N740EV

Service difficulty reports · 282

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 = 'N740EV' 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 ASOA201703171340Seat Track · corrodedRT SIDE SEAT RAIL AT FS 573-674 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND EC/TC REO 670-53-00-343.Mar 17, 2017 · N740EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703171339Seat Track · corrodedSEAT TRACK CORRODED RBL9 FS 581.00-682.00. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (803), 53-00-49-400-801 (803) AND EC/TC REO 670-53-00-343.Mar 17, 2017 · N740EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703161364Doubler · crackedPAX DOOR INTERNAL PULL IN CAM DOUBLER CRACKED UPPER AFT SIDE. REMOVED AND REPLACED CAM DOUBLER IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.Mar 16, 2017 · N740EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201703151403Frame · corrodedFS 295 FRAME AFT SIDE BETWEEN STR 26L TO 26R HAS CORROSION. REMOVED CORROSION FROM FS 295 FRAME AFT SIDE AND BETWEEN STR 26L TO STR 26R IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS CHECK; MATERIAL REMOVED .003", ORIGINAL .050", REMAINING .047" PER NDMar 15, 2017 · N740EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201703151368Intercostal · corrodedINTERCOSTAL CORRODED IN PAX DOOR BELOW OUTER HANDLE HOUSING (FIG 52-11-06-991-801 ITEM 33). REMOVED AND REPLACED PER SRM 51-42-00-001-001-A01, 51-42-06-001-001-A01, 51-40-11-001-001-A01.Mar 15, 2017 · N740EV · Bombdr CL6002D15 · Passenger/Crew DoorsSDR ASOA201703151367Intercostal · corrodedINTERCOSTAL ABOVE LOWER CONTROL ROD PIVET CORRODED. REMOVED AND INSTALLED PER SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-21-001-001-A01.Mar 15, 2017 · N740EV · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR ASOA201703151366Seat Track · corrodedRT SIDE SEAT TRACK, BS 785 - 862 IS CORRODED IN MULTIPLE AREAS. REMOVED THE SEAT TRACK, FABRICATED A NEW SEAT TRACK AND INSTALLED IAW AMM 53-00-49-000-801 (A03), 53-00-49-400-801 (A03) AND ECTC REO 670-53-00-343.Mar 15, 2017 · N740EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703151365Seat Track · corrodedLEFT SIDE SEAT TRACK BS 785 - 861 IS CORRODED IN MULTIPLE AREAS. REMOVED THE SEAT TRACK, FABRICATED A NEW SEAT TRACK & INSTALLED IAW AMM 53-00-49-000-801 (A03), 53-00-49-400-801 (A03) AND ECTC REO 670-53-00-343.Mar 15, 2017 · N740EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703151357Seat Track · corrodedRT SIDE SEAT RAIL AT FS 713-761 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND ECTC REO 670-53-00-343.Mar 15, 2017 · N740EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703151356Seat Track · corrodedLT SIDE SEAT RAIL AT FS 713-761 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND ECTC REO 670-53-00-343.Mar 15, 2017 · N740EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703151355Intercostal · corrodedINTERCOSTAL CORRODED ABOVE AND AFT OF MID PIVOT (FIG 52-11-06-991-801 ITEM 73). REMOVED AND REPLACED WITH SERVICEABLE ONE PER SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-40-11-001-001-A01.Mar 15, 2017 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201703151349Seat Track · corrodedLT SIDE SEAT RAIL AT FS 861-969 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND ECTC REO 670-53-00-343.Mar 15, 2017 · N740EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703151347Seat Track · corrodedRT SIDE SEAT RAIL AT FS 861-969 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND ECTC REO 670-53-00-343.Mar 15, 2017 · N740EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703151345Seat Track · corrodedRT SIDE SEAT RAIL AT FS 674-713 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND EC/TC REO 670-53-00-343.Mar 15, 2017 · N740EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703151344Seat Track · corrodedLT SIDE SEAT RAIL AT FS 481-573 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND EC/TC REO 670-53-00-343.Mar 15, 2017 · N740EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703151343Seat Track · corrodedRT SIDE SEAT RAIL AT FS 481-573 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND EC/TC REO 670-53-00-343.Mar 15, 2017 · N740EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703151342Seat Track · corrodedLT SIDE SEAT RAIL AT FS 573-674 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND EC/TC REO 670-53-00-343.Mar 15, 2017 · N740EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703151341Seat