N751EV

Service difficulty reports · 281

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 = 'N751EV' 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 ASOA200901082Bulb · inoperativeLT OVERWING EMERGENCY EXIT LWR EMERGENCY LIGHT HAS SEVERAL INOP BULBS.Oct 2, 2009 · N751EV · Cndair CL6002C10 · Emergency LightingSDR ASOA200900577Light · inoperativeEMERGENCY LIGHTS DO NOT OPERATE WHEN TURNED ON WITH EITHER THE COCKPIT OR THE FLIGHT ATTENDANT PANEL SWITCH.May 23, 2009 · N751EV · Cndair CL6002C10 · Emergency LightingSDR ASOA200900213Drag Angle · crackedRT VERTICAL STABILIZER DRAG ANGLE VERIFIED CRACKED. REPAIRED PER REO 670-55-31-041.Feb 16, 2009 · N751EV · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous StructureSDR ASOA200900211Web · crackedRT 280 WEB P/N CC670-34117-6 FOUND CRACK.Feb 14, 2009 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA200900199Bulkhead · corrodedRIGHT FS 280 BULKHEAD LOWER WEB HAS SURFACE CORROSION. BLENDED RT WEB TO WITHIN LIMITS CONDITION IAW SRM 53-11-10.Feb 11, 2009 · N751EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA200900198Floorbeam · corrodedFWD FLOORBEAM ANGLE AT FS 280 IS CORRODED. REMOVED FWD SUPPORT FLOOR ANGLE IAW SRM 51-42-06 AND 51-42-20. DRILLED AND INSTALLED NEW FWD SUPPORT FLOOR ANGLE PER SRM 51-40-11 AND 51-42-06. BAT7023167. RII C/W SATISFACTORY IAW SP 607 & SRM 51-40-11.Feb 11, 2009 · N751EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA200900204Shroud · crackedRT MULTIFUNCTION SPOILER SHROUD CRACKED AT I/B CORNER. REMOVED PAINT, RE-INSPECTED AND FOUND RT MULTIFUNCTION SPOILER SHROUD NOT CRACKED AT I/B CORNER. PRIMED AND PAINTED PER SRM 51-21-16 02-16-09.Feb 9, 2009 · N751EV · Cndair CL6002C10 · SpoilersSDR ASOA200900192Web · corrodedLT SIDE FS 280.00 WEB ABOVE FLOOR CORRODED LOWER RT EDGE. REMOVED WEB IAW SRM 51-42-06, DRILLED NEW WEB IAW SRM 53-11-10, INSTALLED WEB PER SRM 51-42-06.Feb 9, 2009 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA200900191Floorbeam · corrodedFS 280.00 LT CROSS BEAM CORRODED ON TOP FLANGE. REMOVED AND REPLACED 280 LT CROSSBEAM PER SRM 51-40-11 AND 51-42-00.Feb 9, 2009 · N751EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA200900190Floorbeam · corrodedFS 280.00 RT CROSS BEAM CORRODED ON TOP FLANGE. REMOVE AND REPLACED RT CROSSBEAM PER SRM 51-40-11 AND 51-42-00.Feb 9, 2009 · N751EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA200900189Drag Angle · crackedASD AFT SIDEWALL DRAG ANGLE CRACKED.Feb 8, 2009 · N751EV · Cndair CL6002C10 · Entrance StairsSDR ASOA200900188Step · brokenPAX DOOR BOTTOM STEP BROKEN AT LINK ATTACK POINT. REMOVED AND REPLACED BROKEN STAIR PANEL IAW CMM 52-11-00. REMOVED AND REPLACED BROKEN STAIR PANEL IAW CMM 52-11-00.Feb 8, 2009 · N751EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA200900187Step · crackedASD TOP STEP CRACKED. INSTALLED NEW TOP STEP IAW AMM 52-11-04. OPERATIONAL CHECK COMPLIED WITH IAW AMM 52-11-04-710-801. RII COMPLIED WITH IAW S.P. 607 AND AMM 52-11-04.Feb 8, 2009 · N751EV · Cndair CL6002C10 · Entrance StairsSDR ASOA200900089Light · failedDURING ORG CHECK EMERGENCY LIGHT TEST FAILED. NO EMERGENCY LIGHT STATUS MSG OR CABIN EMERGENCY LIGHTING WITH SWITCH IN ON POS...FLT 5189 CX.Jan 20, 2009 · N751EV · Cndair CL6002C10 · Emergency LightingSDR TRAX200800990Sign · inoperativeLT OVERWING EMERGENCY EXIT LOWER LIGHTED EXIT SIGN HAS SEVERAL BULBS INOPERATIVE. REMOVED AND REPLACED LT LOWER EMERGENCY EXIT SIGN BAD BULBS IAW CRJ 700 AMM 33-51-05. (S)Aug 9, 2008 · N751EV · Cndair CL6002C10 · Emergency LightingSDR TRAX200701985Step · damagedASD LOWER STEP