JASC 5753
Service difficulty reports · 31,496
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 UIEA2025060100710Skin · delaminatedLHW I/B FORE FLAP EXTERIOR SURFACE FOUND DELAMINATED.(<P>PERFORMED REPAIR AT DELAMINATED AREA AS PER SRM 51-70-07 PAR 5.A.(1) REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060100711Skin · delaminatedLHW I/B FORE FLAP EXTERIOR SURFACE FOUND DELAMINATED.(<P>PERFORMED REPAIR AT DELAMINATED AREA AS PER SRM 51-70-07 PAR 5.A.(1) REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060100712Skin · delaminatedRHW I/B FORE FLAP EXTERIOR SURFACE FOUND DELAMINATED.(<P>PERFORMED REPAIR AT DELAMINATED AREA AS PER SRM 51-70-07 PAR 5A.(1) REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060200714Structure · damagedLHW O/B MID FLAP FOUND BOLT HOLE ELONGATED.(<P>PERFORMED REPAIR AT ELONGATED BOLT HOLE AS PER SRM 51-70-07 PAR 5.K REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025060200715Structure · damagedRHW O/B MID FLAP FOUND BOLT HOLE ELONGATED.(<P>PERFORMED REPAIR AT ELONGATED BOLT HOLE AS PER SRM 51-70-07 PAR 5.K REV 103. NO FURTHER DEFECTS NOTED.</P>)SDR FDEA202506110922Skin · dentedLH WING, INBOARD FLAP, AFT FLAP LOWER SURFACE WITH DENT LH WING, INBOARD FLAP, AFT FLAP LOWER SURFACE WAS REPAIRED IAW B767 SRM 57-53-01-01A AND SRM 51-70-03-06 PAR 5,B FIG. REV 90 AUG 15,2024 PAINT WAS RESTORED IAW B767 AMM 51- 21-10-307-020 REV 145 APR 2SDR AALA202507248553Skin · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD MAIN FLAP HAS AREA OF DELAMANATION AT OUTBOARD LOWER TRAILING EDGE. INSTALLED WEDGE PANEL. PER SRM 51-40-02.SDR VNAA20250610018Cradle · gougedHN00218095 S/N: 634 DISCREPANCY: RH INBOARD FLAP VANE ACTUATOR AT W.S.102.90 CRADLE ASSY IS GOUGED. CORRECTIVE: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR ASSEMBLY FOR RH WS102.9 (PN CC670-14300-9-01, SN PR1943). LOCATED AND MACHINED 3EA HOLES ON NEW SERVICEASDR VNAA20250610017Cradle · gougedHN00218094 S/N: 633 DISCREPANCY: RH INBOARD FLAP VANE ACTUATOR AT W.S.65.50 CRADLE ASSY IS GOUGED. CORRECTIVE: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR ASSEMBLY FOR RH WS65.5 (PN CC670-14300-9-01, SN PR1932). LOCATED AND MACHINED 3EA HOLES ON NEW SERVICEABLSDR DALA2025060904393Bearing · corrodedSHIP 3162 RIGHT WING OUTBOARD FLAP TO MAIN TRACK FLAP CARRIAGE CONNECTION N 3 LUG SPHERICAL BEARING BALL INNER DIAMETER SURFACE HAS PITTING CORROSION. CORRECTIVE ACTION: COMPLIED WITH ER/A 626505-14. (1012822).SDR DALA2025060904392Bearing · corrodedSHIP 3162 LEFT WING OUTBOARD FLAP TO MAIN TRACK FLAP CARRIAGE CONNECTION N 3 FITTING LUG SPHERICAL BEARING BALL INNER DIAMETER SURFACE HAS PITTING CORROSION. CORRECTIVE ACTION: COMPLIED WITH ER/A 626514-14. (1012789).SDR DALA2025060904391Bearing · corrodedSHIP 3162 RIGHT WING INBOARD FLAP TO MAIN TRACK FLAP CARRIAGE CONNECTION N 2 FITTING LUG SPHERICAL BEARING BALL INNER DIAMETER SURFACE HAS PITTING CORROSION. CORRECTIVE ACTION: COMPLIED WITH ER/A 626514-14. (1012755).SDR SWAA2025071579385Panel · elongatedELONGATED HOLES ON ACCESS PANEL 561AB AT LT WING 2025-366021<[01]. TOOL USED CALIPER PN: 500-197-30; SN: B20189334; DUE DATE: 