N724FD

Service difficulty reports · 218

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 = 'N724FD' 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 07FDEA04278Angle · damagedDAMAGED ANGLE SHEET BETWEEN FRAME 60-61, STGR 28 RT, CARGO DOOR AREA. REPLACEMENT OF ANGLE SHEET IAW SRM 51-72-10.Sep 25, 2007 · N724FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA04277Fitting · damagedDAMAGED FITTING BETWEEN FRAME 63-63A, STGR 43 RT, CARGO DOOR AREA. REPLACEMENT OF FITTING IAW SRM 51-72-10.Sep 25, 2007 · N724FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA04276Frame · crackedCRACKED HOLE "H1" ON FRAME 46 LT, STR 27. REPAIR PERFORMED BY OVERSIZING HOLE IAW SB A300-53-6122 AND REV 02 OF SB 53-6125 (OVERSIZING, FRAME FOOT CUT OUT AT HOLE H1 AND COLD EXPANSION), IAW EA 6-5315-82931.Sep 25, 2007 · N724FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA04272Skin · chafedLT OUTER FLAP CHAFING DAMAGE AT TOP SKIN AT RIB 4 AND 15A AFT OF T/E SKIN SPLICE. REPAIR PERFORMED BY SMOOTHLY BLEND THE DAMAGED AREAS WITHOUT INCREASING DEPTH IAW TD FOK/154/2005 ISSUE A, APPROVED BY EA 6-5753-92138 AND RAS/FOK/154/2005 ISSUE A.Sep 25, 2007 · N724FD · Airbus A300B4622R · Trailing Edge FlapsSDR 07FDEA04271Skin · chafedLT AND RT CENTER FLAP CHAFING DAMAGE AT TOP SKIN AT RIB 15 AND 23 AFT OF T/E SKIN SPLICE. REPAIR PERFORMED BY SMOOTHLY BLEND THE DAMAGED AREAS WITHOUT INCREASING DEPTH IAW TD FOK/153/2005 ISSUE A, APPROVED BY EA 6-5753-92137 AND RAS/FOK/153/2005 ISSUE A.Sep 25, 2007 · N724FD · Airbus A300B4622R · Trailing Edge FlapsSDR 07FDEA04268Skin · damagedFOUND OLD DAMAGE (DENTS AND BULGES) ON LEADING EDGE SKIN BETWEEN RIB 15-16 OF SLAT NR 2 LT. REPAIR PERFORMED BY CUT OUT SKIN AND INSTALLING EXTERNAL PATCH REPAIR IAW TD FOK/158/2005 ISSUE A, APPROVED BY EA 6-5743-92143 AND RAS/FOK/158/2005 ISSUE A.Sep 25, 2007 · N724FD · Airbus A300B4622R · Leading Edge DevicesSDR 07FDEA04265Plate · crackedCRACKED SHEAR PLATES BETWEEN FRAME 38-38.1, STRG 44 LT, FWD CARGO COMPARTMENT. REPAIR PERFORMED BY REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10.Sep 25, 2007 · N724FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA04264Plate · crackedCRACKED SHEARPLATES BETWEEN FRAME 38-38.1, STRG 44 RT AND BETWEEN FRAME 38.1- 38.2, STRG 44 LT, FWD CARGO COMPARTMENT. REPAIR PERFORMED BY REPLACEMENT OF BOTH SHEAR PLATES IAW SRM 51-72-10.Sep 25, 2007 · N724FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA04263Floorbeam · corrodedHEAVY CORROSION ON CROSSBEAM, FRAME 38.2 RT TO LT, Y-805 TO 805. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15/FIG 207.Sep 25, 2007 · N724FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 07FDEA04262Frame · corrodedCORROSION ON TEE SEGMENT FRAME 39 LOWER FLANGE BETWEEN STRINGER 52-53 LT. REPAIR PERFORMED BY CUTTING OUT THE DAMAGE PART AND REPLACE THE TEE SEGMENT, SPLICED WITH AN ANGLE AND A SPLICE IAW EA 6-5314-82906 AND RAS 038386/005/2005 ISSUE A.Sep 25, 2007 · N724FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA04260Web · crackedCRACKED WEB BETWEEN FRAME 16A-18, Y 2462, FLOOR STRUCTURE SECTION 12. REPLACEMENT OF WEB IAW SRM 51-72-10.Sep 24, 2007 · N724FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA04259Longeron · corrodedHEAVY CORROSION ON LONGERON BETWEEN FRAME 11-14, Y 730, FLOOR STRUCTURE SECTION 12. REPLACEMENT OF LONGERON IAW SRM 51-72-10.Sep 24, 2007 · N724FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA04257Skin · delaminatedRT ELEVATOR FRONT SPAR, UPPER AND LOWER SKIN DELAMINATED AND GLASS FIBER PLY DEBONDED. REPAIR PERFORMED BY INSTALLING HI-LOKS IN DELAMINATED SKIN NEAR LIGHTNING HOLE, FILLING EDGES WITH RESIN, BOND GLASS FIBER WITH RESIN, LEAVE DELAMINATION AT UPPER AND LOWERSep 24, 2007 · N724FD · Airbus A300B4622R · Elevator, Plate/SkinSDR 07FDEA04250Panel · wornWEARED HOLES IN LATERAL PANELS (INBOARD AND OUTBOARD), RIB 8 UPPER SPAR OF PYLON NR 1 LT. REPAIR PERFORMED BY INSTALLATION OF BUTTERFLY DOUBLERS ON BOTH PANELS IAW SRM 54-51-31/CONFIG 2/PB 201.Sep 24, 2007 · N724FD · Airbus A300B4622R · Nacelle/Pylon, Plate/SkinSDR 07FDEA04249Panel · wornWEARED HOLES IN LATERAL PANELS (INBOARD AND OUTBOARD), RIB 8 UPPER SPAR OF PYLON NR 2 RT. REPAIR PERFORMED BY INSTALLATION OF BUTTERFLY DOUBLERS ON BOTH PANELS IAW SRM 54-51-31/CONFIG 2/PB201.Sep 24, 2007 · N724FD · Airbus A300B4622R · Nacelle/Pylon, Attach FittingsSDR 07FDEA04246Skin Panel · wornELONGATED HOLES OF HYDRAULIC PIPE SUPPORT BRACKET AND LOWER SKIN PANEL NR 2, BOTH WINGS. REPAIR PERFORMED BY OVERSIZING HOLES, SPOTFACING AND BUSHING USING THE PRINCIPLES OF REPAIR INSTRUCTION R571-50532 IAW EA 6-5720-82902 AND RAS/BAE/1000997/2005 ISSUE A.Sep 24, 2007 · N724FD · Airbus A300B4622 · Wing, Plate/SkinSDR 06FDEA2371Warning System · malfunctionedAT OAK AS POWER WAS BROUGHT UP FOR T/O, GOT A NR 1 REV UNLOCKED LIGHT, HAD NOT YET TOGA'S. REDUCED POWER AND REJECTED T/O. TAXIED BACK TO NR 1, RAN UP ENGINE NR 1 AS PER MX CONVERSATION, NO LIGHT. THEN TOOK OFF UNEVENTFULLY. DID NOT RETURN TO GATE. ENGINJun 20, 2006 · N724FD · Airbus A300B4622R · Engine Thrust ReverserSDR 05FDEA04009Proximity Sensor · no testAFTER T/O GEAR WOULD NOT RETRACT IN EITHER POSITION. PITCH TRIM NR 1 TRIPPED AND WOULD NOT RESET. AUTO THROTTLE LEVERS WERE ON BUT THROTTLES WOULD NOT RESPOND. CAPT ADF/RMI FAILED. RETURNED TO MSY. ON LANDING THRUST REVERSE WOULD NOT DEPLOY CAPT ADC FAILNov 29, 2005 · N724FD · Airbus A300F4622R · Landing Gear Position and Warning
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