMAGED SEAT TRACK, LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE SEAT TRACK IAW SRM 51-41-02. REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.Nov 9, 2010 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001751Seat Track · corroded(2 EA) SEAT TRACK ANCHOR POINTS AT FS 574-605 LBL 9 HAS CORROSION. SEAT TRACK REPLACED IAW SRM 51-41-04.Nov 9, 2010 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001750Seat Track · corrodedSEAT TRACK AT FS 612-617 LBL 9 HAS CORROSION. SEAT TRACK REPLACED IAW SRM 51-41-04.Nov 9, 2010 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001749Seat Track · corrodedSEAT TRACK AT FS 559+86-559+96, RBL 9 HAS CORROSION. SEAT TRACK REPLACED IAW SRM 51-41-04.Nov 9, 2010 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001748Seat Track · corrodedSEAT TRACK AT FS 559+112-574, RBL 9 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-41-02. REPAIR IS CLASSIFIED AS A MINOR REPAIR IAW SOP 5702.Nov 9, 2010 · N927EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001747Stringer · corrodedFRAME FS 333.00 SECTOR AT STRINGER 27 IS CORRODED. REMOVED FRAME IAW SRM 51-42-06. INSTALLED FRAME IAW SRM 51-42-06.Nov 9, 2010 · N927EV · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR ASOA201001746Intercostal · damagedFS 484, RBL 27 AND RBL 36 INERCOSTAL REPAIR CLIPS ARE CRACKED FROM UPEPR FASTENER TO EDGE OF PART. REPAIR TO THE INTERCOSTAL COMPLETED IAW REO 601R-53-41-059 AND MEETS ALL THEIR REQUIREMENTSNov 9, 2010 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001745Rib · crackedRT BATT RIB IS CRACKED AT TOP FASTENER. COMPLIED WITH EC/TC REO 601R-57-51-046 REPAIR NR 2.Nov 9, 2010 · N927EV · Cndair CL6002B19 · Wing, Rib/BulkheadSDR ASOA201001744Rib · crackedLT BATT RIB IS CRACKED AT TOP FASTENER. COMPLIED WITH REO 601R-57-51-046 REPAIR NO.2 STEPS 1, 2, 3 AND 4. COMPLIED WITH REO 601R-57-51-046 REPAIR NR 2 STEPS 5-10.Nov 9, 2010 · N927EV · Cndair CL6002B19 · Wing, Rib/BulkheadSDR ASOA201001743Floorbeam · corrodedLBL 27, FLOORBEAM CAP IS CORRODED AROUND NUTPLATES AT FS 605.00. BLENDED CORROSION ON FLOORBEAM & FOUND TO BE OUT OF LIMITS IAW SRM 53-61-43, 53-00-00 FIG 101. REMOVED FLOORBEAM CAP IAW SRM 51-42-06, 51-42-21. LOCATED AND DRILLED FLOORBEAM CAP IAW REO 601R-Nov 9, 2010 · N927EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001742Placard · wornCREW ESCAPE HATCH SILKSCREENS AND PLACARDS ARE WORN. APPLIED NEW SILKSCREENS ON CREW ESCAPE HATCH IAW MM 11-10-03-400-801.Nov 9, 2010 · N927EV · Cndair CL6002B19 · Placards and MarkingsSDR ASOA201001729Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROX .2" IN LENGTH 60 PERCENT FSH LOCATED AT TOP OF AFT CARGO DOOR TRACK FAILED NDT INSP. COMPLIED WITH EC/TC REO 601R-53-61-1541 AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-1541Nov 5, 2010 · N927EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201001728Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .1" IN LENGTH 50 PERCENT FSH FAILED NDT INSP. REPAIRED PER EC/TC REO 601R-53-61-1230 AND REPAIR C/W REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230 REV D.Nov 5, 2010 · N927EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201001724Bulkhead Web · crackedFOUND FS 559 RT BULKHEAD WEB HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT WL 59-10 INBD OF RBL 18.0, FAILED NDT INSP. REPAIRED PRESSURE BULKHEAD WEB AND CAP ANGLES7 IAW REO 601R-53-41-260, REV