N743FD

Service difficulty reports · 263

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 = 'N743FD' 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 08FDEA02955Attach Fitting · damagedELONGATED HOLES FOUND AT STRINGER COUPLING 5 AND 13, C 40 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 17, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 08FDEA02953Skin · corrodedFOUND CORROSION ON LT WING TOP SKIN RIB 26-27 LT REPAIR PERFORMED BY BLEND OUT CORROSION, NDT FOR CORROSION FREE CONDITION IAW RAS/BAE/1007630/2008 ISS A, APPROVED BY EA 6-5720-123019.Jul 17, 2008 · N743FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA02952Skin · damagedDURING ACCOMPLISHMENT OF EO 6-5750-7-5000 PT.3 FOUND DAMAGED HOLE ON LT INBOARD FLAP TOP SKIN NEAR RIB 7. REPAIR PERFORMED BY REAM UP THE HOLE TO DIAMETER 0.1865 -0.1895 INCH , INSPECT THE HOLE BY NDT AND INSTALL HL11VF-6 IAW RAS /FOK/165/2008 ISS.A, APPROVEDJul 17, 2008 · N743FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA02951Cover · chafedFOUND CHAFING MARKS ON CROSS SHEET C56-57A, RT NEAR EMERGENCY EXIT. REPAIR PERFORMED BY SMOOTH REWORK , NDT FOR CRACK FREE CONDITION AND FLAP PEENING IAW. RAS /EFW/9000061/2008 ISS.A , APPROVED BY EA 6-5316-123049.Jul 17, 2008 · N743FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02912Stringer · corrodedFOUND CORROSION ON STRINGER P 54 LT BETWEEN C59-61, P 53 LT AND P 48 LT BETWEEN C59-60 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201A.Jul 16, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 08FDEA02911Stringer · corrodedFOUND CORROSION ON STRINGER P 56 LT, C59-62 STRINGER REPAIR PERFORMED IAW. SRM 53-10-14 FIG. 201A.Jul 16, 2008 · N743FD · Airbus A300F4622R · Fuselage Main, StructureSDR 08FDEA02910Stringer · corrodedFOUND CORROSION ON STRINGER P 54 LT, C55-56 AND P56 LT, C 57.2-57.3 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201A.Jul 16, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 08FDEA02909Doubler · corrodedFOUND CORROSION ON KRUEGER FLAP DOUBLER AT C 38, P 28-33 RT REPAIR PERFORMED BY CORROSION REMOVAL, NDT FOR CORROSION FREE CONDITION AND FLAP PEENING IAW RAS/EFW/9000060/2008 ISS A, APPROVED BY EA 6-5314-120076.Jul 16, 2008 · N743FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA02908Skin · chafedFOUND CHAFING MARKS ON LT INBOARD FLAP TOP SKIN RIB 1C. REPAIR PERFORMED BY INSTALLING EXTERNAL PATCH IAW RAS/FOK/161/2008 ISS B, APPROVED BY EA-5752-120086A.Jul 16, 2008 · N743FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA02907Sill · corrodedFOUND CORROSION ON SILL BEAM IN AFT CARGO COMPARTMENT, C 59-63A REPAIR PERFORMED BY UPPER FLANGE REPLACEMENT WITH SMALL DEVIATIONS IAW RAS/EFW/9000066/2008 ISS A, APPROVED BY EA 6-5317-123013.Jul 16, 2008 · N743FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02900Skin · corrodedFOUND CORROSION AT AFT CARGO DOOR C 59-63A, INNER SKIN PANEL (BETWEEN LONGERON 3-4) OUT OF LIMIT. REPAIR PERFORMED BY SMOOTH BLEND OUT OF CORROSION, NDT FOR CRACK FREE CONDITION AND FLAP PEENING IAW RAS/DAHAM/4025300/2008 ISS A, APRROVED BY EA 6-5232-123025.Jul 15, 2008 · N743FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR 08FDEA02899Skin · corrodedFOUND CORROSION AT AFT CARGO DOOR C 59-63A, INNER SKIN PANEL (NEAR LONGERON 5) OUT OF LIMIT. REPAIR PERFORMED BY SMOOTH BLEND OUT OF CORROSION, NDT FOR CRACK FREE CONDITION AND FLAP PEENING IAW RAS/DAHAM/4025300/2008 ISS A, APPROVED BY EA 6-5232-123025.Jul 15, 2008 · N743FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR 08FDEA02898Floorbeam · corrodedFOUND CORROSION ON CROSSBEAM C 72 OUT OF LIMIT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 15, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 08FDEA02897Skin · damagedFOUND OLD REPAIR (REWORKED AREA) ON SKIN PANEL C 67, P 48 RT RELATED TO RAS- DA/HAM1376.2/96, WHICH IS SMALLER THAN DETECTED. REPAIR RENEWED IAW RAS/EFW/9000065/2008 ISS A (REWORK OF THE AREA, PERFORM FLAP PEENING, ENSURE CORROSION FREE CONDITION), APPROVED Jul 15, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA02896Stringer · corrodedFOUND CORROSION AT STRINGER P 56 LT, C 76-77 OUT OF LIMIT. REPAIR PERFORMED BY CUT OUT OF CORRODED FLANGE AND INSTALLING REINFORCEMENT PROFILE IAW RAS/EFW/9000063/2008 ISS A, APPROVED BY EA 6-5318-120098.Jul 15, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 08FDEA02895Stringer · corrodedFOUND CORROSION AT STRINGER P 56 RT, C 76-77 OUT OF LIMIT. REPAIR PERFORMED BY CORROSION REWORK, NDT FOR CORROSION FREE CONDITION AND FLAP PEENING IAW RAS/EFW/9000064/2008 ISS A, APPROVED BY EA 6-5318-120098.Jul 15, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 08FDEA02894Skin · damagedFOUND LIGHTNING STRIKE AT FRAME 5-7, 11 O`CLOCK POSITION. REPAIR PERFORMED BY BUSH INSTALLATION IAW SRM 53-10-12 FIG 221.Jul 15, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA02893Floorbeam · corrodedFOUND CORROSION SPOTS ON CROSSBEAM C 62 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 15, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 08FDEA02891Floorbeam · corrodedFOUND CORROSION SPOTS ON CROSSBEAM C 56 AND C 58 SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.Jul 15, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 08FDEA02888Skin · chafedFOUND SCRATCHES AT SKIN PANEL C64-65 IN THE AREA OF RA ANTENNA. REPAIR PERFORMED BY REWORK OF AREA AND NDT FOR CRACK FREE CONDITION IAW RAS RAS/EFW/9000071/2008 ISS A , APPROVED BY EA 6-5317-123028.Jul 15, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA02887Frame · crackedFOUND ON RT AFT PAX DOOR FRAME SEGMENT UNDER BEAM 8 BROKEN REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 15, 2008 · N743FD · Airbus A300B4622R · Passenger/Crew DoorsSDR 08FDEA02886Fitting · corrodedFOUND CONNECTING FITTINGS AT C 63 WITH CORROSION OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 15, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 08FDEA02805Support · corrodedFOUND CORROSION ON KRUEGER FLAP STRUCTURE RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 10, 2008 · N743FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA02804Fitting · corrodedFOUND CORROSION ON KRUEGER FLAP STRUCTURE RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 10, 2008 · N743FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA02803Skin · corrodedFOUND CORROSION ON SKIN PANEL C 39-40, P 39-40 RT. REPAIR PERFORMED BY CORROSION REWORK AND INSTALLING A DOUBLER AND SHIMS IAW RAS/70511475/007/2008 ISS A, APPROVED BY EA 6-5315-120075.Jul 10, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA02802Skin · damagedFOUND OLD FLUSH DOUBLER RPAIR ON RT CENTER FLAP NOSE SKIN WITHOUT ANY OLD DOCUMENTATION. REPAIR RENEWED IAW SRM 57-50-00 FIG 208.Jul 10, 2008 · N743FD · Airbus A300F4622R · Trailing Edge FlapsSDR 08FDEA02749Attach Fitting · corrodedFOUND CORROSION AT CLIP C 64, P 55-56 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 8, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 08FDEA02748Attach Fitting · corrodedFOUND CORROSION AT CLIP C 66, P 56-57 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 8, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 08FDEA02747Attach Fitting · corrodedFOUND CORROSION AT CLIP C 68, P 56-57 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 8, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 08FDEA02746Pressure Panel · dentedFOUND NICK IN PRESSURE MEMBRANE AT C 51, TRACK 5, RT REPAIR PERFORMED BY SMOOTH REWORK, NDT FOR CRACK FREE CONDITION IAW RAS 70511614/009/2008 ISS A , APPROVED BY EA 6-5315-120080.Jul 8, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, BulkheadSDR 08FDEA02745Fitting · crackedFOUND CRACK IN CONNECTING FITTING C 62 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 8, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 08FDEA02614Seat Track · corrodedFOUND CORROSION ON SEAT TRACK, C17-19, Y 450. REPAIR PERFORMED IAW SRM 53-12-16 FIG 201.Jul 1, 2008 · N743FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02613Longeron · corrodedFOUND