N722FD

Service difficulty reports · 191

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 = 'N722FD' 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 08FDEA04632Carriage · corrodedLEFT WING CENTER FLAP NR 3 TRACK CARRIAGE UPPER FLANGE ASSY IS CORRODED AT THE LUGS. REMOVED AND REPLACED THE LEFT NR 3 FLAP TRACK FWD CARRIAGE UPPER BRIDGE REF A300-600 AMM 27-54-27-4.Oct 30, 2008 · N722FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA04615Structure · crackedNR 2 ENGINE INBD T/R, CORE COWL SECTION HAS A CRACK AT THE AFT UPPER SECTION ABOVE THE LOCK HANDLE. MATERIAL ID PER P/W CMM 78-32-34, 0.050, PO 607468.1. HEAT TREAT IAW TPS 1003; REV "A" (HT102408.2). STOP DRILL THE CRACK TO 0.0625 PER P/W CMM 78-32-34. Oct 29, 2008 · N722FD · Airbus A300B4622R · Engine Thrust ReverserSDR 08FDEA04487Attach Fitting · crackedTHE 3RD LEFT SEAT TRACK INBD TRACK SUPPORT LINK IS CRACKED AT FRAME 48. REMOVED & REPLACED THE TRACK LINK FITTING IN REF TO SRM 51-40-21. APPLIED TOP COAT IN REF TO SRM 51-73-10.Oct 22, 2008 · N722FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04486Attach Fitting · crackedTHE 3RD LEFT SEAT TRACK INBD TRACK SUPPORT IS CRACKED AT FRAME 49. REMOVED & REPLACED THE TRACK LINK FITTING IN REF TO SRM 51-40-21. APPLIED TOP COAT IN REF TO SRM 51-73-10.Oct 22, 2008 · N722FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 08FDEA04485Attach Fitting · crackedTHE 3RD LEFT SEAT TRACK INBD TRACK SUPPORT IS CRACKED AT FRAME 48. REMOVED & REPLACED THE TRACK LINK FITTING IN REF TO SRM 51-40-21. APPLIED TOP COAT IN REF TO SRM 51-23-10.Oct 22, 2008 · N722FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04448Skin · gougedRIGHT OUTBD FLAP L/E INBD END IS GOUGED IN THE EXTERNAL SKIN.Oct 20, 2008 · N722FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA04389Frame · gougedMAIN CABIN FRAME 33 IS GOUGED AT APPROXIMATELY LONGERON 15 L.Oct 17, 2008 · N722FD · Airbus A300B4622R · Fuselage Main, FrameSDR 08FDEA04403Support · crackedNR 1 PYLON INBD SIDE PANEL SUPPORT IS CRACKED AT RIB 8A, (PANEL 414CR). REMOVED & REPLACED PYLON SIDE PANEL SUPPORT REF SRM 51-40-21. LOCATED & DRILLED FASTENER HOLES IN THE NEW PYLON SIDE PANEL SUPPORT REF SRM 51-40-44.Oct 17, 2008 · N722FD · Airbus A300B4622R · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA04370Skin · gougedLEFT OUTBD FLAP L/E IS GOUGED AT THE INBD END OF THE FLAP. BLENDED GOUGE SMOOTH IAW SRM 51-73-10. LT WING OUTBD FLAP LE NOSE SKIN BETWEEN RIB NR 1 & 2 FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00. FABBED & INSTALLED OUTBD FLAP LE REPAIR IAW SRM 57-50-00. TOct 15, 2008 · N722FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA04356Skin · corrodedAFT CARGO DOOR INTERNAL SKIN IS CORRODED AT THE FWD LOWER CORNER. REMOVED CORROSION IAW A300-600 SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 51-30-00. ORIGINAL MATERIAL 0.063. REMAINING MATERIAL 0.051. MATERIAL REMOVED 0.011. USED UT GAUGE T8Oct 15, 2008 · N722FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR 08FDEA04347Skin · gougedLEFT CENTER FLAP L/E HAS A GOUGE IN THE EXTERNAL SURFACE LOCATED APPROX MIDWAY BETWEEN NR 3 & 4 FLAP TRACKS. REPAIRED LEFT CENTER FLAP