JASC 5753
Service difficulty reports · 31,515
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 UIEA200600192Panel · crackedR/W-O/B MID FLAP COVE PANEL CRACKED AT SUPPORT ARM APPROX 14". AREA IS BETWEEN NR 7/8 CANOE-MARKED.SDR UIEA200600190Structure · chafedR/W-I/B AFT FLAP-UPPER SURFACE HAS TWO CHAFE MARKS FROM LONG SCREWS IN COVE PANEL ARM. CHAFE AREA ON I/B END-MARKED.SDR SWAA062703Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT STA 240. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA062683Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING OUTBOARD FORE FLAP DELAMINATED AT INBOARD LOWER SURFACE. REPAIRED FORE FLAP PER SRM.SDR IXXA060597SSkin · damagedDURING PRE-FLIGHT INSPECTION FOUND A HOLE ON THE RT IB FLAP TRAILING EDGE. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DRAWING NR AB84-57-100 DATED 7/28/06, AND DACO SRM 57-2-1.SDR IXXXA060597SSkin · damagedDURING PRE-FLIGHT INSPECTION FOUND A HOLE ON THE RIGHT HAND INBOARD FLAP TRAILING EDGE. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS PER COTNEY DRAWING NUMBER AB84-57-100 DATED 7/28/06,SDR 06FDEA2684Skin · dentedRIGHT HAND WING - INBOARD FLAP AFT INBOARD SEGMENT LOWER SKIN FOUND DENTED. RIGHT HAND WING INBOARD FLAP AFT INBOARD SEGMENT LOWER SKIN DENTED AREA. REPAIRED AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR UIEA200600187Skin · damagedLT INBOARD AFT FLAP HAS A .375 INCH DIAMETER HOLE AT BOTTOM SKIN. ACCOMPLISHED 250 DEGREES F. PREPREG PERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG 5 AND 51-40-12.SDR UIEA200600188Skin · damagedRT INBOARD AFT FLAP HAS A .250 INCH DIAMETER HOLE AT BOTTOM SKIN. ACCOMPLISHED 250 DEGREES F. PREPREG PERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG 5 AND SRM 51-40-12.SDR SWAA062663Torque Tube · corrodedDURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD MID FLAP, OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED MID FLAP TORQUE TUBE PER MM.SDR SWAA062661Skin · debondedDURING SCHEDULED 20Y CHECK, FOUND LT WING OUTBOARD FORE FLAP, LOWER SKIN DISBONDED AT INBOARD T/E WEDGE. REMOVED AND REPLACED LT OUTBOARD FORE FLAP PER MM.SDR SWAA062656Flap · corrodedDURING SCHEDULED 10Y CHECK, FOUND LT WING IB FORE FLAP CORRODED AT IB SHAFT. REMOVED AND REPLACED FORE FLAP IAW MM.SDR SWAA062629Wedge · debondedDURING SCHEDULED 20Y CHECK, FOUND LT WING IB MID FLAP T/E WEDGE UPPER AND LOWER AREAS DISBONDED. REMOVED AND REPLACED LT WING MID FLAP IAW MM.SDR ASAA0680807Skin · gougedRIGHT OUTBOARD FLAP INBOARD VANE IS GOUGED ON EXISTING REPAIR AT INBOARD LEADING EDGE. REMOVED EXISTING REPAIR DOUBLER. INSTALLED SKIN FILLER AND EXTERNAL DOUBLER PER SRM 57 03.SDR ASAA0680806Skin · gougedLEFT OUTBOARD FLAP INBOARD VANE IS GOUGED ON EXISTING REPAIR AT INBOARD LEADING EDGE. REMOVED EXISTING REPAIR DOUBLER. INSTALLED SKIN FILLER AND EXTERNAL DOUBLER PER SRM 57 03.SDR ASAA0641034Skin · puncturedLEFT OUTBOARD FORE FLAP REPAIR DOUBLER I/B END DAMAGED FROM TORQUE BOX SCREW. REMOVED PREVIOUS REPAIR DOUBLER, FABRICATED NEW REPAIR DOUBLER AND INSTALLED PER SRM 57-53-01 REPAIR 1 PG 201, 202.SDR QXEA200601921Flap Track · corrodedPDX C4 RIGHT HAND INBOARD FLAP OUTBOARD TRACK UPPER RAMP TOP SURFACE HAS TWO PITS. REPAIRED IAW RD 8-57-986.SDR IXXA06SMN227SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, LT WING.- OTBD VANE T/E CORRODED AND CRACKED, XOLDI 6.224.SDR 06FDEA02642Skin · dentedSNRM N01661: LHW: I/B FLAP UPP SURFACE FOUND WITH DENTS AS MARKED. SNRM N01661: LHW I/B FLAP UPPER SURFACE SKIN FABRICATED AND REPLACED AS PER EA NR 1-5730-102313. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA02641Skin · dentedRHW: I/B FLAP UPPER SURFACE FOUND WITH DENTS AS MARKED. RHW I/B FLAP UPPER SURFACE SKIN FABRICATED AND REPLACED AS PER EA NR 1-5730-102313. WING PLATES AND SKIN INBD FLAP UPPER SKIN REPLACEMENT. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR SWAA062560Torque Tube · corrodedDURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD MID FLAP, INBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED TORQUE TUBE PER MM.SDR SWAA062559Torque Tube · corrodedDURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD FORE FLAP INBOARD AND OUTBOARD TORQUE TUBES CORRODED. REMOVED AND REPLACED INBOARD AND OUTBOARD TORQUE TUBES PER MM.SDR 06FDEA2642Skin · dentedI/B FLAP UPPER SURFACE FOUND WITH DENTS AS MARKED.SDR 06FDEA2641Skin · dentedI/B FLAP UPPER SURFACE FOUND WITH DENTS AS MARKED.SDR SWAA062546Skin · crackedDURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD MID FLAP L/E SKIN CRACKED AT EXHAUST GATE PUSH ROD CUTOUT. REPAIRED MID FLAP SKIN PER SRM.SDR SWAA062531Wedge · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING MID FLAP WEDGE PANEL DELAMINATED AT OUTBOARD T/E. REMOVED AND REPLACED MID FLAP WEDGE PANEL PER MM.SDR SWAA062530Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD SIDE. REMOVED AND REPLACED LT OUTBOARD FLAP PER MM.SDR ARWA20060705Hinge Fitting · crackedDURING SERVICE CHECK INSPECTION FOUND LEFT WING OUTBOARD FLAP HINGE BASE FITTING AT STATION 219 CRACKED; O/B FITTING. REMOVED LEFT OUTBOARD FLAP ASSEMBLY IAW M/M 27-51-2 FOR REPAIR. PERFORMED WING FLAP SYSTEM ADJUSTMENT AND TEST IN ACCORDANCE DC-8 M/M 27-50-SDR 06FDEA02591Hinge Fitting · damagedEXISTING REPAIR FOUND AT RT WING O/B FLAP I/B HINGE ACTUATOR ATTACH FITTING. EXISTING REPAIR AT RT WING O/B FLAP I/B HINGE ACTUATOR ATTACH FITTING EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED PER DELTA ENG'G REPAIR/AUTHORIZATION 332715- 14, EO 1-5100-7-5001SDR 06FDEA02585Hinge Fitting · damagedEXISTING REPAIR FOUND AT RT WING O/B FLAP O/B HINGE ACTUATOR ATTACH LUG FITTING. EXISTING REPAIR FOUND AT RT WING O/B FLAP O/B HINGE ACTUATOR ATTACH LUG FITTING EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED PER DELTA ENG'G REPAIR/AUTHORIZATION 332719-14 E.O.1-5SDR 06FDEA02584Fitting · damagedEXISTING REPAIR AT RT WING INBD FLAP SUPPORT STRUCTURE AFT UPPER ROLLER. EXISTING REPAIR AT RT WING INBD FLAP SUPPORT STRUCTURE AFT UPPER ROLLER EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED PER DELTA ENG'G REPAIR/AUTHORIZATION 364949-14 E.O.1-5100-7-5001A PTSDR DHL2006809508Skin · delaminatedLT WING NR 4 FLAP VANE INTERNAL SKIN DELAMINATED. REMOVED AND REPLACED NR 4 LT FLAP VANE IAW MM 27-51-14 PG 201-202. REFER TO NR 058548 FOR OPS CHECK.SDR DHL2006809505Skin · damagedLT INBD FLAP UPPER SKIN HAS AN INTERIM REPAIR (STA XW 104.000 - 106.000). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED PANEL PLATING WITH EXISTING INTERIM REPAIR IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PANEL PLATING WITH PLATING (AL2024T3 0SDR 06FDEA2571Hinge Fitting · crackedLEFT HAND WING OUTBOARD FLAP INBOARD MID HINGE SUPPORT FITTING FOUND CRACKED. LEFT HAND WING OUTBOARD FLAP ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-30. OUTBOARD FLAP VANE ADJUSTMENT AND TEST CARRIED AS PER AMM 27-50-32-5. OUTBOARD FLAP ADJUSTMENT AND SDR SWAA062497Torque Tube · corrodedDURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD FORE FLAP OUTBOARD TORQUE TUBE CORRODED. REMOVED AND REPLACED INBOARD FORE FLAP TORQUE TUBE PER MM.SDR SWAA062489Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED INBOARD T/E. REPAIRED FORE FLAP SKIN PER SRM.SDR USAA060906Structure · wornFOUND RT OTBD MID FLAP, METAL WORN ON LOWER SIDE. BLEND OUT DAMAGE, PANTA PROCESS PERFORMED. INSTALLED FILLER AND DOUBLER IAW SRM 51-70-10, DEFECT SIZE: 1" BY .5".SDR USAA2010082391749Flap · delaminatedSAL - Q4 - MAJOR REPAIR - DELAMINATION ON LEFT WING INBOARD FOREFLAP 7 INCHES FROM LEADING EDGE & 46.5 INCHES INBOARD END BETWEEN WBL 110 TO WBL 126. REPAIRED LEFT WING INBOARD FOREFLAP 7 INCHES FROM LEADING EDGE & 46.5 INCHES INBOARD END BETWEEN WBL 110 TO WSDR UPS06247457Carriage · wornINSPECTION TYPE:C WEAR IN NR 7 FLAP CARRIAGE SIDE ROLLER ASSY BRACKETS. FLAP CARRIAGE REPLACED IAW MM 27-51-13.SDR UPS06247428Link · corrodedINSPECTION TYPE:C NR 5 FLAP CARRIAGE BEARING LINK BEARING A DRIFT AND BUSHING CORRODED. CORROSION FOUND ON INNER SURFACE OF BEARING LINK. BEARING LINK ASSY AND BUSHING REPLACED IAW MM 27-51-03.SDR UIEA200600176Panel · crackedDURING REGULAR INSPECTION, RT WING OB MID FLAP COVER PANEL DISCOVERED CRACKED ON UNDERSIDE APPROX 4 INCH ADJACENT TO SUPPORT ARMS AT STA 862/866. REPAIRED IAW SRM 51-40-14 AND EO 4757A300.SDR UIEA200600177Panel · crackedDURING REGULAR INSPECTION, LT WING OB MID FLAP COVE PANEL DISCOVERED CRACKED ON UNDERSIDE APPROX 22 IN ADJACENT TO SUPPORT ARMS LOCATED AT STA 1100/1122. REPAIRED IAW SRM 51-40-12 AND EO 4757A301.SDR 06FDEA2564Fitting · corrodedRIGHT HAND WING FLAP VANE SUPPORT NR 4 TO TRACK FOUND WITH CORROSION. RIGHT HAND WING FLAP VANE SUPPORT NR 4 TO TRACK CORROSION REPAIRED AS PER FEDEX EA 1-5750-100683, WINGS - RIGHT HAND NR 4 FLAP VANE TO TRACK SUPPORT CORROSION REMOVAL AND REPAIR. REPAIR CLSDR 06FDEA2563Fitting · corrodedRIGHT HAND WING FLAP VANE SUPPORT NR 2 TO TRACK FOUND WITH CORROSION. RIGHT HAND WING FLAP VANE SUPPORT NR 2 TO TRACK CORROSION REPAIRED AS PER FEDEX EA 1-5750-100681, WINGS - RIGHT HAND NR 2 FLAP VANE TO TRACK SUPPORT CORROSION REMOVAL AND REPAIR. REPAIR CLSDR 06FDEA2562Fitting · corrodedRIGHT HAND WING FLAP VANE SUPPORT NR 3 TO TRACK FOUND WITH CORROSION. RIGHT WING FLAP VANE SUPPORT NR 3 TO TRACK CORROSION REPAIRED AS PER FEDEX EA 1-5750-100682, WINGS - RIGHT HAND NR 3 FLAP VANE TO TRACK SUPPORT CORROSION REMOVAL AND REPAIR. REPAIR CLASSIFSDR 06FDEA2561Fitting · corrodedLEFT HAND WING OUTBOARD FLAP VANE FITTING ON NR 2 TRACK FOUND WITH CORROSION. LEFT HAND WING OUTBOARD FLAP VANE FITTING ON NR 2 TRACK CORROSION REPAIRED AS PER FEDEX EA 1-5750-100680. LEFT HAND NR 2 FLAP VANE TO TRACK SUPPORT CORROSION REMOVAL AND REPAIR. RSDR USAA060886Skin · crackedRT OTBD FLAP LEADING EDGE 10 FT 2" FROM OTBD EDGE. REMOVED DAMAGE (COMPOSITE) PERFORMED COMPOSITE LAY UP REPAIR PER SRM 57-53-00, DEFECT SIZE: 1.25" L BY 1".SDR UPS06247456Carriage · wornINSPECTION TYPE:C NR 8 FLAP CARRIAGE AFT SIDE ROLLERS FWD ATTACH HOLES WORN. FLAP CARRIAGE REPLACED IAW MM 27-51-13.SDR UPS06247434Carriage · corrodedINSPECTION TYPE:C NR 4 FLAP CARRIAGE FWD LOWER FLANGE CORRODED. FLAP CARRIAGE REPLACED IAW MM 27-51-03.SDR UPS06247386Carriage · corrodedINSPECTION TYPE:C NR 5 FLAP CARRIAGE HAS CORROSION ON LWR FWD FLANGE UPPER AND LOWER SURFACES CARRIAGE REPLACED IAW MM 27-51-03.
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