N726FD

Service difficulty reports · 237

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 = 'N726FD' 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 07FDEA03013Frame · dentedSEVERAL DENTS IN DIAPHRAGM FRAME 47-52, TR 1-2 LT AND FRAME 51-53, TR. 2-3 RT, DENTS ACCEPTED IN STATE WITH NDT INSPECTION (CRACK FREE) IAW EA 6-5315-103290 AND RAS: 046817/006/2006 ISS."A".Aug 22, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, FrameSDR 07FDEA03012Skin Panel · noneEXISTING OLD EXTERNAL DOUBLER AT FRAME 17-18, STRG 39-41 LT DID NOT FIND IAW, REPAIR DRAWING R53610848. REPAIR RENEWED WITH INSTALLING OVERSIZE FASTENERS IAW EA 6-5312-103314 AND RAS/AS/143/2006 ISS "A".Aug 22, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA03011Skin Panel · corrodedCORROSION ON BULK CARGO DOOR SKIN PANEL (AROUND THE DOOR HANDLE), OUTSIDE. REPAIR PERFORMED BY BLEND OUT UNTIL CORROSION REMOVAL IAW EA 6-5234-103310 AND RAS/DABRE/7006925/2006 ISS "A".Aug 22, 2007 · N726FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR 07FDEA03001Skin Panel · damagedFOUND SEVERAL MISDRILLED/ELONGATED HOLES BETWEEN FRAME 38.1-38.2, STGR 31, LT. REPAIR PERFORMED WITH BUSHING REPAIR AND INSTALLING 4, 8MM DIA LOCK FASTENERS IAW EA 6-5314-103278 AND RAS/DABRE/7006911/2006 ISS "A".Aug 21, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA02997Angle · corrodedDAMAGED REINFORCING ANGLE IN KRUEGER FLAP AREA RT WING. REPAIR PERFORMED BY REPLACEMENT OF REINFORCEMENT ANGLE IAW SRM 57-41-11.Aug 21, 2007 · N726FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR 07FDEA03005Fitting · crackedFINDING CRACKS DURING ACCOMPLISHMENT OF SB A300-57-6049 AND A300-57-6086 IN CENTER WING BOX CORNER ANGLE FITTING (HOLE A (LT/RT), Q, G , I (LT). REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL IAW EA 6-5710-103311 AND RAS/AS/0159/2006 ISS A AND RAS /0468Aug 21, 2007 · N726FD · Airbus A300B4622R · Wing Main, Frame StructureSDR 07FDEA03004Stringer · corrodedCORROSION ON STRG 56 LT AND RT OUTER FLANGE BETWEEN C76-77. REPAIR PERFORMED BY BLEND OUT WITHIN THE LIMITS AS PER REPAIR REF EA 6-5318-103300, APPROVED BY RAS/DATLS/0003345/2006 ISS "B".Aug 21, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA03003Shear Plate · crackedCRACKED SHEARPLATE BETWEEN FRAME 79-80, STRG. 26, LHS. REPAIR PERFORMED BY REPLACEMENT OF SHEARPLATE IAW SRM 51-72-10.Aug 21, 2007 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03002Gusset · corrodedCORRODED GUSSET PLATE AT FRAME 79, STRG 26, LT AND RT. REPAIR PERFORMED BY REPLACEMENT OF PLATES IAW SRM 51-72-10.Aug 21, 2007 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA03000Skin Panel · damagedMISDRILLED HOLE (DOUBLEHOLE DIA 9 MM) IN OUTER SKIN BETWEEN FRAME 38.1-38.2, STRINGER 27, LHS. REPAIR PERFORMED WITH REPAIR BUSHING DUE TO MISSDRILLED HOLE IAW SRM 53-10-12/FIG 221 AND EA 6-5314-103335.Aug 21, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA02999Skin Panel · damagedWEAR MARKS ON THE FUSELAGE SKIN (KARMAN STRUCTURE AREA) BETWEEN FRAME 38.1/39 AND STRINGER 30/32 RT. REPAIR WITH SMOOTH BLEND OUT AND REINSTALLATION OF ORIGINAL OR OVERSIZED FASTENERS IAW EA 6-5314-103265 AND RAS/DA/BRE/7006916/2006 ISS "C".Aug 21, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA02593Sill · corrodedHEAVY CORROSION ON UPPER FLANGE OF THE AFT CARGO DOOR SILL BEAM BTW C59-64 RT. REPAIR PERFORMED BY REPLACEMENT OF UPPER FLANGE IAW EA 6-5317-103276 AND RAS/DATLS/0003386/2006.Jul 24, 2007 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA02568Skin · dentedTWO SIMILAR DEFORMATIONS ON SKIN PANEL (BOTH RHS AND LHS) BETWEEN C51 AND C52, P39-40. REPAIR PERFORMED BY DRESSING BACK