N744FD

Service difficulty reports · 271

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 = 'N744FD' 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 08FDEA03963Skin · chafedFOUND 2 AREAS OF CHAFING MARKS ON RT SLAT NR 1 LOWER SKIN. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS IAW RAS/FOK/234/2008 ISS A, APPROVED BY EA 6-5742-123083.Sep 22, 2008 · N744FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA03962Skin · chafedFOUND 2 AREAS OF CHAFING MARKS ON LT SLAT NR 1 LOWER SKIN. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS IAW RAS/FOK/226/2008 ISS A, APPROVED BY EA 6-5742-123060.Sep 22, 2008 · N744FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA03961Track · damagedHEAVY CORROSION FOUND ON ROLLER TRACK AND DURING REPAIR A HOLE WAS MISDRILLED HOL, C 63, Y140 LT. REPAIR PERFORMED BY INSTALLING A BUSHING IN ROLLER TRACK IAW RAS/DAHAM/4025692/2008 ISS A, APPROVED BY EA 6-5317-123138.Sep 22, 2008 · N744FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03960Skin · chafedFOUND CHAFING MARKS ON RT CENTER FLAP TOP SKIN RIB 13-15 AND 20-21. REPAIR PERFORMED BY CUT OUT THE SKIN AREA AND CHAFING PLATE AT RIB 13-13A AND INSTALL AN EXTERNAL DOUBLER AND A NEW CHAFING PLATE, BLEND OUT CHAFING MARK AT RIB 20-21 AND INSTALL A NEW CHAFSep 22, 2008 · N744FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA03896Skin · wornFOUND ELONGATED HOLES ON RT WING BOTTOM SKIN AND PYLON SUPPORT BRACKET. REPAIR PERFORMED BY DRAWING R571-50532 (OVERSIZING THE HOLES INSTALL FREEZE PLUGS), APRROVED BY RAS/BAE/10078756/2008 ISS A AND EA 6-2900-123069.Sep 16, 2008 · N744FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA03895Skin · damagedFOUND ELONGATED HOLES ON LT WING BOTTOM SKIN AND PYLON SUPPORT BRACKET. REPAIR PERFORMED BY DRAWING R571-50532 (OVERSIZING THE HOLES INSTALL FREEZE PLUGS), APRROVED BY RAS/BAE/10078756/2008 ISS A AND EA 6-2900-123069.Sep 16, 2008 · N744FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA03894Sill · damagedFOUND OLD REPAIR WITH SOME MISSING FASTENER ON AFT CARGO DOOR SILL BEAM WITHOUT OLD RECORD AVAILABLE. REPAIR WAS PERFORMED IAW SRM 53-17-18 PB 201 PARA 10 , MISSING FASTENER INSTALLED, NDT FOR CRACK FREE CONDITION PERFORMED, APPROVED BY RAS/EFW/9000103/2008Sep 16, 2008 · N744FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA03893Skin · corrodedFOUND CORROSION ON TOP SKIN LOWER SURFACE ON OUTER SHROUD BOX , RIB 25-29 LT. REPAIR PERFORMED BY CUT OUT RIBS TO GAIN ACCESS, BLEND OUT THE CORROSION AND REPROTECT THE AREA AND INSTALL REPAIR ANGLES TO THE CUT RIBS IAW RAS/BAE/1007773/2008 ISS A, APPROVED BYSep 16, 2008 · N744FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA03892Attach Fitting · chafedFOUND CHAFING MARKS AT REAR MLG DOOR ACTUATOR FITTING OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 16, 2008 · N744FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 08FDEA03890Rib · chafedFOUND CHAFING MARKS IN RT WING STRUCTURE RIB 27-28, IN AREA OF NACA DOOR. REPAIR PERFORMED