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 FDEA202405280878Skin · cracked1EA CRACK (15MM) WAS FOUND AT L/H WING CENTER FLAP RIB17 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED FLANGE REPAIR AT RIB17 S-2.8~R/S AND DOUBLER REPAIR AT RIB17~18 S-2.1~R/S LH CENTER FLAP I.A.W FEDEX EA NO:T6-5750-T0379330 P1, SEQ NO:1249, TITLE:WINSDR IPXA2024062585094Support Beam · crackedLEFT WING O/B FLAP O/B HINGE PANEL SUPPORT FRAME IS CRACKED. INSTALLED REPLACEMENT SUPPORT FRAME AT L/H WING O/B FLAP O/B HINGE PANEL REF. MD-11 SRM 51-35-01-OG-0.SDR FDEA202405270823Rib · cracked1EA CRACK (10MM) WAS FOUND AT R/H WING CENTER FLAP RIB20 AFT AREA OF TOP SURFACE RIB FLANGE ACCOMPLISHED THE FLANGE REPAIR AT RIB20 S-2.7~2.8 AND DOUBLER REPAIR AT RIB19~20 S- 2.1~R/S RH CENTER FLAP I.A.W FEDEX EA NO:T6-5750-T0379321 P1, SEQ NO:1236, TITLE:SDR FDEA202405270822Rib · crackedONE CRACK (8MM) WAS FOUND AT R/H WING CENTER FLAP RIB17 AFT AREA OF TOP SURFACE RIB FLANGE ACCOMPLISHED THE FLANGE REPAIR AT RIB17 S-2.8~R/S AND DOUBLER REPAIR AT RIB17~18 S- 2.1~R/S RH CENTER FLAP I.A.W FEDEX EA NO:T6-5750-T0379321 P1, SEQ NO:1236, REPAISDR FDEA202405270821Rib · crackedONE CRACK (8MM) WAS FOUND AT R/H WING CENTER FLAP RIB11 AFT AREA OF TOP SURFACE RIB FLANGE ACCOMPLISHED THE FLANGE REPAIR AT RIB11 S-2.8~R/S AND DOUBLER REPAIR AT RIB11~12 S- 2.1~R/S RH CENTER FLAP I.A.W FEDEX EA NO:T6-5750-T0379321 P1, SEQ NO:1236, REPAIRSDR UIEA2024052200401Skin · delaminatedLHW I/B MID FLAP L/E FAIRING TO I/B EDGE 157" FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052200402Skin · delaminatedRHW O/B FORE FLAP L/E FAIRING I/B EDGE110" FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052200403Skin · delaminatedLHW I/B FORE FLAP L/E FAIRING I/B EDGE 230" FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052200404Skin · delaminatedRHW I/B AFT FLAP LOWER T/E I/B EDGE 172" FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052200405Skin · delaminatedRHW O/B MID FLAP L/E FAIRING I/B EDGE14" FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052200406Skin · delaminatedRHW O/B FORE FLAP L/E FAIRING 158" TO I/B EDGE FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052200407Skin · delaminatedLHW I/B AFT FLAP UPPER T/E FROM I/B EDGE 122" FOUND DELAMINATION(<P>PERFORMED PERMANENT COMPOSITE HOTBOND REPAIR SRM 51-70-07 PAR 5A REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052300408Skin · dentedRHW O/B AFT FLAP LOWER T/E 24" TO I/B PNL EDGE FOUND DENT(<P>PERFORMED PERMANENT METAL TO METAL HOTBOND REPAIR SRM 51-70-10 REPAIR 4 REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052300409Skin · dentedLHW O/B AFT FLAP LOWER T/E 36" TO I/B PNL EDGE FOUND DENT(<P>PERFORMED PERMANENT METAL TO METAL HOTBOND REPAIR SRM 51-70-10 REPAIR 4 REV.100 REV DATE:20 FEB 2024. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052300431Access Panel · chafedLHW O/B T/E AFT FLAP O/B UPPER ACCESS PANEL 588IT EXTERIOR SURFACE SERVERAL AREA FOUND CHAFING(<P>PERMANENT METAL TO METAL HOTBOND REPAIR AS PER RI NO. RI-57-51-16892 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024052300422Skin · dentedLH WING, INBOARD FLAP SURFACE LEADING EDGE AREA UPPER OUTSIDE CORNER WITH TWO DENTS.(<P>LH WING, INBOARD FLAP, MAIN FLAP WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 5 PAG 2-6 AND SRM 51-70-17-0G-0 PAR 4.A FIG 10 PAG 13,14,34 REV 49 APR 15/-2024. NO FURTHESDR UIEA2024052400439Skin · dentedRH WING, INBOARD FLAP, MAIN FLAP, AT 2" FROM TRAILING EDGE AND 6" FROM INBOARD EDGE, DENT ON UPPER SKIN(<P>RH WING, INBOARD FLAP, MAIN FLAP WAS REPAIRED IAW SRM 57-53-01-2R-1 TABLE I FIG 201 SHEET 5 PAG.2,3,6 AND SRM 51-70-03-0G-0 PAR 5.A FIG.5 PAG 10,11,25 RESDR AALA202405288208Flaperon · noneAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND FLAPERON UPPER SURFACE HAS EXISTING REPAIR 21 INCHES FROM INBOARD END AND 14 INCHES FROM LEADING OF SKIN AT WS 593. ACCOMPLISHED PERMANENT REPAIR ON RIGHT HAND FLAPERON UPPER SURFACE PER SRM 57-65-01-2R PROCEDURE 1 REPSDR FDEA202405250908Skin · gougedLH INNER FLAP UPPER FACE GOUGE AT FRONT SPAR PLUS 13.5", RIB8A-1" ACCOMPLISHED THE DOUBLER REPAIR AT LH I/B FLAP UPPER SURFACE RIB7~9, S-2.1~2.2 I.A.W FEDEX EA NO:T6-5750-T0379379 P1, SEQ NO:1250, TITLE:WING-FLIGHT SURFACES-LH INNER FLAP- DENT AND WEAR DAMSDR AALA202405290303Rib · gougedAIRCRAFT WAS IN BASE MAINTENANCE: L/H INBD MAIN FLAP OUTBD RIB HAS SEVERAL GOUGES ON UPPER AREA. (040-130). MAINTENANCE ACCOMPLISHED A PERMANENT REPAIR ON L/H I/B MAIN FLAP O/B RIB I.A.W. B777-300 SRM 57-53-01-2R-1 TABLE I.SDR FDEA202405230723Skin · delaminatedLEFT WING, INBOARD MAIN FLAP, LEADING EDGE WITH DELAMINATION AT 31" FROM OUTBOARD EDGE. LEFT WING, INBOARD MAIN FLAP, LEADING EDGE AT 31" FROM OUTBOARD EDGE WAS REPAIRED IAW B767 SRM 57-53-01-2R TABLE I PAG 1,2,5 AND SRM 51-70-17-0G PAR 4.A FIG 10 PAG 24-2SDR FDEA202405230722Skin · dentedRH WING, INBOARD AFT FLAP, LOWER SURFACE, DENT NEAR INBOARD EXTERNAL HINGE. RH WING, INBOARD AFT FLAP, LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-53-01-2R FIG 201 (SHEET 4) NOTE A AND SRM 51-70-03-0G PAR 5.L FIG 16 REV 88 DEC 15/2023SDR JJBA20240611024Shroud · crackedRH OUTBD FLAP SHROUD OUTBD HINGE FOUND CRACKED. RH OUTBD FLAP SHROUD OUTBD HINGE REPLACEDSDR FDEA202405220717Skin · delaminatedLH WING, OUTBD FLAP, APPROX WBL 355.0 TO 400 LE FLAP WITH TWO DELAMINATIONS LH WING, OUTBD FLAP, APPROX WBL 355.0 TO 400 LE FLAP WAS REPAIRED IAW B767 SRM 57-53- 01-2R REP 1 TABLE I FIG 201 AND SRM 51-70-17-0G PAR 4.A FIG 10 REV 88 DEC 15/2023SDR ASAA2024052151407Skin · dentedFOR TRACKING OF SDR FOR SECOND CLUSTER OF DENTS ON L/H WING INBOARD FLAP LOWER SURFACE GROUNDED - YES. FOR TRACKING OF SDR FOR SECOND CLUSTER OF DENTS ON L/H WING INBOARD FLAP LOWER SURFACESDR SWAA2024062488644Skin · crackedL/H WING I/B AFT FLAP LOWER SURFACE SKIN CRACK AT 28.25' O/B EDGE & 5' T/E<[01] NSTALLED REPAIR AT L/H WING I/B AFT FLAP ON LOWER SURFACE SIZE OF REPAIR 