E.Nov 4, 2010 · N927EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201001477Battery Pack · inoperativeRIGHT EXIT EMERGENCY EXIT INDENTIFICATION SIGN INOP. R & R NR 4 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04. OPS CHECK GOOD.Sep 29, 2010 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201001349Anchor Fitting · crackedAFT ANCHOR FITTING CRACKED. C/W INSP IAW REO 601R52-11-1846 NO FUTHER CRACK PROPAGATION NOTED AT THIS TIME ACFT OK FOR SERVICE. (CLOSED]Sep 15, 2010 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001043Light · inoperativeRT EMERGENCY FLOOR LEVEL EXIT LIGHT INOPERATIVE. R & R RT EMERGENCY FLOOR LEVEL EXIT PANEL IAW AMM 33-51-10. OPS CHECK GOOD NO DEFECTS AT THIS TIME.Jul 26, 2010 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201001028Lamp · burned outRT NR 2 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED RT NR 2 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. RELAMPED RT NR 2 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21 OPS CHECK GOOD.Jul 22, 2010 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201001013Light · inoperativeRIGHT FWD EMERGENCY LIGHT INOP. R & R RT FWD EMERGENCY LIGHT IAW AMM 33-51-21.Jul 16, 2010 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201000993Door · bindingF/A REPORTS PASSENGER DOOR HARD TO OPEN. INSPECTED PAX DOOR AND OPS CHECKS IAW AMM 52-11-00. NO DEFECTS NOTED. OK FOR SERVICE. (CLOSED)Jul 8, 2010 · N927EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201000499Lamp · burned outAFT CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED AFT CEILING EMERGENCY FLOOD LIGHT LAMP IAW AMM 33-51-16. OPS CK GOOD. RELAMPED AFT CEILING EMERGENCY FLOOD LIGHT LAMP IAW AMM 33-51-16. OPS CHK GOOD.Apr 7, 2010 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA200901375Light · inoperativeNR 2 CEILING EMERGENCY LIGHT INOP.Dec 10, 2009 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA200901113Bulkhead · crackedFOUND CRACK AT PARKING BRAKE CABLE AT FS 202.75 AT BL 23.71 PRESSURE BULKHEAD. WORK COMPLETED IAW EC/TC REO 601R 53-11-1785.Oct 8, 2009 · N927EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA200900838Sign · inoperativeEMERGENCY EXIT SIGN AT PASSENGER BOARDING DOOR INOP.Aug 1, 2009 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA200900496Unknown · unknownGOT A FUEL IMBALANCE IN FLIGHT. RAN QRH GOT FUEL BALANCED AFTER EXTENDED AMOUNT OF TIME. ON LANDING STILL HAD 200 LBS ON THE HEAVY SIDE. EMERGENCY DECLARED, ENROUTE TO ATL, ACFT DIVERTED TO CHA DUE TO MTC, FLT 5474 DEL 114 MINS.Apr 24, 2009 · N927EV · Cndair CL6002B19 · Aircraft Fuel SystemSDR ASOA200801539Web · crackedPAX DOOR FWD WEB HAS CRACKS IN RADIUS WHERE STAIRS 832DT AND CT MEET, 832CT AND MIC FIXED STEPS MEET. REPAIRED PAX DOOR FWD WEB IAW REO 601R-52-11-702.Nov 19, 2008 · N927EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA200801540Web · crackedPAX DOOR AFT WEB IS CRACKED IN STEP JOINT RADIUS (832DT AND 832CT) AND (832CT AND FIX MID STEP).Nov 19, 2008 · N927EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA200801505Isolator · brokenFS 621.00 REAR PRESSURE BULKHEAD FWD FACE HAS TWO ISOLATORS BROKEN. REPLACED ISOLATORS AT FS 621.00 REAR PRESSURE BULKHEAD FWD FACE IAW SRM 51-42-10.Nov 13, 2008 · N927EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA200801503Fitting · crackedFS 280 RBL 9 I/B CLIP CRACKED. REMOVED AND REPLACED