N741EV

Service difficulty reports · 325

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 = 'N741EV' 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 ASOA201704111445Slat · corrodedRT WING INBD SLAT HAS CORROSION AT TELESCOPIC DUCT CONNECTION POINT. FOUND DURING GASKET REPLACEMENT. COMPLIED WITH EA 43-2017-041 AND EA 43-2017-041 FOR REPAIR OF RT INBD SLAT RIB.Apr 11, 2017 · N741EV · Cndair CL6002C10 · Leading Edge DevicesSDR ASOA201704101444Former · corrodedPAX DOOR LOWER FWD FORMER CORRODED AROUND LOWER TENSION TIE AREA. COMPLIED WITH EC/TC EA 20-2017-059 AND EA 20-2017-059. FOR REPAIR OF PAX DOOR.Apr 10, 2017 · N741EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201704081443Riser · buckledPASSENGER DOOR AFT SIDE FRAME NEAR TOP STEP BUCKLED. REMOVED AND REPLACED AFT RISER P/N 601R317071-11 IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, & DRAWING 601R317071.Apr 8, 2017 · N741EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201704061439Frame · corrodedFS 319.7 FRAME HAS CORROSION DAMAGE (FWD & AFT SIDES) STR 26L -26R. COMPLIED WITH ECTC REO 670-53-21-1407.Apr 6, 2017 · N741EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201704051438Riser · crackedFWD RISER ON PAX DOOR FOUND 2 EA. CRACKS. REPAIRED FWD RISER IAW SRM TR 52-0025, 52-11-04--201-004-A01.Apr 5, 2017 · N741EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201704041437Stiffener · crackedASD MOTOR LOWER STIFFENER CRACKED. REMOVED AND REPLACED PAX DOOR STIFFENER PER SRM 51-42-06-001-001-A01,51-40-06-001-001-A01 AND 51-40-11-001-001-A01.Apr 4, 2017 · N741EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201704041436Retainer · corrodedAVI BAY DOOR SEAL RETAINER FOUND TO BE CORRODED. REMOVED AND REPLACED AVI DOOR SEAL RETAINER PER SRM 51-42-06-001-001-A01, 51-23-00-001-001-A01.Apr 4, 2017 · N741EV · Cndair CL6002C10 · Electrical/Electronic Compartment DoorsSDR ASOA201704011434Seat Track · corrodedRT SIDE SEAT RAIL SEGMENT FROM FS 785.15-852 HAS CORROSION DAMAGE. REMOVED AND REPLACED WITH SERVICEABLE SEAT RAIL AT RT SIDE FS 785.15-852 IAW AMM 53-00-49-000-801 A17 & 53-00-49-400-801 A17 COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AApr 1, 2017 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703311433Seat Track · corrodedRT SIDE SEAT RAIL HAS CORROSION DAMAGE FS 712-761.85. REMOVED AND REPLACED WITH SERVICEABLE SEAT RAIL AT RT SIDE FS 712-761.85 IAW AMM 53-00-49-000-801 A17 & 53-00-49-400-801 A17 COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRITTEN.Mar 31, 2017 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703311432Seat Track · corrodedRT SIDE FLOOR SEAT RAIL FS 677-712 HAS CORROSION DAMAGE. REMOVED AND REPLACED WITH SERVICEABLE SEAT RAIL AT RT SIDE FS 677-712 IAW AMM 53-00-49-000-801 A17 & 53-00-49-400-801 A17 COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRITTEN.Mar 31, 2017 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703311431Seat Track · corrodedFLOOR SEAT RAIL FS 830.40-985 LBL 9 HAS CORROSION DAMAGE. REMOVED AND REPLACED WITH SERVICEABLE SEAT RAIL AT FS 830.40-985 AT LBL 9 IAW AMM 53-00-49-000-801 A17 & 53-00-49-400-801 A17 COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRITTEMar 31, 2017 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703311430Seat Track · corrodedFLOOR SEAT RAIL FS 830.40-985 RBL 9 HAS CORROSION DAMAGE. REMOVED AND REPLACED WITH SERVICEABLE SEAT RAIL AT FS 830.40-985 AT