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 ASOA201707121755Seat Track · corrodedLT SIDE SEAT RAIL AT FS 485-575 HAS CORROSION IN MULTIPLE AREAS. REMOVED, FABBED A NEW SEGMENT AND INSTALLED PER 53-00-49-000-801 A01, 53-00-49-400-801-A17 AND EC/TC REO 670-53-00-343.Jul 12, 2017 · N751EV · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201707121754Seat Track · corrodedRT SIDE SEAT RAIL AT FS 379-485 HAS CORROSION IN MULTIPLE AREAS. REMOVED, FABBED A NEW SEGMENT AND INSTALLED PER 53-00-49-000-801 A01, 53-00-49-400-801-A17 AND EC/TC REO 670-53-00-343.Jul 12, 2017 · N751EV · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201704175038Transducer · failedPILOT REPORTED ON LANDING, THE BRAKENG WAS ASYMETRIC WITH ACFT PULLING RIGHT AT GATE. LEFT INBD BTMS SHOWED 00 AND LT INBD BRAKE WAS COLD TO TOUCH. MX REMOVED AND REPLACED THE LT INBD WHEEL SPEED TRANSDUCER, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TOApr 17, 2017 · N751EV · Cndair CL6002C10 · Landing Gear Brake SystemSDR ASOA201702035010Bulb · inoperativeDURING SCHEDULED MX INSPECTION, THE ROW 17 OVERHEAD EMERGENCY LIGHT WAS DISCOVERED INOPERATIVE. MX REMOVED AND REPLACED THE LIGHT BULB OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.Feb 3, 2017 · N751EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2016061614931Lens · missingEMERGENCY EXIT SIGN COVER MISSING FROM GALLEY NR 2. INSTALLED EMERGENCY EXIT LIGHT COVER IAW AMM 33-51-00. ACFT OK FOR SERVICE.Jun 16, 2016 · N751EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2016053114908Light · missingGALLEY FLOOR TRACK LIGHT MISSING. INSTALLED MISSING EMERGENCY LIGHT STRIP IN GALLEY IAW AMM 33-57-01.May 31, 2016 · N751EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2016041514705Bulb · burned outBULB BURNED ON ENTRANCE DOOR LOWER EXIT LIGHT. R & R LIGHT IAW AMM 33-51-05, OPS CHECK GOOD.Apr 15, 2016 · N751EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2016021114507Threshold · corrodedCARGO DOOR THRESHOLD CORRODED. REPLACED IAW SRM 53-61-23-101-001-A01.Feb 11, 2016 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2016021114506Floorbeam · corrodedCORROSION FOUND ON LBL 27, FS 1031 FLOORBEAM. REPAIRED THE FLOORBEAM IAW SRM 53-61-43-101-001-A01.Feb 11, 2016 · N751EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2016021114505Floorbeam · corrodedCORROSION FOUND ON LBL 9, FS 1031 FLOORBEAM. REPAIR THE FLOORBEAM IAW SRM 53-61-43-101-001-A01.Feb 11, 2016 · N751EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2015122914287Battery Pack · inoperativeF/A REAR MEGAPHONE NOT WORKING. TIGHTENDED R2 BATTERIES AS REQUIRED IAW GMM 3-8.6.Dec 29, 2015 · N751EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2015101513893Lens · missingLIGHTED PLACARD AT SERVICE DOOR PLACARD MISSING. INSTALLED SERVICE DOOR COVER IAW AMM 33-51-00.Oct 15, 2015 · N751EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015051412850Lens · crackedSERVICE DOOR EXIT SIGN CRACKED. REMOVED AND INSTALLED NEW SERVICEABLE DOOR EXIT SIGN COVER LENS IAW AMM TASK 33-51-05-000, 400,-801-A01, OPS CHECKED GOOD.May 9, 2015 · N751EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015051412849Doubler · corrodedDOUBLER ON RT INTERCOSTAL AT BS 349 CORRODED BEYOND LIMITS. COMPLIED WITH DOUBLER FABRICATION IAW SNIEO SH670-32003501. FABRICATED AND INSTALLED DOUBLER IAW SNIEO 670-320003 S01 501.May 5, 2015 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015051412848Shear Tie · corrodedCLEAT PN SH670-37014-1 ON RT INTERCOSTAL AT FS 349 IS CORRODED BEYOND LIMITS. COMPLIED WITH SNIEO SH670-32014, SN 02 AS WRITTEN. RECEIVED ECTC SNIEO- 32014 501 FABRICATED AND INSTALLED ANGLE, PN 51-670-32014-1 IAW SNIEO 670-32015 501.May 5, 2015 · N751EV · Cndair CL6002C10 · Fuselage Internal Mounting StructureSDR ASOA2015051412847Stringer · corrodedSTR 20R HAS EXFOLIATION CORROSION ON FLANGES BETWEEN FS 319.70 AND FS 349.00. REMOVED STR 20R SEGMENT BETWEEN FS 319.70 AND FS 349.00 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. PICKED UP ALL ATTACHING HOLES IN STR 20R, REF SRM 51-40-11-001-001 & DWGMay 2, 2015 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2015051412846Striker · corrodedSERVICE DOOR SEAL STRIKER CORRODED. REMOVED SERVICE DOOR SEAL STRIKER IN REF TO SRM 51-42-06-001-001 A01. INSTALLED NEW SERVICEABLE SERVICE DOOR SEAL STRIKER IN REF TO SRM 51-42-06-001-001-A01.Apr 24, 2015 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015051412845Strap · damagedOVERSIZE HOLE, RT