Track · corrodedLT SIDE SEAT RAIL AT FS 674-713 IS CORRODED IN MULTIPLE AREAS. REMOVED SEAT TRACK, FABBED A NEW ONE FROM STOCK MATERIAL AND INSTALLED PER AMM 53-00-49-000-801 (A17), 53-00-49-400-801 (A17) AND EC/TC REO 670-53-00-343.Mar 15, 2017 · N740EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703151336Floorbeam · corrodedBS 280 CRAWLWAY FLOORBEAM ANGLE HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDED AREAS ARE WITHIN ALLOWABLE LIMITS IAW SRM 53-00-00-101-001-A01.Mar 15, 2017 · N740EV · Cndair CL6002C10 · Fuselage Structure (General)SDR ASOA201703151335Seat Track · corrodedRT SIDE SEAT TRACK BS 379 - 481 IS CORODED IN MULTIPLE AREAS. COMPLIED WITH EC/TC REO 670-53-00-343, AND GREO 670-53-00-343 REV M. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A17, AND 53-00-48-400-801 A17Mar 15, 2017 · N740EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703141405Riser · corrodedPAX DOOR FORWARD RISER IS CORRODED IN MULTIPLE AREAS. BLENDED CORROSION ON FWD RISER AND FOUND TO BE OUT OF LIMITS IAW SRM 52-00-01-101-001-A01. REMOVED AND REPLACED FWD RISER PER SRM 51-42-12-001-001-A01 AND DWG 601R31707. THIS IS A MAJOR REPAIR.Mar 14, 2017 · N740EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201703141402Frame · corrodedFS 295 FRAME AFT SIDE BETWEEN STR 26L TO 26R HAS CORROSION. REMOVED CORROSION FROM FS 295 FRAME AFT SIDE AND BETWEEN STR 26L TO STR 26R IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS CHECK; MATERIAL REMOVED .003", ORIGINAL .050", REMAINING .047" PER NDTMar 14, 2017 · N740EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201703141395Riser · crackedPAX DOOR AFT RISER IS CRACKED AT BOTTOM FWD STEP. PAX DOOR REPLACED AFT RISER AND STIFFENER IAW SRM 51-42-06-001-001 A01 AND 51-40-11-001-001 A01.Mar 14, 2017 · N740EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201703141363Doubler · corrodedTCAS ANTENNA DOUBLER HAS CORROSION. REMOVED AND REPLACED THE DOUBLER IAW SRM 57-42-06-001-001-A01.Mar 14, 2017 · N740EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201703141362Intercostal · corrodedASD INTERCOSTAL UNDER PRESSURE VENT FLAP IS CORRODED. REMOVED AND REPLACED IAW SRM 51-42-00-001-001-A01.Mar 14, 2017 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2016080415156Bulb · burned outLOWER EXIT SIGN BY MAIN ENTRANCE HAD ONE BULB BURNED. REPLACED THE LAMP IAW AMM 33-51-05. OPS CHECKED GOOD.Jul 31, 2016 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2016080415155Bulb · burned outROW 12 CD LOWER EXIT SIGN HAD ONE LIGHT BULB BURNED. REPLACED THE BULB IAW AMM 33-51-05. OPS CHECKED GOOD.Jul 31, 2016 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2016071915127Fire Detector · false indicationAT 2000 FT, RECEIVED RT ENGINE FIRE WARNING. COMPLIED WITH IMMEDIATE ACTION CHECKLIST AND QRH PROCEDURES AND RETURNED TO LAND. LANDED AT LESS THAN 100 FPM ON THE 63000 LB CART. ACFT RETURNED TO DEPARTURE, FALSE FIRE WARNING DURING FLIGHT. REMOVED AND REPLJul 19, 2016 · N740EV · Cndair CL6002C10 · Detection SystemSDR ASOA2016050414754Megaphone · inoperativeMEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14. OPS CHECKED GOOD.May 4, 2016 · N740EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2015112814142Wire · disconnectedTHE EMERGENCY EXIT SIGN FOR THE FORWARD CABIN SERVICE DOOR DS173, FAILED THE OPS TEST. FOUND WIRES TO EMERGENCY EXIT SIGN DS173 FOR THE FORWARD CABIN SERVICE DOOR TO BE DISCONNECTED. CONNECTED WIRE IAW AMM, OPS TEST OF EMERGENCY LIGHTS NOW GOOD. OPS TEST OF Nov 28, 2015 · N740EV · Cndair CL6002C10 · Light System WiringSDR ASOA2014081511088Battery Pack · dischargedEMERGENCY LIGHTS FAILED OPS TEST. TROUBLESHOT IAW FIM 33-51-00-810-804 AND FOUND ESPU BATTERY PACK NR 3 & NR 4 TO BE UNSERVICABLE. REPLACED BATTERY PACK IAW 33-51-17-400-801. PERFORMED OPS CHECK TASK 33-51-17-710-801, OPS TESTED GOOD OK TO CLOSE PANEL 273AAug 11, 2014 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2014081511087Riser · crackedDISCOVERED FWD RISER CRACKED AT BOTTOM PAX DOOR STEP. REPAIRED IAW EA 32-2014-043.Jul 31, 2014 · N740EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014081511086Panel · damagedPANEL 631DZ HAS ONE ELONGATED HOLE. FURTHER INVESTIGATION FOUND THAT UNDERLYING STRUCTURE WAS DRILLED INTO. REMOVED LOWER ANGLE AT SLAT TRACK 2-3 AND SEAL ASSY, INSPECTED SLAT TACK RIB AND FOUND NO DAMAGE BLENDED SMALL DRILL START FROM ANGLE, REPAIRED IAW REJul 30, 2014 · N740EV · Cndair CL6002C10 · Wing, Plate/SkinSDR ASOA2014081511085Unknown · damagedWHILE PERFORMING SB 670BA-57-015 01 ON RT SIDE GO-NO-GO GAUGE GOES ALL THE WAY IN TOP AND BOTTOM HOLE LOCATIONS. REPAIRED IAW REO 670-57-21-721.Jul 25, 2014 · N740EV · Cndair CL6002C10 · Wing StructureSDR ASOA2014081511084Floor Support · crackedRT COCKPIT FLOOR SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED RT COCKPIT FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, SRM 51-42-06-001-001, AND DWG CC670-33199.Jul 24, 2014 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014081511083Floor Support · crackedLT COCKPIT FLOOR SUPPORT IS CRACKED. REMOVED AND RPLACED FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01 AND DWG CC670-33199. MAJOR REPAIR.Jul 24, 2014 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014081511081Lock Fastener · missingON REMOVAL OF RT SIDEWALL SEAT TRACK BS 785.15-FS 863.00 FOUND TWO LOCK FASTENERS MISSING. INSTALLED THE LOCK FASTERNERS IAW SRM 51-42-20-001-001-A01. MAJOR REPAIR.Jul 23, 2014 · N740EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014081511080Bulkhead Web · corrodedRT BS 280 BULKHEAD WEB IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. FABRICATED RT LOWER WEB AND RT BUTTSTRAP IAW REO 670-53-11-594. MAJOR REPAIR.Jul 21, 2014 · N740EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014081511079Bulkhead Web · corrodedLT 280 BULKHEAD WEB IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. FABRICATED LT LOWER WEB AND LT BUTTSTRAP IAW REO 670-53-11-594. MAJOR REPAIR.Jul 21, 2014 · N740EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014081511078Bracket · corrodedCORROSION FOUND ON FLOOR BRACKET. R & R BRACKET IAW DWG SH670-31996 AND SRM 51-42-06-001-001-A01Jul 20, 2014 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014081511077Seat Track · corrodedRT SIDE SEAT TRACK CORRODED AT BS 785.15. REMOVED SEAT TRACK FROM BS 785.15 - 863 IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.Jul 20, 2014 · N740EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014081511076Seat Track · corrodedLT SIDE SEAT TRACK CORRODED AT APPROX BS 785.15. REMOVED SEAT TRACK FROM BS 784 - 861 IAW AMM 53-00-49-000-801-403. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801, A03.Jul 20, 2014 · N740EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014081511075Floorbeam · corrodedCORROSION ON FLOORBEAM AROUND SCREW HOLE BS 333, LBL 16. REPAIRED IAW EC/TC EA 25-2014-237 AND EA 25-2014-237. MAJOR REPAIR.Jul 19, 2014 · N740EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014081511074Angle · corrodedPAX DOOR LOWER SILL MID CAP ANGLE CORRODED. REMOVED FWD & AFT CAP ANGLES IAW SRM 51-42-06-001-001-A01. FOUND TO BE CORRODED, REPLACE FWD AND AFT CAP ANGLES. INSTALLED FWD & AFT CAP ANGLES, SRM 51-42-06-001-001-A01 PAX DOOR LOWER SILL REF DWG SH 670-31821.Jul 19, 2014 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014081511073Angle · corrodedPAX DOOR CUTOUT LOWER SILL KICKPLATE ANGLE HAS CORROSION DAMAGE AT FWD END. REMOVED KICKPLATE ANGLE FROM PAX DOOR OBTAINED NEW ANGLE LOCATED DRILL HOLES, DEBURED AS REQUIRED AND INSTALLED NUTPLATES IAW SRM 51-40-11-001-001, 51-45-00-001-001. INSTALLED KICKPJul 19, 2014 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014081511072Floorbeam · corrodedPACKER CORRODED ON BS 310 FLOORBEAM, LBL 4. REMOVED PACKER IAW SRM 51-42-06-001-001-A01. INSTALLED NEW PACKER IAW SRM 51-42-06-001-001-A01.Jul 19, 2014 · N740EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014081511071Floorbeam · corrodedPACKER CORRODED ON FS 333 FLOORBEAM, RBL 8. REMOVED PACKER IAW SRM 51-42-06-001-001-A01. INSTALLED NEW PACKER IAW SRM 51-42-06-001-001.Jul 19, 2014 · N740EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014081411067Floor Support · corrodedCORROSION FOUND ON RT FLOOR SUPPORT BS 349-364. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.Jul 19, 2014 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014081411066Door Sill · corrodedDOOR SILL BS 319-349 IS CORRODED. REMOVED AND REPLACED DOOR SILL IAW SRM 51-42-06-001-001-A01, 51-42-06-001-001-A01, AND DWG SH670-31996.Jul 19, 2014 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014081411065Skin · chafedFUSELAGE SKIN CHAFED JUST AFT OF BS 977 STRINGER 27. BLENDED DAMAGE IAW RM (TR) 51-12-00-001-001-A01, & REO 670-53-00-290, REV C.Jul 18, 2014 · N740EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
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