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 FDEA200907152622Fitting · chafedFOUND NICKS AND CHAFING MARKS ON LT PYLON AFT ATTACH LUGS REPAIR PERFORMED BY BLEND OUT THE DAMAGE , NDT FOR CRACK FREE CONDITION IAW. RAS/BAE/1009953/2009 ISS.A , APPROVED BY EA 6-5740-129166.Jul 15, 2009 · N751FD · Airbus A300B4622R · Nacelle/Pylon, Attach FittingsSDR FDEA200907142619Skin · wornFOUND ELONGATED HOLES ON RT PYLON SUPPORT BRACKET AND BOTTOM WING SKIN. REPAIR PERFORMED IAW DWG R571-50532ISS A , APPROVED BY RAS /BAE/1009863/2009 ISS A AND EA 6-2900-131227.Jul 14, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907142618Skin · wornFOUND ELONGATED HOLES ON LT PYLON SUPPORT BRACKET AND BOTTOM WING SKIN. REPAIR PERFORMED IAW DWG R571-50532ISS A , APPROVED BY EA 6-2900-131227.Jul 14, 2009 · N751FD · Airbus A300B4622 · Wing, Plate/SkinSDR FDEA200907142617Rib · chafedFOUND CHAFING MARKS ON RT INNER FLAP RIB 12, RIB 27 AND RIB 18-19 TOP AND BOTTOM SKIN. REPAIR PERFORMED BY BLEND OUT AT RIB 12 FRONT SPAR-STR.2.1 AND RIB 27, CUT OUT REPAIR IAW SRM 57-50-00 FIG 205 AT RIB 12-STR.2.1-2.2 TOP SKIN, CUT OUT REPAIR AT RIB 18- 19 Jul 14, 2009 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA200907142615Frame · crackedFOUND OLD REPAIR ON UPPER FRAME FOOT C 42 LT, C 45 LT AND C 46 RT (FRAME FOOT WAS CUT AND HOLES OVERSIZED). IN HOLE C42 LT AND C 45 LT WRONG FASTENER INSTALLED. AFTER FASTENER REMOVAL WAS FOUND A CRACK IN HOLE C42 LT. REPAIR PERFORMED BY INSTALLING THE COJul 14, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA200907142614Floorbeam · misrepairedFOUND ON CROSSBEAM C 61 Y-200 AN OLD REPAIR, NOT PERFORMED IAW SRM. REPAIR PERFORMED BY REPLACEMENT OF CROSSBEAM IAW SRM 51-72-10.Jul 14, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA200907142613Skin · chafedFOUND CHAFING MARKS ON RT WING BOTTOM SKIN PANEL 3 BETWEEN RIB 12-13. REPAIR PERFORMED BY BLEND OUT THE DAMAGE, NDT FOR CRACK FREE CONDITION IAW RAS/BAE/1010206/2009 ISS A, APPROVED BY EA 6-5730-131253.Jul 14, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907132606Beam · corrodedFOUND COROSION IN THE AREA OF ACCESS DOOR 312AR LOWER BEAM C 84-85, P 30-36 RT. REPAIR PERFORMED BY BLEND OUT THE CORROSION , NDT FOR DAMAGE FREE CONDITION AND INSTALLING A REINFORCING ANGLE IAW RAS/EFW/9000202/2009 ISS. A, APPROVED BY EA 6-5310-129162.Jul 13, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA200907132605Hinge Fitting · corrodedFOUND CORROSION IN THE RUDDER HINGE FITTINGS 2, 4, 5, 6,AND 7. REPAIR PERFORMED BY BLENDING OUT THE CORROSION , NDT FOR CORROSION FREE CONDITION IAW. RAS/DAHAM/4027851/2009 ISS.A , APPROVED BY EA 6-5540-131228.Jul 13, 2009 · N751FD · Airbus A300B4622R · Rudder/Tab, Attach FittingsSDR FDEA200907132603Web · corrodedFOUND CORROSION UNDERNEATH DOOR STOP FITTING 7 AND 8 IN WEB OF LT FWD PAX DOOR. