N751FD

Service difficulty reports · 308

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 = 'N751FD' 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 FDEA201202010414Skin · corrodedLT WING UPPER SURFACE AT STA 634 SKIN FOUND CORRODED. PERFORMED REPAIR IAW EA 6-5720-150420, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Feb 1, 2012 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA201201310390Frame · crackedDURING HFEC ROTATING PROBE INSPECTION ON RT FRAME 47. FOUND ONE CRACK INDICATION APPROX 25 PERCENT FSH ON FRAME. REPAIRED IAW EO 6-5310-7-5017B P6. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.Jan 31, 2012 · N751FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201201310391Frame · damagedDURING HFEC ROTATING PROBE INSPECTION ON RT FRAME 47 DAMAGED. REPAIRED PER EA 6-5310-150425 . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 114.Jan 31, 2012 · N751FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201201310394Frame · crackedDURING HFEC ROTATING PROBE INSPECTION ON RT FRAME 47, FOUND A CRACK INDICATION. PERFORMED REPAIR IAW EA 6-5310-150425. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 114.Jan 31, 2012 · N751FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201201310393Frame · crackedDURING HFEC ROTATING PROBE INSPECTION ON RT FRAME 47, FOUND A CRACK INDICATION. PERFORMED REPAIR IAW EA 6-5310-150425. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Jan 31, 2012 · N751FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201201310392Frame · chafedDURING HFEC ROTATING PROBE INSPECTION ON RT FRAME 47 FOUND INDICATION OF HOLE DAMAGE. PERFORMED REPAIR IAW EA 6-5310-150425. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Jan 31, 2012 · N751FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA201201310389Floor Panel · puncturedBULK CARGO COMPARTMENT FLOOR PANEL 162AW FOUND PUNCTURED. R & R IAW AMM 25-56-11, REV 52.1. NEW FLOOR PANEL FABRICATED IAW DWG NR SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Jan 31, 2012 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201201280361Skin · gougedAFT CARGO DOOR CUTOUT FUSELAGE SIDE SKIN AT FRAME 4302, STRINGER 28RT FOUND GOUGED. REPAIRED PER EA 6-5310-150424. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 114.Jan 28, 2012 · N751FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201201190249Scuff Plate · crackedDURING INSPECTION AT SCUFF PLATE BELOW LT AFT PASSENGER/CREW DOOR A CRACK INDICATION FOUND ON 01 FASTENER HOLE APPROX .2500" LENGTH. PERFORMED REPAIR IAW SRM 53-18-18, FIG 201, REV 76. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Jan 19, 2012 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201201180239Floor Panel · dentedBULK CARGO COMPARTMENT FLOOR PANEL NR 161GF FOUND DENTED ON SEVERAL LOCATIONS. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. R & R IAW AMM 53-10-35, REV 52.1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Jan 18, 2012 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201201180238Floor Panel · dentedBULK CARGO COMPARTMENT FLOOR PANEL NR 161JF FOUND DENTED ON SERVERAL LOCATIONS. NEW FLOOR PANEL FABRICATED IAW DWG NR SRZ-25-005 REV J. R & R IAW AMM 53-10-35, REV 52.1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Jan 18, 2012 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201201160186Floor Panel · delaminatedAFT CARGO COMPARTMENT FLOOR PANEL NR 151GF, FOUND DELAMINATED. NEW FLOOR PANEL 151GF FABRICATED IAW DWG SRZ-25-005, REV J. REMOVED AND REPLACED AS PER AMM 53-10-33-04 REVISION 52.1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Jan 16, 2012 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201201160185Floor Panel · delaminatedAFT CARGO COMPARTMENT FLOOR PANEL NR 152JF, FOUND DELAMINATED. R & R IAW AMM 53-10-33-04, REV 52.1. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005 REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100. REV 113.Jan 16, 2012 · N751FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201201090059Skin · scratchedRT WING INBD FLAP BETWEEN RIB 14 AND RIB 15 FWD LOWER AREA SKIN FOUND SCRATCHED. REPAIRED IAW SRM 57-50-00, FIG 205, REV 76. CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100, REV 113.Jan 9, 2012 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA201201090058Attach Fitting · crackedAVIONICS COMPARTMENT, DETAILED INSPECTION CARRIED OUT AT THE CROSSBEAM ON NLG FRAME 15A. WEB FACE AT ATTACHMENT FITTING OF RACK 107VU FOUND CRACKED. DETAILED INSPECTION CARRIED OUT AND ACCOMPLISHED REPAIR IAW EA 6-5310-150413, PART 1. REPAIR CLASSIFIED MJan 9, 2012 · N751FD · Airbus A300B4605R · Fuselage, Landing Gear Attach FittingsSDR FDEA200907242731Keelbeam · corrodedOLD REPAIR LT WING LOWER KEELBEAM AREA HAD NEW CORROSION AROUND FASTENERS C46.2 AND C47. REPAIR PERFORMED IAW EA 6-5730-131271.Jul 24, 2009 · N751FD · Airbus A300B4622R · Wing, Center BoxSDR FDEA200907242730Skin · corrodedSKIN CORROSION OUTER SHROUD BOX RT SIDE WORX 439.65 BOTTOM REPAIR PERFORMED IAW EA 6-5750-131267.Jul 24, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907242729Skin · corrodedCORROSION AROUND SEVERAL FASTENERS WING BOTTOM SKIN AT STA WORX 439.65 AND WORX 755.15. REPAIR PERFORMED IAW EA 6-5750-131268.Jul 24, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907242728Skin · corrodedCORROSION AROUND SEVERAL FASTENERS, LT WING TOP SKIN AREA AFT OF REAR SPAR. RIB 27-28 REPAIR PERFORMED IAW EA 6-5750-131268.Jul 24, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907242727Skin · corrodedCORROSION AROUND SEVERAL FASTENER HEADS RT WING TOP SKIN AT RIB 27 AFT OF REAR SPAR. REPAIR PERFORMED IAW EA 6-5750-131268.Jul 24, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907232723Skin Panel · corrodedTOP SKIN PANEL, RT WING AFT OF REAR SPAR BETWEEN RIB 1 AND RIB 5, CORROSION WAS DETECTED. REPAIR PERFORMED IAW EA 6-5730-131269.Jul 23, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907232722Skin Panel · corrodedWING TOP SKIN PANEL BETWEEN RIB 1 AND RIB 14 CORROSION AROUND SEVERAL BOLTS AND GROUND POINT AS WELL AS A UNIDENTIFIED FASTENER REPAIR PERFORMED IAW EA 6-5730-131269.Jul 23, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907232721Skin Panel · corrodedWING TOP SKIN PANEL RT, FOUND CORROSION AT RIB 14 AROUND ONE FASTENER. REPAIR PERFORMED IAW EA 6-5730-131269.Jul 23, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907232720Skin Panel · corrodedRT WING TOP SKIN PANEL CORROSION AT GROUND POINT AND AROUND BOLTS BETWEEN RIB 25 AND RIB 27. REPAIR PERFORMED IAW EA 6-5730-131269.Jul 23, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907232719Skin · corrodedWRONG