FS 280 RBL 9 INBOARD CLIP IAW SRM 51-42-21.Nov 13, 2008 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200801502Fitting · crackedFS 280 LBL 9 I/B STRINGER CLIP CRACKED. REMOVED INBOARD STRINGER CLIP IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE STRINGER CLIP IAW SRM 51-42-21.Nov 13, 2008 · N927EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA200801501Fitting · crackedFS 280 LBL 9 O/B CLIP CRACKED. THIS SDR WILL REMAIN OPEN PENDING MTC DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION.Nov 13, 2008 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200801500Angle · crackedLEFT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED .1 INCH LONG AT LBL 27. REPLACED ANGLE AT LT FS 484 LBL 27 IAW REO 601R-53-411-059, STEPS 8-11 AND 14. COMPLIED WITH ASA EC/TC REO 601R-53-41-059.Nov 13, 2008 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200801499Fitting · crackedFS 280 LBL 9 O/B CLIP CRACKED. REPLACED O/B CLIP FS 280, RBL 9 IAW CRJ 200 SRM 51-40-11 AND SRM 51-42-21.Nov 13, 2008 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA200801498Angle · crackedCARGO DOOR BEAM AFT BOTTOM ANGLE AT THE REAR PRESSURE BULKHEAD IS CRACKED .5 INCH LONG IN O/B RADIUS. REMOVED CRACKED BRACKET FROM CARGO DOOR BEAM/AFT BULKHEAD. LOCATED, DRILLED & INSTALLED NEW SERVICEABLE BRACKET. ALL WORK PERFORMED IAW SRM 51-42-21.Nov 13, 2008 · N927EV · Cndair CL6002B19 · Cargo/Baggage DoorsSDR ASOA200801487Cover · out of positionEMERGENCY LIGHT COVER BY PAX DOOR FELL OFF, KNOCKED OFF DURING DEPLANING.Nov 9, 2008 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA200801411Step · crackedASD BOTTOM STEP IS CRACKED.Oct 28, 2008 · N927EV · Cndair CL6002B19 · Entrance StairsSDR TRAX200800949Coalescer Bag · dirtyFUEL SMELL IN FLIGHT. SUSPECT BOTH LT AND RT PACK SOCKS. SMELL MOST INTENSE WHEN INCREASE OUTFLOW TEMP TO MAINTAIN CABIN TEMP. REPLACED BOTH COALESCER SOCKS PER CRJ 200 AMM 21-51-13. OPS CHECK GOOD. (S)Jul 31, 2008 · N927EV · Cndair CL6002B19 · Humidity Control SystemSDR TRAX200800684Dcu · malfunctionedON APP INTO ATL FUEL TOTALIZER WENT TO -0- RIGHT MFD PANEL SHOWED NO FUEL IN LEFT TANK AND THE AUTO INHIBIT INDICATOR CAME ON. RIGHT TANK READ 1920 LBS. ALL INDICATIONS RETURNED TO NORMAL ON LANDING. FLT 4801 DEL 42 MINS. REMOVED AND REPLACED DCU 1 AND DCUMay 23, 2008 · N927EV · Cndair CL6002B19 · Central ComputersSDR TRAX200800116Flap System · failedFLAP FAIL AT ZERO ON APPROACH, EMERGENCY DECLARED. FLTS 4291, 4907 CX AND ON 1/22/08 FLT 4450 CX.Jan 20, 2008 · N927EV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR TRAX200701104Handle · crackedPAX DOOR OUTER HANDLE CRACKED.Aug 3, 2007 · N927EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR TRAX200701103Step · crackedPAX DOOR BOTTOM STEP CRACKED.Aug 3, 2007 · N927EV · Cndair CL6002B19 · Entrance StairsSDR TRAX200600994Angle · crackedRIGHT FS 625.00 OBLIQUE ANGLE CRACKED. REPAIRED IAW ALL SRMS. (CLOSED)Nov 6, 2006 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200600993Angle · crackedLEFT FS 625.00 OBLIQUE ANGLE CRACKED. REMOVED CRACKED OBLIQUE ANGLE IAW CRJ 200 SRM 51-42-06. APPLIED TOPCOAT TO SERVICEABLE OBLIQUE ANGLE P/N 601-35012-51 IAW CRJ 200 SRM 51-42-21. INSTALLED OBLIQUE ANGLE WITH LOCK FASTENERS HST10AG5-5, PO 9147-1 AND HST10ANov 6, 2006 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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