N725FD

Service difficulty reports · 221

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 = 'N725FD' 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 08FDEA04302Skin · gougedSKIN DAMAGE LOCATED AT FR46/47 S41L. REPAIRED AS PER EA 6-5330-121701.Sep 9, 2008 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA04301Skin · gougedSKIN DAMAGE LOCATED AT FR40/41 AND S37L. REPAIRED AS PER EA 6-5330-121701.Sep 9, 2008 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA04300Skin · gougedSKIN DAMAGE LOCATED AT FR47/48 S41LT. REPAIRED AS PER EA 6-5330-121701.Sep 9, 2008 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 08FDEA03526Selector Valve · failedLANDING GEAR FAILED TO RETRACT, FOLLOWED ECAM AND QRH GEAR HANDLE DOWN AND RETURNED TO LAND. SYSTEM B WAS USED AND SYS A DID NOT WORK EITHER. REMOVED AND REPLACED LANDING GEAR ELECTRO HYDRAULIC SELECTOR VALVE 3GA PRECAUTIONARY. PERFORMED LEAK CHECK SATISFACAug 19, 2008 · N725FD · Airbus A300B4622R · Landing Gear Retraction/Extension SystemSDR 08FDEA00261Connector · damagedON DESCENT NR 1 ENG THRUST WOULD NOT INCREASE, FOLLOWED BY OIL PRESS LOW WARNING. PRESS SHOWED NEAR ZERO, S/D ENG NR 1, ENG NR 1 WINDMILL APPROX 10 MIN, PER CREW DEBRIEF, ON DESCENT WITH THROTTLES AT IDLE. ADVANCED THROTTLES TO LEVEL OFF, NR 1 ENG W/N RESPONJan 23, 2008 · N725FD · Airbus A300B4622R · Engine Oil System WiringSDR 08FDEA00247Connector · damagedON DESCENT NR 1 ENG THRUST WOULD NOT INCREASE, FOLLOWED BY OIL PRESSURE LOW WARNING, PRESSURE SHOWED NEAR ZERO, SHUT DOWN ENG NR 1 (ENG NR 1 WINDMILL APPROX 10 MIN). PER FLIGHT CREW DEBRIEF: THEY WERE ON DESCENT WITH THROTTLES AT IDLE. ADVANCED THROTTLES Jan 23, 2008 · N725FD · Airbus A300B4622R · Engine Oil System WiringSDR 07FDEA03325Skin · misrepairedOLD FLUSH DOUBLER REPAIR FOUND ON SLAT NR 2 RT THAT REQUIRES REWORKING. REPAIR RENEWED IAW TD FOK/065/2006 ISSUE C, APPROVED BY EA 6-5740-99182A AND RAS/FOK/065/2006 ISSUE A.Sep 3, 2007 · N725FD · Airbus A300B4622R · Leading Edge DevicesSDR 07FDEA03324Beam · crackedAFTER HFEC INSPECTION FOUND 18MM LONG CRACKS IN GANTRY BEAM 3 LT AND RT AT FRAME 49 LOWER INBOARD FLANGE. CRACK REPAIR PERFORMED ON FRAME 49 GANTRY 3 LT AND 3 RT PER DRW R538-10426 WITH ENLARGED DIAPHRAGM WORK AREA WHILE MAINTAINING AN EDGE DISTANCE OF 1.5 RISep 3, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, StructureSDR 07FDEA03323Attach Fitting · crackedCRACKED FITTING AT FRAME 63 OF SILL BEAM. REPLACEMENT OF FITTING IAW SRM 51-72-10.Sep 3, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 07FDEA03320Fitting · corrodedHEAVY CORROSION AT ASSY FITTING FRAME 63, STRG 45 LHS. REPLACEMENT OF FITTING IAW SRM 51-72-10.Sep 3, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 07FDEA03315Rib · crackedCRACK DAMAGE ON LT WING LEADING EDGE CLOSING RIB WOFX-277.9. REPAIR PERFORMED BY TRIMMING OUT THE DAMAGED AREA, LOCALLY MANUFACTURING AND INSTALLING AN INFILL PACKER AND REPAIR ANGLE USING EXISTING AND NEW FASTENER POSITIONS IAW TD/J1/02572/2006 ISSUE A APPSep 3, 2007 · N725FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR 07FDEA03314Frame · damagedTOOLING MARKS WERE FOUND AT FRAME 12A BETWEEN STRG 26-27 RT. REPAIR PERFORMED BY REMOVING FASTENERS, SMOOTH BLEND OUTS, FOR ELIMINATE THE DEEPEST MARK A 13MM SKIN HOLE DIA WAS PERFORMED, ROTO TEST AND HFEC INSPECTION WITH NIL FINDINGS AND ONE 13MM DIAMETER Sep 3, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA03313Frame · damagedNUMEROUS FASTENERS WERE FOUND TO BE NON CONFORMING AND ELONGATED ON FITTING FRAME 12A, FRAME 12A AND CORNERS RT AND LT SIDES. REPAIR PERFORMED BY DETAILED VISUAL AND ROTO TEST INSPECTIONS IN DAMAGED HOLES. REPLACMENT OF FITTING, CORNER SPLICE AND CORNER ANSep 3, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA03312Angle · damagedNUMEROUS FASTENERS WERE FOUND TO BE NON CONFORMING AND ELONGATED ON FITTING FRAME 12A, FRAME 12A AND CORNERS RT AND LT SIDES. REPAIR PERFORMED BY DETAILED VISUAL AND ROTO TEST INSPECTIONS IN DAMAGED HOLES, REPLACMENT OF FITTING, CORNER SPLICE AND CORNERSep 3, 2007 · N725FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03311Fitting · misrepairedNUMEROUS FASTENERS WERE FOUND TO BE NON CONFORMING AND ELONGATED ON FITTING FRAME 12A, FRAME 12A AND CORNERS RT AND LT SIDES. REPAIR PERFORMED BY DETAILED VISUAL AND ROTO TEST INSPECTIONS IN DAMAGED HOLES, REPLACEMENT OF FITTING, CORNER SPLICE AND CORNER Sep 3, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, StructureSDR 07FDEA03310Fitting · misrepairedNUMEROUS FASTENERS WERE FOUND TO BE NON CONFORMING AND ELONGATED ON FITTING FRAME 12A, FRAME 12A AND CORNERS RT AND LT SIDES. REPAIR PERFORMED BY DETAILED VISUAL AND ROTO TEST INSPECTIONS IN DAMAGED HOLES, REPLACEMENT OF FITTING, CORNER SPLICE AND CORNER ANGLSep 3, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, StructureSDR 07FDEA03309Fitting · damagedNUMEROUS FASTENERS WERE FOUND TO BE NON CONFORMING AND ELONGATED ON FITTING FRAME 12A, FRAME 12A AND CORNERS RT AND LT SIDES. REPAIR PERFORMED BY DETAILED VISUAL AND ROTO TEST INSPECTIONS IN DAMAGED HOLES, REPLACEMENT OF FITTING, CORNER SPLICE AND CORNER ANSep 3, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 07FDEA03282Skin Panel · dentedDENT FOUND AT FRAME 65, STRG 41-42 RT. REPAIR PERFORMED BY REMOVAL OF AFFECTED FASTENERS, ROTO-TEST INSPECTION WITH NIL FINDINGS, EDDY CURRENT INSPECTION OF SKIN, INTERNAL BONDED DOUBLER AND INTERNAL BUTT STRAP WITH NIL FINDINGS AND INSTALLATION OF NEW FASTENAug 31, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA03296Floor Support · damagedZ-SECTION ANGLE ( X3892, Y730 ) OF LAVATORY FLOOR STRUCTURE IS CRACKED BY DAMAGE UNDER THE FITTING ( Z-174, Y925 ). REPAIR PERFORMED IAW SRM 51-71-40/FIG 201.Aug 31, 2007 · N725FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03295Rib · chafedFOUND AT ALL SPEED AILERON HINGE RIBS LT/RT DEEP CHAFING MARKS, ON THE INTERMEDIATE RIB 6A POSITIONS ON BOTH WINGS. REPAIR PERFORMED BY BLENDING AND REPROTECTION AT POSITIONS RIB 6A AS PER TD/J1/S1/0234/2006 ISSUE B APPROVED BY EA 6-5751-99137 AND RAS/BAE/1Aug 31, 2007 · N725FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR 07FDEA03294Rib · chafedFOUND AT ALL SPEED AILERON HINGE RIBS LT/RT DEEP CHAFING MARKS. ON THE INTERMEDIATE RIBS WIAX21-9 POSITIONS ON BOTH WINGS, DAMAGE WAS ALSO FOUND AT THE INTERMEDIATE RIB WIAX13-9 ON THE RT WING. REPAIR PERFORMED BY BLENDING AND REPROTECTION AT POSITIONS RIBAug 31, 2007 · N725FD · Airbus A300B4622R · AileronsSDR 07FDEA03293Rib · chafedFOUND AT ALL SPEED AILERON HINGE RIBS LT/RT DEEP CHAFING MARKS. ON THE INTERMEDIATE RIBS WIAX21-9 POSITIONS ON BOTH WINGS, DAMAGE WAS ALSO FOUND AT THE INTERMEDIATE RIB WIAX13-9 ON THE RT WING. REPAIR PERFORMED BY BLENDING AND REPROTECTION AT POSITIONS RIBAug 31, 2007 · N725FD · Airbus A300B4622R · AileronsSDR 07FDEA03292Attach Fitting · damagedDAMAGED