N719FD

Service difficulty reports · 159

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 = 'N719FD' 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 08FDEA02455Floorbeam · corrodedBULK CARGO BAY UNDER FLOOR AREA STA FR 66, AND BETWEEN LBL 26 TO LBL43, FLOOR SUPPORT AND "T" CHANNEL HAS CORROSION. REMOVED AND REPLACED "T" CHANNEL/FLOOR SUPPORT ASSEMBLY IAW SRM 51-40-44 AND 51-40-21.Jun 25, 2008 · N719FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 08FDEA02408Floor Support · corrodedMAIN CARGO FLOOR SUPPORT AT RBL 77 HAS CORROSION AROUND FASTENER HOLES FOR FLOORBOARD FROM FR 13A TO FR 16A. REMOVED AND REPLACED FLOORBOARD SUPPORT IAW SRM 51-73-10 AND 51-40-21.Jun 24, 2008 · N719FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA02355Skin · gougedRT LOWER FUSELAGE AFT OF FR 16A ABOVE STRINGER 40R HAS A 1 INCH GOUGE. INSTALLED DOUBLER REPAIR IAW SRM 53-12-12 FIG 201, PAINTED IAW SRM 53-23-10. STRUCTURAL REPAIR INSPECTION INTERVALS IAW SRI 53-12-12-2-003-0.Jun 20, 2008 · N719FD · Airbus A300B4622 · Fuselage Main, Plate/SkinSDR 08FDEA02244Seat Track · corrodedMAIN CARGO SEAT TRACK EXFOLIATED FROM FR14 C TO FR 19 LBL 37 (YD). REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-21 AND 51-40-44.Jun 12, 2008 · N719FD · Airbus A300B4622 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02242Seat Track · corrodedMAIN CARGO SEAT TRACK CORRODED FROM FR 14 C TO FR 19, RBL 37 (-YD). REMOVED SEAT TRACK IAW SRM 51-40-21 LOCATED HOLES AND DRILLED IAW SRM 51-40-44. INSTALLED NEW SEAT TRACK IAW SRM 51-40-21.Jun 12, 2008 · N719FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02192Stringer · corrodedAIRCON BAY AT BILGE AREA BETWEEN FR 41 AND 42 STR 51R HAS CORROSION, BELOW WATER SEPARATOR. REMOVED AND REPLACED STR 51R IAW SRM 51-40-21.Jun 7, 2008 · N719FD · Airbus A300B4622 · Fuselage Main, Longeron/StringerSDR 08FDEA02147Seat Track · corrodedMAIN CARGO SEAT TRACK EXFOLIATED FROM FR 14C TO FR 19 LBL 17 (YE). REMOVED AND REPLACED SEAT TRACK P/N A53612518200 IAW SRM 51-40-21 AND SRM 51-40-40.Jun 4, 2008 · N719FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA05141Computer · unknownAT FL/340 GOT ECAM FUEL ADVISORY FOR 8000 LBS IMBALANCE. LEFT INNER TANK DECREASING SLOWLY THROUGH 2000 LBS IAW QRH, PULLED AND RESET FQI CHAN 1 AND 2 C/B, NO HELP. ALL COCKPIT INDICATIONS: QTY, FUEL USED, MANUAL FUEL CALCULATIONS INDICATED LOSS OF 8-10,00Dec 27, 2007 · N719FD · Airbus A300B4622 · Fuel Indicating SystemSDR 07FDEA04245Fitting · corrodedFOUND CORROSION AT CORNER FITTING C32 LT AND RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR 07FDEA04244Fitting · corrodedFOUND CORROSION AT CORNER FITTING C33 LT AND RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR 07FDEA04243Fitting · corrodedFOUND CORROSION AT FITTING OF DOOR SILL BEAM C25 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, Attach FittingsSDR 07FDEA04242Stringer · corrodedFOUND CORROSION AT STRINGER SEGMENT P 45 LT, C 26. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, Longeron/StringerSDR 07FDEA04241Stringer · corrodedFOUND CORROSION AT STRINGER SEGMENT P 44 RT, C 26 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, Longeron/StringerSDR 07FDEA04240Profile · corrodedFOUND CORROSION AT PROFILE C 54.2-54.3 P51 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR 07FDEA04239Stringer Splice · corrodedFOUND CORROSION AT SPLICE C 19, P 52 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, Longeron/StringerSDR 07FDEA04238Stringer · corrodedFOUND CORROSION AT STRINGER SEGMENT C65 P 35 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, Longeron/StringerSDR 07FDEA04237Floorbeam · corrodedFOUND CORROSION AT CROSS BEAM C 64 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, Floor BeamSDR 07FDEA04236Fitting · corrodedFOUND CORROSION AT FITTING C63. