N754EV

Service difficulty reports · 199

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 = 'N754EV' 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 ASOA2012110802442Floor Support · crackedFWD EQUIPMENT COMPARTMENT FLOOR SUPPORT NEXT TO ADG PUMP BETWEEN FUSELAGE SKIN AND FRAME (FS 193) IS CRACKED. COMPLIED WITH REO 670-53-11-509 ON FWD E & E BAY FLOOR TYPE 2 REPAIR. FOUND TO BE SATISFACTORY. SOct 20, 2012 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012103102413Drag Angle · crackedPAX DOOR AFT SIDE RISER PANEL DRAG ANGLE CRACKED AT CENTER. REMOVED DRAG ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED NEW REPAIR PARTS DRAG ANGLE IAW SRM 51-11-04-201-002-A01.Oct 20, 2012 · N754EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2012083102154Flashlight · inoperativeF/A FLASHLIGHT INOPERATIVE. R & R THE FWD F/A FLASHLIGHT IAW AMM 33-21-12. OPS CHECKED GOOD.Aug 27, 2012 · N754EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2012083102153Flashlight · inoperativeF/O FLASHLIGHT INOPERATIVE. REPAIRED F/O FLASHLIGHT IAW AMM 25-61-02.Aug 27, 2012 · N754EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2012083102152Flashlight · inoperativeF/A FLASHLIGHT INOPERATIVE. REPAIRED IAW AMM 25-61-02, OPS CHECKED GOOD.Aug 27, 2012 · N754EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA201201683Door · lack of lubeFORWARD PASSENGER DIFFICULT TO OPEN. REMOVED EXCESS LUBRICATION AND OPS CHECKED PAX DOOR IAW AMM 5-11-01. OPS CHECKED GOOD.May 26, 2012 · N754EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201201649Megaphone · unserviceableMEGAPHONE HAS MISSING NUTPLATE AND WILL NOT STAY TOGETHER. R & R MEGAPHONE IAW AMM 25-61-14. IPC REF 25-61-14, FIG 1C ITEM 5. OPS CHECKED GOOD.May 14, 2012 · N754EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA201200867Cover · brokenEMERGENCY LIGHT AT PAX DOOR HAS BROKEN COVER. R & R COVER ASSY IAW AMM 33-51-11. OPS CHECKED GOOD.Mar 9, 2012 · N754EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201200404Actuator · failedIN CRUISE FLIGHT, AUTOPILOT ENGAGED, RECEIVED UNCOMMANDED RUDDER INPUTS (YD 1 WAS DEFFERRED AT THE TIME) INPUTS WERE LT AND RT OF CENTER AND NEEDED FULL RUDDER DEFLECTION AT TIMES TO COUNTER THE DEFLECTION. DECLARED AN EMERGENCY AND LANDED. R & R YAW DAMPERFeb 5, 2012 · N754EV · Cndair CL6002C10 · Rudder ActuatorSDR ASOA201101048Lens · missingEXIT SIGN MISSING F/A GALLEY AREA. GALLEY AREA EXIT SIGN LENS FOUND AND INSTALLED AMM 33-51-00,May 22, 2011 · N754EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201100454Structure · corrodedCORROSION IN BELLY OF FUSELAGE IN AV BAY BETWEEN FS 349 AND 364 BETWEEN STR 25L AND 26L. REPAIRED IAW REO 670-53-21-662.Mar 8, 2011 · N754EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201100443Intercostal · corrodedCORROSION ON INTERCOSTAL ON 26L AT FS 349 TO FS 364 ON LT SIDE OF INTERCOSTAL. REMOVED INTERCOSTAL IAW SRM 51-42-06, INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001.Mar 7, 2011 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201100442Crossbeam · corrodedFS 280 CROSSBEAM CORRODED. INSTALLED CROSSBEAM REF