3' DIAMETER PER B737SRM 51-70-10-2R-0 PARAGRAPH(20.B) MATERIAL USED ADHESIVE AF163-2K-06 PO#2053056 AND TOOSDR DALA2024052305447Strut · corrodedSHIP 3102 CORROSION INTERCONNECTING STRUT OB FLAP AND MISSING WORD TOP PLACARD L H WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT OB FLAP AS PER A320 FAM AMM-27-51 -44-000-001-A AND AS PER A320 FAM AMM 27-51-44-400-001-A. (0352524)SDR SWAA2024052288626Fairing · crackedFOUND SMALL CRACK ON LEFT HAND INBOARD FLAP CANOE TAILCONE ON OUTBOARD SIDE. REMOVED LH INBD FLAP TRACK FAIRING TAIL CONE. INSTALLED NEW TAIL CONE ON L/H AFT INBOX FLAP IAW AMM 27-51-18SDR FDEA202405210713Skin · delaminatedRH WING,INBOARD FLAP, MAIN FLAP WITH DELAMINATION AT WBL 289.4 RH WING, INBOARD FLAP, MAIN FLAP AT WBL 289.4 WAS REPAIRED IAW B767 SRM 57-53-01-2R REPAIR 1 FIG 201 TABLE II AND SRM 51-70-06-0G PAR 5G FIG 3 REV 88 DEC 15/2023SDR IPXA2024052660130Flap Track · damagedLEFT HAND INBOARD FLAP TRACK #4 DAMAGED VERIFIED MOVEABLE FLAP TRACK FAIRING REMOVAL AND FLAP RETRACTION NECESSARY TO ACCESS BLENDED AREAS REQUIRING CAD PLATING. INBOARD FAIRING OF LEFT INBOARD FLAP. OPENSDR IPXA2024061365489Rib · crackedTHE R/H CENTER FLAP ASSY, HAS A CRACK (1EA) AT RIB LOCATION 26, AFT SIDE. INSTALLED DOUBLER. IAW A300-600 SRM 51-40-21 AND SRM 57-50-00 REVIEWEDSDR SWAA2024062587678Skin · delaminatedL/W OUB AFT FLAP INB LOWER T/E I/B TIP SKIN AREA DELAMINATED MKD DOT<[01] FLAP IS BEEING REPLACED ON WORK CARD TTG8Q00TMGD9;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02SDR IPXA2024052859705Bearing · damagedLEFT INBOARD TRAILING EDGE FLAP BEARINGS DAMAGED. LEFT IBD MID FLAP REINSTALLED, REF 27-51-01-404-030, RIG AND OPS CHECKED GOOD, REF 27-51-01-805-001. VERIFIED INSTALL AND RIGGING PER GMM CHAP 4SDR IPXA2024052059705Bearing · damagedLEFT INBOARD TRAILING EDGE FLAP BEARINGS DAMAGED.SDR FDEA202405190696Rib · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND 3EA CRACKS AT RIB25 BETWEEN STGR2.8 AND REAR SPAR, AND RIB26 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0379257 P1. TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 11, 20SDR FDEA202405190695Rib · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND 3EA CRACKS AT RIB20 BETWEEN STGR2.7 AND REAR SPAR, AND RIB21 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA: 6-5750-T0379257 P1. TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 11, 20, 2SDR FDEA202405190694Rib · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB11 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0379257 P1. TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 11, 20, 21, 25 AND 26 AT STR. 2.7 /2.8 - ALI 57SDR FDEA202405190693Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB25 BETWEEN STGR2.8 AND REAR SPAR, AND RIB26 BETWEEN STGR2.8 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0379258 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 11, 12SDR FDEA202405190692Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB18 