JASC 5753
Service difficulty reports · 31,513
Reports filed under 5753 · Trailing Edge Flaps, 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 jasc_code = '5753' 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 jasc_code = '5753' 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 IPXA2015080792100Skin · delaminatedINSPECTION TYPE:C, LT WING INBD MID FLAP UPPER T/E PANEL DELAMINATED. FIBERGLASS LAYUP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A, 1, FIG 5, REV 74.SDR IPXA2015080792099Skin · delaminatedINSPECTION TYPE: C, RT WING INBD FORE FLAP UPPER T/E WEDGE DELAMINATED. FIBERGLASS LAYUP REPAIR PERFORMED IAW SRM 51-70-07 PAR 5A, 1, FIG 5, REV 74.SDR SWAA2015080342465Flap Track · looseLEFT WING INBOARD FLAP INBOARD AFT FLAP TRACK AFT ATTACH POINT LOOSE. R & R FLAP TRACK IAW AMM.SDR AALA20150730001Skin · delaminatedLEFT INBOARD AFT FLAP TRAILING EDGE UPPER SURFACE FOUND DELAMINATED. COMPOSITE REPAIR ACCOMPLISHED IAW SRM 51-70-05 REPAIR 2.SDR SWAA2015081142646Skin · delaminatedLEFT WING INBD FLAP, FORE FLAP TOP SURFACE DELAMINATED APPROX 36" INBD OF OTBD EDGE. REPAIRED FORE FLAP IAW SRM.SDR IPXA2015080792102Fairing · chafedINSPECTION TYPE: C, RT WING INBD MID FLAP OTBD L/E FAIRING CHAFING. FIBERGLASS LAYUP REPAIR PERFORMED IAW SRM 51-70-07.SDR SWAA2015073142382Flap · delaminatedRIGHT WING INBOARD AFT FLAP DELAMINATED TRAILING EDGE. R & R AFT FLAP IAW AMM.SDR DALA2015073004748Guide Vane · damagedNICKS AND GOUGES FOUND ON INBD GUIDE VANE L/E OF INBD RT WING TE FLAP. THE GUIDE VANE WAS REPAIRED IAW SRM 57-03D.SDR FDEA201507292434Skin · gougedRIGHT WING INBOARD FLAP, UPPER PANEL EXTERNAL SKIN HAS GOUGE. REMOVED DOUBLER & REWORKED IAW SRM 51-70-10 REPAIR 2 EA F-5730-T0318678 PT 1. MAJOR REPAIR.SDR SWAA2015080442501Fairing · crackedLEFT WING NR 2 FLAP TRACK, AFT CANOE FAIRING, AFT TAIL CONE CRACKED AT FASTENER HOLE. REPAIRED FAIRING IAW SRM.SDR SWAA2015080342456Bracket · crackedLEFT WING NR 1 FLAP TRACK BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.SDR SWAA2015072942285Skin · delaminatedRIGHT WING INBOARD AFT FLAP DELAMINATED ON TRAILING EDGE. R & R AFT FLAP IAW MM.SDR SWAA2015090943518Skin · damagedLEFT WING TE FLAP UPPER SKIN CREASED AT XFLS 216. R & R SKIN IAW SRM & DWG.SDR SWAA2015082643230Angle · crackedRIGHT WING NR 6 FLAP TRACK ANGLE, CRACKED ON OTBD SIDE TE AREA. R & R ANGLE IAW SRM & DWG.SDR SWAA2015082443103Support Angle · crackedRIGHT WING NR 6 FLAP TRACK SUPPORT ANGLE CRACKED ON INTERNAL STRUCTURE, TE AREA AT LEVEL OF FAIR STATION 42.84. R & R ANGLE IAW SRM & DWG.SDR SWAA2015082443102Angle · crackedRIGHT WING NR 6 FLAP TRACK ANGLE CRACKED ON INTERNAL STRUCTURE, TE AREA BETWEEN FAIR STATION 14 TO 27. R & R ANGLE IAW SRM & DWG.SDR SWAA2015082443101Stiffener · crackedRIGHT WING NR 6 FLAP TRACK STIFFENER CRACKED ON INTERNAL AREA. R & R STIFFENER IAW DWG.SDR SWAA2015082042996Channel · crackedLEFT NR 3 FLAP TRACK CHANNEL CRACKED AT STATION 42.84 ON INTERNAL STRUCTURE TE AREA. R & R CHANNEL IAW SRM & DWG.SDR SWAA2015081942956Angle · crackedLEFT WING NR 3 FLAP TRACK