N743FD
Service difficulty reports · 263
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 = 'N743FD' 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.
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 = 'N743FD' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 08FDEA03571Skin · damagedKRUEGER FLAP WAS DAMAGED DURING FUNCTION CHECKS REPAIR PERFORMED BY REPLACEMENT OF KRUEGER FLAP ASSY IAW AMM 27-87-11/401.SDR 08FDEA03515Shroud · corrodedFOUND CORROSION ON TOP SKIN OF OUTER SHROUD BOX, RIB 25-28 RT OUT OF LIMIT. REPAIR PERFORMED BY CUT AWAY THE AFFECTED RIBS, REWORK OF CORROSION AND INSTALLING MANUFACTURED ANGLES TO THE CUT RIB POSITIONS IAW RAS/BAE/1007548/2008 ISS, APPROVED BY EA 6-5751-120SDR 08FDEA03513Shroud · corrodedFOUND CORROSION ON TOP SKIN OF OUTER SHROUD BOX, RIB 25-28 LT OUT OF LIMIT. REPAIR PERFORMED BY CUT AWAY THE AFFECTED RIBS, REWORK OF CORROSION AND INSTALLING MANUFATURED ANGLES TO THE CUT RIB POSITIONS IAW RAS/BAE/1007548/2008 ISS A, APPROVED BY EA 6-5751-12SDR 08FDEA03510Structure · corrodedFOUND CORROSION UNDER STATIC DISCHARGER ON RT WING TIP. REPAIR PERFORMED BY CORROSION REWORK AND INSTALLING AN EXTERNAL PATCH IAW RAS/FOK/160/2008 ISS A, APPROVED BY EA 6-5730-120085.SDR 08FDEA03509Track · damagedROLLER TRACK IN AFT CARGO COMPARTMENT,C 56-58, Y -1470 WAS DAMAGED. REPAIR SOLUTION IAW SRM 53-10-15 WAS NOT APPLICABLE DUE TO EXISTING SHEAR PLATES BETWEEN C 57-57.3 ROLLER TRACK REPAIR WAS PERFORMED IAW RAS/EFW/9000085/2008 ISS A, APPROVED BY EA 6-5316-SDR 08FDEA03484Fitting · corrodedFOUND CORROSION ON LT MLG FWD PICK UP FITTING HOLE NR 8 AND NR 13. REPAIR PERFORMED BY BLEND OUT THE CORROSION, OVERSIZE THE HOLES IAW DRAWING R572-40266 AND INSTALLING BOLTS A228S32X IAW RAS/BAE/1006539/2008 ISS A , APPROVED BY EA 6-5751-1210094.SDR 08FDEA03483Spar · corrodedFOUND CORROSION ON LT MLG FWD PICK UP FITTING AREA ON REAR SPAR (HOLE NR 8, NR 13). REPAIR PERFORMED BY BLEND OUT THE CORROSION IAW RAS/BAE/1006539/2008 ISS A, APPROVED BY EA 6-5751-1210094.SDR 08FDEA03482Nut · corrodedFOUND CORROSION ON LT FWD PICK UP SPHERICAL BEARING NUT. REPAIR PERFORMED BY REPLACEMENT OF NUT IAW AMM 321124/401.SDR 08FDEA03479Panel · corrodedFOUND CORROSION ON RUDDER SIDE PANEL AT BR NR 1, LT. REPAIR PERFORMED BY REPLACEMENT OF LIGHTNING STRIKE PROTECTION PLATE AND LAMINATING IAW RAS/DAHAM/4025191/2008 ISS B, APPROVED BY EA 6-5541-120083.SDR 08FDEA03478Doubler · corrodedFOUND CORROSION ON DOUBLER AT BULK CARGO DOOR CUT OUT C 67-69, P 45-46 RT. REPAIR PERFORMED BY CORROSION REWORK, NDT FOR CORROSION FREE CONDITION AND FLAP PEENING IAW RAS/EFW/9000073/2008 ISS A, APPROVED BY EA 6-5317-123021.SDR 08FDEA03477Skin · corrodedFOUND CORROSION ON INNER SKIN AT BULK CARGO DOOR CUT OUT C 67-69, P 45-46 RT. REPAIR PERFORMED BY CORROSION REWORK, NDT FOR CORROSION FREE CONDITION AND FLAP PEENING IAW RAS/EFW/9000073/2008 ISS A, APPROVED BY EA 6-5317-123021.SDR 08FDEA03476Pan · crackedLT SLAT