RBL 9 IAW AMM 53-00-49-000-801 A17 & 53-00-49-400-801 A17 COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRITTEMar 31, 2017 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703311429Seat Track · corrodedRT SIDE SEAT RAIL SEGMENT FROM FS 570 - 677 HAS CORROSION DAMAGE. REMOVED AND REPLACED WITH SERVICEABLE SEAT RAIL AT RT SIDE FS 570-677 IAW AMM 53-00-49-000-801 A17 & 53-00-49-400-801 A17 COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRMar 31, 2017 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703311428Seat Track · corrodedFLOOR SEAT RAIL 686.00-838.00 RBL 9 HAS CORROSION DAMAGE. REMOVED AND REPLACED WITH SERVICEABLE SEAT RAIL AT FS 686.00-838.00 AT RBL 9 IAW AMM 53-00-49-000-801 A17 & 53-00-49-400-801 A17 COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRIMar 31, 2017 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703301415Seat Track · corrodedFLOOR SEAT RAIL 686.00-838.00 LBL 9 HAS CORROSION DAMAGE. REMOVED AND REPLACED WITH SERVICEABLE SEAT RAIL AT FS 581.00-686.00 AT RBL 9 IAW AMM 53-00-49-000-801 A17 & 53-00-49-400-801 A17 COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRIMar 30, 2017 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703301414Seat Track · corrodedFLOOR SEAT RAIL 581.00-686.00 RBL 9 HAS CORROSION DAMAGE. REMOVED AND REPLACED WITH SERVICEABLE SEAT RAIL AT FS 581.00-686.00 AT RBL 9 IAW AMM 53-00-49-000-801 A17 & 53-00-49-400-801 A17 COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRIMar 30, 2017 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703291422Hinge · gougedREFER TO CO#10155817 JOB 71015587 OP 43. ASD HINGE LUGS DOOR SIDE 3 DAMAGED LUGS 6,20,23 - MTC - COMPLIED WITH EC/TC REO 670-52-91-511 AND REO 670-52-91-511.Mar 29, 2017 · N741EV · Cndair CL6002C10 · Fuselage, Door HingeSDR ASOA201703291413Seat Track · corrodedFLOOR SEAT RAIL FOUND CORRODED AT 581.00-686.00 AND LBL 9. REMOVED AND REPLACED SEAT RAIL IAW AMM 53-00-49-001-001-A03 AND EC/TC REO 670-53-00-343 AND REO 670-53-00-343.Mar 29, 2017 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201703291412Door Sill · corrodedFLOOR SILL AFT OF SERVICE DOOR HAS CORROSION. COMPLIED WITH EC/TC REO 670-53-00-390 AND REO 670-53-00-390. FOR REPAIR OF FLOOR SILL.Mar 29, 2017 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201703291411Hinge · gougedASD HINGE LUGS DOOR SIDE 3 DAMAGED LUGS 6,20,23. COMPLIED WITH EC/TC REO 670-52-91-511 AND REO 670-52-91-511.Mar 29, 2017 · N741EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201703211435Stringer Clip · corrodedFRAME CLIP CORRODED AT STR 19L FS 1015. REMOVED AND REPLACED FS 1015, STR 19L CLIP IAW SRM 51-42-06-001-001 A01, AND DRW MM670-36080.Mar 21, 2017 · N741EV · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR ASOA201701015001Pump · erraticPILOT REPORTED LEFT ENG BETWEEN 16,000 AND FL220 ENGINE WILL ROLLBACK FROM 87.2 TO 85.9. THE ENGINE WILL ROLL UP AND DOWN TILL FL220 THEN IT STABILIZES. MX REMOVED AND REPLACED FUEL PUMP ASSY ON LEFT ENGINE WITH OPERATIONAL AND LEAK CHECKS GOOD. A/C WAS APPROVJan 1, 2017 · N741EV · Cndair CL6002C10 · Engine Fuel PumpSDR ASOA201612273091Engine · power lossTHE CREW REPORTED DURING CLIMB BETWEEN 18000-21000 FT, THE LEFT ENGINE N1 ROLLED BACK FROM 86.7% TO 83.9% 5 TIMES. ALL OTHER ENGINE INDICATIONS WERE NORMAL. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE FADEC AND THE NR 1 ENGINE FUEL METTERING UNIT,AND TDec 27, 2016 · N741EV · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR ASOA2016090515357Lens · brokenLEFT SIDE EXTERIOR EMERGENCY LIGHT LENS COVER IS BROKEN. REMOVED AND REPLACED THE LENS COVER IAW AMM 33-51-15, OPS CHECKED GOOD.Sep 5, 2016 · N741EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015111714063Lamp · burned outGALLEY LOWER AFT EXIT, COURTESY LIGHT HAVE 2 LIGHT BULBS BURNED. RELAMPED GALLEY AFT EXIT SIGN IAW GMM 3-8, OPS CHECKED GOOD.Nov 17, 2015 · N741EV · Cndair CL6002C10 · Passenger Compartment LightingSDR ASOA2015111714062Lamp · burned out12 AB LOWER EXIT SIGN HAVE 2 LIGHT BULBS BURNED. RELAMPED 2 BULBS AT 12 AB EXIT SIGN IAW GMM 3-8. OPS CHECKED GOOD.Nov 17, 2015 · N741EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015100813874Bulb · burned outISLE OVERHEAD EMERGENCY LIGHT INOPERATIVE AT SEATS 10B,C. REMOVED INOPERATIVE BULB AND INSTALLED NEW BULB IAW AMM 33-51-09, OPS CHECK GOOD.Oct 8, 2015 · N741EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015091713776Battery Pack · dischargedCAPTAIN'S FLASHLIGHT INOPERATIVE. REPLACED BATTERIES IN CAPTAIN'S FLASHLIGHT AND OPS CHECK GOOD IAW AMM 25-61-00. ACFT OK FOR SERVICE.Sep 17, 2015 · N741EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2015032012438Engine · contaminatedSMOKE AFT LAV WARNING AFTER TAKEOFF. A DISTINCT ODOR WAS NOTICED THROUGHOUT THE ENTIRE ACFT WHICH SMELLED LIKE SOMETHING WAS BURNING. ACFT RETURNED TO DEPARTURE AFTER T/O. PERFORMED ENGINE DRYOUT IAW AMM 72-00-00 TO DRY COMPRESSOR WASH FLUID.Mar 18, 2015 · N741EV · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR ASOA2014081311056Stringer · chafedSTRINGER 7R BS 1144 IS CHAFED. BLENDED OUT DAMAGE IAW SRM 51-12-00-001-001-A01AND SRM 5-51-16. MAJOR REPAIR.Aug 10, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2014081311055Stringer · corrodedSTRINGER 18R CORRODED FROM BS 280-287. . REMOVED SECTION OF STRINGER IAW SRM 51-42-06-001-001 & SRM 51-42-21-001-001. REPAIRED IAW EA 12-2014-167 REV A2. MAJOR REPAIR.Aug 4, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2014081311054Intercostal · chafedCHAFE DAMAGE ON WEB OF INTERCOSTAL BETWEEN BS 1144 - 1154.48. DRILLED UP NEW INTERCOSTAL IAW SRM 51-40-11001-001-DWG MM670-360-86. MAJOR REPAIR.Aug 2, 2014 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014081311053Light · deterioratedRIGHT NR 7 EMERGENCY LIGHT TRACK DELAMINATED. REMOVED AND REPLACED THE EMERGENCY LIGHT TRACK IAW AMM 33-51-01, REV A.Jul 31, 2014 · N741EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2014080611023Stringer Splice · corrodedSTRINGER SPLICE 25R AT BS 333 CORRODED OUT OF LIMITS. REMOVED AND REPLACED IAW SRM 51-42-06-001-001-A01, 51-42-06-001-001-A01 AND DWG SH670-32420.Jul 31, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2014081311052Stringer Splice · corrodedSTRINGER SPLICE 18R CORRODED BS 284 - 292. REPAIRED IAW EA 12-2014-167.Jul 29, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2014081311051Stringer · corrodedSTRINGER 27 CORRODED BS 295. REMOVED STRINGER BETWEEN BS 280 - 295 IAW SRM 51-42-06-001-001-A01. INSTALLED NEW STRINGER IAW SRM 51-42-06-001-001-A01. MAJOR REPAIR.Jul 25, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2014080611022Stringer Splice · corrodedSTRINGER 26R FWD SPLICE FOUND TO BE CORRODED BETWEEN BS 329-333. BLENDED CORROSION, AND FOUND TO BE IN A NO DAMAGE ALLOWED AREA IN REF TO SRM 53-21-03-101 & 51-21-06-001-001. INSTALLED NEW