WING STRAP IAW RNC. RECEIVED REO 670-21-775 REPAIR TO LOWER WING ASSY P1 DATED 2015-04-22. COMPLIED WITH REO 670-57-21-775 P1 DATED 2015-04-22. RECEIVED PERMANENT REO 670-57-21-775 REV-- DATED 2015-04-26 AND REQUESTED EC/TC. RECEIVED AND Apr 22, 2015 · N751EV · Cndair CL6002C10 · Wing Miscellaneous StructureSDR ASOA2015051412844Angle · corrodedGALLEY DOOR FLOOR PROTECTOR ANGLES HAS CORROSION, 4. REMOVED 4 EA GALLEY DOOR FLOOR SUPPORT ANGLES IN REF TO SRM 51-42-06-001-001-A01. INSTALLED 4 EA NEW GALLEY DOOR FLOOR SUPPORT ANGLES IN REF TO SRM 51-42-06-001-001-A01.Apr 21, 2015 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015051412843Plate · corrodedSERVICE DOOR JOINT PLATE HAS CORROSION. R & R SERVICE DOOR FWD FITTING IN REF TO SRM 51-42-21-001-001-A01.Apr 21, 2015 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015051412842Structure · corrodedSERVICE DOOR WEB FLOOR PROTECTORS HAVE CORROSION 3. 3 EA FLOOR PROTECTORS ARE CORRODED OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED 4 EA FLOOR PROTECTORS AT SERVICE DOOR IN REF TO SRM 51-42-06-001-001-A01. INSTALLED 3EA NEW FLOOR PROTECTORS, REINSTALApr 21, 2015 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015051412841Blanking Plate · corrodedBLANKING PLATE AT BS 349-364, RT HAS CORROSION, SERVICE DOOR. REMOVED CORROSION ON BLANKING PLATE AT FS 349-364 RT IN REF TO SRM 51-21-06-001-001-A01. COMPLIED WITH EC/TC REO 670-53-00-390 AND REO 670-53-00-390, REV, DATED 01/22/2014 AS WRITTEN.Apr 21, 2015 · N751EV · Cndair CL6002C10 · Service DoorsSDR ASOA2015051412840Door Sill · corrodedLOWER ANGLE SILL AT SERVICE DOOR HAS CORROSION. SEVERE CORROSION OUT OF LIMITS IAW SRM NO DAMAGE ALLOWED AROUND FASTENERS 53-21-23-101-002-A01. REMOVED LOWER ANGLE SILL AT SERVICE DOOR IN REF TO SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE LOWER ANGLApr 21, 2015 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015051412839Angle · corrodedUPPER ANGLE AT SERVICE DOOR HAS CORROSION, SEVERE CORROSION IS OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED UPPER ANGLE IAW SRM 51-42-06-001-001-A01, 7 51-42-21-001-001-A01 AND INSTALLED IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.Apr 21, 2015 · N751EV · Cndair CL6002C10 · Service DoorsSDR ASOA2015051412838Angle · corrodedLOWER ANGLE AT PAX DOOR HAS CORROSION. SEVERE CORROSON IS OUT OF LIMITS IAW CRJ 53-21-23-101-001-A01. R & R LOWER PAX DOOR SILL ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31875.Apr 21, 2015 · N751EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2015051412837Angle · corrodedUPPER ANGLE AT PAX DOOR HAS CORROSION. SEVERE CORROSION IS OUT OF LIMITS IAW CRM 53-21-23-101-001-A01. R & R UPPER MIDCAP ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-41-02-001-001-A01 AND DWG SH670-31825.Apr 21, 2015 · N751EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2015051412836Floor Support · corrodedRIGHT FLOOR SUPPORT AT BS 280 - 319.7 HAS CORROSION. REMOVED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01. INSTALLED IAW SRM 51-42-13-001-001-A01, 51-42-06-001-001-A01 AND 51-45-00-001-001-A01.Apr 21, 2015 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015051412835Angle · crackedBS 280 WEB ANGLE CRACKED AT LBL 26. REMOVED CRACKED ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG CC670-34010.Apr 20, 2015 · N751EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2015051412834Angle · crackedBS 280 WEB ANGLE CRACKED AT RBL 26. R & R ANGLE IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.Apr 20, 2015 · N751EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2015051412833Floorbeam · crackedRIGHT COCKPIT FLOORBEAM IS CRACKED. RECEIVED AND COMPLIED WITH ECTC REO 670-53-11-896 AND REO 670-53-11-896, REV DATED 03-17-2015 AS WRITTEN.Apr 20, 2015 · N751EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2015051412832Seat Track · corrodedLT SIDE WALL SEAT TRACK CORRODED AT BS 785.15 - 863. CORROSION IS OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.Apr 20, 2015 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015051412831Seat Track · corrodedRIGHT SIDE SEAT TRACK CORRODED AT BS 485 - 565. CORROSION OUT OF LIMITS IAW SRM 53-31-49-11-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.Apr 20, 2015 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015051412830Seat Track · corrodedRT SIDE WALL SEAT TRACK CORRODED AT BS 708 - 761.85. CORROSION IS OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, A03 AND AMM 