THE DENTS, PERFORMING ROTOTEST AND HFEC AND INSTALLING HL11VF5 FASTENERS IAW EA 6-53-15-103318 AND RAS 046898/014/2006.Jul 23, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA02566Crossbeam · corrodedCORROSION ON CROSSBEAM AT C67 RT (-Y805 TILL -Y1470, P/N A539-74360-200) AND C56A LT (Y805 TILL Y1470, P/N A539-74268-200). AFTER BLENDING, REMAINING THICKNESS WAS OUT OF LIMIT. REPAIR PERFORMED BY INSTALLING SPLICE IAW SRM 53-10-15/FIG 207.Jul 23, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, StructureSDR 07FDEA02564Fitting · corrodedCORROSION ON FITTING AND DAMAGED REINFORCING ANGLE IN KRUEGER FLAP AREA RT. REPAIR WAS PERFORMED BY REPLACEMENT OF FITTING IAW SRM 57-45-11 AND REINFORCEMENT ANGLE IAW SRM 57-41-11.Jul 23, 2007 · N726FD · Airbus A300B4622R · Leading Edge DevicesSDR 07FDEA02563Structure · corrodedHEAVY CORROSION IN KRUEGER FLAP AREA LT ON FITTING P/N: A535-10217-200 RIBLET (P/N A572-41993-200) IS CRACKED. REPAIR WAS PERFORMED BY REPLACEMENT OF FITTING IAW SRM 57-45-11 AND CHANGE RIBLET IAW SRM 57-41-11/FIG 1.Jul 23, 2007 · N726FD · Airbus A300B4622R · Leading Edge DevicesSDR 07FDEA02281Spar · crackedDAMAGED HOLES (CRACKS IN HOLE 1, 2, 3, 4, 5, 6, 8) ON C44 CENTER SPAR WEB REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL CRACKS ARE REMOVED IAW EA 6-5710-103327 AND RAS 046993/014/2006 ISS A.Jun 26, 2007 · N726FD · Airbus A300B4622R · Wing SparSDR 07FDEA02280Crossbeam · misrepairedFOUND CORROSION AT CROSSBEAM C58 RT ( P/N A539-74268) OUTBOARD OUT OF LIMIT AND OLD REPAIR ON CROSSBEAM C62 LT (P/N A539-70091) NOT CONFORM TO SRM REPAIR PERFORMED IAW SRM 53-10-15 FIG 207 AT CROSSBEAM C 62 LT AND 58 RT.Jun 26, 2007 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA02216Skin · chafedCHAFING MARK FOUND ON LEADING EDGE NOSE SKIN, RT WING, BETWEEN TRACK 3 AND WOFX-69.00. REPAIR PERFORMED BY REWORK OF SKIN AND IS APPROVED BY EA 6-5741-103287 AND RAS/BAE/1003389/2006 ISSUE "A".Jun 20, 2007 · N726FD · Airbus A300B4622R · Wing, Plate/SkinSDR 07FDEA02189Floorbeam · misrepairedOLD CORROSION REPAIR ON TOP CAP BEAM C38.2 LT, THIS SPLICE REPAIR IN FWD CARGO COMPARTMENT IS NOT REPAIRED IAW OLD DOCUMENTATION OR ALLOWABLE SRM REFERENCE. TOP CAP BEAM WAS REPAIRED FOLLOWING PRINCIPLE OF SRM 53-10-15 / FIG 207.Jun 19, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR 07FDEA02195Stringer · damagedDAMAGED STRINGERS FOUND BETWEEN C28-29, STRG 53 RT AND BETWEEN C27-28, STRG 40 LT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14/FIG 201.Jun 19, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR 07FDEA02194Fitting · corrodedCORROSION AT MANHOLE FITTING BETWEEN C38.1-C38.2, WHICH WAS GRINDED THROUGH THE FITTING WITH THE SKIN PANEL AFFECTED. REPAIR PERFORMED BY BLEND OUT AND INSTALLATION WASHER IN BLEND VOID AND ADDITIONAL FASTENER IAW SRM 53-14-12/FIG 208, EA 6-5334-103277 AND RAJun 19, 2007 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA02193Beam · corrodedFWD CARGO DOOR, CORROSION ON SILL BEAM AND AROUND SEVERAL FASTENER HOLES FOUND. REPAIR PERFORMED BY REWORK AND INSTALLING REPAIR ANGLE IAW EA 6-5313-103279 AND RAS/DABRE/7006910/2006 ISSUE "A".Jun 19, 2007 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA02190Support Fitting · corrodedCORROSION ON Y-Z LATCH SUPPORT FITTING, C25A, RT. REPAIR PERFORMED IAW SRM 53-13-13 / FIG 204, SHEET 1 AND 2.Jun 19, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR 07FDEA02176Plate · damagedFRETTING MARKS ON INNER FLANGE C55 AND 57.2 LT AND C58 RT, P14-15 LT/RT, AND TOOL MARKS ON EMERGENCY EXIT TOP COVERPLATE LT/RT REPAIR PERFORMED BY BLEND OUT AND POLISHING TO SMOOTH CONTOUR IAW EA 6-5316-103275 