N744EV

Service difficulty reports · 326

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 = 'N744EV' 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 ASOA2014091811261Floor Support · corrodedFLOOR SUPPORT HAS CORROSION BS 333 RBL 9. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, SRM. REPAIRED IAW REO 670-53-21-1123. MAJOR REPAIR.Aug 30, 2014 · N744EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014091811260Floor Support · corrodedFLOOR SUPPORT HAS CORROISON AT FWD END OF ASD, NEAR BS 310. INSTALLED NEW FLOOR SUPPORT IAW DWG SH670-31810 AND SRM 51-42-06-001-001-A01. MAJOR REPAIR.Aug 30, 2014 · N744EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014091811259Door Sill · corrodedPAX DOOR SILL HAS CORROSION SEVERAL PLACES AT BS 310-349. INSTALLED NEW DOOR SILL IAW DWG SH670-31810 AND SRM 51-42-06-001-001-A01. MAJOR REPAIR.Aug 30, 2014 · N744EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014091711255Floor Support · corrodedFLOOR SUPPORT HAS CORROSION AT LBL 9 AT BS 333. R & R PACKER IAW DWG SH670-32120 AND SRM 51-42-06-001-001. MAJOR REPAIR.Aug 30, 2014 · N744EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014091711254Floor Support · corrodedFLOOR SUPPORT HAS CORROSION AT BS 320 AT RBL 45. REMOVED THE SERVICE DOOR LOWER SILL ANGLE, REFERRED TO AS UPPER SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. DRILLED AND INSTALLED FLOOR SILL UPPER SUPPORT KOT MOUNTING ANGLE IAW SRM 51Aug 30, 2014 · N744EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014091711253Floor Support · corrodedFLOOR SUPPORT HAS CORROSION AT RBL 45 AT BS 319. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 670-53-21-1125. FABRICATED ANGLES FOR REPAIR IAW SRM 51-24-21-001-001-A01 FROM 70750-0.063" & REO 670-53-21-1125.Aug 30, 2014 · N744EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014091711252Structure · corrodedCORROSION ON PACKER ON FLOOR SUPPORT AT FS 333 AT LBL9. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED PACKER CORROSION IAW SRM 51-21-06-001-001-A01 MATERIAL REMOVED EXCEED LIMITS. INSTALLED NEW PACKER ON FLOOR SUPPORT AT FS 333 ON IAW SAug 30, 2014 · N744EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014091711251Hinge · deterioratedAFT MLG DOOR HINGE FWD HOLE IS OVERSIZED OVER SB 670BA-57-020 LIMITS. REMOVED AFT LANDING GEAR DOOR HINGE AND FASTENERS IAW SRM 51-42-21-001-001-A01. COMPLIED WITH REO 670-57-21-734 P-1. DRILLED BRUSH CAD, AND RESTORED FINISH TO NEW SERVICEABLE FITTING, IAAug 27, 2014 · N744EV · Cndair CL6002C10 · Landing Gear DoorsSDR ASOA2014091611250Seat Track · corrodedLEFT SEAT TRACK BS 813 - 985 CORRODED IN SEVERAL AREAS ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 (A03), AMM 53-00-49-400-801 (A03).Aug 25, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611249Seat Track · corrodedRIGHT SEAT TRACK BS 693 - 813 CORRODED IN SEVERAL AREAS ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 (A03), EC/TC 670-53-00-343 BP570692, AND AMM 53-00-46-400-801-A03.Aug 25, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611248Seat Track · corrodedLEFT SEAT TRACK BS 693 - 813 CORRODED ALONG THE LENGTH THE TRACK. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-000-801(A03) AND AMM 53-00-49-400-801-A03.Aug 25, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611247Seat Track · corrodedRIGHT SEAT TRACK BS 813 - 985 CORRODED IN SEVERAL AREAS ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801(A03), AMM 53-00-49-400-801-A03, AND REO 670-53-00-343.Aug 25, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611246Seat Track · corrodedRIGHT SEAT TRACK FROM BS 581 - 677 CORRODED AND SCRATCHEED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, SRM 53-31-49-101-001-A01, AND AMM TASK 53-00-49-400-801.Aug 21, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611245Seat Track · corrodedLEFT SEAT TRACK BS 581 - 677 CORRODED AND SCRATCHED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-00-49-000-801-A03, AND SRM 51-45-00-001-001-A01. MAJOR REPAIR.Aug 21, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611244Floorbeam · crackedDURING INSTALLATION OF THE BS 280 FLOORBEAM, FOUND A CRACKED ANGLE AT RBL38.50. REMOVED THE DAMAGED ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED SERVICEABLE ANGLE FABRICATED IAW SNIEO CC670-34010, EXCEPT WHERE ALTERNATE FASTENERS WERE SPECIFIED BY SB 670BAAug 21, 2014 · N744EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014091611242Seat Track · corrodedRIGHT SEAT