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 GR4D20160720005Flap Track · corrodedLEFT A-FLAP TRACK HAS CORROSION INSIDE BORE OF ATTACH HOLE. CORROSION WAS FOUND DURING NORMAL SCHEDULED INSPECTION OF THAT AREA, REF MSG 3, CMP 575111.SDR GR4D20160720004Fitting · corrodedTHE LOWER A FLAP TRACK FITTING ON THE RT WING HAS CORROSION INSIDE BORE OF ATTACH HOLE. CORROSION WAS FOUND DURING NORMAL SCHEDULED INSPECTION OF THAT AREA, REF MSG 3, CMP 575111.SDR GR4D20160720003Attach Fitting · corrodedTHE LOWER A-FLAP TRACK FITTING ON THE LT WING HAS CORROSION INSIDE BORE OF ATTACH HOLE. CORROSION WAS FOUND DURING NORMAL SCHEDULED INSPECTION OF THAT AREA. REF MSG 3, CMP 575111.SDR GR4D20160720002Attach Fitting · corrodedTHE UPPER A-FLAP TRACK ATTACH FITTING ON THE LT WING HAS CORROSION INSIDE BORE OF ATTACH HOLE. CORROSION WAS FOUND DURING SCHEDULED INSPECTION OF THAT AREA, REF MSG 3 CMP 575111.SDR GR4D20160720001Attach Fitting · corrodedTHE UPPER A-FLAP TRACK ATTACH FITTING ON THE LT WING HAS CORROSION INSIDE BORE OF ATTACH HOLE. CORROSION WAS FOUND DURING SCHEDULED INSPECTION OF THAT AREA, REF MSG 3, CMP 575111.SDR SWAA2016080254379Skin · delaminatedRIGHT WING INBOARD FOREFLAP DELAMINATED. R & R THE FLAP IAW AMM.SDR COEA2016071822917Lug · corrodedDURING HEAVY CHECK, RT OUTBOARD FLAP, INBOARD FLAP SUPPORT BEAM, LOWER INBOARD LUG HAS CORROSION. REPAIRED IAW SRAS CETS-3311/16.SDR SWAA2016080454536Skin · delaminatedLEFT WING OTBD FORE FLAP UPPER SKIN DELAMINATED. REPAIRED SKIN IAW SRM.SDR REXA2016071401413Plate · crackedRIGHT OTBD FLAP MID HINGE ASSY INBD SIDE, GUIDE PLATE IS CRACKED. REMOVED AND REPLACED THE GUIDE PLATE IAW SRM 51-42-06.SDR SWAA2016071853915Skin · delaminatedRT WING INBD AFT FLAP DELAMINATED UPPER AND LOWER SURFACES. R & R AFT FLAP IAW MM.SDR MTNA20160715001Mount · crackedRIGHT INBOARD FLAP CAM GUIDE MOUNT CRACKED BEYOND MANUFACTURER'S ACCEPTABLE LIMITS. REPAIRED IAW AMM JIC 57-52-00RAI 10000.SDR SWAA2016081554801Fitting · corrodedRIGHT WING INBOARD FLAP TRACK FORWARD MOUNTING FITTING CORRODED. REPAIRED THE FITTING IAW EA.SDR FDEA201607132370Skin · crackedAGING AIRCRAFT, EXISTING REPAIR AT RT WING INBD FLAP SEGMENT UPPER SURFACE AT XIFH 171.3 -XIFH 177.3. EVALUATED AND FOUND CRACK COMMON TO SKIN. RIGHT WING INBD FLAP, INBD FLAP SEGMENT UPPER SURFACE XIFH 171.3-XIFH 177.3. CARRIED OUT REPAIR IAW EA 1-5750-T03SDR FDEA201607132432Hinge · corrodedRIGHT WING, INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.289", FINAL HOLE DIA: 1.328" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED ANSDR FDEA201607132431Hinge · corrodedRIGHT WING, INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT INBD BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.290", FINAL HOLE DIA: 1.328" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRSDR FDEA201607132415Hinge · corrodedLT WING, INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.188", FINAL HOLE DIA: 1.235" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED AND ISDR FDEA201607132413Hinge · corrodedLEFT WING, INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT INBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.188", FINAL HOLE DIA: 1.235" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED ANDSDR SWAA2016071553872Bracket · crackedLEFT WING INBD FLAP, OTBD TRACK, OTBD UPPER ANGLE CRACKED. R & R BRACKET IAW SRM.SDR SWAA2016071553871Flap · delaminatedRIGHT WING OTBD AFT FLAP DELAMINATED ON INBD LOWER CORNER. R & R AFT FLAP IAW AMM.SDR SWAA2016081654866Flap Track · corrodedRT WING NR 8 FLAP TRACK FORWARD ATTACHMENT CORRODED. REPAIRED 8 FLAP TRACK IAW EA.SDR SWIA201642441Panel · chafedRIGHT INBD FLAP PANEL 684LB CHAFED. REPLACED THE PANEL IAW SRM.SDR SWAA2016081554796Fitting · corrodedLEFT WING NR 4 FLAP TRACK FORWARD FITTING CORRODED. REPAIRED THE FITTING IAW EA.SDR SWAA2016071453790Skin · delaminatedRIGHT WING INBOARD AFT FLAP DELAMINATED. R & R THE FLAP IAW AMM.SDR DALA2016071305246Vane · wornWEAR ON AFT OTBD CORNER UPPER SURFACE ON OTBD FLAP, INBD VANE AT RT WING. AFT OTBD CORNER UPPER SURFACE ON OTBD FLAP, INBD VANE AT RT WING WAS REPAIRED IAW ER/A 492663-14MA, REV ORIG.SDR DALA2016071305244Vane · delaminatedDELAMINATE RT WING OTBD FLAP, INBD VANE NR 1. RT WING OTBD FLAP INBD VANE NR 1 WAS REPAIRED IAW SRM 57-03D, PAR 11 AND A/C 0995, CARD 2000-8149-04.SDR FOTR20160712002Skin · delaminatedRIGHT I/B FLAP UPPER SKIN SHOWS EVIDENCE OF DELAMINATION AT T/E WS 313.SDR SWIA201642435Panel · gougedLEFT WING INBOARD FLAP PANEL 584GB GOUGED. BLENDED THE GOUGED AREA IAW SRM.SDR DALA2016072105476Vane · corrodedCORROSION ON MID INBD STUD ALSO INNER FITTING ON OUTBD FLAP, OUTBD VANE AT LT WING. THE GUIDE VANE WAS REPLACED.SDR SWAA2016071253702Skin · delaminatedLEFT WING INBOARD TRAILING EDGE FLAP DELAMINATED ON OUTBOARD END. R & R AFT FLAP IAW AMM.SDR FDEA201607092345Flap · damagedFOUND LT INB'D AFT FLAP HAS DAMAGE. INSTALLED LT I/B AFT FLAP AND OPS CHECK OK PER AMM27-51-12-4. A/C OK FOR SERVICE.SDR SWAA2016081154737Skin · delaminatedLEFT WING OUTBOARD FORE FLAP DELAMINATED. REPAIRED THE FLAP IAW SRM.SDR SWAA2016071853950Skin · delaminatedLEFT WING OTBD FORE FLAP LOWER SURFACE DELAMINATED AT T/E. REPAIRED FORE FLAP IAW SRM.SDR REXA2016070701344Vane · chafedLEFT WING INBD FLAP VANE L/E CHAFED IN THREE PLACES INBD, CTR AND O/B AREAS. I FLAP VANE SKIN REMOVED AND REPLACED IAW REO 601R-57-52-004.SDR SWAA2016072654255Flap Track · corrodedRIGHT WING NR 8 FLAP TRACK AFT LOWER HOLE CORRODED. REPAIRED FLAP TRACK IAW CMM.SDR DALA2016072105475Vane · corrodedCORROSION ON OUTBD LOWER FACE MID VANE OUTBD FLAP RT WING. DUE TO EXCESSIVE CORROSION THE GUIDE VANE WAS REPLACED IAW SRM 57-03D PAR 11.SDR DALA2016072005448Vane · wornWEAR AT OUTBOARD FLAP VANE 3 RT WING. FLAP VANE REPLACED IAW SRM 57-03D PAR.11.SDR DALA2016070605123Vane · damagedRT NR 4 VANE HAS RUBBING MARKS. R & R VANE REF AMM 27-51-03.SDR FDEA201607032241Bushing · corrodedLEFT WING OTBD FLAP VANE FITTING F, BUSHING HOLE, CORRODED. BUSHING HOLE CORROSION REWORKED PER SRM 57-50-02-2R FIGURE 201 AND FOUND EXCEED LIMIT. EXISTING HOLE SIZE 0.860" X 0.5655", FINAL HOLE SIZE: 0.9565" X 0.6585", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.67SDR FDEA201607032237Bushing · corrodedLT WING OUTBOARD FLAP VANE FITTING 'B' BUSHING HOLE CORROSION. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.935" X 0.650", FINAL HOLE SIZE: 1.0325" X 0.740", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OSDR FDEA201607032236Bushing · corrodedLEFT WING OTBD FLAP VANE FITTING C, BUSHING HOLE CORRODED. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.856" X 0.597", FINAL HOLE SIZE: 0.997" X 0.704", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OVERSISDR FDEA201607032235Bushing · corrodedLT WING OTBD FLAP VANE FITTING D, BUSHING HOLE, CORRODED. BUSHING HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIGURE 201. EXISTING HOLE SIZE 0.876" X 0.580", FINAL HOLE SIZE: 0.953" X 0.660", MAXIMUM ALLOWABLE LIMIT: 0.940" X 0.670". OVERSIZSDR FDEA201607032232Hinge Bracket · corrodedLEFT WING OTBD FLAP, FLAP SIDE, INBD AFT HINGE PIVOT INBD HOLE BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT CMM 57-52-04. EXISTING HOLE: DIA 1.154", FINAL HOLE: DIA 1.217", MAXIMUM ALLOWABLE HOLE: DIA 1.150". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA1SDR DALA2016070505098Vane · damagedRIGHT NR 3 FLAP VANE HAS A RUBBING AREA WITH A HOLE THROUGH. R & R VANE IAW AMM 27-51-03.SDR SWIA201642415Skin · chafedREPLACE RT INBD FLAP VANE CENTER L/E PN 601R14303-52 FOUND CHAFED. REMOVED AND INSTALLED SERVICEABLE RT INBD FLAP, CENTER L/E IAW SRM.SDR SWAA2016072054091Flap Track · crackedRIGHT WING NR 7 FLAP TRACK TAIL CONE CRACKED. REPAIRED FLAP TRACK TAIL CONE IAW SRM.SDR A6WA201644061Lug · chafedRIGHT O/B FLAP, CENTER HINGE ARM FWD ATTACH POINT, O/B LUG IS CHAFED. REPAIRED IAW REO 601R-57-53-1048 REV.SDR FDEA201607012214Hinge · corrodedRIGHT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE: DIA 1.330", FINAL HOLE: DIA 1.336", MAXIMUM ALLOWABLE HOLE: DIA 1.220". OVERSIZE BUSHING FABRICATED SDR FDEA201607012213Hinge · corrodedRIGHT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT INBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE: DIA 1.330", FINAL HOLE: DIA 1.336", MAXIMUM ALLOWABLE HOLE: DIA 1.220". OVERSIZE BUSHING FABRICATED IAW SDR FDEA201607012212Hinge · corrodedLEFT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT OUTBOARD HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.294", FINAL HOLE DIA: 1.327", MAXIMUM ALLOWABLE HOLE DIA: 1.220", OVERSIZE BUSHING FABRICATED ANDSDR FDEA201607012211Hinge · corrodedLEFT WING INBOARD FLAP (FLAP SIDE) OUTBOARD AFT HINGE PIVOT INBOARD HOLE BORE CORRODED. HINGE REWORKED AND FOUND EXCEED LIMIT PER CMM57-52-03. EXISTING HOLE DIA: 1.294", FINAL HOLE DIA: 1.327", MAXIMUM ALLOWABLE HOLE DIA: 1.220". OVERSIZE BUSHING FABRICATED
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