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 ASOA2015081113616Angle · crackedIN FLIGHT COMPARTMENT THE PILOT'S SIDE WINDSHIELD POST THE LOWER OTBD ANGLE FITTING IS CRACKED. REMOVED CRACKED WINDSHIELD FITTING ON THE LOWER AFT SIDE OF PILOTS SIDE WINDSHIELD POST IAW SRM 51-42-21. DRILLED, LOCATED AND INSTALLED NEW SERVICEABLE WINDSHIELAug 11, 2015 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015081113615Angle · crackedFS 280 LOWER "J" ANGLE IS CRACKED AT RBL 9. COMPLIED WITH EC/TC REO 601R-53-11-171 AND MET ALL THE REQUIREMENTS OF REO 601R-53-11-171.Aug 11, 2015 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015081113614Angle · crackedFS 280 LOWER "J" ANGLE IS CRACKED AT LBL 9. COMPLIED WITH EC/TC REO 601R-53-11-171 AND MET ALL THE REQUIREMENTS OF REO 601R-53-11-171.B.Aug 11, 2015 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015081113610Floorbeam · crackedFS 280, RBL 9 INBD AND OUTBD ANGLES ARE CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-21.Aug 11, 2015 · N927EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015081013613Stiffener · gougedINTERNAL PASSENGER DOOR, PRESSURE RELIEF DOOR INNER STIFFENER IS GOUGED APPROXIMATELY .100 LONG, .100 WIDE AND .020 DEEP. COMPLIED WITH REO 601R-52-11-1040, REV ISSUE 2006/10/30. REPAIR TO THE NICK, 1 GOUGE DAMAGE ON THE VENT FLAP ON THE PAX DOOR IS COMPLETEAug 10, 2015 · N927EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2015081013612Bulkhead · chafedBS 621 PRESSURE BULKHEAD HAS 5 SCREW CHAFES AT LBL 18, 27, RBL 18, 27, 36, WL 103. REMOVED CHAFED MARKS BY BLENDED MATERIAL OFF 0.006". DETERMINED WITHIN LIMIT IAW REO 601R-53-61-2155, STEP 1 TO 5, REV A 2013-08-13. COMPLIED WITH EC/TC, REO 601R-53-61-2155 Aug 10, 2015 · N927EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015081013609Angle · corrodedSERVICE DOOR LOWER SILL UPPER ANGLE HAS PITTED CORROSION. REMOVED UNSERVICEABLE DOOR SILL ASSY IAW SRM 51-42-06, 51-42-21, 51-42-13. INSTALLED DOOR SILL ASSEMBLY WHICH INCLUDES ANGLE 601R38303-105, ITEM 3 AND ANGLE 601R38303-253, ITEM 4 IAW SRM 51-42-06, 51-4Aug 10, 2015 · N927EV · Cndair CL6002B19 · Service DoorsSDR ASOA2015081013608Attach Bracket · corrodedATTACH BRACKET FOR SERVICE DOOR AFT DRAIN CORRODED. R & R THE ATTACH BRACKET IAW SRM 51-41-02.Aug 10, 2015 · N927EV · Cndair CL6002B19 · Service DoorsSDR ASOA2015081013607Stringer · crackedBS 379, STR 3L HAS A CRACK. CUT THE DAMAGED SECTION OF STRINGER. LOCATE AND DRILLED EXTRUSION S6807, NEW SERVICEABLE EXTRUSION. ALL WORK WAS DONE IAW SRM TR 53-51. FABRICATED SPLICES FROM S6957-17 AND S6957-18 IAW SRM TR 53-51. COMPLIED WITH SRM 53-00-03, Aug 10, 2015 · N927EV · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR ASOA2015081013606Angle · crackedBS 280, STR 3L, UPPER ANGLE IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06, AND 51-42-21.Aug 10, 2015 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015081013605Isolator · brokenBS 621 PRESSURE BULKHEAD HAS TWO BROKEN ISOLATORS. REMOVED AND REPLACED THE ISOLATOR IAW SRM 51-42-06, AND SRM 51-42-06.Aug 10, 2015 · N927EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015081013604Angle · crackedFS 484, ANGLE AT LBL 36 IS CRACKED. REMOVED AND REPLACED THE ANGLE6 IAW SRM 51-42-21, AND REO 