TRACK BS 485 - 581 CORRODED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, REO 670-53-00-343, REV F, AND AMM 53-00-49-400-801. MAJOR REPAIR.Aug 21, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611241Seat Track · corrodedLEFT SEAT TRACK BS 517-581 CORRODED AND SCRATCHED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, REO 670-53-00-343, GREO 670-53-00-343 REV F, AND AMM 53-00-49-400-801.Aug 21, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611240Seat Track · corrodedRIGHT SEAT TRACK BS 349 - 485 CORRODED AND SCRATCHED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-900-801, REO 670-53-00-343, REV F, AND AMM 53-00-49-400-801. MAJOR REPAIR.Aug 21, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611239Seat Track · corrodedRIGHT SEAT TRACK BS 379 - 485 CORRODED AND SCRATCHED ALONG THE ENTIRE LENGTH. THIS REPAIR IS CLASSIFIED AS A REMOVED AND REPLACED THE SEAT TRACK IAW AMM TASK 53-00-49-000-801, REO 670-53-00-343, GREO 670-53-00-343, REV F, AND AMM TASK 53-00-49-400-801. MAAug 21, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611238Seat Track · corrodedLEFT SEAT TRACK BS 379 - 485 CORRODED AND SCRATCHED ALONG THE LENGTH OF THE TRACK. R & R THE SEAT TRACK IAW AMM 53-00-49-000 AND AMM 53-00-49-400-801. MAJOR REPAIR.Aug 21, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611237Seat Track · corrodedRIGHT SEAT TRACK BS 485 - 570 CORRODED ALONE THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801. MAJOR REPAIR.Aug 21, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611236Seat Track · corrodedLEFT SEAT TRACK BS 485 - 570 IS CORRODED AND SCRATCHED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801. MAJOR REPAIR.Aug 21, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611235Seat Track · corrodedSEAT TRACK BS 860 - 969 CORRODED & SCRATCHED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.Aug 21, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611234Seat Track · corrodedSEAT TRACK BS 860 - 969 CORRODED & SCRATCHED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801. MAJOR REPAIR.Aug 21, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611233Seat Track · corrodedSEAT TRACK BS 785-860 CORRODED ALONG THE LENGTH OF THE TRACK. R & R THE SEAT TRACK IAW AMM TASK 53-00-49-000-801, & REO 670-53-00-343, REV F. MAJOR REPAIR.Aug 21, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611232Seat Track · corrodedSEAT TRACK BS 785 - 860 CORRODED & SCRATCHED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, AMM 53-00-49-40-801, AND EC/TC REO 670-53-00-343.Aug 21, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611231Seat Track · corrodedSEAT TRACK BS 712 - 761 CORRODED ALONG THE LENGTH OF THE TRACK. R & R SEAT TRACK IAW AMM 53-00-49-000 AND 400-801-A03.Aug 21, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611230Seat Track · corrodedSEAT TRACK BS 712 - 761 CORRODED & SCRATCHED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801. MAJOR REPAIR.Aug 21, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611229Seat Track · corrodedSEAT TRACK BS 570 - 675 CORRODED & SCRATCHED ALONG THE LENGTH OF THE TRACK. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.Aug 21, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091011212Seat Track · corrodedSEAT TRACK BS 675 - 712 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. R & R SEAT TRACK IAW AMM TASKS 53-00-49-000-801, 53-00-49-400-801, AND REO 670-53-00-343.Aug 21, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611228Seat Track · corrodedSEAT TRACK BS 570 - 675 CORRODED & SCRATCHED ALONG THE LENGTH OF THE TRACK. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01, FIG 53-31-49-991-804. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 A03 AND AMM TASK 53-00-49-400-801.Aug 20, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014091611227Bulkhead Web · corrodedDURING ACCOMPLISHEMENT OF SB FOUND RT BULKHEAD LOWER WEB BS 280 CORRODED. BLENDED CORROSION DAMAGE IAW SRM 51-21-06-001-001-A01 DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. COMPLIED WITH REO 670-53-11-594. LOCATED & DRILLED UP HOLES IN STAug 19, 2014 · N744EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014091611226Bulkhead Web · corrodedDURING ACCOMPLISHMENT OF SB FOUND LT BULKHEAD LOWER WEB BS 280 CORRODED. BLENDED CORROSION DAMAGE IAW SRM 51-21-06-001-001-A01. FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. R & R BULKHEAD WEB IAW REO 670-53-11-594. LOCATED & DRILLED UP HOAug 