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR 07FDEA04234Floorbeam · corrodedFOUND CORROSION AT TOP CAP BEAM C63 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, Floor BeamSDR 07FDEA04233Wedge · corrodedFOUND CORROSION AT WEDGE C 59-60, P 52 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR 07FDEA04230Stringer · corrodedFOUND CORROSION AT STRINGER P 51 LT, C 59-60; P 52 LT AT C58-59 AND P 53 LT AT C58-59. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, Longeron/StringerSDR 07FDEA04223Floorbeam · corrodedFOUND CORROSION AT TOP CAP BEAM C64 SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, Floor BeamSDR 07FDEA04222Floorbeam · corrodedFOUND CORROSION AT FLANGE OF TOP CAP BEAM C 30 LT SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, Floor BeamSDR 07FDEA04219Stringer · failedFOUND OLD STRINGER REPAIR C20-21, P 54 LT NOT COMPATIBLE WITH P TO F CONVERSION. STRINGER REPAIR RENEWED IAW SRM 53-10-14 FIG 201.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, Longeron/StringerSDR 07FDEA04218Stringer · failedFOUND OLD STRINGER REPAIRS C20-21, P 53 LT NOT COMPATIBLE WITH P TO F CONVERSION. STRINGER REPAIR RENEWED IAW SRM 53-10-14 FIG 201.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, Longeron/StringerSDR 07FDEA04214Floorbeam · corrodedFOUND CORROSION AT FLANGE OF TOP CAP BEAM C 32. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, Floor BeamSDR 07FDEA04213Floorbeam · corrodedFOUND CORROSION AT STRUT OF TOP CAP BEAM C 38.2, REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, Floor BeamSDR 07FDEA04212Bulkhead · damagedFOUND DENTS AT PRESSURE BULKHEAD FLOOR STRUCTURE C 49-50 (WITH CRACK 2MM) AND C 50-51 AT TR 4-5 LT ; C 52-53 AT TR 2-3 LT, C 48-49 AT TR 4-5 RT. REPAIR PERFORMED BY INSTALLING A DOUBLER AT TR 4-5 LT, C49-50 AND LET THAT DENTS AT THE OTHER AREAS AS IT IAW EA 6Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, BulkheadSDR 07FDEA04209Floorbeam · corrodedFOUND CORROSION AT TOP CAP BEAM UPPER FLANGE 27. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10Sep 24, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, Floor BeamSDR 07FDEA04207Skin · delaminatedFOUND DELAMINATION AT RUDDER SIDE PANEL IN THE AREA OF HINGE ATTACHMENT FITTINGS, LT: BR1, BR4, BR5, BR6, BR7 RT: BR1-BR6 REPAIR PERFORMED IAW SRM 55-41-12 FIG 216.Sep 24, 2007 · N719FD · Airbus A300B4622 · Rudder, Plate/SkinSDR 07FDEA04206Spar · corrodedFOUND AT LT PYLON SPAR RIB 18 AT PYLON TO WING FITTING CORROSION. REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5440-70338 AND RAS 027276/007/2003.Sep 24, 2007 · N719FD · Airbus A300B4622 · Nacelle/Pylon, Frame/Spar/RibSDR 07FDEA04204Fitting · corrodedFOUND AT LT AFT WING TO PYLON FITTING PITTING MARKS INTO THE PYLON LUG BORE REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR AND NDT FOR CRACK FREE IAW EA 6-5720-70339 AND RAS /BAE/1352/2003 ISS A.Sep 24, 2007 · N719FD · Airbus A300B4622R · Wing, Nacelle/Pylon Attach FittingsSDR 07FDEA04203Skin · dentedFOUND ABRASION AT SLAT NR 1 RT TRAILING EDGE LOWER SKIN RIB 21 REPAIR PERFORMED BY INSTALLING AN EXTERNAL DOUBLER AND BONDING THE INTERNAL STRUCTURE IAW EA 6-5742-7034 AND RAS/FOK/173/2003 ISS A.Sep 24, 2007 · N719FD · Airbus A300B4622 · Leading Edge DevicesSDR 07FDEA04202Beam · corrodedFOUND CORROSION AT BEAM C 38-39 KRUEGER FLAP FWD FAIRING RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11.Sep 24, 2007 · N719FD · Airbus A300B4622 · Leading Edge DevicesSDR 07FDEA04201Skin · dentedFOUND DENT AT SLAT NR 1 LT ON LOWER TRAILING EDGE SKIN NEAR RIB 23 REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR AND NDT FOR CRACK FREE IAW EA 6-5742-70345 AND RAS/FOK/197/2003 ISS A.Sep 24, 2007 · N719FD · Airbus A300B4622 · Leading Edge DevicesSDR 07FDEA04199Skin · chafedFOUND ABRASION AT SLAT NR 1 LT ON TRAILING EDGE LOWER SKIN RIB 21. REPAIR PERFORMED BY INSTALLING A EXTERNAL DOUBLER AND BONDING THE INTERNAL STRUCTURE IAW EA 6-5742-70335 AND RAS/FOK172/2003 ISS A.Sep 24, 2007 · N719FD · Airbus A300B4622 · Leading Edge DevicesSDR 07FDEA04137Panel · crackedCRACK FINDING DURING INSPECTION IAW SB 57-6086 HOLE NR F -1MM IN BOTTOM PANEL AND HOLE NR G-8MM IN FWD