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 13, 2009 · N751FD · Airbus A300B4622R · Passenger/Crew DoorsSDR FDEA200907102576Skin · damagedFOUND ON RT INNER FLAP SB 57-6098 NOT PROPERLY INSTALLED AND AFTER SKIN REMOVAL FOUND DAMAGED/ELONGATED HOLES AND GAUGES IN THE STRUCTURE. REPAIR PERFORMED BY REPLACEMENT OF RIB 25A AND REPAIR THE DAMAGES IAW RAS/FOK/138/2009 ISS. B, APPROVED BY EA 6-5750-Jul 10, 2009 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA200907102575Rib · damagedFOUND ON LT INNER FLAP DURING ACCOMPLISHMENT OF EO 6-5750-7-5000, DAMAGED HOLES IN FLAP STRUCTURE AFTER RIB 7 WAS REMOVED. REPAIR PERFORMED BY REPLACEMENT OF RIB 7 AND REPAIR OF DAMAGES IAW RAS/FOK/135/2009 ISS.D, APPROVED BY EA 6-5750-131241.Jul 10, 2009 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA200907102574Rib · damagedFOUND ON RT INNER FLAP DURING ACCOMPLISHMENT OF EO 6-5750-7-5000 DAMAGED HOLES IN FLAP STRUCTURE AFTER RIB 7 WAS REMOVED. REPAIR PERFORMED BY REPLACEMENT OF RIB 7 AND REPAIR OF DAMAGES IAW RAS/FOK/133/2009 ISS.D, APPROVED BY EA 6-5750-129178.Jul 10, 2009 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA200907102573Skin · chafedFOUND ON LT INNER FLAP UPPER AND LOWER SKIN CHAFING MARKS, DENT AND SCRATCHES. RIB 12-19 REPAIR PERFORMED BY BLEND OUT THE CHAFING MARK AT RIB 12/FRONT SPAR -STR.2.1 , CUT OUT THE SKIN AT RIB 12 /STR.2.1-2.2 AND PERFORM REPAIR IAW SRM 57-50-00 PARA 4.E, CUTOJul 10, 2009 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA200907102572Structure · damagedFOUND ON LT INNER FLAP SB 57-6098 NOT PROPERLY INSTALLED AND AFTER SKIN REMOVAL FOUND DAMAGED/ELONGATED HOLES AND GOUGES IN THE STRUCTURE. REPAIR PERFORMED BY REPLACEMENT OF RIB 25A AND REPAIR THE DAMAGES IAW RAS/FOK/148/2009 ISS. D, APPROVED BY EA 6-5750-1Jul 10, 2009 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA200907102571Attach Fitting · chafedFOUND NICKS AND CHAFING MARK ON RT PYLON AFT ATTACH FITTINGS. REPAIR PERFORMED BY BLEND OUT THE DAMAGES IAW RAS/BAE/1009953/2009 ISS.A, APPROVED BY EA 6-5740-129167.Jul 10, 2009 · N751FD · Airbus A300F4605R · Nacelle/Pylon, Attach FittingsSDR FDEA200907102568Frame · damagedFOUND DEEP GROOVES UNDER FWD AND AFT FITTINGS AFTER DOOR STOP FITTING REMOVAL AT LT FWD DOOR FRAME. REPAIR PERFORMED BY BLEND OUT DAMAGE , NDT FOR CRACK FREE CONDITION , SPOTFACING THE HOLES AND INSTALLING A FILLER IAW RAS 70522655/009/2009 ISS. A, APPROVEJul 10, 2009 · N751FD · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA200907102567Frame · damagedFOUND DEEP GROOVES UNDER FWD AND AFT FITTINGS AFTER DOOR STOP FITTING REMOVAL. AT LT FWD DOOR FRAME REPAIR PERFORMED BY BLEND OUT THE DAMAGE, NDT FOR CRACK FREE CONDITION , SPOTFACING THE HOLES AND INSTALLING A FILLER IAW RAS 70522655/009/2009 ISS. A, APPROVJul 10, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA200907082536Skin · corrodedFOUND CORROSION ON SKIN PANEL C 92-95, P9-14 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 8, 2009 · N751FD · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA200907082535Skin · corrodedFOUND CORROSION ON SKIN PANEL C 92-95, P9-14 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 8, 2009 · N751FD · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR FDEA200907082534Rib · corrodedFOUND CORROSION ON RT OTBD FLAP RIB 27 REPAIR PERFORMED BY REPLACEMENT OF RIB 27 IAW RAS/FOK/111/2009 ISS. A, APPROVED BY EA 6-5750-129187.Jul 8, 2009 · N751FD · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA200907082533Skin · chafedFOUND CHAFING MARKS ON LT WING L/E BETWEEN TRACK 11 AND WING TIP. REPAIR PERFORMED BY BLEND OUT, NDT FOR CRACK FREE CONDITION IAW RAS/BAE/101216/2009 ISS. A , APPROVED BY EA 6-5740-131230.Jul 8, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907082532Failsafe · corrodedFOUND CORROSION ON RT FWD PAX DOOR 1 LOWER FAIL SAFE RING. REPAIR PERFORMED BY BLEND OUT THE CORROSION , NDT FOR CRACK FREE CONDITION IAW RAS 70520367/004/2009 ISS. A , APPROVED BY EA 6-5310-131247Jul 8, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA200907082531Failsafe · corrodedFOUND CORROSION ON LT FWD PAX DOOR 1 LOWER FAIL SAFE RING. REPAIR PERFORMED BY BLEND OUT THE CORROSION , NDT FOR CRACK FREE CONDITION IAW RAS 70520367/004/2009 ISS A , APPROVED BY EA 6-5310-131247.Jul 8, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA200907082530Skin · chafedFOUND CHAFING MARKS ON RT WING L/E BETWEEN INBD AND OTBD RIBS. REPAIR PERFORMED BY BLEND OUT, NDT FOR CRACK FREE CONDITION IAW. RAS/BAE/1010212/2009 ISS. A, APPROVED BY EA 6-5740-131235.Jul 8, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200907082529Skin · corrodedFOUND CORROSION ON AFT CARGO DOOR LWR INNER SKIN AT LONGERON 5, C 59A-63. REPAIR PERFORMED BY BLEND OUT THE CORROSION , NDT FOR CRACK FREE CONDITION IAW RAS/DAHAM/4027914/2009 ISS. A, APPROVED BY EA 6-5230-131223.Jul 8, 2009 · N751FD · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA200907082528Structure · corrodedFOUND CORROSION ON T-SECTION C 92 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 8, 2009 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200907082527Spar · wornFOUND ELONGATED HOLE IN SPAR FOR DRAIN PIPE ON PYLON NR 1. REPAIR PERFORMED BY REAM UP THE HOLE AND REPAIR IAW DWG R546-10359, APPROVED BY RAS 70520790/004/2009 ISS A AND EA 6-5410-131237.Jul 8, 2009 · N751FD · Airbus A300B4622R · Nacelle/Pylon, Frame/Spar/RibSDR FDEA200907082524Frame · damagedFOUND MISDRILLED FASTENER HOLE IN C 64, ADJACENT TO P44 LT REPAIR PERFORMED BY REAM UP THE HOLE IN FITTING AND INSTALLING A SHOULDERED BUSHING IAW RAS/EFW/9000206/2009 ISS. B, APPROVED BY EA 6-5310-129175.Jul 8, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, FrameSDR FDEA200907072518Stringer · corrodedFOUND CORROSION ON STRINGER P56 RT, C 57.3-58 STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Jul 7, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200907072517Lug · wornFOUND DURING MLG CHANGE MLG FITTING FWD LUG OUT LIMIT IAW AMM 57-20-30. REPAIR