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 07FDEA03253Fitting · damagedDAMAGE FOUND IN ALL LAYERS OF HOLE (APPEARED TO BE TOOL MARKS) INSIDE CENTER WING BOX, FRAME 47 LHS LOWER CORNER ANGLE FITTING. REPAIR PERFORMED BY OVERSIZING HOLE AND INSTALLING FASTENER NSA5351-10 WITH TRANSITION FIT IAW EA 6-5710-99144 AND RAS/043285/014Aug 30, 2007 · N725FD · Airbus A300B4622R · Wing, Center BoxSDR 07FDEA03251Floorbeam · corrodedHEAVY CORROSION ON TOP CAP BEAM FRAME 63, BETWEEN Y805 TO Y1470. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 / FIG 207.Aug 30, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 07FDEA03250Floorbeam · corrodedHEAVY CORROSION ON TOP CAP BEAM FRAME 56, BETWEEN Y805 TO Y1470. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 / FIG 207.Aug 30, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 07FDEA03249Floorbeam · corrodedHEAVY CORROSION ON TOP CAP BEAM FRAME 56, BETWEEN Y805 TO Y1470. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 / FIG 207.Aug 30, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 07FDEA03248Skin · chafedCHAFING MARK IN SKIN OF LEADING EDGE RT WING, BETWEEN TRACK 3 AND 4. REPAIR PERFORMED BY REPLACEMENT OF SKIN PANEL IAW SRM 51-72-10 (SRM 57-41-12/ FIG 6/ITEM 5).Aug 30, 2007 · N725FD · Airbus A300B4622R · Wing, Plate/SkinSDR 07FDEA03247Floorbeam · corrodedCORROSION AT TOP CAP BEAM FRAME 66, Y600 LHS, CARGO COMP FLOOR STRUCTURE. SPLICE REPAIR PERFORMED IAW SRM 53-10-15/FIG 207.Aug 30, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 07FDEA03245Profile · damagedDEFORMED LONGITUDINAL PROFILE BETWEEN FRAME 65-66 RHS OF AD OF FLOOR SUPPORT STRUCTURE. REPAIR PERFORMED BY REPLACEMENT OF LONGITUDINAL PROFILE IAW SRM 51-72-10.Aug 30, 2007 · N725FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03244Profile · damagedDEFORMED LONGITUDINAL PROFILE BETWEEN FRAME 65-66 LHS OF AD OF FLOOR SUPPORT STRUCTURE. REPAIR PERFORMED BY REPLACEMENT OF LONGITUDINAL PROFILE IAW SRM 51-72-10.Aug 30, 2007 · N725FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03243Stringer · corrodedCORROSION FOUND AT STRG 44 LT BETWEEN FRAME 16A-17. STRUCTURE REPAIR PERFORMED IAW SRM 53-12-14 / FIG 201.Aug 30, 2007 · N725FD · Airbus A300F4622R · Fuselage Main, Longeron/StringerSDR 07FDEA03242Stringer · corrodedCORRODED STRINGER COUPLING BETWEEN FRAME 74-75, STRG 30 RHS. REPAIR PERFORMED BY REPLACEMENT OF CONNECTING SECTION IAW SRM 51-72-10.Aug 30, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA03240Frame · damagedFOUND DEVIATIONS BETWEEN RAS/AS/212/2003A AND A/C CONDITION AND DEVIATIONS TO SB 53-6125 ON FRAME 45, STRG 26-28 RHS AND LHS. REPAIR: HOLES H1 RT AND LT AND H2 FRAME 45 LT: COLD WORKING, BUSH INSTALLATION IN FRAME AND DOUBLER, NEW NOMINAL FASTENER NSA5351V4 IAug 30, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA03238Skin Panel · corrodedEXTERNAL CORROSION ON SKIN PANEL RHS AT TWO PLACES BETWEEN FRAME 39-40, STRG 28-29 AND BETWEEN FRAME 39-40, STRG 27-28, BOTH PLACES