601R-53-41-1940, REV.Aug 10, 2015 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015081013603Angle · crackedBS 484, ANGLE AT LBL 27 IS CRACKED. R & R THE ANGLE IAW SRM 51-42-21 & 51-40-11.Aug 10, 2015 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015081013600Angle · crackedFS 484, ANGLE AT RBL 36 IS CRACKED AT PREVIOUS REPAIR. REMOVED ANGLE AT FS 484.0, RBL 36 IAW SRM 51-42-21. FABRICATED, DRILLED, LOCATED AND INSTALLED ANGLE, PN 601R-53-41-1940-2 IAW REO 601R-53-41-1940, REV-- DATED 2015/08/13, GREO 601R-53-41-059, REV B DATEAug 10, 2015 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015081013599Angle · crackedBS 484, ANGLE AT RBL 27 IS CRACKED. R & R ANGLE IAW RM 51-42-21 & 51-40-11.Aug 10, 2015 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015080913611Angle · crackedNLG CUTOUT AFT LT CORNER IS CRACKED APPROXIMATELY .5"L. C/W ECTC REO 601R-53-11-0048 IAW REO 601R-53-11-0048, REV C1.Aug 9, 2015 · N927EV · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA2015080913598Frame · corrodedFS 349, FRAME IS CORRODED AT STR 27. REMOVED LT AND RT FRAME STRAP IAW SRM 51-42-06. REINSTALLED LT AND RT FRAME STRAP GUSSETS AT FS 349 IAW SRM 51-42-06. REMOVED LT AND RT VERTICAL POST ATTACHED TO TRANSVERSE BEAM AND FS 349.00 IAW SRM 51-42-21. REINSTALLED Aug 9, 2015 · N927EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015080913597Skin · corrodedLOWER FUSELAGE SKIN BS 559+80 - 559+112, STRINGER 26L - 26R CORRODED. FOUND OUT OF LIMITS IAW SRM 53-00-31. BLENDED DAMAGE IAW SRM 51-21-06. PERFORMED ULTRASONIC THICKNESS OF SKIN IAW NDTM 51-20-04. FOUND WITHIN LIMITS IAW EA 26-2015-100.Aug 9, 2015 · N927EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2014122911985Skin · damagedMULTIPLE GOUGES AND DENTS ON FUSELAGE AND REPAIR DOUBLERS FROM BS 589 TO FS 605, BETWEEN STR 21R AND STR 27. BLENDED MULTIPLE GOUGES AND DENTS ON FUSELAGE AND REPAIR DOUBLERS FROM FS 589 TO FS 605, BETWEEN STR 21R AND STR 27 IAW SRM 51-12-00. R & R 4 FASTENDec 26, 2014 · N927EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2014071110850Flashlight · inoperativeF/A'S FLASHLIGHT DOES NOT WORK. R & R FLASHLIGHT IAW AMM 25-60-00.Jul 9, 2014 · N927EV · Cndair CL6002B19 · Emergency EquipmentSDR ASOA2013082608910Bulb · burned outRT AFT EXTERNAL EMERGENCY LIGHT INOPERATIVE. R & R BULB IAW AMM 33-51-21. OP'S CHECKED GOOD.Aug 24, 2013 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2013060403755Skin · corrodedCORROSION WAS FOUND UNDER SELF-CONTOURING SEALING PAD FROM STR26 TO STR24, FROM 409+80 TO 409+400 ON BELLY SKIN. REPAIRED IAW SRM 51-21--06 AND REO 601R-53-31-789.May 24, 2013 · N927EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2013060403754Floor Support · corrodedFLOOR SUPPORT SCREW HOLES HAVE CORROSION. REMOVED CORROSION IAW SRM 51-21-06-00.May 17, 2013 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013060403753Floor Support · corrodedRT FLOOR SUPPORT CORRODED IN CARGO COMPT AT FS 559 + 112. REPAIRED IAW SRM 51-21-06-00, REO 601R-53-00-256 AND REO 601R-53-00-526 01.May 17, 2013 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013060403752Floor Support · corrodedRT FLOOR SUPPORT CORRODED IN CARGO BAY AT FS 618. REPAIRED IAW SRM 1-1-06-00 AND REO 601R-53-00-526.May 17, 