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 IPXA1666374Skin · wornINSPECTION TYPE:C, RT WING OTBD T/E AFT FLAP UPPER SURFACE PANEL 688KT MID AFT AREA FOUND WORN. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 2, REV 59.SDR FDEA201104101421Hinge Fitting · corrodedRT WING INBD FLAP OTBD HINGE (FLAP SIDE) XW254.000, PIVOT INBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-52-03, REV 69. ACCOMPLISHED EA 1-5750-149736, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201104101420Pivot Assy · corrodedRT WING OTBD FLAP INBD HINGE (FLAP SIDE) XW486.403, PIVOT BOARD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-04, REV 69. ACCOMPLISHED EA 1-5750-149728. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201104101419Hinge Fitting · corrodedRT WING OTBD FLAP INBD HINGE (FLAP SIDE) STA XW486.403, PIVOT INBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-04, REV 69. ACCOMPLISHED EA 1-5750-149728. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR SWAA112619Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LT WING AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR IPXA11166097Skin · dentedINSPECTION TYPE:10YR, LT OTBD FLAP LWR SKIN HAS EXTERNAL DENT WITH FILLER BUT NO EXTERNAL DOUBLER INSTALLED AT RIB 3A AND RIB 4 TRAILING EDGED. ACCOMPLISHED REPAIR ON LT OTBD FLAP T/E LWR SKIN AT RIB 3A AND RIB 4 IAW EO A300-5750-25611-F, APPENDIX A.SDR V0XR201104080002Flap Track · damaged(V0XR) LT INBOARD FLAP TRACK DAMAGED. REMOVED AND REPLACED FLAP TRACK. W/C 5079.SDR V0XR201104080001Flap Track · damaged(V0XR) LT OUTBOARD FLAP TRACK DAMAGED. REMOVED AND REPLACED FLAP TRACK. W/C 5078.SDR UALA2011040701678Attach Bracket · out of toleranceRIGHT INBOARD TE AFT FLAP, INBOARD PUSHROD ATTACH BRACKET HAS BEARING LOOSE AND COMING OUT OF BRACKET. REPLACED BRACKET AND BEARING ASSY. BRACKET IS SECURED ON FLAP.SDR HNAA2011050600118Shaft · corrodedRT NR 4 FLAP CARRIAGE HAS 3 WORN AND CORRODED MAIN ROLLER SHAFTS. R & R RT NR 4 FLAP CARRIAGE MAIN ROLLER SHAFT IAW -8300 AMM 57-50-43.SDR HNAA20110506117Bolt · corrodedLT NR 4 FLAP CARRIAGE GUARD BOLT IS CORRODED. R & R LT NR4 FLAP CARRIAGE GUARD BOLT IAW -8300 AMM 57-50-43.SDR HNAA2011050600116Shaft · corrodedLT NR 4 FLAP CARRIAGE HAS 3 MAIN ROLLER SHAFTS THAT ARE WORN AND CORRODED. R & R LT NR 4 FLAP CARRIAGE MAIN SHAFTS ISW -8300 AMM57-52-00.SDR SWAA112706Flap · delaminatedDURING SCHEDULED SPV CHECK, FOUND RT WING O/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR IPXA11166107Skin · gougedINSPECTION TYPE:4C, RT WING INBD FLAP UPPER SURFACE HAS EXISTING REPAIR DOUBLER WITH GOUGES BETWEEN STGR 2.1- 2.2 AND RIB 15-17. REPAIRED RT WING INBD FLAP UPPER SURFACE BETWEEN STGR 2.1 - 2.2 AND RIB 15 - 17 IAW STA-SA EA 300-5330-01-A3017 AND EO A300-5750-SDR FDEA201104051331Skin · crackedRT WING INBD FLAP UPPER SKIN AFT SEGMENT INBD UPPER CHORD FOUND WITH APPROX 8.5 INCH CRACK AFTER REMOVING THE SEGMENT FOR ACCESS TEE-FITTING. COMPLIED WITH "EO1-5100-7-5001 A5 PART 1, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR SWAA112529Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED AT I/B TRAILING EDGE. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA112508Flap · delaminatedDURING SCHEDULED 18Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR IPXA11M66554Vane · gougedINSPECTION TYPE:4C, LT INBD FLAP VANE T/E HAS GOUGE AND DELAMINATION ON INBD SIDE. REPAIR LT INBD FLAP VANE ALONG T/E NEAR STA XIFH138, REF EO MD11-5750-42438-A AND STASA EA 011-5750-01-A3055, REV IR.SDR UALA2011040401589Repair · looseRT WING INBD TRAILING EDGE FLAP HAS REPAIR UNDER INBD FLAP CANOE THAT IS COMING LOOSE AFT EDGE OF FLAP. REPLACED REPAIR PATCH.SDR IPXA11666029Fairing · delaminatedINSPECTION TYPE:7C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5, REV 49.SDR IPXA11666028Fairing · delaminatedINSPECTION TYPE:7C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A(1) FIG 5, REV 49.SDR NSVA2011071Flap · damagedCREW DISCOVERED 2 GASHES ON LEFT FLAP ROOT NEXT TO FUSELAGE. CAUSE OF DAMAGE IS UNKNOWN AT THIS TIME. IAH MAINTENANCE IS SENDING A ROAD TRIP TO INSPECT, REPAIR AND FERRY BACK TO IAH. FERRIED TO IAD, MAPPED FLAP DAMAGE, INSTALLED FLAP FROM 193CJ.SDR SWAA112448Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND RT WING O/B AFT FLAP T/E DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR DALA1123929871Vane · chafedRIGHT WING LOWER SURFACE FLAP O/B FIXED VANE O/B SIDE L/E HAS 1EA CHAFED SPOT DUE TO THAT IT IS CHAFING ON PNL 1604 O/B MOUNT ANGLE. PREPARED AREA. FABRICATED FILLER AND DOUBLER .020 7075-T6.BONDED USING BMS 5-101 TY2G10 ADHESIVE FILM IAW DC9 SRM 51-70-2.SDR A6WA201140374Vane · chafedLT INBD FLAP VANE L/E CHAFED IN 3 EA POSITIONS. FOUND TO BE WITHIN LIMITS IAW REO 601R-51-52-004. REPAIRED AS REQUIRED.SDR USAA2011051391851Strut · corrodedSAL - S4 - CORROSION ON LEFT WING INTERCONNECTING STRUT ASSEMBLY AT RIB 14. REPLACED LEFT WING INTERCONNECTING STRUT ASSEMBLY AT RIB 14 IAW A319 AMM 27-51-44.SDR IPXA11M65999Skin · dentedINSPECTION TYPE:3C, LT INBD FLAP LOWER SKIN DENTED/GOUGED APPROX AT STA 150, 15 INCHES FWD OF T/E. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-50-01, REPAIR 1, FIG 201.SDR DHLA201100043Doubler · crackedRT INBD FLAP.- FLAP JOINT RIB ANGLE DOUBLER SHOWS (2EA) CRACKS 1" AND .5". REMOVED CRACKED ANGLE DOUBLER IAW SRM 51-1-21. FABRICATED NEW ANGLE DOUBLER (AL2024T3 0.063") IAW SRM 57-2-0 FIG. 2, SHEET 2, SRM 51-9-0 FIG. 68A. CLEANED, TREATED AND PRIMED AREA + ANGSDR ASAA1149487Fitting · chafedLEFT O/B TRAILING EDGE ABOVE O/B END OF FORE FLAP ROLLER GUIDE FITTING CHAFED. REMOVED AND REPLACED FORE FLAP ROLLER GUIDE FITTING IAW B737 400 SRM 57 51 90 AND SRM 51 40 02.SDR FDEA201103311264Rib · crackedRIGHT INBOARD FLAP RIB 25A CRACKED REMOVED AND REPLACED RIB 25A AT RT FLAP IAW SRM 51-40-21 PARA.7 AND 51-40- 44 PAGE 6, TABLE 4 FOR LOCATED AND DRILLED.SDR MU1Z2011020200004Strut · bentFLAP INTERCONNECTING STRUT ON BOTH LT AND RT SIDES PROXIMITY SENSORS BENT.SDR SWAA112379Skin · delaminatedDURING SCHEDULED SPV CHECK, FOUND LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR FDEA201103301253Skin · gougedLEFT WING, INBD FLAP, FORE FLAP HAS AREA AT MOST OUTBD L/E GOUGED. REMOVED PREVIOUS REPAIR FROM LT INBD FOREFLAP IAW SRM REV 103, 51-30-2. FABRICATED NEW REPAIR IAW SRM 57-50-4, FIG 4 AND 57-50-2, FIG 3 INSTALLED DOUBLER IAW SRM 51-30-2 AND 57-50-4, FIG 4SDR UIEA2011033000234Skin · gougedR21 WING OTBD AFT FLAP NR 688JT GOUGED AT WBL 689.05. (PENDING)SDR DALA1126361802Fairing · delaminatedLEFT WING I/B MID FLAP O/B LEADING EDGE NOSE FAIRING FOUND DELAMINATION. PREPREG LAY-UP