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 SWIA2020080751675Intercostal · corrodedPAX DOOR DD4 MID INTERCOSTAL CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM AND DWG.Jun 5, 2020 · N751EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020080751674Angle · corrodedPAX DOOR ANGLE DD7A FWD OF BS 325 WAS CORRODED. INSTALLED A NEW ANGLE IAW SRM AND DWG.Jun 5, 2020 · N751EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020080751673Intercostal · corrodedPAX DOOR INTERCOSTAL DD7A AFT OF FS320 CORRODED. (C-CHECK) RO 8/5/2020 INSTALLED NEW INTERCOSTAL REF CRJ 700 SRM , AND DWG. COMPLIED WITH TASK CARDJun 5, 2020 · N751EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020080751672Intercostal · corrodedPAX DOOR AFT DD5 INTERCOSTAL CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM AND DWG.Jun 5, 2020 · N751EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020080751671Intercostal · corrodedPAX DOOR AFT DD2 INTERCOSTAL CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM, AND DWG.Jun 5, 2020 · N751EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020080751670Intercostal · dentedPAX DOOR FWD DD1 INTERCOSTAL DENTED IN RADIUS. REMOVED AND INSTALLED A NEW INTERCOSTAL IAW SRM AND DWG.Jun 5, 2020 · N751EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020080751669Former · crackedPAX DOOR FORMER FS329 CRACKED. INSTALLED A NEW FORMER IAW SRM AND DWG.Jun 5, 2020 · N751EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020080751668Angle · crackedPAX DOOR ANGLE FS333 CRACKED. REMOVED AND INSTALLED A NEW PAX ANGLE IAW SRM AND DWG. RESTORED FINISH IAW SRM.Jun 5, 2020 · N751EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020080751667Former · crackedPAX DOOR FORMER CRACKED AT BS 333. REMOVED AND INSTALLED A NEW PAX DOOR FORMER IAW SRM, AND DWG.Jun 5, 2020 · N751EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020080751666Intercostal · crackedPAX DOOR AFT DD7 INTERCOSTAL CRACKED. REMOVED AND INSTALLED A NEW INTERCOSTAL IAW SRM AND DWG,Jun 5, 2020 · N751EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020080751665Stringer · corrodedSTRINGER 20L, BS 310 TO 333 HAD MULTIPLE LOCATIONS OF CORROSION. REPLACED THE STRINGER IAW DWG, AND SRM.Jun 5, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020080751712Cotter Pin · missingRIGHT INBD FLAP, INBD ACTUATOR ASSY, FWD AND AFT LUG ASSEBLIES, THREE BOLTS MISSING COTTER PINS AND REMAINNG BOLT COTTER PIN DEFORMED BEYOND USE. VERIFIED TORQUE ON RT INBD FLAP, INBD HINGE ARM ASSY MOUNTING HARDWARE AND INSTALLED FOUR NEW COTTER PINS IAW Jun 4, 2020 · N751EV · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2020080751664Rivet · damagedRIGHT OTBD FLAP, 2 SETS OF WORKING RIVETS IN CLOSE PROXIMITY TO EACH OTHER, ONE VERTICLE AND ONE HORIZONTAL. LOCATED ON TOP OF FLAP, SLIGHTLY INBD OF INBD ACTUATOR ASSY. REPLACED 12 RIVETS ON THE RT OTBD FLAP IAW REO.Jun 4, 2020 · N751EV · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2020080751663Rivet · damagedRIGHT OTBD FLAP, 2 SETS OF WORKING RIVETS IN CLOSE PROXIMITY TO EACH OTHER, ONE VERTICLE AND ONE HORIZONTAL. LOCATED ON TOP OF FLAP, SLIGHTLY OTBD OF CENTER ACTUATOR ASSY. REPLACED 15 RIVETS ON THE RT OTBD FLAP IAW REO.Jun 4, 2020 · N751EV · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2020080751662Intercostal · corrodedINTERCOSTAL AT STRINGER 20R, BETWEEN BS 310 AND 319 HAD CORROSION AT MULTIPLE LOCATIONS. THE INTERCOSTAL IS EXFOLIATED 100%, ORIGINAL MATERIAL THICKNESS IS .063" AND FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED THE INTERCOSTAL IAW DWG, AND SRM.Jun 3, 2020 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020080751704Seat Track · corrodedSEAT TRACK, RBL 9, BS 485 - 693 HAD CORROSION. REPLACED THE SEAT TRACK SECTION IAW AMM.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020080751703Seat Track · corrodedSEAT TRACK, BS 693 TO 830.4, RBL 9 HAD CORROSION. REPLACED THE SEAT TRACK IAW AMM.