L/E FROM RIB 16 TO RIB 17 IAW SRM 57-50-00.Oct 14, 2008 · N722FD · Airbus A300B4622R · Trailing Edge FlapsSDR 08FDEA04346Cusp Web · crackedMAIN CARGO DECK RT CUSP 4 INCHES AFT OF FRAME 79, WEB IS CRACKED. REMOVED CRACKED WEB IAW SRM 51-40-21 & INSTALLED A NEW WEB IAW SRM 51-40-21 & DWG A53981113.Oct 14, 2008 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA04345Cusp Web · crackedMAIN CARGO DECK LT CUSP 4 INCHES AFT OF FRAME 79, WEB IS BENT & CRACKED. REMOVED CRACKED WEB IAW SRM 51-40-21 & INSTALLED NEW WEB IAW DWG NR A53981113.Oct 14, 2008 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 08FDEA04331Stiffener · crackedRIGHT WING AILERON ACTUATOR BEAM STIFFENER IS CRACKED JUST OUTBD OF RIB 6A INSIDE PANEL 675 BB. REMOVED & REPLACED STIFFENER IAW SRM 51-40-21; PARA 5 & 7 AND DWG 25A57246859.Oct 13, 2008 · N722FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR 08FDEA04330Stiffener · crackedLEFT WING AILERON ACTUATOR BEAM STIFFENER IS CRACKED JUST OUTBD OF RIB 6A. REMOVED LEFT WING AILERON ACTUATOR BEAM UPPER ATTACH STIFFENER JUST OUTBD OF RIB 6A IAW A300-600 SRM 51-40-21. FABRICATED A NEW STIFFENER IAW FEDEX EA 6-5720-123668. LEFT WING AILERONOct 13, 2008 · N722FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR 08FDEA04327Frame · crackedLEFT HORIZONTAL STAB L / E PANEL 341 AB OUTBD BOTTOM FORMER IN CRACKED. STOP DRILLED THE CRACK IAW SRM 51-23-10. HFEC STOP DRILL PER NTW 51-10-08. VERIFIED THE CRACK STOPS. FABRICATED & INSTALLED REPAIR ANGLES IAW SRM 55-12-19.Oct 13, 2008 · N722FD · Airbus A300B4622R · Horizontal Stabilizer, Spar/RibSDR 07FDEA02290Computer · faultedATB - AFTER T/O - ECAM AND OVH SYS 2 FLAP FAULT. UNABLE TO CLEAR FAULT. FOUND NR 2 SFCC FAULTING MAIN CONTROL VALVE UPON ARRIVAL. RESET SFCC AND RAN FLAPS, AGAIN FAULTED MAIN CONTROL VALVE. BOTH TIMES NR 2 FLAP SYS FAULT LIGHT ON OVERHEAD CAME ON AND WOULDJun 27, 2007 · N722FD · Airbus A300B4622R · Trailing Edge Flap Control SystemSDR 06FDEA03625Skin · damagedLEFT WING LOWER SURFACE PANEL 550NB PANEL LAND HAS ONE EA DRILL START NEXT TO HOLE COMPLIED WITH EA 6-5730-104975, OPENED HOLE TO 0.402, COLD WORKED AND FINAL REAMED TO 0.418. FABBED AND INSTALLED BUSHING AND DRILLED NEW HOLE IAW TD/J1/S1/03541/2006.Oct 12, 2006 · N722FD · Airbus A300B4622R · Wing, Plate/SkinSDR 06FDEA03416Web · corrodedFWD CARGO WEB, BETWEEN FRAMES 38 - 38.1 AT STR 43 LT CORRODED FWD AND AFT CORNERS. REMOVED AND REINSTALLED DUCT AFTER WEB REPAIR IAW A300-600 AMM 36-12-00-4. REMOVED CORROSION AND FOUND A 4" CRACK IN WEB IAW NTM 51-10-08. REMOVED AND REPLACED WEB IAW SRM Sep 25, 2006 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 06FDEA03409Track · misrepairedAFT CARGO COMP, L/R ROLLER TRACK NR 3 BETWEEN FS 62-63 HAS PREVIOUS REPAIR, 2 SPLICES ANGLE DOUBLER AT BOTTOM W/APPROX MEASUREMENTS 18 BY 2". PREVIOUSLY INSTALLED REPAIR LOCATED AT AFT CARGO LT SIDE ROLLER TRACK NR 3 BETWEEN FS 62-63 WAS DETERMINED NOT TO BE Sep 23, 2006 · N722FD · Airbus A300B4622R · Fuselage Main, StructureSDR 06FDEA03408Shear Plate · corrodedWEB CORRODED IN FWD CARGO BETWEEN FS 38.1 TO 38.2 AT STR 43L, REMOVED AND REPLACED SHEAR PLATE IAW A300-600 SRM 51-72-10.Sep 23, 2006 · N722FD · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 06FDEA03407Plate · crackedRT HORIZONTAL STAB COMPARTMENT BETWEEN FS 87 AND 86 WEB AT STR 36R IS DENTED AND CRACKED. REMOVED AND REPLACED PLATE AND L-SECTION AT RT HORIZONTAL STAB COMPARTMENT BETWEEN FS 87 AND 86 AT STR 36R IAW A300-600 SRM 51-72-10.Sep 23, 2006 · N722FD · Airbus A300B4622R · Horizontal Stabilizer Miscellaneous StructureSDR 06FDEA03371Crossbeam · misrepairedBULK CARGO FLOOR STRUCTURE CROSS BEAM FS 64 RT SIDE MID HAS PREVIOUS REPAIR 2 EACH SPLICES ANGLE DOUBLER WITH APPROX MEASUREMENTS OF 2X9". PREVIOUS INSTALLED REPAIR LOCATED AT BULK CARGO FLOOR STRUCTURE CROSS BEAM FRAME 64 RIGHT SIDE MID, WAS DETERMINED THAT Sep 19, 2006 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 06FDEA03370Floor Support · corrodedBULK CARGO FRAME 67 LEFT SIDE FLOOR LEVEL FLOOR BOARD SUPPORT HAS 2 EACH AREAS OF CORROSION AROUND TIE DOWN ADAPTER. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED FLOOR SUPPORT IAW A300-600 SRM 53-10-15.Sep 19, 2006 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 06FDEA03369Floorbeam · corrodedBULK CARGO COMP UNDER FLOOR STRUCTURE AT FRAME 67 BETWEEN STR 44 AND 48 HAS EXFOLIATION CORROSION, RT SIDE. REMOVED AND REPLACED FLOORBEAM AT FRAME 67 BETWEEN STR 44R AND STR 44L IAW A300-600 SRM 53-10-15.Sep 19, 2006 · N722FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 06FDEA03368Floorbeam · corrodedBULK CARGO FRAME 67 FLOOR LEVEL CENTERLINE, 1 AREA OF CORROSION ON THE FLOORBEAM. REMOVED CORROSION, MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-00 FIG 104, TABLE 108. REMOVED FLOORBEAM AT FS 67, FABBED AND INSTALLED NEW FLOORBEAM IAW A300Sep 19, 2006 · N722FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 06FDEA03367Structure · corrodedBULK CARGO COMPT UNDER FLOOR STRUCTURE BETWEEN FS 63 AND 64 AT STR 54 HAS CORROSION UNDER NUTPLATE. REMOVED AND REPLACED PROFILE LONGITUDINAL IAW A300-600 SRM 51-40-21.Sep 19, 2006 · N722FD · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR 06FDEA03366Shear Plate · corrodedFWD CARGO PIT, WEB CORRODED BETWEEN FRAME 36 AND 37 AT STR 43 RT FWD AND AFT LOWER CORNERS. REMOVED AND REPLACED SHEAR PLATE BETWEEN FRAME 36 AND 37 AT STR 43 RT IAW A300-600 SRM 51-72-10.Sep 19, 2006 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 06FDEA03365Angle · crackedAVIONICS COMPARTMENT ZONE 122, MAIN CABIN FLOOR CROSS BEAM RIB 10 RT SIDE HAS CRACKED FITTING. REMOVED AND REPLACED ANGLE ON MAIN CARGO FLOOR CROSS BEAM AT RIB 10 IAW A300-600 SRM 51-72-10.Sep 19, 2006 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 06FDEA03364Crossbeam · corrodedCORROSION ON CROSS BEAM AT FRAME 16 BETWEEN SEAT TRACK 4R AND 5R IN UPPER MAIN DECK CARGO COMP ZONE 220. REMOVED AND REPLACED FLANGE DUE TO CORROSION BLENDED OUT OF LIMITS IAW A300-600 SRM 51-74-10, 53-21-15, AND 51-72-10.Sep 19, 2006 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 06FDEA03362Web · damagedWEB CRACKED AND PUNTURED JUST AFT OF CLS BEAR CLAW AT FS 37 REMOVED AND REPLACED WEB IAW A300-600 SRM 51-72-10.Sep 19, 2006 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 06FDEA03361Plate · damagedFWD CARGO