SRM 51-42-13-001-001Mar 7, 2011 · N754EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201100437Floorbeam · corrodedFLOOR PANEL 141ALF FORWARD SUPPORT ANGLE AT FS 280 IS CORRODED. REMOVED PANEL 161ALF IAW SRM 51-41-02. OK TO INSTALL, INSTALLED PNL 131ALF IAW SRM 51-41-02. REMOVED CORRODED SUPPORT ANGLE FROM FRAME AT FS 280 LBL 9 TO RBL 9 IAW SRM 51-42-06. LOCATED,DRILLEMar 7, 2011 · N754EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201100419Drag Angle · crackedLEFT VERTICAL STAB DRAG ANGLE CRACKED AT AFT END. COMPLIED WITH EC/TC REO 670-55-31-018 IAW REO 670-55-31-018.Mar 4, 2011 · N754EV · Cndair CL6002C10 · Vertical StabilizerSDR ASOA201100404Crossbeam · corrodedFS 280 CROSSBEAM CORRODED. BLENDED CORROSION ON FS 280 BEAM FOUND TO BE OUT OF LIMITS SRM 51-12-00-001-001-A01 AND SRM 53-00-00-001-001-A01. R & R FS 280 CROSSBEAM IAW SRM 51-42-06-001-001 AND 51-42-21-001-001 AND 51-42-13-001-001.Feb 28, 2011 · N754EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201100403Floor Support · corrodedCORROSION ON FLOOR SUPPORT ON RIGHT SIDE OF AFT CARGO BAY BETWEEN FS 985.00 AND FS 1015. BLENDED CORROSION ON RT FLOOR SUPPORT SILL IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW NDT INSP PROCDURE UT-3 MIN. MATERIAL REMAINFeb 28, 2011 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201100402Drag Angle · crackedLEFT VERTICAL STAB DRAG ANGLE CRACKED AT AFT END. PERFORMED EDDY CURRENT INSP ON LT SIDE FWD VERTICAL STAB DRAG ANGLE IAW NDT INSP PROCEDURES ET-2. VERIFIED DRAG ANGLE IS CRACKED AT AFT ENG. CRACK IS .65IN IN LENGTH. CUT AND REMOVED DAMAGE AT LT VERTICALFeb 28, 2011 · N754EV · Cndair CL6002C10 · Vertical StabilizerSDR ASOA201100401Floorbeam · corrodedFS 280 FORWARD FLOORBEAM ANGLE IS CORRODED OUT OF LIMITS SRM 53-00-00-101-001-A01. REMOVED FS 280 FWD FLOORBEAM ANGLE PER SRM'S 51-42-21-001-001-A01 AND 51-42-22-001-001-A01. INSTALLED FS 280 FWD FLOORBEAM ANGLE IAW SRM'S 51-42-06-001-001-A01 & 51-42-21-001Feb 28, 2011 · N754EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201100388Seat Track · corrodedSEAT TRACK HAS CORROSION BETWEEN FS 677.00 - FS 693.00, RBL 9.00. CHECKED THICKNESS FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. INSTALLED SERVICABLE SEAT TRACK IAW AMM 53-00.Feb 25, 2011 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201100387Seat Track · corrodedSEAT TRACK HAS CORROSION BETWEEN FS 581.00 - FS 677.00, RBL 9.00. CHECKED MATERIAL THICKNESS FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. INSTALLED SERVICABLE SEAT TRACK IAW AMM 53-00-49-400-801-A03.Feb 25, 2011 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201100386Seat Track · corrodedSEAT TRACK HAS CORROSION BETWEEN FS 485.00 - FS 581.00, RBL 9.00. REMOVED AND REPLACED CORRODED SEAT TRACK IAW AMM 53-00-49-000-801.Feb 25, 2011 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201100385Seat Track · corrodedSEAT TRACK HAS CORROSION BETWEEN FS 394.00 AND - FS 485.00, RBL 9.00. CHECKED THICKNESS FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. INSTALL SERVICABLE SEAT TRACK FROM FS350-485, RBL9.0 IAW AMM 53-00-49-400-801-A03. INSTALLED