STRINGER SPLICE IAW SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A0Jul 24, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2014081311050Stringer · corrodedSTRINGER 26L CORRODED BS 282. CUT & REMOVED SECTION OF STRINGER BETWEEN BS 280 - 302.5 IAW SRM 53-00-03-201-001, SRM 53-00-53-201-001 AND SRM 53-00-003-201-001-A01. INSTALLED NEW SECTION OF STRINGER IAW SRM 53-00-03-201-001-A01 AND EA 32-2014-040 REV A.Jul 23, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2014081311049Stringer · corrodedSTRINGER 25R CORRODED BS 282. REPAIRED IAW SRM 53-00-03-201-001-A01. MAJOR REPAIR.Jul 23, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2014080611021Angle · corrodedSERVICE DOOR FLOOR PROTECTOR ANGLE CORRODED. REPLACED ANGLE IAW SRM 51-42-06-001-001, SRM 51-42-02-001, 51-42-06-001-001-A01 & 51-42-21-001-001-A01.Jul 23, 2014 · N741EV · Cndair CL6002C10 · Service DoorsSDR ASOA2014080611020Angle · corrodedSERVICE DOOR LOWER SILL ANGLE CORRODED. REMOVED LOWER SILL ANGLE ON SERVICE DOOR IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED LOWER SILL ANGEL AND UPPER SILL ANGLE IAW SRM 51-42-06-001-001-A0Jul 22, 2014 · N741EV · Cndair CL6002C10 · Service DoorsSDR ASOA2014080611019Skin · corrodedCORROSION AROUND NUTPLATES IN ASD INNER SKIN UNDER ACCESS PANEL 832AB. REMOVED CORROSION AROUND NUTPLATES ON ASD INNER SKIN IAW SRM 51-21-06-001-001. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.Jul 20, 2014 · N741EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014080611018Bulkhead Web · corrodedRIGHT FS 280 WEB CORRODED. INSTALLED RT STRAP TO RT WEB IAW REO 670-53-11-594. COMPLIED WITH REO 670-53-11-594, REV-DATED 2011/04/27 AS NEEDED.Jul 18, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014080611017Floor Support · corrodedRIGHT CABIN FLOOR SUPPORT CORRODED FROM BS 286-319.7. COMPLIED WITH REO 670-53-00-390.Jul 18, 2014 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014080611016Floor Support · crackedFOUND THE RT COCKPIT FLOOR SUPPORT ANGLE TO BE CRACKED AT FS 278. R & R RT COCK PIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01, SRM TR-53-0057 & DWG CC670-33199.Jul 17, 2014 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014080411007Floorbeam · crackedFOUND THE LT COCKPIT FLOORBEAM ANGLE TO BE CRACKED AT FS 278. R & R THE SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01, SRM TR-53-005 & DWG CC670-33199, REV B.Jul 17, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014081311048Stringer · corrodedSTRINGER 26R, BS 333-349 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06-001-001-A01 & DWG SH670-31350.Jul 16, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2014081311047Strap · corrodedFRAME STRAP BS 333 CORRODED BETWEEN 25-26R. REMOVED CORROSION IAW SRM 51-21-00-001-001-A01. COMPLIED WITH EA 32-2014-021.Jul 16, 2014 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014080611015Bulkhead Web · corrodedRIGHT FS 280, WEB CORRODED. COMPLIED WITH ECTC REO 670-53-11-597 01 AND GREO 670-53-11-594, REV.Jul 16, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014080611014Floorbeam · corrodedCOCKPIT FLOOR AFT SUPPORT ANGLE CORRODED. REMOVED CORRODED COCKPIT FLOOR SUPPORT ANGLE AND REPLACED WITH SERVICEABLE COCKPIT FLOOR AFT SUPPORT ANGLE AS NEEDED IAW SB 670BA-53-041, REV D DATED 12 MAR 14.Jul 16, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
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