CORROSION ON LONGERON , C12A-14, Y 450 REPAIR PERFORMED IAW SRM 53-12-15 FIG 207.Jul 1, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 08FDEA02612Frame · chafedFOUND CHAFING MARKS AT C 32 AND 37 BETWEEN P 14-15 OUT OF LIMIT. INNER FLANGE REPAIR PERFORMED IAW SRM 53-10-13 FIG 202.Jul 1, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, FrameSDR 08FDEA02611Stringer · corrodedFOUND CORROSION AT STRINGER P 44, C 38.2-39 RT OUT OF LIMIT, STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Jul 1, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 08FDEA02610Stringer · corrodedFOUND CORROSION AT STRINGER P 56, C 70-72 RT OUT OF LIMIT, STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Jul 1, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 08FDEA02609Stringer · corrodedFOUND CORROSION AT STRINGER P 53, C 71-72 LT OUT OF LIMIT STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Jul 1, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 08FDEA02608Stringer · corrodedFOUND CORROSION AT STRINGER P 44, C 70-71 LT OUT OF LIMIT STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Jul 1, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 08FDEA02607Skin · unknownFOUND OLD FLUSH DOUBLER REPAIR ON LT OUTER FLAP NOSE SKIN RIB 11-13 NOT PERFORMED IAW SRM 57-50-00 FIG 208. FLUSH DOUBLER REPAIR RENEWED IAW SRM 57-50-00 FIG 208.Jul 1, 2008 · N743FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA02606None · noneFOUND OLD SPLICE REPAIR IN FWD CARGO COMPARTMENT AT UPPER FLANGE C 38.2 RT WITHOUT ANY OLD DOCUMENTATION. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10 AND DRAWING R537B1760.Jul 1, 2008 · N743FD · Airbus A300B4622R · Standard Practices/StructuresSDR 08FDEA02605Beam · dentedFOUND NICKS AND OLD REWORKS ON BEAM SECTION, C 67-69, P 45 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 1, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, StructureSDR 08FDEA02604Beam · corrodedFOUND CORROSION ON BEAM 10, C 67-69, P 45 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 1, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, StructureSDR 08FDEA02603Floorbeam · corrodedFOUND IN AFT CARGO COMPARTMENT CORRODED CROSSBEAM AT C 66, AD SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.Jul 1, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 08FDEA02602None · noneFOUND OLD FILLER REPAIR ON CROSSBEAM C 57.2 LT BETWEEN Y-140 AND Y-1470 WITHOUT ANY OLD DOCUMENTATION. REPAIR PERFORMED IAW SRM 53-10-15 FIG 208.Jul 1, 2008 · N743FD · Airbus A300B4622R · Standard Practices/StructuresSDR 08FDEA02601Stringer · corrodedFOUND CORROSION AT STRINGER P 57, C 65-72 OUT OF LIMIT STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Jul 1, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 08FDEA02600Skin · misrepairedFOUND OLD DOUBLER REPAIR AT PAX DOOR NR 4 LT LOWER AFT CORNER NOT IAW SRM 52-10-00 FIG 203. PERFORMED (DOUBLER THICKNESS TO LESS) DOUBLER REPAIR RENEWED IAW SRM 52-10-00 FIG 203.Jul 1, 2008 · N743FD · Airbus A300B4622R · Passenger/Crew DoorsSDR 08FDEA02598Profile · corrodedFOUND CORRODED CORNER PROFILE AT C 63-64, P 46 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 1, 2008 · N743FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02597Fitting · corrodedFOUND CORRODED CORNER FITTING AT C 63 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 1, 2008 · N743FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 08FDEA02596None · noneFOUND OLD SPLICE REPAIR IN AFT CARGO COMPARTMENT AT C 63 LT, BETWEEN Y 805 AND Y 1470 WITHOUT ANY OLD DOCUMENTATION. NEW SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG.207Jul 1, 2008 · N743FD · Airbus A300B4622R · Standard Practices/StructuresSDR 08FDEA02595Floor Support · damagedFOUND OLD FILLER REPAIR IN AFT CARGO COMPARTMENT AT FLOOR STRUCTURE C 63-64, Y 805. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 1, 2008 · N743FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
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