SERVICABLE SEAT TRACK AT RBFeb 25, 2011 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201100384Seat Track · corrodedSEAT TRACK HAS CORROSION BETWEEN FS 677.00-FS 693.00, LBL 9.00. AFTER FURTHER INSPECTION FOUND SEAT TRACK TO BE DAMAGED OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED SEAT RAIL AT FS 677.00, LBL 93.00 IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT RAIL IFeb 25, 2011 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201100383Seat Track · corrodedSEAT TRACK HAS CORROSION BETWEEN FS 581.00 - FS 677.00, LBL 9.00. CHECKED MATERIAL THICKNESS FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. INSTALL SERVICABLE SEAT TRACK FROM FS 581-683.5, LBL9.0 IAW AMM 53-00-49-400-801-A03. INSTALLED SERVICABLE SFeb 25, 2011 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201100382Floor Support · corrodedFLOOR SUPPORT ANGLE AT FS 280.00 CORRODED. [OPEN]Feb 25, 2011 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201100378Skin · corrodedCORROSION IN BELLY OF FUSELAGE IN AVIONIC BAY BETWEEN FS 295 AND 310 S27R. REMOVED CORROSION IAW SRM 51-42-06-001-001.Feb 24, 2011 · N754EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201100377Skin · corrodedCORROSION IN BELLY OF FUSELAGE IN AVIONIC BAY BETWEEN FS 364 AND 349 BETWEEN ST 26 AND 27L. REPAIRED IAW SRM 51-71-12-001-001.Feb 24, 2011 · N754EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201100376Skin · corrodedCORROSION IN BELLY OF FUSELAGE IN AVIONIC BAY BETWEEN FS 349 AND 364 BETWEEN STR 25 AND 26L. BLENDED OUT DAMAGE IAW SRM 57-12-00 CUT AND REMOVED DAMAGED FRAME SECTION IAW STEP 1 OF REO 670-53-21-662, P1. REPAIRED IAW REO 670-53-21-662.Feb 24, 2011 · N754EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201100375Skin · corrodedCORROSION IN BELLY OF FUSELAGE IN AVIONIC BAY BETWEEN FS 310 AND 317 BETWEEN STR 26 AND 27L. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. ALODINE, PRIMED AND PAINTED AREA IAW SRM 51-42-06-001-001 AND SRM 51-21-11-001-001.Feb 24, 2011 · N754EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201100012Lens · missingSERVICE DOOR EXIT SIGN COVER MISSING. FOUND EXIT SIGN COVER, RESECURED EXIT SIGN. OPS CHECK GOOD REF AMM 33-51-05. (CLOSED)Jan 3, 2011 · N754EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201001848Relay · intermittentEMERGENCY LIGHT ACTIVATING ON AND OFF STATUS MESSAGE. R & R RELAY K135 IN JB-11, IAW AMM 24-06-11, OPS CHECK GOOD.Nov 30, 2010 · N754EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201000698Light · disconnectedREF DMIL 531871-1 CEILING EMERGENCY LIGHT INOPERATIVE, FOUND EMERGENCY LIGHT TO BE DISCONNECTED. RECONNECTED FWD CEILING EMERGENCY LIGHT IAW AMM 33-51-05. OPS CHECK GOOD. DEFER CLEARED. PLACARD REMOVED.May 8, 2010 · N754EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201000697Light · disconnectedCABIN EMERGENCY LIGHT IN CEILING FIRST LIGHT DOES NOT ILLUMINATE WHEN TESTED. FOUND EMERGENCY LIGHT TO BE DISCONNECTED. RECONNECTED FWD CEILING EMERGENCY LIGHT IAW AMM 33-51-05. OPS CHECK GOOD. DEFER CLEARED. PLACARD REMOVED.May 8, 2010 · N754EV · Cndair CL6002C10 · Emergency