FASTENER INSTALLATION AND SLIGHTLY NEW CORROSION SPOT AROUND FASTENER HOLES AT OLD REPAIR IN THE WING BOTTOM SKIN AREA NEAR RIB 5 (DRW R571-40141-23) REPAIR PERFORMED IN ACCORDANCE WITH EA 6-5710-131263.Jul 23, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907232718Skin · corrodedSEVERAL CORROSION SPOTS AT OLD REWORKED SKIN AREA BOTTOM WING RT SIDE AROUND AND BETWEEN HOLE 5, 6, 114, 115, 129, 116, 117 (DRW 571-40141-23) REPAIR PERFORMED IN ACCORDANCE WITH EA 6-5710-131263.Jul 23, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907232716Skin · misrepairedRT WING, FOUND SOME OF THE HOLES WERE UNDERSIZED AND SOME WERE SLIGHTLY OVERSIZED DOUBLER AFTER VERIFICATION IN ACCORDANCE WITH EO 6-5710-131263 REINSTALLED WITH OVERSIZED FASTENER.Jul 23, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907232715Skin · misrepairedLT WING, FOUND SOME OF THE HOLES WERE UNDERSIZED AND SOME WERE SLIGHTLY OVERSIZED DOUBLER AFTER VERIFICATION IN ACCORDANCE WITH EA 6-5710-131263 REINSTALLED WITH OVERSIZED FASTENERS.Jul 23, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907222693Skin · corrodedCORROSION AT TOP SKIN PANEL EDGE AFT OF REAR SPAR BETWEEN RIB 1 AND 4 REPAIR PERFORMED IN ACCORDANCE WITH EA 6-5730-131270.Jul 22, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907222692Skin · corrodedTOP SKIN PANEL FRONT SPAR BETWEEN RIB 1 AND 14 CORROSION AROUND SEVERAL FASTENER BOLTS REPAIR PERFORMED IN ACCORDANCE WITH EA 6-5730-131270Jul 22, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907222691Skin · corrodedTOP SKIN PANEL FRONT SPAR BETWEEN RIB 14 AND 27 CORROSION AROUND SEVERAL FASTENER BOLTS REPAIR PERFORMED IN ACCORDANCE WITH EA 6-5730-131270Jul 22, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907222690Skin · corrodedTOP SKIN REAR SPAR BETWEEN RIB 2 AND 5 CORROSION AROUND TAPERLOKS REPAIR PERFORMED IN ACCORDANCE WITH EA 6-5730-131270Jul 22, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907212688Crossbeam · corrodedPAX DOOR LT 1 INTERNAL STRUCTURE CORRODED. CORRODED STRUCTURAL PARTS CHANGED BY NEW PARTS IAW SRM 51-72-10; 51-24-00 AND 51-75-10.Jul 21, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA200907212686Shroud · delaminatedLH AND RH OUTER SHROUD BOXES WITH SEVERAL DAMAGES REPAIR PERFORMED IN ACCORDANCE WITH EA 6-5750-131266Jul 21, 2009 · N751FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA200907212685Shroud · delaminatedLT AND RT OUTER SHROUD BOXES WITH SEVERAL DAMAGES REPAIR PERFORMED IN ACCORDANCE WITH EA 6-5750-131266Jul 21, 2009 · N751FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA200907212684Shroud · delaminatedLH AND R/H OUTER SHROUD BOXES WITH SEVERAL DAMAGES REPAIR PERFORMED IN ACCORDANCE WITH EA 6-5750-131266Jul 21, 2009 · N751FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA200907212683Skin · chafedCHAFING MARKS AT LOWER SKIN OF RIGHT NR 1 SLAT BETWEEN ROBS 21 AND 23 REPAIR PERFORMED IN ACCORDANCE WITH EA 6-5740-131244Jul 21, 2009 · N751FD · Airbus A300B4622R · Leading Edge DevicesSDR FDEA200907212682Skin · damagedCHAFING MARKS ON WING LEADING EDGE SKIN BETWEEN WOFX-85.65 AND WOFX-90.65 DISCREPANT AREAS REPAIRED IN ACCORDANCE WITH EA 6-5740-131264Jul 21, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907202677Shroud · damagedDAMAGE AT SHROUD BOX DEFLECTORS LT SIDE. DAMAGE REPAIRED