FITTING AT FRAME 63A BETWEEN STRG 42-46, RHS, ATTACH FITTING REPLACED IAW SRM 51-72-10.Aug 31, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 07FDEA03290Beam · corrodedCORROSION ON AFT CARGO DOOR SILL BEAM AT FRAME 59A AND NEAR FRAME 60, OUT OF LIMIT REPAIR PERFORMED BY EXTEND THE T-SECTION AND INSTALLING FILLER/SHIM AS PER TD/K4/S1/20580/2006. ALL OTHER REQUIREMENTS AS PER SRM 53-17-18 / FIG 204. APPROVED BY EA 6-5317-992Aug 31, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, StructureSDR 07FDEA03289Floor Support · chafedAFTER REMOVAL OF OLD GROOVES AT LONGITUDINAL BEAMS (LT & RT) FRAME 73A-75A, THE REMAINING THICKNESS IS OUT OF LIMIT. BOTH PARTS REPLACED IAW SRM 51-72-10.Aug 31, 2007 · N725FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03288Skin Panel · failedOLD REPAIR DOUBLER PLATES ON BOTTOM WING SKIN PANEL NR 1 BOTH RHS AND LHS, BETWEEN RIB 8 AND TRACK 4 FWD OF FRONT SPAR ARE NOT PERFORMED IAW DRW R572- 40179/PG 9 (SB A300-57-6019). IN ADDITION THE INSTALLED HI-LOCKS ARE IN BAD CONDITION. REPAIR RENEWED BY IAug 31, 2007 · N725FD · Airbus A300B4622R · Wing, Plate/SkinSDR 07FDEA03287Skin Panel · dentedDENT WITH SCRATCH IN SKIN BETWEEN FRAME 14A-15 CLOSE TO STRG 30-32 LT. REPAIR PERFORMED BY BLEND OUT SCRATCH, HFEC INSPECTION OF SKIN WITH NIL FINDINGS AND INSTALLATION OF OVERSIZED FASTENERS IN ROTOTESTED HOLES OF ADJACENT STRINGER IAW EA 6-5312-99150 AND RAAug 31, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA03283Frame · damagedMISDRILLED HOLE IN AFT FITTING FRAME 47 LT, STRG 24 NEAR HOLE G OF SB 53-61-23. REPAIR PERFORMED BY SPOTFACING THE MISDRILLED HOLE, OVERSIZING HOLE G AND INSTALLING FASTENER NSA5357-4 IAW EA 6-5315-99153 AND RAS 0453451/012/2006 ISSUE A.Aug 31, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA03281Diaphragm · damagedTOOLING MARKS AT GANTRY DIAPHRAGM BETWEEN FRAME 51-52 NEAR BEAM 5 RT. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-99148 AND RAS 043415/014/2006.Aug 31, 2007 · N725FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03280Beam · corrodedFOUND HEAVY CORRODED BEAM ON RT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11.Aug 31, 2007 · N725FD · Airbus A300B4622R · Wing Main, Frame StructureSDR 07FDEA03279Beam · corrodedFOUND HEAVY CORRODED BEAM ON RT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11.Aug 31, 2007 · N725FD · Airbus A300B4622R · Wing Main, Frame StructureSDR 07FDEA03278Fitting · corrodedFOUND HEAVY CORRODED FITTING ON RT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11.Aug 31, 2007 · N725FD · Airbus A300B4622R · Wing, Attach FittingsSDR 07FDEA03277Bracket · corrodedFOUND HEAVY CORRODED BRACKET ON RT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11.Aug 31, 2007 · N725FD · Airbus A300B4622R · Wing, Attach FittingsSDR 07FDEA03276Bracket · corrodedFOUND HEAVY CORRODED BRACKET ON RT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11.Aug 31, 2007 · N725FD · Airbus A300B4622R · Wing, Attach FittingsSDR 07FDEA03275Bracket · corrodedFOUND HEAVY CORRODED BRACKET ON LT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11.Aug 31, 2007 · N725FD · Airbus A300B4622R · Wing, Attach FittingsSDR 07FDEA03274Fitting · corrodedFOUND HEAVY CORRODED FITTING ON LT WING IN KRUEGER FLAP AREA, FRAME 38-39. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11.Aug 31, 2007 · N725FD · Airbus A300B4622R · Wing, Attach FittingsSDR 07FDEA03273Sill · corrodedCORROSION AT FWD CARGO DOOR SILL BEAM, BETWEEN FRAME 20A-25A, STRG 43-44 RT REPAIR PERFORMED BY CUT THE UPPER FLANGE OF CORNER FITTING AT C24 AND INSTALLING REPAIR ANGLE IAW EA 6-5313-99224 AND RAS/DABRE/7006397/2006 ISSUE A.Aug 31, 2007 · N725FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03271Stringer · debondedDEBONDED STRINGER ON P36-40, FRAME 20-24 LT. REPAIR PERFORMED BY INSTALLING RIVETS IAW SRM 53-10-14 / FIG 202.Aug 31, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA03270Plate · damagedDAMAGED CORNER SECTION AT LT PYLON AFT MOUNT FITTING REPAIR PERFORMED BY BLEND OUT TO SMOOTH PROFILE AND NDT INSPECTION FOR CRACK FREE IAW EA 6-5720-99222 AND RAS/BAE/1002436/2006 ISSUE A.Aug 31, 2007 · N725FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR 07FDEA03269Plate · damagedDAMAGED CORNER SECTION AT RT PYLON AFT MOUNT FITTING REPAIR PERFORMED BY BLEND OUT TO SMOOTH PROFILE AND NDT INSPECTION FOR CRACK FREE IAW EA 6-5720-99222 AND RAS/BAE/1002436/2006 ISSUE A.Aug 31, 2007 · N725FD · Airbus A300B4622R · Nacelle/Pylon, Main FrameSDR 07FDEA03268Beam · corrodedHEAVY CORROSION AT AFT CARGO DOOR SILL BEAM, BETWEEN FRAME 63-63A, STRG 42-43 RT REPAIR WAS PERFORMED IAW SRM 53-17-18/FIG 205.Aug 31, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, StructureSDR 07FDEA03267Floorbeam · corrodedTOP CAP BEAM FOUND WITH HEAVY CORROSION ON C27 RT CARGO FLOOR STRUCTURE. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 / FIG 207.Aug 31, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 07FDEA03266Frame · corrodedCORROSION FOUND ON FWD FACE OF FRAME 92 ON DOUBLER. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Aug 31, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA03265Frame · corrodedCORROSION FOUND ON FWD FACE OF FRAME 92 ON SEVERAL ANGLES. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Aug 31, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA03264Frame · corrodedCORROSION FOUND ON FWD FACE OF FRAME 92 ON T-SECTION. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Aug 31, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA03262Fitting · crackedCORNER FITTING AT FRAME 30 RT IS CRACKED. REPAIR WAS PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Aug 31, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, StructureSDR 07FDEA03261Skin Panel · damagedFOUND THE HYDRAULIC FITTING HOLES IN PYLON SUPPORT BRACKET IN LOWER SKIN PANEL OF THE RT WING ELONGATED. REPAIR PERFORMED BY OVERSIZING HOLES AND INSTALLATION OF REPAIR BUSHES IAW R571-50532 ISSUE: A APPROVED BY EA 6-5720-99183 AND RAS/BAE/1002415/2006 ISSUE:Aug 31, 2007 · N725FD · Airbus A300B4622R · Wing, Plate/SkinSDR 07FDEA03260Stringer · corrodedCORROSION FOUND ON STRINGER 33 AND 34 LT, FRAME 35-36. SPLICE REPAIR PERORMED IAW PRINCIPLE OF SRM 53-10-14 FIG 201, APPROVED BY EA 6-5314-99178 AND RAS/DABRE/2006 ISS A.Aug 31, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA03259Skin · misrepairedFOUND OLD DOUBLER REPAIR ON FWD RT PAX DOOR LOWER FWD CORNER NOT CONFORM TO SRM REPAIR RENEWED IAW SRM 52-10-00 FIG 204.Aug 31, 2007 · N725FD · Airbus A300B4622R · Passenger/Crew DoorsSDR 07FDEA03254Skin · delaminatedDELAMINATION AT OUTBOARD TRAILING EDGE AREA, RIB 18 OF ALL SPEED AILERON RHS. REPAIR PERFORMED IAW TD FOK/051/2006, APPROVED BY EA 6-5760-99146 AND RAS/FOK/051/2006 ISSUE B.Aug 30, 2007 · N725FD · Airbus A300B4622R · Ailerons
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