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020080751702Seat Track · corrodedSEAT TRACK, BS 693 - 830.4, LBL 9 HAD CORROSION. REPLACED THE SEAT TRACK IAW AMM.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020080751701Seat Track · corrodedSEAT TRACK, LBL 27, BS 364 - 477 HAD MULTIPLE LOCATIONS OF CORROSION. REMOVED AND INSTALLED A NEW SEAT TRACK IAW AMM.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020080751700Seat Track · corrodedSEAT TRACK, RBL 9, BS 349 - 477 HAD MULTIPLE LOCATIONS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020080751699Cup · corroded* THE PAX DOOR INTERNAL SURROUND FUSELAGE SIDE FWD HANDRAIL CUP HAS CORROSION. REMOVED CORROSION FROM PAX DOOR SURROUND FWD. CLOSING FITTING (HANDRAIL CUP). IAW SRM. FOUND TO BE OUT OF LIMITS AND REPLACED WITH NEW IAW SRM. RESTORED FINISH IAW SRM.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020080751698Floorbeam · corrodedTHE BS 280 FLOORBEAM ANGLE HAD CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE ANGLE IAW SRM.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2020080751661Stringer · corrodedSTRINGER 26R, BS 1015 TO 1047 HAD CORROSION. REPLACED THE STRINGER IAW SRM AND DWG.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020080751660Frame · corrodedFWD SIDE OF FRAME AT FS 1015 STRINGERS 26L TO 27, HAD CORROSION. PERFORMED A SPLICE REPAIR TO THE FRAME IAW REO.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2020080751659Floor Support · corrodedFLOOR SUPPORT CAP JUST AFT OF BS 565 TO 477, RBL 9 HAD CORROSION. REMOVED AND INSTALLED A NEW FLOOR SUPPORT IAW SRM.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020080751658Stringer · corrodedSTRINGER 19R, BETWEEN BS 295 AND 310 WAS CORRODED. REPLACED THE STRINGER IAW SRM, DWG, AND REO.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020080751657Floor Support · corrodedFLOOR SUPPORT CAP FROM JUST AFT OF FS 565.0 TO FS 477.0 LBL 9 HAD CORROSION. REPLACED THE FLOOR SUPPORT IAW SRM, AND REO.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020080751656Floor Support · corrodedFLOOR SUPPORT CAP FROM FS 693.0 TO JUST AFT OF FS 565.0 AT LBL 9 HAD CORROSION. REPLACED THE FLOOR SUPPORT IAW SRM, AND REO.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020080751655Structure · corroded* A BAY - AFT OF FS 280 - STGR'S 18 - 21L- JOINT PLATE CORRODED. REMOVED CORROSION FROM FS280 JOINT PLATE BETWEEN STGRS 18L - 21L, MATERIAL LOSS FOUND TO BE WITHIN ALLOWABLE LIMITS REF REO.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2020080751654Floor Support · corrodedLEFT FLOOR SUPPORT BETWEEN BS 549 TO 565 HAD THREE SPOTS OF CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM AND DWG.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020080751653Stringer · corrodedSTRINGER 19L, BETWEEN BS 295 AND 310 WAS CORRODED. REPLACED THE STRINGER WITH NEW IAW REO.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020080751652Stringer · corroded* A BAY - STGR 22L - BETWEEN BS 295 AND 310 WAS CORRODED. REPLACED THE STRINGER IAW DWG, AND SRM.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020080751651Floor Support · corrodedFLOOR SUPPORT JUST FWD OF BS 693 TO JUST AFT OF BS 565, RBL 9 HAD CORROSION. REMOVED AND INSTALLED A NEW FLOOR SUPPORT IAW SRM.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020080751650Seat Track · corrodedCORROSION ON SEAT TRACK CAP FS 693, RBL 9. PERFORMED REPAIR TO THE SEAT TRACK IAW REO.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020080751649Stringer · corrodedSTRINGER 20L FROM BS 295 TO 333 HAD MULTIPLE LOCATIONS OF CORROSION. REMOVED AND INSTALLED A NEW STRINGER IAW DWG, AND SRM.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020080751648Structure · corroded* THE LONGITUDINAL JOINT AT STRINGER 20L FROM FS280.00 TO FS333.00 HAS MULTIPLE LOCATIONS OF CORROSION. REMOVED CORROSION REF CRJ700 SRM FROM THE LONGITUDINAL JOINT AT STRINGER 20L FROM FS280.00 TO FS333.00 AT MULTIPLE LOCATIONS OF CORROSION. FOUND MULTIPLE EJun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202051647Crossbeam · corroded* THE CROSSBEAM CAP AT BS 333, LBL 27 HAD CORROSION. PERFORMED A REPAIR TO THE CROSSBEAM IAW REO. COMPLIED WITH TASK CARD.