TE ANGLE CRACKED ON OTBD SIDE. R & R ANGLE IAW SRM & DWG.SDR SWAA2015073042335Flap · delaminatedLEFT WING OUTBOARD FORE FLAP OUTBOARD END EDGE DELAMINATED. REPAIRED FORE FLAP IAW SRM.SDR DALA2015072804733Vane · damagedAFTER LANDING , WHEN FLAPS WERE RAISED TO 0 THE RT FLAP INDICATOR READS 5 AND LT FLAP INDICATOR READS 0, FELT SLIGHT BINDING WHEN ATTEMPTING TO RETRACT SLATS SO LT FLAPS OUT. INBD AND OTBD FLAP VANE GUIDE OF INBD FLAP WERE REPLACED FOR A SERVICIABLE FLAP VANSDR FDEA201507272399Bracket · corrodedLEFT INBD FLAP, OTBD AFT HINGE PIVOT INBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-03. REPAIRED IAW EA 1-5750-T0139125 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201507272398Bracket · corrodedLEFT INBD FLAP, OTBD AFT HINGE PIVOT INBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-03. REPAIRED IAW EA 1-5750-T0319125 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201507272397Bracket · corrodedRIGHT INBD FLAP, OTBD AFT HINGE PIVOT OTBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-02. REPAIRED IAW EA 1-5750-T0319124 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201507272396Bracket · corrodedRIGHT INBD FLAP, OTBD AFT HINGE PIVOT INBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-52-03. REPAIRED IAW EA 1-5750-T0319124 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR DALA2015072704724Skin · wornWEAR AT UPPER SKIN OF OTBD GUIDE VANE OF OTBD FLAP LT WING. REPAIRED IAW SRM 57-03D, PAR. II .SDR DALA2015072704723Skin · damagedWEAR AT L/E DOUBLER ON INBD GUIDE VANE OF OTBD FLAP, LT WING. INBD GUIDE VANE OF OTBD FLAP LT WING WAS REPAIRED IAW SRM 57-03D, PAR II.SDR AALA201507279003Skin · damagedLT OTBD TE FLAP, UPPER LE SKIN HAS A 10 SQUARE INCH AREA OF DAMAGE & MISSING COMPOSITE MATERIAL, LOCATED 110 INCHES FROM THE INBD END. R & R FLAP IAW JC 19L560287001.SDR SWAA2015081142680Flap · delaminatedLEFT WING OTBD AFT FLAP DELAMINATED AT OTBD CORNER. REPAIRED AFT FLAP IAW SRM.SDR SWAA2015081142679Skin · delaminatedLEFT WING OTBD FORE FLAP LOWER SKIN DELAMINATED AT INBD END. REPAIRED FORE FLAP IAW SRM.SDR DALA2015072704722Skin · dentedDENTS FOUND ON REPAIR OF INBD GUIDE VANE LOWER SURFACE ON LT WING INBD FLAP. THE REPAIR WAS REPLACED IAW SRM 57-03D.SDR DALA2015072604717Skin · dentedDENTS FOUND ON PREVIOUS REPAIR OF MID GUIDE VANE ON THE LT WING OTBD FLAP. A NEW DOUBLER WAS INSTALLED IAW SRM 57-03, PARR II.SDR FDEA201507252385Skin · delaminatedRIGHT WING OTBD FLAP TE WEDGE INBD SIDE UPPER SURFACE, FOUND DELAMINATION ABOUT 5" X 5.5" AT XOFH 455. SURFACE REPAIRED IAW SRM 57-50-80-2R REPAIR 1 & EA 1-5750-T0319001 PART 1. REFER TO WRI 57506042 FOR WORK DETAILS. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-SDR SWAA2015072742231Skin · delaminatedRIGHT WING OTBD AFT TE FLAP DELAMINATED AT INBD END. R & R FLAP ASSEMBLY IAW MM.SDR FDEA201507242377Skin · gougedLEFT WING INBD FLAP, UPPER SURFACE HAS 2 EACH DEEP GOUGE AT WS 258. WORK ACCOMPLISHED IAW EA F-5750-T0318998 P 2.SDR FDEA201507242376Skin · gougedLEFT WING INBD FLAP, UPPER SURFACE HAS 1 EACH DEEP GOUGE AT WS 270. WORK ACCOMPLISHED IAW EA F-5750-T0318998 P 2.SDR FDEA201507242375Hinge · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE BARREL NUTS HOLE SURFACE CORRODED. FOUND WITHIN LIMITS. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201507242374Hinge · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE LOWER MOUNT OTBD HOLE BORE CORRODED. REPAIRED IAW EA 1-5750-T0319119 PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201507242373Hinge · corrodedRIGHT WING OTBD FLAP, INBD FWD HINGE LOWER MOUNT INBD HOLE BORE CORRODED. REPAIRED IAW EA 1-5750-T0319119 PART 1. REPAIR CLASSIFIED AS MINOR GMM 6-2-100.SDR FDEA201507242370Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE LOWER MOUNT INBD HOLE SURFACE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIRED IAW EA 1-5750-T0319116 A PT 1. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100.SDR FDEA201507242369Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE LOWER MOUNT OTBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIRED IAW EA 1-5750-T0319116 PT 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201507242368Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE, LOWER MOUNT INBD HOLE BORE CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIRED IAW EA 1-5750-T0319116 PT 1. REPAIR CLASSIFIED AS GMM 6-2-100.SDR FDEA201507242367Hinge · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BARREL NUTS HOLE SURFACE CORRODED. CORROSION REMOVED IAW CMM 57-44-08. FOUND WITHIN LIMITS IAW DWG & CMM. A REPAIR SHIM WAS FABRICATED & INSTALLED IAW CMM 57-44-08.SDR FDEA201507242366Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE BARREL NUTS HOLE SURFACE CORRODED. REMOVED CORROSION IAW CMM 57-44-09. FOUND WITHIN LIMITS BASED THE DIFFERENCE BETWEEN DWG LIMITS & CMM. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201507242365Hinge · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE LOWER BARREL NUT HOLE BORE CORRODED. REWORKED & FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIR ACCOMPLISHED IAW EA 1-5750-T0319117 PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR IPXA2015080892135Skin · dentedINSPECTION TYPE:C, LEFT WING INBD MID FLAP LOWER PANEL DENTED. METAL HOT BOND REPAIR PERFORMED IAW EO B747-5750-58302-A AND RI-57-50-11015, REV A.SDR FDEA201507232344Skin · damagedLEFT INBD FLAP MID LE UPPER SURFACE DAMAGED. COMPLIED WITH EA 6-5750-T0318847 A P 1. THE REPAIR WAS CATEGORY A. THIS REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR SWIA201541376Skin · dentedTHERE IS A DENT ON THE RT INBD FLAP UPPER SURFACE APPROX 93" FROM INBD EDGE 8" FROM T/E. REPAIRED DENT ON THE RT INBD FLAP UPPER SURFACE APPROXIMATELY 93" FROM INBD EDGE 8" FROM T/E IAW SRM.SDR DALA2015072304579Guide Vane · wornWEAR ON REPAIR OF INBD GUIDE VANE L/E AT RT WING OTBD FLAP. THE GUIDE VANE WAS REPAIRED IAW SRM 57-03, PARR II .SDR SIMA20150722001Skin · delaminatedTRAILING EDGE DELAMINATION ON UPPER & LOWER SKIN LT INBD FLAP. REPAIRED IAW ERS-EM - 57MR-481.
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