IN ACCORDANCE WITH SRM 51-77-10/ PARA 2M (2) (E); 51-77-12 /201/PARA 3 I; 57-41-12 /201/PARA 5B/5C AND 51-75-10 AS WELL AS TD/J1/S1/10227/2009 ISSUE B AND EA 6-5750-131261Jul 20, 2009 · N751FD · Airbus A300B4622R · Wing, Control SurfacesSDR FDEA200907202674Skin · damagedAFTER REMOVAL OF OLD DOUBLER REPAIR FOUND DEEP SCRATCHES IN EXTERNAL SKIN PANEL SCRATCHES REMOVED AND BLENDED OUT IAW RI EA 6-5330-131213 AND RAS/DAHAM/4027755/2009Jul 20, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200907202673Doubler · damagedDURING DOUBLER CHANGE RT SIDE KRUEGER FLAP AREA FOUND 3 OVERSIZE HOLE BUSHING AND OVERSIZED FASTENER INSTALLATION PERFORMED IN ACC. WITH EA 6-5330-131213 AND RAS/DAHAM/4027755/2009Jul 20, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200907172650Frame · damagedFOUND ON FRAME C69, P 49 AREA TOOLING MARKS. REPAIR PERFORMED BY REPLACEMENT OF PART IAW. SRM 51-72-10Jul 17, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA200907172649Skin · chafedFOUND CHAFING MARKS ON LOWER SKIN OF LT SLAT NR 1 REPAIR PERFORMED BY BLEND OUT , NDT FOR CRACK FREE CONDITION IAW. RAS/FOK/156/2009 ISS. A, APPROVED BY EA 6-5740-131245.Jul 17, 2009 · N751FD · Airbus A300B4622R · Leading Edge DevicesSDR FDEA200907172648Fairing · crackedFOUND OLD REPAIR (PATCH) ON LT PYLON AFT FAIRING WITH SMALL DEVIATION (FASTENER PITCH) TO EXISTING OLD RECORDS AND A CLIP IS CRACKED. REPAIR PERFORMED BY REPLACEMENT OF CLIP AND IT IS ACCEPTACLE TO LEAVE THE REPAIR AS IT IS, APPROVED BY RAS ROHR/0998/2008 ANJul 17, 2009 · N751FD · Airbus A300B4622R · Nacelle/Pylon Miscellaneous StructureSDR FDEA200907162642Skin · corrodedFOUND CORROSION IN LT WING LOWER SKIN TOP SURFACE , RIB 14-15, STR.11-13 REPAIR PERFORMED BY BLEND OUT THE CORROSION, NDT FOR CRACK FREE CONDITION IAW. RAS/BAE/1010143/2009 ISS. A, APPROVED BY EA 6-5730-131229Jul 16, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907152621Skin · chafedFOUND CHAFING MARKS ON RT WING L/E BETWEEN TRACK 6-8. REPAIR PERFORMED BY BLEND OUT THE DAMAGE, NDT FOR CRACK FREE CONDITION IAW RAS/BAE/1010220/2009, APPROVED BY EA 6-5740-131232.Jul 15, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907152628Stringer · corrodedFOUND CORROSION SPOTS ON STRINGER P 56 RT , C 76-77 SPLICE REPAIR PERFORMED IAW RAS/EFW/9000188/2009 ISS.A , APPROVED BY EA 6-5310-129191.Jul 15, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200907152625Doubler · corrodedFOUND CORROSION ON ANTENNA DOUBLER C 62-63, P 56LH-56RH. REPAIR PERFORMED BY BLEND OUT THE CORROSION, NDT FOR CRACK FREE CONDITION IAW. RAS/EFW/9000186/2009 ISS. A, APPROVED BY EA 6-5330-131206Jul 15, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200907152624Frame · crackedFOUND IN UPPER FRAME FOOT C 42 LT AFTER FASTENER REMOVAL A CRACK. REPAIR PERFORMED BY OVERSIZING THE HOLE UNTIL CRACK REMOVAL IAW. RAS 018309/010/2009 ISSA. , APPROVED BY EA 6-5310-131257.Jul 15, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA200907152623Track · corrodedFOUND CORROSION IN ROLLER TRACK C 54.3-56, AT Y1470. REPAIR PERFORMED BY SPLICE REPAIR IAW. SRM 53-10-15 FIG.202 WITH DEVIATION IAW RAS/EFW/9000196/2009 ISS.A , APPROVED BY EA 6-5310-131208.Jul 15, 2009 · N751FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach Fittings
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