OUT OF LIMIT. REPAIR PERFORMED BY INSTALLATION OF WEDGED SHIMS ON BOTH SIDES AS WELL AS ONE INTERNAL DOUBLER AND TWO EXTERNAL DAug 30, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA03236Skin Panel · damagedFOUND THE HYDRAULIC FITTING HOLES IN PYLON SUPPORT BRACKET IN LOWER SKIN PANEL OF THE LT AND 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/1002415/2006Aug 30, 2007 · N725FD · Airbus A300B4622R · Wing, Plate/SkinSDR 07FDEA03225Web · damagedFOUND MISMATCHED HOLES IN WEB OF RT HORIZONTAL STABILIZER TIP. REPAIR PERFORMED BY REPLACEMENT OF AFFECTED WEB AND CHANGING SOLID RIVETS BY HI-LOK FASTENERS AT SOME LOCATIONS IAW EA 6-5514-99141 AND RAS/CASA/4583/2006 ISSUE: A.Aug 29, 2007 · N725FD · Airbus A300B4622R · Horizontal Stabilizer StructureSDR 07FDEA03224Longeron · corrodedHEAVY CORRODED LONGERON BETWEEN FRAME 11-15A, CABIN FLOOR STRUCTURE. INSTALLATION OF NEW LONGERON IAW SRM 53-12-15 / FIG 207.Aug 29, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA03223Frame · gougedGOUGES FOUND AT FRAME 55 LHS AND RHS, BETWEEN STRG 14-15. REPAIR PERFORMED BY SMOOTH BLENDING AND NDT INSPECTION IAW EA 6-5316-99140 AND RAS/DATLS/0003069/2006 ISSUE A.Aug 29, 2007 · N725FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA03221Skin · dentedOLD FLUSH DOUBLER REPAIR ON SLAT NR 3 LT, UPPER SKIN, BETWEEN RIB 44-46. BLIND RIVETS WITHOUT PIN, RIB 46 IS MISDRILLED AND RIVETS FORM IS NOT ADHERED. REWORK PER TD FOK/233/2005 ISSUE: C, APPROVED BY EA 6-5744-99139A AND RAS/FOK/2332005 ISSUE: A.Aug 29, 2007 · N725FD · Airbus A300B4622R · Leading Edge DevicesSDR 07FDEA03218Skin · misrepairedOLD FLUSH DOUBLER REPAIR FOUND ON LT SLAT NR 1 AT UPPER SURFACE BETWEEN RIB 8-10. INVALID REPAIR AS PER SRM 57-42-11/FIG 202 WHICH IS ONLY VALID FOR INBOARD OF RIB 19, STRG 1.3 AND 1.4. REPAIR PERFORMED IAW TD FOK/055/2008 ISSUE: D, APPROVED BY EA 6-5742-991Aug 29, 2007 · N725FD · Airbus A300B4622R · Wing, Control SurfacesSDR 07FDEA03205Skin · delaminatedFOUND TWO DELAMINATED AREAS ON BOTTOM SKIN TRAILING EDGE OF LT SPOILER NR 1. DELAMINATION REPAIRS PERFORMED IAW SRM 57-71-11/PG 201/PARA 10, APPROVED BY EA 6-5770-101551.Aug 29, 2007 · N725FD · Airbus A300B4622R · Wing, Control SurfacesSDR 07FDEA00692Downlock Switch · unknownON FINAL, 400 AGL, RECEIVED A "TO LOW GEAR" VERBAL WARNING, LDG GEAR POSITION DETECTION SYS WAS IN POS "1", SWITCHED TO SYS "2" AND CONTINUED PERFORMED GO-AROUND. ON SECOND ATTEMPT, THERE WAS NO WARNING, ALL SYSTEMS SHOWED GEAR DOWN, AND LANDED. IND R PER TMar 7, 2007 · N725FD · Airbus A300B4622R · ATC Transponder SystemSDR 07FDEA00446Smoke Detector · malfunctionedAFTER PUSHBACK AND ENGINE START RECEIVED ECAM FOR AFT CARGO CPT SMOKE. COMPLIED WITH ECAM AND QRH. PREPPED FOR REMOVAL OF NR 1 LWR CARGO COMP FIRE BOTTLE. REF:A300 M.M.CHAPT:26-23-11-4-02. OPENED FWD LWR CARGO DOOR. PULLED AND TAGGED CIRCUIT BREAKERS, REMFeb 11, 2007 · N725FD · Airbus A300B4622R · Smoke Detection
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