LightingSDR ASOA200900619Trim System · malfunctionedRECEIVED STAB CHA1 INOP MSG, 10 MINS LATER RECEIVED TRIM RUNAWAY AURAL WARNING. DISCONNECTED STAB TRIM [EMERGENCY DECLARED]. FLT 5015 CX.Jun 3, 2009 · N754EV · Cndair CL6002C10 · Stabilizer Control SystemSDR ASOA200900369Floorbeam · corrodedWORK ORDER 50921 ZONE 1000 ITEM 13 280 FLOOR SUPPORT BEAM CORRODED AT RBL 9.0 AND LBL 9.0.Mar 25, 2009 · N754EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA200900327Seat Track · corrodedAAR 2000-0014 RBL9 SEAT TRACK AT FS 349.00 HAS POWDER CORROSION. REMOVED CORROSION & FOUND OUT LIMITS. INSTALLED NEW SEAT TRACK IAW SERM 51-41-02Mar 23, 2009 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA200801550Bulb · inoperativeG2 GALLEY EMERGENCY LIGHT HAS SEVERAL INOP BULBS.Nov 22, 2008 · N754EV · Cndair CL6002C10 · Emergency LightingSDR ASOA200801549Bulb · inoperativeRT OVERWING EMERGENCY EXIT LOWER EMERGENCY LIGHT HAS SEVERAL INOP BULBS.Nov 22, 2008 · N754EV · Cndair CL6002C10 · Emergency LightingSDR TRAX200801186Unknown · odorBOTH FAS COMPLAINED OF A STRONG FUEL ODOR DURING FLIGHT. IN AFT CABIN AFT OF ROW 14. RAN APU BOTH A/C PACKS AND FUEL PUMP SYSTEMS NO DEFECTS NOTED REF CRJ-700MM 21-51-00 28-23-02.Sep 16, 2008 · N754EV · Cndair CL6002C10 · Air Distribution SystemSDR TRAX200800137Fuel Cap · unsecureFUEL CAP LEFT OFF IN FLT, PERFORMED AIR RETURN LANDED AT 72000 LBS. EMERGENCY DECLARED.Jan 26, 2008 · N754EV · Cndair CL6002C10 · Fuel StorageSDR TRAX200800059Placard · tornEXIT STICKER ON AIRSTAIR DOOR IS TORN.Jan 8, 2008 · N754EV · Cndair CL6002C10 · Placards and MarkingsSDR TRAX200701036Web · corrodedRIGHT LOWER FS 280 WEB HAS CORROSION. [07-31-07] CORROSION FOUND TO BE OUT OF LIMITS PER: REO 670-53-11-052, REPAIRED IAW THE SAME EO.Jul 21, 2007 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR TRAX200701035Web · corrodedLEFT LOWER FS 280 WEB HAS CORROSION. [07-31-07] CORROSION FOUND TO BE OUT OF LIMITS, REPLACED OF LT LOWER FS 280 WEB PER REO 670-53-11-052.Jul 21, 2007 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR TRAX200701034Floor Support · crackedFS 280 FWD CENTER FLOOR SUPPORT ANGLE CRACKED. COMPLIED WITH INSPECTION OF THE PRESSURIZATION SYSTEM MANUAL MADE MORTOR AND ALTITUDE LIMITATION IAW PART A OF BOMBARDIER ALERT SERVICE BULLETIN A670BA-21-022. NO DEFECTS FOUND.Jul 21, 2007 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR TRAX200701033Crossbeam · crackedRIGHT FS 280 CROSSBEAM CRACKED ON UPPER FLANGE O/B OF RBL 9.0. [07-31-07] REPAIRED IAW MODSUM IS67053110026.Jul 21, 2007 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR TRAX200701032Crossbeam · crackedLEFT FS 280 CROSSBEAM CRACKED ON UPPER FLANGE O/B OF LBL 9.0. COMPLIED WITH E.O. 700-53-0058 REV A.Jul 21, 2007 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR TRAX200700157Light · inoperativeRIGHT OVERWING AFT EMERGENCY LIGHT IS INOP.Feb 3, 2007 · N754EV · Cndair CL6002C10 · Emergency LightingSDR TRAX200600604Light · inoperative2 FWD EMER LIGHTS ON OUTSIDE OF A/C.Aug 10, 2006 · N754EV · Cndair CL6002B19 · Emergency Lighting
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