FITTING. REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CRACK REMOVAL IAW EA 6-5710-73898 AND RAS/AS/310/2003 ISS A.Sep 20, 2007 · N719FD · Airbus A300B4622 · Wing Miscellaneous StructureSDR 07FDEA04135Skin Panel · corrodedFOUND CORROSION AT SKIN PANEL C39-40, P28-32 RT OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW DRAWING R538-10533, APPROVED BY EA 6-5315-70344 AND RAS/AS/0273/2003 ISS A.Sep 20, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, Plate/SkinSDR 07FDEA04134Shim · chafedFOUND SCRUB MARKS AT TORSION BOX LT/RT CROSS SHIM C 56-57, P 15A-16 REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5316-70333 AND RAS/DATLS/0001412/2003 ISS A.Sep 20, 2007 · N719FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR 07FDEA04133Fitting · crackedCRACKS FOUND AT FRAME 47 INTERNAL FITTING LT HOLE NR E (1MM) IN REAR SPAR, HOLE NR G (2MM) IN CORNER FITTING, HOLE NR I (2MM) IN FWD FITTING, HOLE NR N (2MM) IN FWD FITTING, REPAIR PERFORMED BY OVERSIZING THE HOLES (E,G,N) UNTIL CRACK REMOVAL AND CUT OUT THE ESep 20, 2007 · N719FD · Airbus A300B4622 · Wing, Attach FittingsSDR 07FDEA04128Skin · corrodedFUSELAGE SKIN AT LAP JOINT P 51, C 19-20 INTERNAL CORRODED REPAIR PERFORMED BY CUT OUT THE LAP JOINT AND INSTALL EXTERNAL DOUBLER IAW DRAWING R537-06279, APPROVED BY RAS/DABRE/7003251/2003 ISS A.Sep 20, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, Plate/SkinSDR 07FDEA04125Splice · corrodedFOUND CORROSION OUT OF LIMIT AT SPLICE C19, P 54 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 20, 2007 · N719FD · Airbus A300B4622 · Fuselage Main, StructureSDR 07FDEA04123Splice · corrodedFOUND CORROSION OUT OF LIMIT AT SPLICE C19, P 50 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 20, 2007 · N719FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR 07FDEA04122Shim · dentedFOUND SCRUB MARKS AT TORSIONS BOX EMERGENCY EXIT ON LT/RT CROSS SHIMS C56-57A, P15A-16. REPAIR PERFORMED BY REWORK TO SMOOTH CONTOUR IAW EA 6-5316-70333 AND RAS/DATLS/0001412/2003 ISS A.Sep 20, 2007 · N719FD · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR 07FDEA04119Skin · corrodedCORROSION ON SKIN INNER COUPLING PLATE AT C19, P53-54 REPAIR PERFORMED BY BLEND OUT UNTIL CORROSION REMOVAL IAW REA 6-5313-70343 AND RAS/DABRE/700324/2003 ISS A.Sep 20, 2007 · N719FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA02512Thrust Reverser · unknownON POWER-UP FOR TAKEOFF, NR 1 REVERSE UNLOCK LIGHT ILLUMINATED. EXTINGUISHED AFTER RETURNING THROTTLES TO IDLE. RETURNED TO GATE. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 28JUL07 "MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2. NR 1 TJul 18, 2007 · N719FD · Airbus A300B4622 · Engine Thrust ReverserSDR 06FDEA03265Engine · smokeON CLIMBOUT DEPARTURE CONTROL INFORMED US THAT TOWER SAID WE WERE EMITTING BLACK SMOKE OUT OF NR 1 ENGINE. ALL ENGINE PARAMETERS INDICATED NORMAL. ELECTED TO MAKE A PRECAUTIONARY LANDING. PER CREW DEBRIEF- CAPT REPORTED ALL NORMAL INDICATIONS, ON INBND LEGSep 12, 2006 · N719FD · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR 06FDEA1124Skin · dentedDENT IN UPPER FUSELAGE SKIN AT FRAME 69 BETWEEN STR 8L AND 9L APPROX 1.5 X 2" REF N00054. REPAIRED DENT IAW EA 6-5330-97635.Mar 16, 2006 · N719FD · Airbus A300B4622 · Fuselage Main, Plate/SkinSDR 06FDEA1123Repair · unknownRIGHT WING NR 3 SLAT EXISTING REPAIR REQUIRES FILLER TO BE REMOVED FOR NDT OF DOUBLER FOR MATERIAL IDENTIFICATION FOR ASSESSMENT OF REPAIR REF N00300. REMOVED AND REINSTALLED FILLER IAW A300-600 SRM 51-40-21.Mar 16, 2006 · N719FD · Airbus A300B4622 · Standard Practices/StructuresSDR 06FDEA0538Control Head · failedILS RECEIVER UNTUNABLE ON DESCENT INTO CLE. DIVERTED TO KPIT. REMOVED AND REPLACED ILS CONTROL HEAD. OPS CHECKS GOOD REF: A300 MM 34-36-15-4. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 889-2323-006, POS ONL SRL 145 TAG 67288A, ON MFG 889-2323-007Feb 4, 2006 · N719FD · Airbus A300B4622 · Landing and Taxi Aids
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