NR 1 FOLDING NOSE INNER PAN WITH CRACK FINDING REPAIR PERFORMED BY INSTALLING SB A300-6067 WITH INNER PAN REPLACEMENT, APPROVED BY EA 6-5742-120064.SDR 08FDEA03475Structure · damagedSLAT NR 2 LT WAS DAMAGED AT RIB 12-14 REPAIR PERFORMED IAW SRM 57-43-11 PARA 4A.SDR 08FDEA03472Frame · dentedFOUND DEFORMED FRAME FLANGE, C 74, P 26-27 RT. REPAIR PERFORMED BY REWORK OF OUTER FLANGE AT RUN OUT TO ELIMINATE THE DEFORMATION IAW RAS/EFW/9000059/2008 ISS A, APPROVED BY EA 6-5318-123090.SDR 08FDEA03471Frame · crackedFOUND CRACK IN FRAME C 56 RT AT STRINGER P 22 RT. REPAIR PERFORMED IAW R539-71112 AND INSTALLING A REPAIR T-PROFILE IAW. RAS/EFW/9000062/2008 ISS C, APPROVED BY EA 6-5316-123030 A.SDR 08FDEA03470Rib · chafedFOUND CHAFING MARKS ON LT WING TRAILING EDGE STRUCTURE RIB 6A-6B. REPAIR PERFORMED BY REWORK OF CHAFING MARK AT RIB 6A AND NDT FOR CRACK FREE CONDITION AND REWORK CHAFING MARK AT INTERMEDIATE RIB WITH INSTALLING A NEW RUBBING PLATE IAW RAS/BAE/1007587/2008 SDR 08FDEA03469Skin · corrodedCORROSION ON RT WING TOP SKIN, AFT OF REAR SPAR, RIB 3-6, AROUND HOLES 118, 119, 120,121 (DRAWING R571-40141). REPAIR PERFORMED BY CORROSION BLEND OUT IAW RAS/BAE/1007607/2008 ISS A, APPROVED BY EA 6-5720-123018.SDR 08FDEA03468Skin · crackedCORROSION ON LT WING TOP SKIN, AFT OF REAR SPAR, RIB 3-6, AROUND HOLES 119, 120,121 (DRAWING R571-40141) AND CRACK FINDING AT HOLE 49. REPAIR PERFORMED BY CORROSION BLEND OUT IAW RAS/BAE/1007607/2008 ISS A , APPROVED BY EA 6-5720-123018.SDR 08FDEA03467Support Bracket · wornELONGATED HOLE ON LT PYLON TO WING SUPPORT BRACKET AND BOTTOM SKIN. REPAIR PERFORMED BY OVERSIZING THE HOLES AND INSTALLING FREEZE PLUGS IAW. DRAWING R571-50532 ISS A AND RAS/BAE/1007780/2008, APPROVED BY EA 6-2900-123041.SDR 08FDEA03413Panel · delaminatedFOUND DELAMINATION ON RT OUTER SHROUD BOX TOP SKIN HONEYCOMB REPAIR PERFORMED BY IAW SRM 51-77-12 AND RAS/BAE/1007735/2008 ISS A, APPROVED BY EA 6-5751-123040.SDR 08FDEA03412Window Frame · damagedFOUND ON FUSELAGE NOSE SECTION, WINDSHIELD FRAME LT, C 2-7 AN OLD REPAIR (DEVIATED RIVETS INSTALLED). REPAIR PERFORMED BY REMOVING EXISTING REPAIR, OVERSIZE THE HOLES AND INSTALL RIVETS IAW RAS/70512490/028/2008 AND EA 6-5311-123044.SDR 08FDEA03411Skin · chafedFOUND CHAFING MARKS ON LT CENTER FLAP UPPER SKIN AFT OF REPAIR SPAR, RIB 4-4A AND 15-16. REPAIR PERFORMED BY REWORK OF CHAFING MARKS AND INSTALLING A NEW CHAFING PLATE IAW RAS/197/2008 ISS A, APPROVED BY EA 6-5754-123032.SDR 08FDEA03410Skin · chafedFOUND CHAFING MARKS ON LT CENTER FLAP UPPER SKIN RIB 13-13A. REPAIR PERFORMED BY REWORK OF CHAFING MARKS AND INSTALLING A NEW CHAFING PLATE IAW, RAS/197/2008 ISS A, APPROVED BY EA 6-5753-123011.SDR 08FDEA03384Skin · chafedFOUND CHAFING MARKS ON SLAT NR 1 RT LOWER SKIN. REPAIR PERFORMED BY BLEND OUT THE DAMAGE IAW RAS/FOK/153/2008 ISS A, APPROVED BY EA 6-5742-120090.SDR 08FDEA03383Skin · delaminatedFOUND DELAMINATION AT SPOILER 5 RT, LT/RT HINGE