AND RAS/DATLS/0003334/2006 ISS A AND RAS/DATLS/00Jun 18, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, StructureSDR 07FDEA02175Skin · unknownLT/RT ON SILL BEAM AND EXTERNAL SKIN, INTERNAL DOUBLER CORROSION AND DAMAGED HL, COLLARS (FOLLOWING P/N AFFECTED: A539-80110-207, A539-80071-205, A539-80071-205, A539-80108- 205, A539-81259-211, A539-80177-201, A539-80108-204, A539-81259-210, A539-80177-200).Jun 18, 2007 · N726FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR 07FDEA02174Skin · unknownOLD REPAIR (FLUSH DOUBLER) REPAIR ON RT OUTBOARD SLAT NR 3 JACK RIB 6 NOT CONFORM TO SRM (FILLER MATERIAL, RIVET PITCH, USED FASTENER). REPAIR PERFORMED BY NEW FLUSH REPAIR, APPROVED BY EA 6-5744-103280 REV A AND RAS/FOK/213/2006 ISS. C.Jun 18, 2007 · N726FD · Airbus A300B4622R · Wing, Control SurfacesSDR 07FDEA02173Skin · unknownOLD BONDING REPAIR RT AILERON LOWER SKIN T/E WITH NEW DELAMINATION REPAIR PERFORMED BY METAL SKINNED HONEYCOMB PATCH REPAIR IAW SRM 51-77-12 PB 200 PARA 4 AND RAS/FOK/097/ 2004 ISS A.Jun 18, 2007 · N726FD · Airbus A300B4622R · Wing, Plate/SkinSDR 07FDEA02172Skin · unknownOLD BONDING REPAIR LT AILERON LOWER SKIN T/E WITH NEW DELAMINATION REPAIR PERFORMED BY METAL SKINNED HONEYCOMB PATCH REPAIR IAW SRM 51-77-12 PB 200 PARA 4.Jun 18, 2007 · N726FD · Airbus A300B4622R · Wing, Plate/SkinSDR 07FDEA02171Doubler · misrepairedFOUND OLD DOUBLER REPAIR , C77-78, P27 RT NOT CONFORM TO SRM REPAIR PERFORMED BY NEW DOUBLER INSTALLATION IAW SRM 53-10-12 FIG 228, APPROVED BY EA 6-5318-103319.Jun 18, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA02170Doubler · noneOLD DOUBLER REPAIR C 19-20, P 38-40 LT, IN CONFLICT WITH P TO F CONVERSION REPAIR PERFORMED BY NEW DOUBLER INSTALLATION IAW EA 6-5313-103273 AND RAS/DABRE/7006901/2006 ISS A.Jun 18, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA02169Panel · misrepairedFOUND OLD DOUBLER REPAIR C19-20, P 43-44 RT, NOT CONFORM TO SRM. REPAIR PERFORMED BY NEW DOUBLER INSTALLATION IAW EA 6-5312-103293 AND RAS/AS/137/2006 ISS A.Jun 18, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR 07FDEA02168Door · chafedFOUND OLD DOUBLER INSTALLED ON BULK CARGO DOOR FWD LOWER CORNER, WHICH WAS NOT CONFIRM TO RAS (THICKNESS AND MATERIAL) REPAIR WAS PERFORMED BY INSTALLING A NEW DOUBLER IAW EA 6-5234-103320 AND RAS/DABRE/7006375/2006 ISS A.Jun 18, 2007 · N726FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR 07FDEA02090Skin Panel · wornELONGATED HOLES ON LT WING-PYLON SUPPORT BRACKET AND BOTTOM SKIN REPAIR PERFOMED BY OVERSIZING THE HOLE AND MANUFACTURE A FREEZE PLUG IAW DWG R571- 50532, APPROVED BY EA 6-5720-103269 AND RAS/BAE/1003287/2006 ISS. AJun 7, 2007 · N726FD · Airbus A300B4622R · Wing, Plate/SkinSDR 07FDEA02089Skin Panel · wornELONGATED HOLES ON RT WING-PYLON SUPPORT BRACKET AND BOTTOM SKIN, RIB 8 AREA REPAIR PERFORMED BY OVERSIZING HOLES AND MANUFACTURING FREEZE PLUGS IAW DWG R571-50532 ISS. A. APPROVED BY EA 6-5720-103269 AND RAS/BAE/1003287/2006 ISS. AJun 7, 2007 · N726FD · Airbus A300B4622R · Wing, Plate/SkinSDR 07FDEA02088Panel · crackedCRACK (L<25MM) ON PYLON NR 2, RIB 8, OUTBOARD SIDE DOUBLER REPAIR PERFORMED IAW SB 54-6015 AND DWG R546-10124, APPROVED BY EA 6-5451-103251.Jun 7, 2007 · N726FD · Airbus A300B4622R · Nacelle/Pylon, Plate/SkinSDR 07FDEA02087Frame · crackedC44 RT AND C46 RT, FOUND OLD DOUBLER REPAIR ON FRAME DUE TO CRACKING FINDINGS IAW SB 53-6122 REPAIR PERFORMED BY REPLACEMENT OF FRAME C 44 (P/N A538-12310-201) AND 46 (P/N A538-12312-201) IAW SRM 51-72-10.Jun 7, 2007 · N726FD · Airbus A300B4622R · Fuselage Main, Frame
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