HOT BOND REPAIR CARRIED OUT AT DELAMINATION AREA IAW SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 FIG 5.SDR FDEA201103291213Support Beam · crackedWHILE GIVING OK TO INSTALL LT MLG AFT TRUNION FAIRING, BELLCRANK SUPPORT BEAM ASSY ON INBOARD TRAILING EDGE FLAP WITH CRACK. CRACKED BEAM ASSY REMOVED AND REPLACED IAW AMM 20-11-00-2 REV. 100. REPAIR IS CLASSIFIED AS MINOR.SDR UIEA2011032900188Skin · debondedPANEL NR 688IT OF RT OTBD AFT FLAP INNER SKIN DISBOND, WBL 747.678 RT, WBL 799.20 RT (REPAIR IAW NR T2011A57B-624)SDR USAA2011040191309Bolt · failedFLT 1017 - AFTER ARRIVAL, IT WAS NOTED THAT A STRUCTURAL FAILURE OF THE RT WING INBOARD FLAP TRACK ARM WAS SUSTAINED. IT WAS DETERMINED AFTER INITIAL INSPECTION THAT THE RIGHT WING INBOARD FOREFLAP, CENTER TRACK ARM FITTING FORWARD BOLT FAILED. REPLACED RIGHSDR AALA20110329TUL02Panel · damagedTHE RIGHT WING INBOARD FLAP HAS A DAMAGED AREA .75 INCH LONG BY .25 INCH WIDE, 41 INCHES FROM THE INBOARD EDGE SEAL AND 4.25 INCHES FORWARD OF TRAILING EDGE. RIGHT INBOARD FLAP REMOVED DAMAGED MATERIAL AS PER SRM 57-01-00, DYE CHECK SHOWS NO FURTHER CRACK MIGSDR FDEA201103291217Structure · corrodedLT WING OTBD FLAP, INBD FWD HINGE ACTUATOR OTBD HOLE FOUND CORRODED. ACCOMPLISHED EA 1-5750-149730, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201103291216Hinge · corrodedLT WING OTBD FLAP, INBD FWD HINGE ACTUATOR, INBD HOLE FOUND CORRODED. ACCOMPLISHED EA 1-5750-149730. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201103291212Hinge · corrodedLT WING OTBD FLAP, OTBD FWD HINGE ACTUATOR INBD HOLE FOUND CORRODED. ACCOMPLISHED EA 1-5750-149725, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR DALA1126351802Fairing · delaminatedRIGHT WING I/B MID FLAP O/B LEADING EDGE NOSE FAIRING FOUND DELAMINATION. PREPREG LAY-UP HOT BOND REPAIR CARRIED OUT AT DELAMINATION AREA IAW SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 FIG 5.SDR UALA2011032801489Skin · damagedLT INBOARD AFT FLAP INBOARD END POTTING SPLIT OPEN BOTH UPPER AND LOWER SKIN. MAJOR REPAIR ACCOMPLISHED: AREA FROM FWD SPAR T/E AFT 13 INCH ON UPPER SKIN AND 12 INCH ON LOWER SKIN AND OUTBOARD FROM INBD END OTBD 8 INCHES BOTH SIDES HAS DELAMINATION & FROZEN SDR SWAA112327Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR IPXA1165767Skin · dentedRT WING INBD T/E FLAP HAS DENT LWR SKIN D441887. REPAIRED IAW EO A300-5750-40771-B.SDR FDEA201103281211Hinge Fitting · corrodedLT WING OTBD FLAP OTBD FWD HINGE ACTUATOR INBD HOLE FOUND CORRODED. ACCOMPLISHED EA 1-5750-149725. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR FDEA201103281210Hinge Fitting · corrodedLT WING OTBD FLAP, OTBD FWD HINGE BARREL NUT FITTING. SURFACE FOUND CORRODED FLAP HINGE ARC0503-403, XW638.3059. REWORKED AS PER CMM 20-11-02 REV 69. FOUND WITHIN LIMITS PER DWG ARC0503 SHEET 2, REV BG AND CMM 57-44-09 REV 15, FIG 601 REWORK LIMITS. RSDR FDEA201103281209Hinge · corrodedLT WING OTBD FLAP, OTBD FWD HINGE LOWER MOUNT SURFACE FOUND CORRODED FLAP HINGE ARC0503-403. XW638.3059. ACCOMPLISHED EA 1-5750-149725. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR SWAA112275Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING O/B AFT FLAP I/B END UPPER SURFACE DELAMINATED. REPAIRED AFT FLAP PER SRM.
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