BY POLISHING THE DAMAGED STRUCTURE TO SMOOTH CONTOUR, CUT OUT DAMAGED STRUTURE AND INSTALLING A REPAIR ANGLE AT NACA DOOR SURROUND REAR STIFFENER IAW RAS BAE10076602008Sep 16, 2008 · N744FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR 08FDEA03887Skin · damagedFOUND OLD REPAIR AFT OF REAR SPAR AT RIB 9 (RAS/BAE/0081/2002 ISS C, UNREPAIRED CRACK WITH CRACK STOP HOLE IN BOTTOM SKIN). REPAIR PERFORMED BY NDT FOR CRACK FREE CONDITION (NO CRACK FOUND AFTER REMOVAL OF REPAIR PLATES) FOR EVERY HOLE AFFECTED BY THE REPAIR Sep 16, 2008 · N744FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA03875Skin · crackedFOUND OLD REPAIR AFT OF REAR SPAR AT RIB 9 RAS/BAE/0081/2002 ISS C, UNREPAIRED CRACK WITH CRACK STOP HOLE IN BOTTOM SKIN. REPAIR PERFORMED BY DRILLING CRACK STOP HOLE, INSTALLING A CRACK STOP PLUG AND REPAIR PLATE IAW DRAWING R573-40199, APPROVED BY RAS/BAE/1Sep 15, 2008 · N744FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA03874Spar · crackedFOUND ON LOWER SPAR OF PYLON NR 1 UPPER SURFACE CRACK IN CENTER STIFFENER AT RIB 10A. REPAIR PERFORMED BY CUT OUT THE CRACKED AREA AND INSTALLING A DOUBLER IAW DRAWING R546-10349, APPROVED BY RAS/70512822/010/2008 ISS A, APPROVED BY EA 6-5451-123098.Sep 15, 2008 · N744FD · Airbus A300B4622R · Nacelle/Pylon, Frame/Spar/RibSDR 08FDEA03873Longeron · wornFOUND ELONGATED HOLE ON AFT FAIRING ADAPTER LONGERON, PYLON NR 1. REPAIR PERFORMED BY WELDING THE LONGERON OVERSIZE FASTENER HOLE AND REDRILL THE FASTENER HOLE SAME AS ORIGINAL IAW RAS/ROHR/0776/2008 ISS A, APPROVED BY EA 6-5455-123139.Sep 15, 2008 · N744FD · Airbus A300B4622R · Nacelle/Pylon, Frame/Spar/RibSDR 08FDEA03870Sill · corrodedFOUND CORROSION AT FWD CARGO DOOR SILL BEAM, C 20-25 REPAIR PERFORMED BY CORROSION REWORK, NDT FOR CORROSION FREE CONDITION, UPPER FLANGE REPAIR BETWEEN C 24-26 PER DRAWING R537-06913 AND INSTALLING OF BUSHES IAW SRM 53-13-18 FIG 202, APPROVED BY RAS/EFW/90001Sep 15, 2008 · N744FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA03868Fitting · corrodedFOUND CORROSION ON RUN OUT FITTING C16-17, P 44 RT OUT OF LIMIT. REPAIR PERFORMED IAW SRM 53-12-14 FIG 201.Sep 15, 2008 · N744FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA03814Track · corrodedCORROSION FOUND ON ROLLERTRACK C54-56 RT. A REPAIR IAW SRM 53-10-15 FIG 202 IS NOT POSSIBLE. REPAIR PERFORMED BY CUTTING THE ROLLER TRACK AT C 55, INSTALLING TWO SEPARATE L- PROFILES ON CROSS BEAM IAW RAS/EFW/900090/2008 ISS A, APPROVED BY EA 6-5316-123089Sep 11, 2008 · N744FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03813Track · corrodedCORROSION FOUND ON ROLLERTRACK C54-56 LT. A REPAIR IAW SRM 53-10-15 FIG 202 IS NOT POSSIBLE. REPAIR PERFORMED BY CUTTING THE ROLLER TRACK AT C 55, INSTALLING TWO SEPARATE L- PROFILES ON CROSSBEAM IAW RAS/EFW/900089/2008 ISS A, APPROVED BY EA 6-5316-123087.Sep 11, 2008 · N744FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03812Web · crackedFOUND CRACK IN WEBS ABOVE CENTER TANK TANK AT C 47, BETWEEN BEAM 3-4 