N721FD

Service difficulty reports · 231

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 = 'N721FD' 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 08FDEA02856Stringer · corrodedAFT CARGO COMPT, STRINGER 54 LT WITH CORROSION BETWEEN FR 65 AND FR 66. STRINGER 54 LT WAS REPAIRED AS PER SRM 53-10-14 FIG 201.Jun 5, 2008 · N721FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 08FDEA02855Stringer · corrodedAFT CARGO COMPT, STRINGER 53 LT WITH CORROSION NEXT TO RIVETS BETWEEN FR 65 AND FR 66. STRINGER 53 LT WAS REPLACED AS PER SRM 53-10-14 FIG 201.Jun 5, 2008 · N721FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 08FDEA02753Cargo Track · corrodedFWD CARGO COMPT ROLLER TRACK NR 4 BETWEEN FR 27-32 WITH CORROSION. NEW ROLLER TRACK INSTALLED AS PER AMM 25-52-51-4-01.Jun 2, 2008 · N721FD · Airbus A300B4622R · Cargo CompartmentsSDR 08FDEA02752Cargo Track · corrodedFWD CARGO COMPT ROLLER TRACK NR 3 BETWEEN FR27-32 WITH CORROSION. NEW ROLLER TRACK INSTALLED AS PER AMM 25-52-21-4 01.Jun 2, 2008 · N721FD · Airbus A300B4622R · Cargo CompartmentsSDR 08FDEA02059ABulkhead · crackedAFT PRESSURE BULKHEAD - CRACK IN THE SKIN AT INTERIOR OF A HOLE (AT 3 O'CLOCK) IN THE APU DUCT FLANGE ATTACHMENT. AFT PRESSURE BULKHEAD SKIN WAS REPAIRED AS PER EA 6-5310-121644.May 28, 2008 · N721FD · Airbus A300B4622R · Fuselage Main, BulkheadSDR 08FDEA02707Seat Track · wornSEAT-TRACK AT Y-1959 WORN AT FRAME 29. SEAT-TRACK WAS REPAIRED AS PER FEDEX EA 6-5310-117332.May 28, 2008 · N721FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02092Skin · corrodedLT WING, WING TOP SKIN FOUND WITH CORROSION NEXT TO REAR SPAR, BETWEEN RIBS 27 AND 28. REPAIRED AS PER EA 6-5710-121647.May 28, 2008 · N721FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA02059Seat Track · damagedCABIN FLOOR, SEAT-TRACK Y-1959 DAMAGED AT FR 29.May 28, 2008 · N721FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02599Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON INBD FLAP RT, RIB 24B, LOWER AND TOP SKIN T/E. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO EXISTING SRM REPMay 27, 2008 · N721FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA02706Fitting · wornPYLON NR 2, WING/PYLON AFT ATTACH FITTING AT RIB 18 WITH PLAY AT BEARING HOUSING. THE FEDEX EA 6-5451-117329 WAS ACCOMPLISHED.May 26, 2008 · N721FD · Airbus A300B4622R · Nacelle/Pylon, Attach FittingsSDR 08FDEA02791Seat Track · corrodedCABIN FLOOR, CORROSION ON TRACK Y730 BETWEEN FR 11-11A. TRACK REPLACED AS PER SRM 51-72-10.May 23, 2008 · N721FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02621Seat Track · corrodedCABIN FLOOR, CORROSION ON SEAT-TRACK Y953 BETWEEN FRAMES 11 AND 12. SEAT-TRACK REPLACED IN ACCORDANCE WITH SRM 51-72-10.May 23, 2008 · N721FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02058Seat Track · corrodedCABIN - FLOOR - SEAT-TRACK Y953 WITH CORROSION NEXT TO FRAME 15A. REPLACED IAW SRM 51-72-10.May 21, 2008 · N721FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02589None · nonePREVIOUS REPAIR FOUND LOCATED ON RUDDER RT STA270-869 RIB BR2-7, OUTER SKIN. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PERMANENT REPAIR WAS PERFORMED IAW FEDEX EA 6-5540-118158R. NOT May 21, 2008 · N721FD · Airbus A300B4622R · Standard Practices/StructuresSDR 08FDEA02382Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON RUDDER RT STA 270-869 RIB BR 2-7, OUTER SKIN. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR WAS FOUND IAW FEDEX EA-6-118158R.May 21, 2008 · N721FD · Airbus A300B4622R · Rudder, Plate/SkinSDR 08FDEA02790Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON LT FUSELAGE, STA 4415-4521 AT FR 68-70 BETWEEN STGR 36-44 LT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR NOT IN ACCORDANCE WITH PREVIOMay 19, 2008 · N721FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA02623Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON FUSELAGE LT STA 1212-1260, STGR 28-30 LT, FR 15-16A, BELOW FWD LT DOOR. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMIANTION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO May 19, 2008 · N721FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA02622Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON LT WING, RIB 4-5, AT SHROUD BOX TOP SKIN. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR NOT IN ACCORDANCE WITH APPROVED DATA. NEW REPAIR INSTMay 19, 2008 · N721FD · Airbus A300B4622R · Wing, Plate/SkinSDR 08FDEA02620Seat Track · corrodedPREVIOUS REPAIR FOUND LOCATED ON SEAT-TRACK LT, STA Y953, FRAME 14-14C. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUS REPAIRED PART REPLACED BY NEW SEAT-TRACK Y953 IN ACCORDANCE May 19, 2008 · N721FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02057Seat Track · deformedCABIN FLOOR, DEFORMATION ON SEAT-TRACK Y1959 BETWEEN FR 20 AND 21.May 19, 2008 · N721FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02056Structure · damagedFWD CARGO COMPT, SCRATCHES AND DEFORMATIONS AT FRAME 20A BETWEEN STGR 39-41 RT.May 14, 2008 · N721FD · Airbus A300B4622R · Fuselage Main, StructureSDR 07FDEA04754Autothrust Sys · failedON TAKEOFF ROLL LIMC 17R ACCELERATED TO 120KTS CAPTS PFD WENT TOTALLY BLANK, FOLLOWED BY BOTH ATS SWITCHES DISENGAGING. HIGH SPEED ABORT FOLLOWED BY RTO V LIST. TAXI BACK TO GATE. ACN RELEASED FOR SERVICE PER MEL/CDL: 22-30-01-C ATS 1 AND 2 - INOP. ALL THNov 8, 2007 · N721FD · Airbus A300B4622R · Auto Throttle SystemSDR 06FDEA2914Control Unit · jammedGREEN SYSTEM SERVO CONTROL JAMMED. T/S AND REMOVED AND REPLACED JAMMING DECTECTION CONTROL UNIT (4CB) PERFORMED OP`S TEST AND NO HELP REINSTALLED OLD UNIT BACK ON A/C. ALL WORK DONE IAW AMM 27-14-17-4. STILL TROUBLESHOOTING AT THIS TIME. REMOVED AND REPLACEAug 9, 2006 · N721FD · Airbus A300* · Hydraulic System, MainSDR 05FDEA04114Web · bentW/O 00030954, NR N00541, HORIZ STAB COMPT 2 WEBS BETWEEN FRAMES C85 AND C87 BENT 12TH STRINGER UP FROM 0 BL STRINGER AND 1 WEB BETWEEN FRAME C86 AND C87 11TH STRINGER UP FROM O BL STRINGER ("FROM BOTTOM STRINGERS"). REMOVED 3 WEBS, INSTALLED 3 WEBS IAW SRM 51Dec 4, 2005 · N721FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 05FDEA04111Angle · corrodedFWD CARGO COMPT BELOW ROLLER TRAY SUPPORT ANGLE EXFOLIATED 1" FWD OF FRAME C33 RBL 56". REMOVED AND REPLACED ANGLE SUPPORT IAW SRM 51-40-2. FABRICATED SUPPORT ANGLES (2 EACH) PER MAE TRAVELER T5/559357 AND T5/560339. FABRICATED WED (SHEAR WALL) T5/560340 LODec 4, 2005 · N721FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 05FDEA03896Fitting · interferenceCOMPLY WITH EA6-5310-92354, FUSELAGE-SB53-6111- FR46 FITTING/DOUBLER INTERFERENCE. COMPLIED WITH EA 6-5310-92354.Nov 18, 2005 · N721FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 05FDEA03812Rib · crackedNR 1 PYLON FAIRING 475CL INNER BODY NR 5 AND NR 6 RIBS ARE CRACKED.Nov 14, 2005 · N721FD · Airbus A300B4622R · Nacelle/Pylon, Main FrameSDR 05FDEA03785Attach Angle · crackedLT WING IB FIXED L/E PNL IB SUPPORT WEB LWR ATTACH ANGLE HAS CRACK AT JUNCTION OF KRUEGER AND NR 1 SLAT.Nov 13, 2005 · N721FD · Airbus A300B4622R · Leading Edge DevicesSDR 05FDEA03751Floorbeam · crackedAVIONICS COMPT FLOORBEAM FS 10 RBL 40 ANGLE IS CRACKED.Nov 10, 2005 · N721FD · Airbus A300F4622R · Fuselage Main, Floor BeamSDR 05FDEA03750Bracket · crackedNR 1 PYLON FAIRING 475CL RT FWD BRACKET CRACKED.Nov 10, 2005 · N721FD · Airbus A300B4622R · Nacelle/Pylon Miscellaneous StructureSDR 02FDEA00216Frame · crackedCRACK IN UPPER RADIUS RH. ** S/D ** COMINGFeb 8, 2002 · N721FD · Airbus A300B4622R · Fuselage Main, Frame
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