DOOR, FWD LOWER CORNER DENTED AND GOUGED. REMOVED AND REPLACED CORNER PLATE IAW A300-600 SRM 51-40-21 AND 51-72-10.Sep 19, 2006 · N722FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR 06FDEA03360Track · misrepairedFWD CARGO COMP LT ROLLER TRACK NR 2 BETWEEN FRAME 38.1 TO 38.2 HAS PREVIOUS REPAIR, A FLAT DOUBLER INSIDE ROLLER TRACK COVERING THE DRAIN PORT WITH APPROX MEASUREMENTS 8X4". THIS REPAIR AT FWD CARGO LT SIDE ROLLER TRACK NR 2 BETWEEN FS 38.1 TO 38.2 WAS FOUND Sep 19, 2006 · N722FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03359Beam · corrodedAFT CARGO UNDER FLOOR AT FS 60 UNDER ROLLER TRACK NR 1 HAS EXFOLIATING CORROSION ON FWD AND AFT SIDE OF THE SUPPORT STRUCTURE REMOVED AND REPLACED BEAM ASSY IAW A300-600 SRM 53-10-15.Sep 19, 2006 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 06FDEA03358Structure · corrodedAFT CARGO COMP UNDER FLOOR SUPPORT STRUCTURE AT FS 56 UNDER ROLLER TRACK NR 1 HAS EXFOLIATING CORROSION ON THE AFT SIDE. REPLACED AFT CARGO UNDER FLOOR SUPPORT STRUCTURE AT FS 56 UNDER ROLLER TRACK NR 1 IAW A300-600 SRM 53-10-15 FIG 207.Sep 19, 2006 · N722FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 06FDEA03357Floorbeam · misrepairedAFT CARGO COMP FLOOR CROSSBEAM FS 63 LT SIDE BETWEEN LT ROLLER TRACK 2-3, HAS PREVIOUS REPAIR 2 EACH SPLICES ANGLE DOUBLER WITH APPROX MEASUREMENTS 9 BY 2.75". REPAIR WAS FOUND TO BE INCORRECT PER A300-600 SRM 53-10-15 FIG 207, SPLICES ARE MADE OF INCORRECT MSep 19, 2006 · N722FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 06FDEA2257Uplock · malfunctionedAFTER GEAR RETRACTION RT MAIN GEAR DOOR LIGHT STAYED ILLUMINATED. PERFORMED QRH PROCEDURES. THE INBOUND CREW REPORTED THE RT GEAR DOOR OPEN PRIMARY AND SECONDARY INDICATIONS DID FLICKER ON AND OFF INDIVIDUALLY AT DIFFERENT TIMES ONLY TO STAY ILLUMINATED MOSTJun 8, 2006 · N722FD · Airbus A300B4622R · Landing Gear Retraction/Extension SystemSDR 06FDEA1698Switch · failedRIGHT MLG DOOR OPEN AFTER T/O AFTER RETRACT. SWITCHED POS DET TO SYS 1 WITH SAME INDICATION ON ECAM DOOR LIGHT REMAINED ON OVERHEAD. REMOVED AND REPLACED RT GEAR DOOR SWITCH 28GB IN REF TO A300-600 AMM 32-00-00-4. PERFORMED LANDING GEAR INDICATION FUNCTIONAMay 3, 2006 · N722FD · Airbus A300B4622R · Landing Gear Position and WarningSDR 05FDEA01217Hose · leakingMAIN DECK CARGO SMOKE CAME ON DURING CLIMBOUT. RETURNED, LANDED, F/O SMELLED ODOR JUST PRIOR TO MAIN DECK CARGO SMOKE INDICATION AND THE SCENT DISAPPEARED AFTER NR 2 PACK WAS TURNED OFF. FOUND OIL ON BOTH PACK COALESCER BAGS. OIL LEAK AT APU BEING INJESTED May 6, 2005 · N722FD · Airbus A300B4622R · APU Bleed Air SystemSDR 04FDEA00064Altimeter · malfunctionedAT AROUND 60 - 70 KTS ON FIRST TAKEOFF, GOT A NAV ADC FAILURE ON ECAM. AFTER CLEARING RUNWAY FAILURE WENT AWAY. A SECOND TAKEOFF INITIATED AND UNABLE TO TOGA AND GOT A RUNWAY POSITION ERROR. CHECKED MTP AT BLOCK-IN, NO FAULTS OR LIGHTS SET. PERFORMED BITE Jan 7, 2004 · N722FD · Airbus A300B4622R · Altimeter, Barometric/EncoderSDR 02FDEA00217Frame · crackedCRACK IN UPPER RADIUS RT FRAME.Mar 7, 2002 · N722FD · Airbus A300B4622R · Fuselage Main, Frame
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