DAMAGED.Dec 26, 2007 · N751EV · Cndair CL6002C10 · Entrance StairsSDR TRAX200701646Flashlight · dischargedFWD F/A FLASHLIGHT WEAK.Oct 30, 2007 · N751EV · Cndair CL6002C10 · Emergency EquipmentSDR TRAX200701397Light · inoperativeFWD EMERGENCY LIGHT ABOVE ROW TWO IS INOP, CABIN EMERGENCY LIGHTS - CEILING LEVEL FLOODLIGHTS. Sep 24, 2007 · N751EV · Cndair CL6002C10 · Emergency LightingSDR TRAX200701147Warning System · intermittentFIRE SYS FAULT, STATUS MSG. COMES ON & OFF THROUGHOUT FLIGHT.Aug 9, 2007 · N751EV · Cndair CL6002C10 · Fire DetectionSDR TRAX200700881Panel · corrodedFOUND EXFOLIATION CORROSION ON INTERNAL STRUCTURE OF LT OUTBOARD FLAP ASSY IAW TASKCARD 000-57-590-502. REMOVED AND REPLACED LT OUTBOARD FLAP PANEL IAW CRJ 700 AMM 27-52-29. RIG AND OP'S CHECK GOOD IAW CRJ 700 AMM 27-52-00. STARTED REMOVING FLAP FAIRING PANJun 16, 2007 · N751EV · Cndair CL6002C10 · Trailing Edge FlapsSDR TRAX200700857Seat Track · corrodedRT SEAT TRACK CORRODED BETWEEN FS349-364. REPAIRED IAW SRM`S 53-21-49 AND 51-21-06, AND 51-41-02.Jun 15, 2007 · N751EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR TRAX200700855Bulkhead · corrodedLT 280 BULKHEAD LOWER WEB CORRODED. REPAIRED IAW SRM 51-42-06, 70-53-11-052, REO 670-53-11-052, ALL WORK COMPLETE COMPLIED WITH EO 700-53-0062 01Jun 15, 2007 · N751EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR TRAX200700854Bulkhead · corrodedRT 280 BULKHEAD LOWER WEB CORRODED. REPAIRED IAW CRJ700 SRM 51-42-06, REO 670-53-11-052, SRM 51-00-00, AND EO 700-53-0062.Jun 15, 2007 · N751EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR TRAX200700852Crossbeam · corrodedLT 280 CROSSBEAM CORRODED AND CRACKED. REPAIRED IAW CRJ700 SRM 51-42-21, CRJ700 SRM 51-42-06, CRJ 700 SRM 51-42-00, REO 670-53-11-00026, & REO 670-53-11-047.Jun 15, 2007 · N751EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200700839Cover · crackedRIGHT EMERGENCY EXIT DOOR UPPER HANDLE COVER IS CRACKED.Jun 14, 2007 · N751EV · Cndair CL6002C10 · Emergency ExitsSDR TRAX200700837Floor Support · crackedFLIGHT COMPARTMENT FLOORBOARD AFT LANDING BRACKET CRACKED AT FS 280.00. [06-27-07] REPAIRED IAW 51-00-00, 51-00-00, AND REO 670-53-11-047.Jun 14, 2007 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR TRAX200700836Intercostal · corrodedFS 280.00 INTERCOSTAL BETWEEN LBL 9 AND RBL 9 CORRODED ON FWD FACE.Jun 14, 2007 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR TRAX200700518Light · inoperativeRIGHT EMERGENCY EXIT LOWER EXIT LIGHT HAS SEVERAL INOP BULBS.Apr 12, 2007 · N751EV · Cndair CL6002C10 · Emergency LightingSDR ASOA06098Panel · crackedDURING A C-CHECK, THE FORWARD AND AFT PASSENGER DOOR SIDEWALL, AT THE HANDRAIL SUPPORT BRACKET, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FORWARD AND AFT PASSENGER DOOR SIDEWALL, AT THE HANDRAIL SUPPORT BRACKET, IAW REO 670-52-11-104. (Jan 17, 2006 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA06086Step · separatedDURING A HANGAR INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND SEPARATED AT THE ATTACH STAY ROD BRACKET TO THE STEP COMPOSITE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jan 10, 2006 · N751EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA04892Vane · false indicationFOLLOWING TAKEOFF, CREW RECEIVED A STALL FAIL CAUTION MESSAGE. QRH WAS COMPLIED WITH AND APPROXIMATELY 250 KNOTS THE STICK SHAKER BEGAN TO SHAKE THE CONTROLS. THE AIRSPEED WAS INCREASED ABOVE 250 KNOTS AND PITCH LOWERED TO INCREASE ABOVE THE LOW SPEED CUE. Nov 8, 2004 · N751EV · Cndair CL6002C10 · Stall Warning System
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