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2020080751646Gusset · corrodedTHE INTERNAL SURROUND STRUCTURE, FUSELAGE SIDE OF THE AVIONICS BAY DOOR FWD GUSSET AT BS 364, STRINGER 25L HAD CORROSION. BLENDED THE CORROSION IAW SRM, INSTALLED A NEW GUSSET IAW DWG, AND SRM.Jun 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020080751697Seat Track · corrodedSEAT TRACK SECTION AT RBL 9, BS 953 - 989 HAD MULTIPLE LOCATIONS OF CORROSION. REPLACED THE SEAT TRACK IAW AMM.Jun 1, 2020 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020080751696Seat Track · corrodedSEAT TRACK SECTION, LBL 9, BS 830.4 - 953 HAD MULTIPLE LOCATIONS OF CORROSION. REPLACED THE SEAT TRACK IAW AMM.Jun 1, 2020 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020080751695Seat Track · corrodedSEAT TRACK SECTION AT RBL 9, BS 830.4 - 953 HAD MULTIPLE LOCATIONS OF CORROSION. REPLACED THE SEAT TRACK IAW AMM.Jun 1, 2020 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202051645Hinge · gougedPAX DOOR HINGE FUSELAGE SIDE HAS NEW GOUGE ON AFT LUG LANDING. REMOVED THE GOUGE FROM PAX DOOR HINGE AFT LUG LANDING, MATERIAL LOSS FOUND TO BE WITHIN ALLOWABLE LIMITS IAW REO. NO FURTHER DEFECTS NOTED. COMPLIED WITH TASK CARD.Jun 1, 2020 · N751EV · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA2020080751644Hinge · gougedPASSENGER DOOR HINGE, SECOND LUG FROM FORWARD SIDE WAS GOUGED. REMOVED THE GOUGES FROM PAX DOOR HINGE SECOND LUG, MATERIAL LOSS FOUND TO BE WITHIN ALLOWABLE LIMITS IAW REO. NO FURTHER DEFECTS NOTED. COMPLIED WITH TASK CARD.May 31, 2020 · N751EV · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA2020080751711Stop Fitting · chafedTHE GALLEY SERVICE DOOR EXTERNAL SURROUND FUSELAGE SIDE ALL STOP FITTINGS ARE CHAFED. PERFORMED REPAIR OF THE GALLEY SERVICE DOOR EXTERNAL SURROUND FUSELAGE SIDE STOP FITTINGS IAW REO.May 28, 2020 · N751EV · Cndair CL6002C10 · Galley DoorsSDR SWIA2020080751643Fitting · gougedLEFT MLG SIDE STAY FITTING WAS GOUGED WITH RAISED METAL FROM CONTACT WITH SIDE STAY PINTLE NUT COTTER PIN. REMOVED THE DAMAGE FROM THE LT MLG SIDE STAY FITTING IN AREA ABOVE PINTLE PIN NUT IAW SRM. DAMAGE REMOVAL MEASURES 1.090"" LONG BY .980"" WIDE BY .01May 28, 2020 · N751EV · Cndair CL6002C10 · Main Landing GearSDR SWIA2020080751642Former · corrodedPASSENGER DOOR, FWD FORMER CORRODED AROUND LOWER TENSION TIE. REMOVED AND INSTALLED A NEW PAX DOOR FWD FORMER IAW SRM, AND DWG. NO LEAKS NOTED.May 27, 2020 · N751EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020080751641Panel · chafed*LH ENGINE UPPER FAN COWL PANEL 432AT IS CHAFFED ON INNER SKIN AND STIFFENER. LH ENGINE UPPER FAN COWL INNER SKIN BLENDED AND FOUND WITHIN LIMITS IAW SRM. STIFFENER REPAIRED IAW SRM.May 27, 2020 · N751EV · Cndair CL6002C10 · Nacelle/Pylon, Plate/SkinSDR SWIA2020080751714Retainer · gougedTHE FWD BAGGAGE BAY DOOR EXTERNAL SURROUND FUSELAGE SIDE AFT SEAL RETAINER LOWER END WAS GOUGED. THE SEAL RETAINER WAS FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED THE SEAL RETAINER IAW SRM.May 26, 2020 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020080751713Retainer · gougedTHE FWD BAGGAGE BAY DOOR EXTERNAL SURROUND FUSELAGE SIDE FWD SEAL RETAINER LOWER END IS GOUGED. FWD BAGGAGE BAY DOOR EXTERNAL SURROUND FUSELAGE SIDE FWD SEAL RETAINER FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND REPLACED WITH NEW SEAL RETAINER IAW SRM.May 26, 2020 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020080751710Stop Fitting · chafedTHE FWD CARGO DOOR AFT LOWER STOP IS CHAFED. REMOVED AND REPLACED FWD CARGO DOOR STOP FITTING IAW AMM.May 26, 2020 · N751EV · Cndair CL6002C10 · Cargo/Baggage Doors
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