26/JAN/26.; [02] TOOL USED HOT BONDER PN: HCS9200B; SN: 18185847; DUE DATE: 01/OCT/25; [03] TOOL USED SCALE PN: CR5200; SN: 8342514561SDR IPXA2025061600746Angle · crackedLH WING CENTER FLAP O/B TRAILING EDGE ANGLE BROKEN.REMOVED TRAILING EDGE ANGLE FROM L/H CENTER FLAP IAW A300-600 SRM 51-40-21.FABRICATED NEW TRAILING EDGE ANGLE FOR L/H WING CENTER FLAP IAW A300-600 SRM 51-27-00 AND UPS GMM 09.08.01.03. INSTALLED NEW ANGLE FORSDR DALA2025061204471Flap Track · corrodedSHIP 3162 LH WING OB FLAP TRACK #3, INNER AND OUTER RIB 5, AT ECCENTRIC BEARING CORROSION. CORRECTIVE ACTION: REPAIRED PER ER/A 626504-14. (1011304)SDR DALA2025060904395Skin · dentedSHIP 3135 FOUND DENTS ON UPPER AND LOWER SURFACE IB FLAP ON RH WING. CORRECTIVE ACTION: REPAIRED UPPER AND LOWER SURFACE IB FLAP ON RH WING AS PER A319 SRM 57-52-00-300-091. (1011630).SDR SWAA2025071578885Panel · elongatedELONGATED HOLES ON ACCESS PANEL 661AB TRAILING EDGE AT RT WING 2025-365928 <[01]. TOOL USED CALIPER PN: 500-197-30; SN: B20189334; DUE DATE: 26/JAN/26.; [02] TOOL USED HOT BONDER PN: HCS9200B; SN: 18185847; DUE DATE: 01/OCT/25; [03] TOOL USED SCALE PN: CR5200;SDR FDEA202506060843Skin · dentedLEFT WING OTBD FLAP LOWER SKIN FOUND DENT AT 300 MM FROM T/E AND 1700 MM FROM INBOARD SIDE OF FLAP. REPAIRED LH WING OTBD FLAP LOWER SKIN DENT AT 300MM FROM T/E AND 1700MM FROM INBOARD SIDE OF FLAP AS PER B777 SRM 57-53-01-2R-2 & SRM 51-70-04-2R-1 REV 47.5 ASDR FDEA202506060842Skin · dentedRIGHT WING OB FLAP LWR SURFACE FOUND MATERIAL MISSING AT 305 IN TO IB AND 3 IN TO AFT EDGE. REPAIRED RH WING OB FLAP LWR SURFAE MATERIAL MISSING AT 305 IN TO IB AND 3 IN TO AFT EDGE AS PER B777 SRM 57-53-01-2R-2 & SRM 51-70-04-2R-1 REV 47.5 AND EA:G-5750-TSDR FDEA202506060841Skin · dentedRH WING OB FLAP LWR SURFACE FOUND DENT AT 159 IN TO IB AND 10 IN TO AFT EDGE AND CRACK AND MATERIAL MISSING, TOTAL DAMAGE SIZE 10 INCHES BY 10 INCHES. REPAIRED RH WING OB FLAP LWR SURFACE DENT AT 159 IN TO IB AND 10 IN TO AFT EDGE AND CRACK AND MATERIAL MISDR SWAA2025071578884Panel · elongatedELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING (10EA) 2025-365913 <[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189334; DUE DATE: 26/JAN/26; [02] TOOL USED P/N: EPOCH 6LT; S/N: 230529908; CAL DUE: 15-AUG-25.; [03] TOOL USED: HUMIDITY/TEMPERATURE CHART RECORSDR SWI2025F00869Flap Track · wornRH WING FLAP TRACK 2A I/B HAS THICKNESS REDUCTION WEAR OF 1.2MM MAX ALONG AFT SIDE AND IS OUT OF LIMITS. ASSET# TC2-10390, DUE 7-3-25. (C-CHECK RO 07/03/2025)REMOVED AND REPLACED RH WING FLAP TRACK 2A I/B. REF AMM:57-54-25 T. WRENCH:TC2-7219 C/D:3-12-26SDR SWIA20250707605Flap Track · gougedLH WING FLAP TRACK 1A HAS MULTIPLE GOUGING IN RADIUS OF TRACK AND IS OUT OF LIMITS. (C-CHECK RO 07/03/2025)REMOVED AND REPLACED LH WING FLAP TRACK 1A. REF AMM:57-54-25 T. WRENCH:TC2-7219 C/D:3-12-26SDR SWIA2025063000004Flap Track · wornL/H #1 AFT FLAP TRACK WORN ON ROLLER MATING FACE. (C-CHECK RO 06/29/2025)REMOVED AND REPLACED L/H #1 INBOARD FLAP AFT TRACK PER E175 AMM 57-54-25 SN:220413BNA1 PN: 170-39060-003. TW: MCN-9506 CAL DUE 9/11/25. SEALANT PO:335504SDR SWAA2025061678075Wedge · delaminatedLEFT WING I/B MAIN FLAP O/B T/E WEDGE IS DELAMINATED<[01] REMOVED AND REPLACED LEFT WING I/B MAIN FLAP O/B T/E WEDGE IAW SOPM 20-50-01 AND AMM 20-50-11-910-801.;[02] VERIFIED CORRECTIVE ACTIONSDR IXXA20250604002Skin · dentedL/H WING INBD AFT FLAP LOWER SURFACE OF THE L/E PANEL IS DENTED APPROX 4" OTBD OF THE OTBD TRACK FAIRINGSDR IPXA2025061925543Rib · crackedMAJOR REPAIR, THE R/H CENTER FLAP ASSY HAS MULTIPLE CRACKS (2EA) AT RIB 26 AFT SIDE, IN THE TOP SKIN RIB FLANGE. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-97043-REQ1 AND VT-MAE EA 300-5750-27-A4001, REV. -.SDR IPXA2025061925742Rib · crackedMAJOR REPAIR, THE LT CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB 27 AFT SIDE, IN THE TOP SKIN RIB FLANGE. ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-94074-REQ1 AND VT-MAE EA 300-5750-27-A4002, REV. -.SDR IPXA2025061925105Rib · crackedMAJOR REPAIR. THE RT CENTER FLAP ASSY HAS MULTIPLE CRACKS (2EA) AT RIB 13 AFT SIDE, IN THE TOP SKIN RIB FLANGE. ALL DAMAGE. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-94073-REQ1 AND VT-MAE EA 300-5750-27-A4001, REV. -.SDR IPXA2025061925656Rib · crackedMAJOR REPAIR. THE RT CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB 27 AFT SIDE, IN THE TOP SKIN RIB FLANGE. ALL DAMAGE. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-97043-REQ1 AND VT-MAE EA 300-5750-27-A4001, REV. -.SDR IPXA2025061925522Rib · crackedMAJOR REPAIR, THE RT CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB 25 AFT SIDE, IN THE TOP SKIN RIB FLANGE. ALL DAMAGE. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-97043-REQ1 AND VT-MAE EA 300-5750-27-A4001, REV. -.SDR IPXA2025061925238Rib · crackedMAJOR REPAIR, THE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB 16 AFT SIDE, IN THE TOP SKIN RIB FLANGE. ALL DAMAGE MARKED IN RED. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-94073-REQ1 AND VT-MAE EA 300-5750-27-A4001, REV. -.SDR IPXA2025061925447Rib · crackedTHE RIGHT CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB 18 AFT SIDE, IN THE TOP SKIN RIB FLANGE. ALL DAMAGE. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-97043-REQ1 AND VT-MAE EA 300-5750-27-A4001, REV. -. MAJOR REPAIR.SDR IPXA2025061925247Rib · crackedTHE R/H CENTER FLAP ASSY HAS A CRACK (1EA) AT RIB 17 AFT SIDE, IN THE TOP SKIN RIB FLANGE. ALL DAMAGE. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-97043-REQ1 AND VT-MAE EA 300-5750-27-A4001, REV. -. MAJOR REPAIR.SDR IPXA2025061924955Rib · crackedTHE R/H CENTER FLAP ASSY HAS MULTIPLE CRACKS (2EA) AT RIB 11 AFT SIDE, IN THE TOP SKIN RIB FLANGE. ALL DAMAGE MARKED IN RED. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-94073-REQ1 AND VT-MAE EA 300-5750-27-A4001, REV. -. MAJOR REPAIR.SDR IPXA2025060971981Skin · corrodedRIGHT WING INBOARD MAIN FLAP TE LOWER SKIN INSIDE SUSPECT CORROSION, IFS 105.75. ACCOMPLETED REPAIR IAW EO-94005-REQ1 REV1.SDR IXXA202505310006Skin · gougedLW OB FLAP LE HAS SCRAPE MARKS THE LENGTH OF THE FLAP AND JUST IB OF THE OF THE OB ROLLER, THERE'S A GOUGE IN THE FLAPSDR SWAA2025063076575Access Panel · damagedELONGATED HOLE ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2025-335666<[01] TOOL USED CALIPER P/N 500-197-30 S/N B20189334 DUE DATE 26 JAN 26;[02] TOOL USED ON STEP 12:ULTRASONIC EQUIPMENT P/N:EPOCH 650; S/N:201036102; DUE DATE:25-OCT-25.;[03] TOOL USED: HUMIDSDR FDEA202505290890Rib · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND CRACK AT RIB15 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA: 6-5750-T0383581 P1, TITLE: WINGS - FLIGHT SURFACES - RH CENTER FLAP RIB 15 UPPER FLANGE AND BOTTOM SKIN REPAIR - RSC TRACKING. AND PER A300-600 SRM 57-50-SDR FDEA202505290889Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND CRACK AT RIB13 BETWEEN STGR2.6 AND STGR2.7 COMPLIED WITH EA: 6-5730-T0336655 A P2, TITLE: WINGS - PLATES AND SKINS - LH WING CENTER FLAP - SRM REPAIRS - RSC TRACKING. AND PER A300-600 SRM 57-50-00-201 FIG.201 REPAIRSDR FDEA202505290888Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB26 B/W STGR2.6 AND STGR2.8 COMPLIED WITH EA: 6-5730-T0336655 A P2, TITLE: WINGS - PLATES AND SKINS - LH WING CENTER FLAP - SRM REPAIRS - RSC TRACKING. AND PER A300-600 SRM 57-50-00-201 FIG.201 REPAIRESDR FDEA202505290824Skin · dentedLH WING, INBOARD FLAP WITH SEVERAL DENTS LH WING, INBOARD FLAP WAS REPAIRED I.A.W. B767 SRM 57-53-01-2R FIG. 201 (SHEET 2) DETAIL I,SRM 51-70-10-2R REPAIR 2 FIG. 201 (SHEET 2) "C" AND SRM 51-70-03-0G PAR. 5.L FIG 16 REV. 90 AUG 15/2024. ONE DENT ON IFS 229SDR FDEA202505290823Skin · dentedLH WING, INBOARD TRAILING FLAP WITH SEVERAL DENTS LH WING, INBOARD TRAILING FLAP WAS REPAIRED I.A.W. B767 57-53-01-2R FIG. 201 (SHEET 4) NOTE "A" AND SRM 51-70-03-0G PAR. 5.A FIG. 16 REV. 90 AUG 15/2024SDR FDEA202505290822Skin · dentedLH WING, INBOARD FLAP WITH SEVERAL DENTS LH WING, INBOARD FLAP WAS REPAIRED I.A.W. B767 SRM 57-53-01-2R FIG. 201 (SHEET 2) DETAIL I,SRM 51-70-10-2R REPAIR 2 FIG. 201 (SHEET 2) "C" AND SRM 51-70-03-0G PAR. 5.L FIG 16 REV. 90 AUG 15/2024SDR JR2R20250529603Skin · damagedRIGHT HAND INBOARD MAIN FLAP TRAILING EDGE IS DAMAGED. REPAIRED.SDR SWAA2025060275752Fairing · pulledDURING INSPECTION OF#3 CANOE FAIRING FOUND 3 PULLED FASTENERS. <[01] PART INFO ONLY; [02] REMOVED AND REPLACED #3 FLAP AFT FAIRING REF AMM 27-51-18 UP TO STEP 5.G.3.; [03] FINISHED INSTALLATION OF #3 AFT FLAP FAIRING FROM STEP 5.G.3 ON REF AMM 27-51-18.SDR SWAA2025060275257Fairing · loose#6 FLAP TRACK FAIRING TAIL CONE HAS MULTIPLE LOOSE/ MISSING/ PULLED FASTENERS<[01] REMOVED #6 FLAP TRACK TAIL CONE IAW STANDARD INDUSTRY PRACTICES. OK TO CONTINUE ON CDL 57-10-4. AUTH #254650SDR DALA2025052604009Flap Track · corrodedSHIP 3135 CORROSION ON BEARING TRACK 4 O/B FLAP LH WING. CORRECTIVE ACTION: REPLACED BEARING TRACK 4 O/B FLAP LH WING AS PER A320 FAM AMM 57 -53-21-000-001-A AND AMM 57-53-21-400-001-A. (0986303).SDR DALA2025052604008Flap Track · corrodedSHIP 3135 CORROSION BEARING TRACK 3 O/B FLAP LH WING. CORRECTIVE ACTION: REPLACED BEARING TRACK 3 O/B FLAP LH WING AS PER A320 FAM AMM 57 -53-21-400-001-A AND AMM 57-53-21-000-001. (0986297).SDR IPXA2025061662819Skin · chafedRT WING O/B FLAP UPPER SURFACE L/E SKIN IS CHAFED ON O/B END. # 3513 REVIEWED
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