ARM LOWER SURFACE AND TOP SKIN OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF SPOILER IAW AMM 27-61-53 /401.SDR 08FDEA03382Skin · delaminatedFOUND DELAMINATION AT SPOILER 5 LT CENTER HINGE ARM LOWER SURFACE OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF SPOILER IAW AMM 27-61-53 /401.SDR 08FDEA03300Attach Fitting · corrodedCORROSION FOUND IN BOLT HOLES OF FORWARD PYLON TO ENGINE ATTACH FITTING. REPAIR PERFORMED BY REWORK OF CORROSION, NDT FOR CORROSION FREE CONDITION. REPLACE THE TAPERED SHIM AND PROTECT RIB 8 WITH CADMIUM PLATING IAW RAS/70511822/004/2008 ISS A, APPROVED BY ESDR 08FDEA03299Attach Fitting · corrodedCORROSION FOUND IN BOLT HOLES OF FORWARD PYLON TO ENGINE ATTACH FITTING. REPAIR PERFORMED BY REWORK OF CORROSION, NDT FOR CORROSION FREE CONDITION, AND PROTECT RIB 8 WITH CADMIUM PLATING IAW RAS/70511822/004/2008 ISS A, APPROVED BY EA 6-5451-120089.SDR 08FDEA03296Fairing · chafedFOUND CHAFING MARKS ON PYLON NR 2 UPPER AFT FAIRING RIB 19 REPAIR PERFORMED BY REWORK OF CHAFING MARK, NDT FOR CRACK FREE CONDITION AND INSTALLING A STRIP TO LIMIT NEW CHAFING IAW RAS /70511364/010/2008 ISS A , APPROVED BY EA 6-5454-120084.SDR 08FDEA03295Skin · misrepairedFOUND OLD DOUBLER REPAIR ON LT AILERON UPPER SKIN, T/E, RIB 14-15, REPAIR WAS NOT PERFORMED IAW RELATED SRM. REPAIR RENEWED IAW RAS/FOK/163/2008, APPROVED BY EA 6-5761-120087.SDR 08FDEA03243Doubler · corrodedFOUND CORROSION AND SMALL NICK AT ANTENNA DOUBLER C 63-65, P 55 -56 LT REPAIR PERFORMED BY REWORK OF BOTH DAMAGES, NDT FOR CORROSION FREE CONDITION AND FLAP PEENING IAW RAS/EFW/9000072/2008 ISS A, APPROVED BY EA 6-5317-123038.SDR 08FDEA03240Doubler · corrodedFOUND CORROSION AT DOUBLER C 71-72, P 54-56 RT. REPAIR PERFORMED BY REMOVAL OF CORROSION AND FLAP PEENING IAW RAS /EFW/9000070/2008 ISS A, APPROVED BY EA 6-5317-123027.SDR 08FDEA03237Skin · corrodedFOUND CORROSION ON SKIN PANEL C 71-72, P 57 LT. REPAIR PERFORMED BY CORROSION REMOVAL, NDT FOR SKIN THICKNESS AND FLAP PEENING IAW RAS/EFW/9000068/2008 ISS A, APPROVED BY EA 6-5317-123009.SDR 08FDEA03236Structure · dentedDENT AND SCRATCH FOUND AT PAX DOOR 4 LT (DENT OUT OF LIMIT). REPAIR PERFORMED BY REWORK OF DAMAGED AREA, NDT FOR CRACK FREE CONDTION AND FLAP PEENING IAW RAS/DAHAM/4025321/2008 ISS A , APPROVED BY EA 6-5213-123026.SDR 08FDEA03233Structure · corrodedFOUND CORROSION AT T-SECTION, C 93, P 23 REPAIR PERFORMED BY CUT OUT AND INSTALLING A REPAIR PROFILE IAW, RAS/EFW/9000074/2008 ISS A, APPROVED BY EA 6-5319-123033.SDR 08FDEA03232Stringer Splice · corrodedFOUND CORROSION ON STRINGER COUPLING P 56RH, C 65 OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 08FDEA03231Stringer · corrodedFOUND CORROSION ON STRINGER P 54RH, C 71-72 OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 08FDEA03230Stringer · corrodedFOUND CORROSION ON STRINGER P 56 LT, C 64 OUT OF LIMIT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201A.SDR 08FDEA03129Frame · gougedDURING INSPECTION FOUND DAMAGE ON FR 47 LT FORWARD AND AFT FITTING, S21-26L. REPAIR PERFORMED BY SMOOTH REWORK AND SPOT FACING IAW RAS 70511944/017/2008 ISSUE A AND EA 6-5310-120093.SDR 08FDEA03128Frame · gougedDURING INSPECTION FOUND SEVERAL TOOL MARKS WERE FOUND ON FR 47 RT FORWARD AND AFT FITTING, S21-26R. REPAIR PERFORMED BY SMOOTH REWORK AND SPOT FACING IAW, RAS 70511944/017/2008 ISSUE A AND EA 6-5310-120093.SDR 08FDEA03124Fitting · crackedDURING SB53-6123 INSPECTION, SEVERAL CRACKS AND TOOL MARKS WERE FOUND ON BOTH LT AND RT IN SPLICE, IN FR 47 FORWARD AND AFT FITTING. REPAIR PERFORMED BY DEPENDING OF AREA OVERSIZING HOLES, PERFORMING SMOOTH REWORK AND SPOT FACING IAW RAS 70511944/017/2008 ISSSDR 08FDEA03127Frame · gougedDURING INSPECTION FOUND SEVERAL TOOL MARKS WERE FOUND ON FR47 RT FORWARD AND AFT FITTING, STR 21-26. REPAIR PERFORMED BY DEPENDING PERFORMING SMOOTH REWORK AND SPOT FACING IAW RAS 70511944/017/2008 ISSUE A AND EA 6-5310-120093.SDR 08FDEA03123Lug · corrodedCORROSION WAS FOUND ON THE MLG GEAR RIB 5 AFT PINTLE BEARING FORWARD LUG, RT WING. REPAIR PERFORMED BY OVERSIZING THE BORE, REDUCING THE LUG THICKNESS, NDT INSPECTION (NIL FINDINGS), PERFORMING A FINISHING CUT AND INSTALLING OVERSIZE BUSHES, ALL IAW REPAIR INSDR 08FDEA03119Skin Panel · damagedOLD REWORKS AT SKIN PANEL AT AFT CARGO DOOR CUTOUT, FR63A, STR 29 RT. ONE IS OUT OF SRM LIMIT. REPAIR PERFORMED BY REWORK AND FLAP PEENING IAW RAS/EFW/9000067/2008 ISSUE B, APPROVED BY EA 6-5317-120099.SDR 08FDEA03118Floorbeam · corrodedCORROSION ON CARGO FLOOR CROSSBEAM FR56 RT, AFT CARGO COMPARTMENT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 208 SHEET 4.SDR 08FDEA02969Sill · corrodedFOUND CORROSION ON SILL BEAM, FWD CARGO COMPARTMENT, C25A. REPAIR PERFORMED BY CUT OUT THE UPPER FLANGE AND INSTALLING REPAIR ANGLE IAW RAS/EFW/9000051/2008 ISS A, APPROVED BY EA 6-5313-123031.SDR 08FDEA02968None · noneFOUND AT SLAT NR 1 RIB 2A, PLUGGED HOLES, MOST LIKELY FROM PRODUCTION OF SLAT. REPAIR PERFORMED BY LEAVE IT AS IT IS AND TOPCOAT THE AREA IAW RAS/FOK/149/2008 ISS A, APPROVED BY EA 6-5742-120081.SDR 08FDEA02967None · noneFOUND OLD REPAIR AT SLAT NR 1 RT INBOARD ARM BASE, RIB 2 A, WITH REFENCE TO RAS/FOK/054/2004. REPAIR DEVIATES FROM RAS REPAIR RENEWED (SKIN INSERT ) IAW RAS/FOK/148/2008 ISS A, APPROVED BY EA 6-5742-120081.SDR 08FDEA02966Skin · damagedFOUND SEVERAL DAMAGES ON INNER SKIN C 40 AFT FITTING OUTER FLANGE (HOLE 15 AND 16). REPAIR PERFORMED BY SMOOTH REWORK ON INNER SKIN PANEL ABOVE HOLE 15, OVERSIZE HOLE 15, REWORK OF WHOLE FLANGE AT HOLE 16 IAW RAS/70511563/030/2008 ISS A, APPROVED BY EA 6-534SDR 08FDEA02956Frame · damagedFOUND DAMAGED HOLE AT C 40, BETWEEN P 5-6 RT REPAIR PERFORMED BY ENLARGING THE HOLE TO 6MM. PERFORM NDT FOR CRACK FREE CONDITION AND INSTALLING HL11VF8/HL70-8 FASTENER IAW RAS/DAHAM/4025121/2008 ISS A , APPROVED BY EA 6-5315-120079.
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