LT AND RT. REPAIR PERFORMED BY PERFORMING CRACK STOP HOLE AND INSTALLING A DOUBLER IAW RAS /70512671/004/2008 ISS A, APPROVED BY EA 6-5315-123074.Sep 11, 2008 · N744FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA03811Web · crackedFOUND CRACK IN WEBS ABOVE CENTER TANK TANK AT C 47 , BETWEEN BEAM 1-2 LT AND RT. REPAIR PERFORMED BY PERFORMING CRACK STOP HOLE AND INSTALLING A DOUBLER IAW RAS /70512671/004/2008 ISS A, APPROVED BY EA 6-5315-123074.Sep 11, 2008 · N744FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA03809Mount · chafedFOUND CHAFING MARKS ON PYLON NR 1 FWD MOUNT FITTING ON PYRAMID. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARK, NDT FOR CRACK FREE CONDITION AND CADMIUM PLATING IAW RAS/70512885/011/2008 ISS A, APPROVED BY EA 6-5451-123062.Sep 11, 2008 · N744FD · Airbus A300B4622R · Nacelle/Pylon, Attach FittingsSDR 08FDEA03790Fitting · corrodedFOUND CORROSION OUT OF LIMIT ON RT WING, ON STRUCTURE FOR KRUEGER FLAP ATTACHMENT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 10, 2008 · N744FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA03789Fitting · corrodedFOUND CORROSION OUT OF LIMIT ON RT WING, ON STRUCTURE FOR KRUEGER FLAP ATTACHMENT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 10, 2008 · N744FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA03788Fitting · corrodedFOUND CORROSION OUT OF LIMIT ON RT WING, ON STRUCTURE FOR KRUEGER FLAP ATTACHMENT. REPAIR PERFROMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 10, 2008 · N744FD · Airbus A300B4622R · Leading Edge DevicesSDR 08FDEA03756Shear Tie · damagedFOUND ELONGATED HOLES AT FRAME FOOT C 43 RT. REPAIR PERFORMED BY OVERSIZING THE HOLE AND INSTALLING FASTENER EN6115V4 WITH COLLAR NAS172604 IAW RAS /70513306/009/2008 ISS A, APPROVED BY EA 6-5315-123136.Sep 8, 2008 · N744FD · Airbus A300B4622R · Fuselage Internal Mounting StructureSDR 08FDEA03755Floorbeam · corrodedCORROSION FOUND IN AFT CARGO COMPARTMENT AT CROSSBEAM C 60. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.Sep 8, 2008 · N744FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 08FDEA03709Fitting · dentedFOUND NICKS ON LT WING, THRUST AND SIDE LOAD FITTING. REPAIR PERFORMED BY BLEND OUT, NDT FOR CRACK FREE CONDITION IAW RAS/BAE/1007700/2008 ISS.A, APPROVED BY EA 6-5720-123037.Sep 2, 2008 · N744FD · Airbus A300B4622R · Wing, Attach FittingsSDR 08FDEA03708Skin · dentedFOUND DENT IN BULK CARGO DOOR, C67-68, NEAR BEAM 1. REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR, NDT FOR CRACK FREE CONDITION IAW RAS/DAHAM/4025440/2008 ISS A, APPROVED BY EA 6-5234-123054.Sep 2, 2008 · N744FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR 08FDEA03707Skin · dentedFOUND SEVERAL DENTS AND IMPACTS ON RT INBOARD FLAP, LOWER SURFACE THREE DOUBLER REPAIRS (RIB 9-11, 12-16, 12-15) WERE PERFORMED IAW RAS/FOK/233/2008 ISS.C, APPROVED BY EA 6-5752-123073.Sep 2, 2008 · N744FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA03706Rib · chafedFOUND CHAFING MARKS ON LT