19, 2014 · N744EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014091611225Hinge · gougedPAX DOOR HINGE HAS TWO LUGS GOUGED NR 14 AND NR 23 COUNTING FWD TO AFT. REPAIRED IAW REO 670-52-11-511. MAJOR REPAIR.Aug 17, 2014 · N744EV · Cndair CL6002C10 · Fuselage, Door HingeSDR ASOA2014091611243Light · deterioratedEMERGENCY LIGHT WORN & FADED. R & R THE EMERGENCY LIGHT IAW AMM 33-51-01-000-801, 33-51-01-400-801, AND AMM 33-51-01, REV A.Aug 16, 2014 · N744EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2014091811268Skin · damagedFOUR BURNED FASTENERS ON STRINGER 24L BETWEEN FS 1031 AND 1070.70. REMOVED 4 EA BLIND FASTENERS IAW SRM 51-42-10-001-001-A01 AND 53-00-00-201-003-A01, STEP 3.C 1, A. EVALUATED 4EA FASTNER HOLES FOR PERMANENT REPAIR DISPOSITION. REMOVED SEALANT FROM 4EA FASTAug 15, 2014 · N744EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2014091811267Skin · dentedDENT RT FUSELAGE BETWEEN FS 409 AND FS 421 BETWEEN STR 16R AND 17R. COMPLIED WITH EC/TC EA 32-2014-060 PERMANENT REPAIR. EVALUATED DAMAGE AND SUBMITTED TO STS ENGINEERING FOR PERMANENT REPAIR. COMPLIED WITH STS EA 32-2014-060. RECEIVED AND COMPLIED WITH ECAug 15, 2014 · N744EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2014040410272Lamp · burned outNR 5 LT AFT, EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMPS IAW AMM 33-51-15, OPS CHECKED GOOD.Apr 1, 2014 · N744EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2014030610074Lens · damagedEMERGENCY EXIT SIGN BY FWD ENTRY DOOR. R & R EMERGENCY EXIT SIGN COVER/LENS BY FWD ENTRY DOOR IAW AMM 33-51-05, NEF CLEARED.Mar 4, 2014 · N744EV · Cndair CL6002D24 · Emergency LightingSDR ASOA2013060503758Drag Angle · crackedPAX DOOR DRAG ANGLE, AFT SIDE, CRACKED, MARKED. REPAIRED IAW 601R-31772-5.Jun 1, 2013 · N744EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2013012102861Door · out of adjustCATERING REPORTS THAT SERVICE DOOR IS DIFFICULT TO OPEN & CLOSE. ADJUSTED SERVICE DOOR. LINAGE IAW AMM 52-41-00. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.Jan 19, 2013 · N744EV · Cndair CL6002C10 · Service DoorsSDR ASOA2013012102859Door · lack of lubeSERVICE DOOR IS VERY DIFFICULT TO OPEN FROM THE OUTSIDE. LUBRICATED DOOR IAW AMM TASK 12-20-52-640-801-A01. OPS CHECKED GOOD, NO FURTHER DEFECTS NOTED AT THIS TIME.Jan 18, 2013 · N744EV · Cndair CL6002C10 · Service DoorsSDR ASOA2012121202640Control Panel · unserviceableAILERON AND RUDDER TRIM UNCOMMANDED DEFLECTIONS. EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE. R & R AILERON/RUDDER TRIM CONTROL PANEL IAW 700 27-12-10. PERFORMED OPS TEST OF AILERON/RUDDER TRIM IAW AMM 27-11-00-710-802 AND 27-22-00-710-801. NO FAULTS FDec 8, 2012 · N744EV · Cndair CL6002C10 · Aileron Control SystemSDR ASOA2012101802358Flap System · failedFLAPS FAIL & SLATS FAIL. RAN QRH AND FAULTS CLEARED. EMERGENCY DECLARED. SYSTEM RESET IAW MCC, NO FURTHER ACTION REQUIRED.Oct 12, 2012 · N744EV · Cndair CL6002C10 · Trailing Edge Flap Control SystemSDR ASOA2012071301893Sill · corrodedAFT CARGO DOOR SILL CORRODED. REPAIRED IAW SRM 51-42-06-001-001-A01.Jul 6, 2012 · N744EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012071301892Stringer · corrodedAVIONICS COMPARTMENT, STRINGER 26R IS CORRODED BETWEEN BS 333-349. REMOVED AND REPLACED STRINGER IAW SRM 51-42-06-001-001-A01.Jul 5, 2012 · N744EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012071001882Stringer · corrodedSTRINGER 26R IS CORRODED BETWEEN FS 319 - 333. APPLIED FINISH COAT TO ALL BARE FASTENERS SRM 5142-06-001-001-A01.Jul 5, 2012 · N744EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012062801834Floor Panel · crackedRIGHT ELECTRICAL BAY FLOOR AT FS 193 IS CRACKED. REPAIRED IAW REO 670-53-11-509.Jun 27, 2012 · N744EV · Cndair CL6002C10 · Fuselage Floor PanelSDR ASOA2012070901874Floor Support · corrodedAFT CARGO RT FLOOR SUPPORT IS CORRODED BETWEEN FS 1031 - 1051. REMOVED CORROSION DAMAGE IAW SRM 51-21-06-001-001-A01 AND FOUND TO BE OUT OF LIMITS IAW SRM 51-61-43-101-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDUREJun 26, 2012 · N744EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012070901873Floor Support · corrodedAFT CARGO RT FLOOR SUPPORT IS CORRODED BETWEEN FS 1015 - 1031. REMOVED CORROSION DAMAGE IAW SRM DAMAGE IAW SRM 51-21-06-001-001-A01 AND FOUND AREA TO OUT OF LIMITS IAW SRM 51-61-43-101-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INJun 26, 2012 · N744EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
Back to N744EV