2013 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013060403751Floor Support · corrodedLEFT FLOOR SUPPORT IN CARGO BAY CORRODED FROM FS 574 TO 621. REPAIRED IAW SRM 51-21-06-10, REO 601R-53-00-526.May 17, 2013 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013060403750Intercostal · crackedCRACKED INTERCOSTAL ON ASD AFT SIDE LOWER SECTION INSIDE PANEL 832BR. REMOVED DAMAGED INTERCOSTAL IAW SRM 51-42-06 AND DRILLED NEW INTERCOSTAL TO FIT IAW SRM 51-40-11 AND INSTALLED INTERCOSTAL IAW SRM 51-42-06.May 16, 2013 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013060303747Sign · brokenSERVICE DOOR INNER HANDLE EXIT PLACARD SELF ILLUMINATED BROKEN AT LOWER SCREW ATTACHMENT. R & R EXIT PLACARD WITH SERVICEABLE ONE IAW AMM 33-51-09-000-802 AND 33-51-09-400-802. PERFORMED FUNCTIONAL CHECK OF EXIT PLACARD IAW AMM 33-51-09-720-801.May 16, 2013 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2013060303746Angle · crackedANGLE CRACKED AT FRAME BS 625.3, S14R IN AFT EQUIP BAY. REMOVED CRACKED ANGLE IAW SRM 51-42-20. INSTALLED SERIVCABLE ANGLE IAW SRM 51-42-21.May 15, 2013 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013060303745Angle · crackedANGLE CRACKED AT FRAME BS 625.3, S14L IN AFT EQUIP BAY. REMOVED CRACKED ANGLE IAW SRM 51-42-20. INSTALLED REPLACEMENT ANGLE IAW SRM 51-42-21-00.May 15, 2013 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2013060303744Roller · out of adjustPAX DOOR HANDLE TAKES MORE THAN 16LBS OF FORCE TO FULLY UNLATCH. REMOVED SAFETY WIRE AND ADJUSTED PAX DOOR HANDLE ROLLER IAW AMM 52-11-25-830-801. REPLACED SAFETY WIRE ON PAX DOOR HANDLE AMM 20-24-00-910-802. PERFORMED OPS TEST OF PAX DOOR WARNING SYS IAW AMay 14, 2013 · N927EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2013022503064Lens · missingLIGHTED EXIT SIGN ON BULKHEAD NEAR PAX DOOR MISSING COVER. FOUND FLOODLIGHT COVER & RESECURED IAW AMM 33-51-19.Feb 21, 2013 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2013012402903Door · bindingPAX DOOR WILL NOT OPEN. PERFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-08. OPS CHECK GOOD.Jan 21, 2013 · N927EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2012071001884Step · crackedPASSENGER DOOR HAS A CRACK BELOW THE TOP STEP. REPAIRED IAW REO 601R-52-11-279.Jul 6, 2012 · N927EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201201619Lamp · burned outCEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY FLOOD LIGHT. OPS CHECKED GOOD.May 10, 2012 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201201263Overheat Loop · unserviceableLEFT 14TH DUCT WARNING MESSAGE ON DESCENT THRU 18000 FEET. EMERGENCY DECLARED. R & R LT ENG PYLON 14TH STAGE SENSING LOOP IAW AMM 36-21-04.Apr 12, 2012 · N927EV · Cndair CL6002B19 · Overheat DetectionSDR ASOA201200978Lamp · inoperativeLEFT EXTERIOR OVERWING FWD EMERGENCY LIGHT INOPERATIVE. RELAMPED LT SIDE EXTERIOR OVERWING FWD EMERGENCY LIHGT IAW AMM 33-51-21. OPS CHECKED GOOD.Mar 20, 2012 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201200648Light · inoperativeONE CEILING EMERGENCY LIGHT IS OUT. 2ND LIGHT BACK FROM FRONT. RESECURED CEILING EMERGENCY LIGHT IAW AMM 33-51-09. OPS CHECKED GOOD.Feb 28, 2012 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201200118Lamp · burned outTHE AFT EMERGENCY LIGHT OVER THE LEFT WING IS INOPERATIVE. RELAMPED THE AFT LEFT WING EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.Jan 11, 2012 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2011121702379Lamp · burned outNR 4 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-21. OPS CHECKED GOOD.Dec 17, 2011 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201101258Flap System · failedRECEIVED FLAPS FAIL WHEN SELECTED FOR LANDING FAILED AT ZERO (EMERGENCY DECLARED AS A PRECAUTION) REFER TO AFDL 622132-1, AD 2009-06-12.Jun 23, 2011 · N927EV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA201100411Lamp · burned outFWD AND AFT CEILING EMERGENCY LIGHT INOP // (RESOLVED ON W/O: 193469 TASKCARD: N/R-00004 ) / 3/2/11...RELAMPED FWD AND AFT CEILING EMERGENCY LIGHT IAW CRJ200 AMM 33-51-14. OPS CHECK GOOD / ITEM: 1 / 3/2/11...RELAMPED FWD AND AFT CEILING EMERGENCY LIGHTS IAW Mar 2, 2011 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201100319Flashlight · inoperativeF/A FLASHLIGHT INOP. R & R F/A FLASHLIGHT IAW AMM 25-61-00. OPS CHECKS GOOD.Feb 17, 2011 · N927EV · Cndair CL6002B19 · Emergency EquipmentSDR ASOA201100039Bracket · bentRECEIVED NOSE DOOR AND GEAR DISAGREE CAUTION MSGS NOSE GEAR DID NOT RETRACT CYCLED GEAR 2 MORE TIMES - CONDITION REPEATED LANDED AT 50,000 LBS WITH TOUCH DOWN RATE LESS THAN. (ACFT RETURNED TO DEPARTURE AFTER TO -- EMERGENCY DECLARED) COMPLIED WITH GEAR SWINGJan 5, 2011 · N927EV · Cndair CL6002B19 · Nose/Tail Landing GearSDR ASOA201001875Inverter · inoperativeRT OVERWING FLOOR LEVEL EXIT ID INOPERATIVE. R & R NR3 EMERGENCY LIGHT INVERTER IAW MM 33-51-07-000-801 & -400-801. EMERGENCY LIGHTS OPS CK OK IAW MM 33-51-00-710-801.Dec 6, 2010 · N927EV · Cndair CL6002B19 · Emergency LightingSDR ASOA201001843Floorbeam · corrodedMWC 362, LBL 27, FLOORBEAM CAP IS CORRODED AROUND NUTPLATE AT FS 605. "12. C/W EC/TC REO 601R-53-61-3778 AND REO 601R-53-61-3778, REV DATED 08/21/2010 AS WRITTEN. FOUND TO BE SATISFACTORY."Nov 29, 2010 · N927EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001865Anchor Fitting · crackedPAX DOOR ANCHOR FITTING CRACKED. REPLACED AFT PAX DOOR ANCHOR FITTING IAW AMM 52-11-17-000-804 AND 52-11-17-400-804. PAX DOOR OP'S CHECK GOOD RII ACCOMPLISHED ON LISTED WVAC NRI BY INSPECTOR.Nov 22, 2010 · N927EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001829Angle · crackedLEFT AND RIGHT OBLIQUE ANGLES CRACKED FS 621-625, STRG 15 LEFT AND RIGHT. RESOLVED ON W/O: 180442 TASKCARD: N/R-00693. REMOVED LT/RT OBLIQUE ANGLES FROM FS 625 STR 15 IAW CRJ 200 SRM 51-42-21. PREPARED AND DRILLED LT/RT OBLIQUE ANGLES IAW CRJ 200 SRM 51-40-Nov 22, 2010 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001802Floorbeam · crackedLBL 27 FLOORBEAM CAP IS CORRODED AROUND NUTPLATES AT FS 605.00. FLOORBEAM REPAIRED IAW SRM 51-21-11. ACFT RETURNED TO SERVICE.Nov 17, 2010 · N927EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001788Bracket · crackedBRACKET AT FS 559 BETWEEN RBL 9 AND BL 0.0 IS CRACKED AT RBL 9 FWD FASTENER HOLE. REMOVED BRACKET IAW SRM 51-42-06. BRACKET INSTALLED IAW SRM 51-42-06.Nov 15, 2010 · N927EV · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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