N749FD

Service difficulty reports · 180

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 = 'N749FD' 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 07FDEA02975Skin Panel · dentedDENT ON C48-49 CENTER SECTION UPPER SKIN BETWEEN TRACK 1-2 RT DENT ACCEPTABLE AS IT IS APPROVED BY EA 6-5315-112438 AND RAS 052577/013/2007 ISS A.Aug 20, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA02943Fitting · corrodedCORROSION ON UPPER CORNER FITTING C88 RT REPAIR PERFORMED BY DOUBLER INSTALLATION IAW EA 6-5319-10651 AND RAS/DATLS/0003749/2007 ISS B.Aug 16, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, StructureSDR 07FDEA02942Web · crackedCENTER SECTION FOUND WEB CRACKS AT C47, TRACK 2 LT AND 2 RT REPAIR PERFORMED BY INSTALLING DOUBLER ON WEB IAW EA 6-5315-112438 AND RAS 052577/010/2007 ISS A.Aug 16, 2007 · N749FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA02941Stringer · corrodedCORROSION SPOT ON STRINGER P51, C39-40 RT REPAIR PERFORMED BY BLEND OUT CORROSION TO SMOOTH CONTOUR IAW SRM 51-74-10, APPROVED BY EA 6-5315-106536 AND RAS 052622/004/2007 ISS A.Aug 16, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA02940Stringer · corrodedCORROSION SPOT ON STRINGER P50 RT, C39-40 REPAIR PERFORMED BY BLEND OUT CORROSION TO SMOOTH CONTOUR IAW SRM 51-74-10, APPROVED BY EA 6-5315-106536 AND RAS 052622/004/2007 ISS A.Aug 16, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA02939Stringer · corrodedCORROSION SPOT ON STRINGER P39 LT, C46-47 REPAIR PERFORMED BY BLEND OUT CORROSION TO SMOOTH CONTOUR IAW SRM 51-74-10, APPROVED BY EA 6-5315-106536 AND RAS 052622/004/2007 ISS A.Aug 16, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA02938Bulkhead · corrodedCORROSION ON AFT PRESSURE BULKHEAD REPAIR PERFORMED BY BLEND OUT THE CORROSION TO SMOOTH CONTOUR AND REPLACEMENT OF AFFECTED FASTENER IAW SRM 51-74-10 AND 51-40-21, APPROVED BY EA 6-5318-112443 AND RAS/DAHAM/4022393/2007 ISS A.Aug 16, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, BulkheadSDR 07FDEA02937Mount · corrodedCORROSION ON FLANGE AT GALLEY ATTACHMENT C12A-13, Y450-953 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Aug 16, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 07FDEA02936Seat Track · corrodedFOUND CORROSION ON SEAT TRACK C14-15A. REPAIR PERFORMED IAW SRM 53-12-16 FIG 201.Aug 16, 2007 · N749FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02935Skin · damagedOLD REPAIR ON SLAT NR 1 INBOARD EDGE WITHOUT ANY DOCUMENTATION REPAIR RENEWED IAW EA 6-5742-106524 AND RAS/FOK/148/2007 ISS A.Aug 16, 2007 · N749FD · Airbus A300B4622R · Leading Edge DevicesSDR 07FDEA02856Rib · corrodedCORROSION FOUND ON LT MLG RIB 5 FWD LUG REPAIR PERFORMED BY OVERSIZING THE BORE AND CORROSION REMOVAL IAW DRAWING R572-40221, APPROVED BY EA 6-5751-112446 AND RAS/BAE/100519/2007 ISS A.Aug 13, 2007 · N749FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR 07FDEA02854Web · misrepairedUNKNOWN REPAIR ON WEB A538-32103-206, C47, TRACK 3-4 RT REPAIR RENEWED (DOUBLER REPAIR) IAW EA 6-5315-112439 AND RAS 052826/005/2007 ISS A.Aug 13, 2007 · N749FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA02838Crossbeam · misrepairedOLD SPLICE REPAIR ON TOP CAP BEAM C 63 NOT CONFORM TO SRM REPAIR RENEWED IAW SRM 53-10-15 FIG 207.Aug 13, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, StructureSDR 07FDEA02837Fitting · damagedPYLON NR 1 FWD PYLON-WING ATTACH FITTING LUG WITH LITTLE WAVE DAMAGE REPAIR PERFORMED BY BLEND OUT IAW SRM 51-74-10, APPROVED BY EA 6-5451-106518 AND RAS /BAE/1005084/2007 ISS A.Aug 13, 2007 · N749FD · Airbus A300B4622R · Nacelle/Pylon, Attach FittingsSDR 07FDEA02836Skin · delaminatedFOUND OLD REPAIR ON LT AILERON , LOWER SKIN TRAILING EDGE WITH SIGN OF DELAMINATION. REPAIR RENEWED IAW SRM 517712 PB 201, PARA 4.Aug 13, 2007 · N749FD · Airbus A300B4622R · Wing, Plate/SkinSDR 07FDEA02835Skin Panel · damagedSTRUCTURE DAMAGE IN LOWER SKIN C25, P44-46 LT SKIN AND STRINGER REPAIR PERFORMED IAW SRM 53-10-12 FIG 229 AND 53-10-14 .Aug 13, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA02441Stringer · corrodedFOUND CORROSION OUT OF LIMIT ON P 56 RT (A539-86212) BETWEEN C63-68 AND P55 RT (A539-86217) BETWEEN C65-66. SPLICE REPAIR PERFORMED IAW SRM 563-10-14 FIG 201 .Jul 12, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA02440Frame · corrodedIN THE AREA OF FWD AND AFT SIDE OF FRAME 932 SOME AREAS WITH CORROSION REPAIR PERFORMED BY REPLACEMENT OF THE FOLLOWING PARTS IAW SRM 51-72-10. T-SECTION A539-89317-206, ANGLE SECTION A539-89317-228, A539-893127-229, A539-89317-224, A539-89317-225, A538-8931Jul 12, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA02432Crossbeam · corrodedHEAVY CORROSION ON CROSSBEAMS, C 61 RT (P/N A539-78476-200), C60 LT (A539-73599), C58 LT (P/N A539-74268). CROSSBEAM REPAIR PERFORMED ON C58 LT AND C60 LT IAW SRM 53-10-15 FIG 207 AND REPLACEMENT OF PART ON C61 .Jul 11, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, StructureSDR 07FDEA02430Fitting · corrodedHEAVY CORROSION ON C58 LT CORNER FITTING. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 11, 2007 · N749FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA02429Floorbeam · misrepairedOLD TOP CAP BEAM REPAIR ON C55 NOT CONFORM TO SRM. TOP CAP BEAM REPAIR RENEWED IAW SRM 53-10-15 FIG 208.Jul 11, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 07FDEA02427Floorbeam · corrodedTOP CAP BEAM C30 LT IS CORRODED TOP CAP BEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207 AND SRM 51-72-10.Jul 11, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 07FDEA02426Floorbeam · misrepairedOLD TOP CAP BEAM REPAIR NOT CONFORM TO SRM, AFT CARGO COMPARTMENT, C57 LT TOP CAP BEAM REPAIR RENEWED IAW SRM 53-10-15 FIG 208.Jul 11, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 07FDEA02423Stringer · corrodedCORROSION FOUND ON STRINGER P55, C70-71, RT/LT STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Jul 11, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA02422Stringer · damagedOLD REPAIR ON P37, C54.3 RT NOT CONFORM TO SRM. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Jul 11, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA02421Fitting · corrodedCORROSION DETECTED ON CORNER FITTING AT C63 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 11, 2007 · N749FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA02419Fitting · crackedFOUND 2 CRACKS (13MM AND 6MM,LT SIDE) AND 1 CRACK (5MM RT SIDE) ON C 12 A STIFFENER FITTING. REPAIR PERFORMED BY MODIFICATION OF STRUCTURE IAW SB A300-53-6137, APPROVED BY EO 6-5340-7-5002 PART 5600.Jul 11, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 07FDEA02381Floorbeam · misrepairedOLD TOP CAP BEAM REPAIR , C62, LT, ARE NOT CONFORM TO SRM. REPAIR RENEWED IAW SRM 53-10-15 FIG 208.Jul 6, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 07FDEA02188Doubler · corrodedUPPER SKIN PANEL C87 RT JOINT STRAP DOUBLER WITH CORROSION REPAIR PERFORMED BY BLEND OUT THE CORRODED AREA IAW EA 6-54319-112442 AND RAS/DAHAM/4022370/2007 ISS. B.Jun 19, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA02187Fitting · corrodedCORNER FITTING C27 LT/RT WITH CORROSION REPAIR PERFORMED BY REPLACEMENT OF PARTS (P/N A537-73644-202 AND A537-73644-203) IAW SRM 51-72-10.Jun 19, 2007 · N749FD · Airbus A300B4622R · Fuselage Main, Attach Fittings
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