WING, LEADING EDGE RIB, BETWEEN RIB 1-5 REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS, NDT FOR CRACK FREE CONDITION IAW RAS/BAE/1007859/2008 ISS.A , APPROVED BY EA 6-5741-123061.Sep 2, 2008 · N744FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR 08FDEA03705Skin · damagedFOUND OLD DOUBLER REPAIR NOT PERFORMED IAW RAS/FOK/138/98 (TOP AND LOWER DOUBLER), LOWER DOUBLER MISSING, RIB 17A-18 TRAILING EDGE. DOUBLER REPAIR RENEWED IAW RAS/224/2008 ISS.A, APPROVED BY EA 6-5752-123082.Sep 2, 2008 · N744FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA03704Frame · damagedFOUND DURING MODIFICATION IAW EO 6-5310-7-5015 PT. 2 FOUR ELONGATED HOLES IN FRAME FOOT AT C 43, P 36 LT. REPAIR PERFORMED BY REAM UP THE HOLES , NDT FOR CRACK FREE CONDITION IAW RAS/70513493/2008 ISS. A, APPROVED BY EA 6-5315-123137.Sep 2, 2008 · N744FD · Airbus A300B4605R · Fuselage Main, FrameSDR 08FDEA03703Floorbeam · corrodedFOUND CORROSION ON CROSSBEAM C 56 LT OUT OF LIMIT. SPLICE REPAIR PERFORMED IAW. SRM 53-10-15 FIG.207Sep 2, 2008 · N744FD · Airbus A300B4605R · Fuselage Main, Floor BeamSDR 08FDEA03680Support · damagedFOUND DAMAGED Z-PROFILE (TO LESS EDGE MARGIN) AT C74, P26 LT. REPAIR PERFROMED BY DRILLING AN ADDITIONAL HOLE AND INSTALLING ADDITIONAL FASTENER LN9198-4800CF IAW RAS/EFW/9000083/2008 ISS A, APPROVED EA 6-5318-123078.Sep 1, 2008 · N744FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA03679Angle · damagedFOUND DAMAGED ANGLE (ELONGATED HOLES) AT C75, P 26 RT. REPAIR PERFORMED BY REWORK THE HOLES AND INSTALLING RIVETS HL 10VF8 IN AFFECTED HOLES IAW RAS/EFW/9000084/2008 ISS A, APPROVED BY EA 6-5318-123076.Sep 1, 2008 · N744FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA03678Skin · dentedFOUND DENT AND SCRATCH IN OUTER SKIN, C59-59A, P 37-38 RH. REPAIR PERFORMED BY REWORK THE DENT AND SCRATCH IAW SRM 51-73-10, APRROVED BY RAS/EFW/9000082/2008 ISS.A AND EA 6-5317-123075.Sep 1, 2008 · N744FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA03677Spar · corrodedCORROSION FINDINGS AROUND PYLON NR 2 SPIGOT BEARING HOLES, UPPER SPAR RIB 12-13. REPAIR PERFORMED BY CORRSOION REMOVAL, NDT FOR CORROSION FREE CONDITION AND SURFACE PROTECTION IAW. RAS/70512899/009/2008 ISS.A, APPROVED EA 6-5451-123134.Sep 1, 2008 · N744FD · Airbus A300B4622R · Nacelle/Pylon, Frame/Spar/RibSDR 08FDEA03676Skin · chafedFOUND SCRUB MARKS AT OUTER SKIN C 38.1-38.2, P 43-45 RT DOUBLER REPAIR PERFORMED IAW SRM 53-10-12 FIG.225 , APPROVED BY RAS/EFW/9000088/2008 ISS.A AND EA 6-5314-123093.Sep 1, 2008 · N744FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA03675Door Frame · chafedFOUND SCRUB MARKS AT EMERGENCY EXIT C 55, P14-15 RT. REPAIR PERFORMED BY BLEND OUT , NDT FOR CRACK FREE CONDITION IAW RAS/EFW/9000086/2008 ISS.A, APPROVED BY EA 6-5316-123092.Sep 1, 2008 · N744FD · Airbus A300B4622R · Fuselage Main, StructureSDR 08FDEA03674Door Frame · chafedFOUND SCRUB MARKS AT EMERGENCY EXIT C 57.2, P14-15 LT REPAIR PERFORMED BY BLEND OUT , NDT FOR CRACK FREE CONDITION