53-00-49-00-400-801, A03.Apr 20, 2015 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015051412829Seat Track · corrodedLEFT SIDE SEAT TRACK CORRODED AT BS 677 - 708. CORROSION OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.Apr 20, 2015 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015051412828Seat Track · corrodedRIGHT SIDE WALL SEAT TRACK CORRODED AT FS 565 - 677. CORROSION IS OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED THE SEAT TRACK IAW AMM 53-00-49-000-801 A03 AND REPLACED IAW AMM 53-00-49-400-801-A03.Apr 20, 2015 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015051312825Seat Track · corrodedLEFT SIDE SEAT TRACK CORRODED AT BS 485 - 565, SIDE WALL. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 & 53-00-49-400-801-A03.Apr 20, 2015 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015051312824Seat Track · corrodedRIGHT SIDE FLOOR SEAT TRACK CORRODED AT BS 349 - 485. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 & 53-00-49-400-801-A03.Apr 20, 2015 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015051312823Seat Track · corrodedRIGHT SIDEWALL SEAT TRACK CORRODED AT BS 893 - 969. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.Apr 20, 2015 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015051312822Seat Track · corrodedLEFT SIDE SEAT TRACK CORRODED AT BS 708 - 761.85 SIDE WALL. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, A03 AND AMM 53-00-49-00-400-801, A03.Apr 20, 2015 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015051312821Seat Track · corrodedLT SIDE SEAT TRACK CORRODED AT BS 677 - 708 SIDE WALL. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03.Apr 20, 2015 · N751EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015051312820Intercostal · corrodedINTERCOSTAL BETWEEN BS 319-349 STR 20R HAS CORROSION. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED INTERCOSTAL AT STR 20R BETWEEN BS 319 - 349 IAW SRM 51-42-06-001-001 & SRM 51-42-21-001-001 & DWG SH670-31950. DRILL UP & INSTALL SEApr 20, 2015 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015051312819Fitting · corrodedFWD SOCK FITTING BETWEEN FRAMES 280 AND 265 LT INTERCOSTAL CORRODED LOWER FLANGE. BLENDED NOSE JACK FITTING LT INTERCOSTAL REF SRM 51-21-06-001-001. COMPLIED WITH EA 32-2015-180.Apr 19, 2015 · N751EV · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR ASOA2015051312818Frame · corrodedFRAME AT BS 319 BETWEEN 26L-26R FWD SIDE HAS CORROSION. REMOVED CORROISON BS 319 BETWEEN STR 26L AND STR 26R ON FRAME ATTACH FLANGE, WEB, AND RADIUS IAW SRM 51-21-06-001-001-A01.Apr 19, 2015 · N751EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2015051312817Floorbeam · corrodedBS 280 FWD FLOORBEAM ANGLE CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. FLOORBEAM ANGLE AT BS 280 R & R IAW SB 670BA-53-041.Apr 19, 2015 · N751EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2015051312816Bulkhead Web · corrodedBS 280, BULKHEAD WEB LT SIDE CORRODED. COMPLIED WITH EC/TC REO 670-53-11-594 AND GREO 670-53-11-594, REV DATED 04/27/2011. Apr 19, 2015 · N751EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2015051312815Bulkhead Web · corrodedF/S 280 BULKHEAD WEB RT SIDE CORRODED. COMPLIED WITH EC/TC REO 670-53-11-594 01 AND GREO 670-53-11-594, REV DATED 04/27/2011.Apr 19, 2015 · N751EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2015051312814Floorbeam · corrodedBS 280 FLOORBEAM, LT SIDE CORRODED. FLOORBEAM R & R IAW SB 670BA-53-041.Apr 19, 2015 · N751EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2015051312813Floorbeam · corrodedF/S 280, FLOORBEAM RT SIDE CORRODED. FLOORBEAM R & R IAW SB 670BA-53-041.Apr 19, 2015 · N751EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2015051312812Strap · corrodedF/S 280 CIRCUMFERENTIAL STRAP BETWEEN STR 22L-21R HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, FS 280 BUTT STRAP FROM STR 26L-26R. DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED REMAINING CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED CORROSIApr 18, 2015 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015051312811Frame · corrodedFRAME AT FS 310 BETWEEN STR 26L-26R FWD SIDE HAS CORROSION. REMOVED CORROSION AT FS 310, FRAME ATTACH ANGLE RADIUS, AND WEB FROM STR 26L TO 26R IAW SRM 51-21-06-001-001-A01. RECEIVED EA 32-2015-158 AND COMPLIED WITH EA 32-2015-158.Apr 18, 2015 · N751EV · Cndair CL6002C10 · Fuselage Main, Frame
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