PERFORMED BY OVERSIZING BORES, SPOTFACING LUG FACES AND BUSHING REPAIR IAW DWG R572-40221 ISS G, APPROVED BY RAS/BAE/1010287/2008 ISS A AND EA 6-5740-131231.Jul 7, 2009 · N751FD · Airbus A300B4622R · Wing, Landing Gear Attach FittingsSDR FDEA200907072516Lug · wornFOUND DURING MLG CHANGE, MLG FITTING FWD LUG OUT LIMIT IAW AMM 57-20-30. REPAIR PERFORMED BY OVERSIZING BORES, SPOTFACING LUG FACES AND BUSHING REPAIR IAW DWG R572-40221 ISS G, APPROVED BY RAS/BAE/1010287/2008 ISS A AND EA 6-5740-131231.Jul 7, 2009 · N751FD · Airbus A300F4622R · Wing, Landing Gear Attach FittingsSDR FDEA200907072514Attach Fitting · chafedFOUND CHAFING MARK ON RT PYLON FWD ATTACH FITTING. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARK AND NDT FOR CRACK FREE CONDITION IAW RAS/BAE/1009894/2009 ISS.A, APPROVED BY EA 6-5710-129186.Jul 7, 2009 · N751FD · Airbus A300B4622R · Wing, Attach FittingsSDR FDEA200907072512Web · damagedFOUND SHEAR WEB AT P 25LH , C 57.2 DAMAGED. REPAIR PERFORMED BY TRIMMING THE DAMAGED FLANGE AND INSTALLING A REPAIR ANGLE IAW RAS/EFW/9000194/2009 ISS B, APPROVED BY EA 6-5310-129185.Jul 7, 2009 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200907072511Plate · crackedFOUND CRACK IN WEB OF INTEGRAL MANHOLE PLATE C 38.2, P 54-55 LT. REPAIR PERFORMED BY CUT BACK CRACKED STIFFENER AND INSTALLING A MILLED STIFFENER IAW RAS /EFW/9000197/2009 ISS A, APPROVED BY EA 6-5310-129179.Jul 7, 2009 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200907072510Skin · delaminatedFOUND ON RUDDER, THE RT LWR LIGHTENING PROTECTION PLATE DEBONDED. REPAIR PERFORMED BY REPLACEMENT OF PART, INSPECT THE AREA AND PERFORMED BONDING REPAIR IAW RAS/DAHAM/4027852/2009 ISS A, APPROVED BY EA 6-5540-129190.Jul 7, 2009 · N751FD · Airbus A300B4622R · Rudder, Plate/SkinSDR FDEA200907072509Fitting · damagedFOUND TOOLING MARKS ON RT LWR KEEL AT FRAM 47 RT. REPAIR PERFORMED BY BLEND OUT THE DAMAGE, NDT FOR CRACK FREE CONDITION IAW RAS 70521186/004/2009 ISS. A, APPROVED BY EA 6-5310-129174.Jul 7, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA200907072508Skin · corrodedFOUND CORROSION ON SKIN PANEL C92 P16-AD OUT OF SRM LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jul 7, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200907072507Fitting · damagedDURING MODIFICATION IAW EO 6-5340-7-5002 P7, FOUND OVERSIZED FASTENER IN C12A LT FITTING INSTALLED. REPAIR PERFORMED BY INSTALLATION OF SECOND OVERSIZE FASTENER AS DEVIATION TO EO 6-5340-7-5002 P7 IAW RAS 70521310/007/2009 ISS A, APPROVED BY EA 6-5310-129156.Jul 7, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA200907072506Fitting · damagedDURING MODIFICATION IAW EO 6-5340-7-5002 P7, FOUND OVERSIZED FASTENER IN C12A RT FITTING INSTALLED. REPAIR PERFORMED BY INSTALLATION OF SECOND OVERSIZE FASTENER AS DEVIATION TO EO 6-5340-7-5002 P7 IAW RAS 70521310/007/2009 ISS. A, APPROVED BY EA 6-5310-129156Jul 7, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA200907072505Beam · crackedFOUND CRACK IN LT BEAM NR4 LWR FLANGE AT C49. REPAIR PERFORMED IAW DWG R538-10581 WITH DEVIATION IAW RAS 70520550/004/2009 ISS. A, APPROVED BY EA 6-5310-131201.Jul 7, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA200907072503Skin · corrodedFOUND CORROSION ON SKIN AND ANTENNA DOUBLER C 62-63 P 57. REPAIR PERFORMED BY BLEND OUT THE CORROSION AND INSTALLING AN INTERNAL DOUBLER IAW RAS/EFW/9000186/2009 ISS. B, APPROVED BY EA 6-5330-131206.Jul 7, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA200907072501Beam · crackedFOUND CRACK IN BEAM 5 LT C 52-53. REPAIR PERFORMED BY DWG R538-10583-02, EXCEPT TRIMMING THE REPAIR ANGLE BY 2 ROWS, APPROVED BY RAS 70520670/009/2009 ISS. A AND EA 6-5310-129194.Jul 7, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA200906252305Coupling · corrodedFOUND CORROSION ON STRINGER COUPLING P 44-45, C 26-27 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Jun 25, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200906252304Stringer · corrodedFOUND CORROSION ON STRINGER P51 AND P57, C C77-78. SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG. 201 ON P 57 AND SPLICE REPAIR IAW RAS/EFW/9000193/2009 ISS A, APPROVED BY EA 6-5310-129184, PERFORMED ON P 51.Jun 25, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200906252303Stringer · corrodedFOUND CORROSION ON STRINGER 56, 57 LT AND 56 RT, C 76-77 REPAIR PERFORMED BY BLEND OUT THE CORROSION ON STRINGER P 56, 57 LT AND INSTALLING AN ANGLE ON P 56 RT IAW RAS/REFW/9000188/2009 ISS.A , APPROVED BY EA 6-5310-129191 .Jun 25, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200906252302Stringer · corrodedFOUND CORROSION ON STRINGER P56 AND 57, C72-75. SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Jun 25, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA200906252301Skin · damagedFOUND OLD BLEND OUT REPAIR ON RT WING TOP SKIN RIB 4-5 DEEPER THAN REPORTED. REPAIR PERFORMED BY NDT FOR CRACK FREE AND CORRSOION FREE CONDITION WITH REMAINING MATERIAL ACCEPTABLE IAW RAS/BAE/0934/2004 ISS. C , APPROVED BY EA 6-5730-131233.Jun 25, 2009 · N751FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA200906252300Beam · corrodedFOUND CORROSION ON AFT CARGO DOOR SILL BEAM UPPER FLANGE C-59-63. REPAIR PERFORMED IAW SRM 53-17-18, PAGE BLOCK 201, PAR.10 (DRAWING R539-70133 REV.G) EXCEPT CUT THE VERTICAL CORNER OF REPAIR ANGLE AT C59 IAW RAS/EFW/9000187/2009 ISS.A , APPROVED BY EA 6-531Jun 25, 2009 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA200906252299Frame · crackedFOUND CRACKED FASTENER HOLES 5 AND 6 AND DAMAGED HOLE 8 IN CENTER WEB OF FRAME 44. REPAIR PERFORMED BY OVERSIZING THE HOLES 5 AN 6 AND COUNTERSINKS HOLE 8, NDT FOR CRACK FREE CONDITION AND INSTALLING CONICAL WASHER IAW RAS 70520180/009/2009 ISS.A, APPROVED BYJun 25, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, Frame
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