IAW. RAS/EFW/9000080/2008 ISS.A, APPROVED BY EA 6-5316-123071.Sep 1, 2008 · N744FD · Airbus A300B4622R · Fuselage Main, StructureSDR 08FDEA03673Door Frame · chafedFOUND SCRUB MARKS AT EMERGENCY EXIT C 55 AND C 57.2, P14-15 LT AND C 55, P 14-15 RT. REPAIR PERFORMED BY BLEND OUT , NDT FOR CRACK FREE CONDITION IAW RAS/EFW/9000079/2008 ISS.A, APPROVED BY EA 6-5316-123070,Sep 1, 2008 · N744FD · Airbus A300B4622R · Fuselage Main, StructureSDR 08FDEA03672Rib · chafedFOUND CHAFING MARKS ON RT WING TRAILING EDGE AREA ON RIB FOR ASA ATTACHMENT. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS , PERFORM NDT FOR CRACK FREE CONDITION IAW. RAS/BAE/1007863/2008 ISS.A , APPROVED BY EA 6-5751-123063Sep 1, 2008 · N744FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR 08FDEA03671Rib · chafedFOUND CHAFING MARKS ON LH WING TRAILING EDGE AREA ON RIB FOR ASA ATTACHMENT. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS , PERFORM NDT FOR CRACK FREE CONDITION IAW. RAS/BAE/1007863/2008 ISS.A , APPROVED BY EA 6-5751-123063Sep 1, 2008 · N744FD · Airbus A300F4622R · Wing, Rib/BulkheadSDR 08FDEA03670Fitting · corrodedFOUND IN AFT CARGO COMPARTMENT A CORNER FITTING C63 LT WITH CORROSION. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 1, 2008 · N744FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 08FDEA03669Stiffener · dentedFOUND IN AFT CARGO COMPARTMENT STIFFENER AT CROSS BEAM C 56 RT DENTED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 1, 2008 · N744FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA03668Fitting · corrodedFOUND IN AFT CARGO COMPARTMENT CORNER FITTING AT C56 LT WITH CORROSION. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 1, 2008 · N744FD · Airbus A300B4622 · Fuselage Main, Attach FittingsSDR 08FDEA03442Skin · misrepairedFOUND OLD DOUBLER ON FUSELAGE C 2-3, RT NOT IAW SRM 53-11-12 FIG 201. DOUBLER REPAIR RENEWED IAW SRM 53-11-12 FIG 201.Aug 15, 2008 · N744FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA03441Fitting · chafedFOUND OLD IMPACT MARKS ON INNER SURFACE OF RT PYLON TO WING LUG NEXT TO BRACKET A571-41040-001. REPAIR PERFORMED BY BLEND OUT THE MARKS TO SMOOTH CONTOUR , NDT FOR CRACK FREE CONDITION IAW RAS/BAE/1007776/2008 ISS A, APPROVED BY EA 6-5720-123053.Aug 15, 2008 · N744FD · Airbus A300B4622R · Wing, Attach FittingsSDR 08FDEA03440Skin · chafedFOUND CHAFING MARKS ON LT INBOARD FLAP, RIB 11-12, TOP SKIN REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS, NDT FOR CRACK FREE CONDITION IAW RAS/FOK/228/2008 ISS A, APRROVED BY EA 6-5752-123079.Aug 15, 2008 · N744FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA03439Diaphragm · dentedFOUND NICKS AND DENTS IN DIAPHRAGM, TRACK 1-2, RT REPAIR PERFORMED SMOOTH BLEND OUT OF THE NICKS, PERFORM NDT INSPECTION FOR CRACK FREE CONDITION AND LEAVE THE DENTS AS IS IAW RAS/70512735/014/2008ISS. A, APPROVED BY EA 6-5315-123080.Aug 15, 2008 · N744FD · Airbus A300B4622R · Fuselage Main, Structure
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