BETWEEN STGR2.8 AND REAR SPAR, AND RIB19 BETWEEN STGR2.8 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0379258 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 11, 12SDR FDEA202405190691Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 4EA CRACKS AT RIB11 BETWEEN STGR2.8 AND REAR SPAR, RIB12 BETWEEN STGR2.8 AND REAR SPAR, AND RIB13 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0379258 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP SDR SWAA2024052187226Skin · debondedR/H AFT O/B TRAILING EDGE FLAP DISBONDED<[01] APPLIED PERMANENT REPAIR PER SRM 51-70-10.SDR DALA2024052005353Roller · excess playSHIP 3132 EXCESSIVE PLAY CRUISE ROLLER OB FLAP ON RH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER OB FLAP ON RH WING AS PER AIRBUS CMM 57- 53-21 TASK 57-53-21-000-810-B01. (0348746)SDR DALA2024052005352Roller · excess playSHIP 3132 EXCESSIVE PLAY CRUISE ROLLER OB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER OB FLAP ON LH WING AS PER AIRBUS CMM 57- 53-21 TASK 57-53-21-000-810-A01. (0348830)SDR FDEA202405180688Skin · delaminatedRH WING OUTBOARD FLAP LEADING EDGE WITH TWO DELAMINATIONS BETWEEN WS 720.2 AND WS 616.2 RH WING OUTBOARD FLAP LEADING EDGE BETWEEN WS 720.2 AND WS 616.2 WAS REPAIRED IAW B767 SRM 57-53-01-2R REP 1 TABLE I PAG 1-5 AND SRM 51-70-03-0G PAR 5.A FIG 5 REV 88 DESDR IPXA2024061336460Structure · crackedTHE L/H CENTER FLAP ASSY, HAS MULTIPLE CRACKS (2EA) AT RIB LOCATION 27, AFT SIDE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-90495-REQ1 AND VT-MAE EA 300-5750-27-A3607, REV. -. JOB COMPLETE. VERIFIED. REVIEWEDSDR IPXA2024061336422Rib · crackedTHE L/H CENTER FLAP ASSY, HAS A CRACK (1EA) AT RIB LOCATION 26, AFT SIDE. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-90495-REQ1 AND VT-MAE EA 300-5750-27-A3607, REV. -. JOB COMPLETE. VERIFIED. REVIEWEDSDR IPXA2024061336403Rib · crackedTHE L/H CENTER FLAP ASSY, HAS A CRACK (1EA) AT RIB LOCATION 25, AFT SIDE. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-90495-REQ1 AND VT-MAE EA 300-5750-27-A3607, REV. -.SDR SWAA2024052886910Skin · delaminatedL/W O/B AFT FLAP; I/B AFT CORNER DISBONDED<[01] FINAL STATEMENT: REMOVED DAMAGE DELAMINATED UPPER AND LOWER SKINS ON L/W O/B AFT FLAP WEDGE I/B CORNER AS PER B737 SWRM 51-70-10-2R-4. PARAG. (7-A-1). INSTALLED HOT BONDER PERMANENT REPAIR AT L\W O\B AFT FLAP ON SDR ASAA2024051651408Skin · dentedLESSOR ITEM 32: LH WING INBOARD FLAP LOWER SURFACE BEHIND WHEELS FOUND WITH MULTIPLE DENTS. GROUNDED - YES. REPAIRED L/H WING INBOARD FLAP LOWER SURFACE BEHIND WHEELS FOUND WITH MULTIPLE DENTS WITH CAT A PERMANENT REPAIR IN 2EA AREAS. DAMAGE #1 IS AT WING STASDR DALA2024051705294Hinge · excess playFREEPLAY ON JOINT BTW FLAP AND FLAP OUTBD HINGE AT LH WING. LT WING FLAP OUTBD HINGE WAS REPAIRED IN ACCORDANCE WITH PRI 617504-14 REV 2 AND ER/A 617504-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 09MAY24. ADDITI
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