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 USAA2009033190740Flap · delaminatedCLT - C1 - MAJOR REPAIR - DELAMINATION ON LEFT OUTBOARD AFT FLAP AT INBOARD END. REPAIRED LEFT OUTBOARD AFT FLAP AT INBOARD END IAW B757 SRM 51-70-17.SDR IPXA09155192Skin · gougedINSPECTION TYPE:N/A RT WING T/E FLAP GOUGED ON LOWER SURFACE. COMPLETED REPAIR PER EO A300-5750-32923A & A300 SRM 57-50-00-20.SDR FDEA200903271082Skin · misrepairedFOUND OLD REPAIR ON LT CENTER FLAP TRAILING EDGE TOP SKIN NOT PERFORMED IAW RAS/FOK/024/2009 ISS A. PATCH REPAIR RENEWED IAW RAS/FOK/024/2009 ISS A, APPROVED BY EA 6-5750-129123.SDR IPXA09555565Skin · delaminatedINSPECTION TYPE:C RT OTBD AFT FLAP LOWER SURFACE HAS DELAMINATED 36 INCH FROM OTBD EDGE AND 7.0 INCH FWD OF THE T/E. FOUND TO BE OUT OF LIMITS PER SRM 57-53-01-1A. SANDED CLEANED AND PREPPED AREA FOR REPAIR IAW SRM 51-70-05 PARG 5. PREP PLIES WITH GRAFIT BTSDR IPXA09555564Skin · delaminatedINSPECTION TYPE:CRH, OTBD/B AFT FLAP LOWER SURFACE HAS DELAMINATED 36 INCHES FROM OTBD EDGE AND 7.0 INCH FWD OF THE T/E. FOUND TO BE OUT OF LIMITS PER SRM 57-53-01-1A. SANDED CLEANED AND PREPPED AREA FOR REPAIR IAW SRM 51-70-05 PARG 5. PREP PLIES WITH GRAP SDR IPXA09555562Skin · gougedINSPECTION TYPE:C LT OTBD MAIN FLAP INBD UPPER SKIN PANEL HAS 3 SMALL GOUGES IN SKIN OF EXISTING REPAIR. FOUND OUT OF LIMITS PER SRM 57-53-01-1A 2. REMOVED SKIN PANEL IAW SRM 51-40 -02 3, SANDED AND REMOVED UPPER SKIN FOR REPAIR IAW SRM 51-70-10-2R4 4. REMOSDR SWAA092021Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING O/B TRAILING EDGE FLAP I/B AFT END DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR IPXA09555274Flap · dentedINSPECTION TYPE:C2 RIGHT WING INBOARD FLAP HAS DENT 14.5 INCHES UP FROM T/E AND MFS 238. REPAIRED DENT PER SRM 51-10-2R-2.SDR IPXA09555200Skin · damagedINSPECTION TYPE:C2 LT WING I/B AFT FLAP HAS DAMAGED SKIN ON LOWER SURFACE 2 INCHES FROM I/B END AND 9 INCHES FROM AFT END. REPAIRED LT WING I/B AFT FLAP IAW SRM 51-70-04-0G.SDR SWAA091996Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED I/B. REMOVED AND REPLACED AFT FLAP PER MM.SDR UIEA200900022Support Fitting · failedDENT ON OUTBOARD AFT FLAP NOSE AND MID FLAP DUE TO OUTBOARD FLAP FITTING FAILURE. REPAIRED PER SRM 51-70-17. REPLACED SUPPORT ARM.SDR FDEA200903251040Bracket · damagedLEFT WING FLAP TRACK FAIRING PANEL NR 533 BB MOUNT BRACKET SAFETY WIRE HOLES ON THE LT AND RT SIDES ARE RIPPED OUT. SAFETIED LT WING FLAP TRACK FAIRING 532 BB, LT AND RT AFT ATTACHED BOLTS REF AMM 20-11-11-0 AND EA 6-5750-127936.SDR FDEA200903251039Bracket · damagedLEFT WING FLAP TRACK FAIRING PANEL NR 533 BB MOUNT BRACKET SAFETY WIRE HOLES ON THE LT AND RT SIDES ARE STRIPPED OUT. SAFETIED LEFT WING FLAP TRACK FAIRING 533 BB, LT AND RT AFT ATTACHED BOLTS REF AMM 20-11-11-0 AND E.A. 6-5750-127936, REV "A".SDR IPXA09155264Skin · gougedINSPECTION TYPE:4C SURVEY SEQUENCE NUMBER 124-W4-01 EXT DOUBLER RT INBOARD FLAP UPPER SURFACE HAS GOUGE DAMAGE. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW A300 SRM 57-50-00 PG 218 FIG 205.SDR SWAA091969Wedge · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING TRAILING EDGE O/B FORE FLAP TRAILING EDGE WEDGE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA091954Flap · delaminatedDURING SCHEDULED CV CHECK, FOUND RT WING TRAILING EDGE I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.SDR IPXA09855147Angle · crackedINSPECTION TYPE:N/A LEFT O/B FLAP I/B SIDE T-ANGLE CRACKED. REPAIRED PER EO DC8-5750-32819-A.SDR FDEA200903241023Tee Fitting · corrodedLT WING OTBD FLAP VANE TEE FITTING NR 4 FROM INBD TRACK ATTACH BORE FOUND WITH CORROSION. COMPLIED WITH EA 1-5750-128667. CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.SDR FDEA200903241022Vane · corrodedLT WING OTBD FLAP VANE T-FITTING NR 1 FROM INBD TRACK ATTACH BORE FOUND CORRODED. COMPLIED WITH EA 1-5750-128666. CLASSIFIED AS A MAJOR REPAIR AS PER GMM 6-2-100 REV. 107.SDR FDEA200903241021Skin · dentedDENT, RT INBD FLAP LEADING EDGE AT XIFH284. SMOOTHENED AS PER SRM 51-21-01 VOL. II REV. 40 AND FOUND WITHIN LIMIT AS PER SRM 57-00-01 FIG. 2 VOL. I REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.SDR C8GA20090130Skin · delaminatedWHILE IN HEAVY MX IT WAS NOTED THAT THE LT WING INBD AFT FLAP IS CRACKED AT EDGE WBL 124. REMOVED DAMAGED SKIN AND CORE DIM 7" X 1.5", FABRICATED REPAIR CORE DIM 7" X .5" FROM 5052-44-3/16 AND 2 EA DOUBLER'S FROM 2024 T3 .016" DIM 5" X 3", 8.5" X 3". HOT BONSDR C8GA20090129Skin · delaminatedWHILE IN HEAVY MX IT WAS NOTED THAT THE LT WING INBD FLAP IS DELAMINATED ON THE LWR T/E. REMOVED DAMAGE AREA, FABRICATED DOUBLER. HOT BONDED REPAIR, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA20090128Skin · delaminatedWHILE IN HEAVY MX IT WAS NOTED THAT THE LT WING INBD FOREFLAP IS DELAMINATED ON THE LWR SURFACE NEAR THE INBD END. REMOVED LT INBD FOREFLAP, REMOVED DAMAGE AREA DIM 5" DIA. CIRCLE. FABRICATED DOUBLER FROM 2024 T3 .016". HOT BONDED REPAIR, NO OTHER DEFECTS WESDR C8GA20090127Skin · delaminatedWHILE IN HEAVY MX IT WAS NOTED THAT LT WING OTBD MID-FLAP HAS AN AREA OF DELAMINATION ON THE T/E OTBD END. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER. INSTALLED HOT BOND REPAIR. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA20090126Skin · delaminatedWHILE IN HEAVY MX IT WAS NOTED THAT THE LT WING OTBD MID-FLAP HAS AREA OF DELAMINATION ON T/E ON OTBD END. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER. INSTALLED HOT BOND REPAIR. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA20090096Skin · delaminatedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RT OUTBOARD MIDFLAP T/E WBL 442 IS DELAMINATED. REMOVED DAMAGED AREA 43 X 3 INCHES, FABRICATED FILLER 43 X 3 INCHES FROM 2024 T3 .016 INCH AND 2 EA DOUBLERS 3 X 3 INCHES FROM 2024 T3 .016. HOT BONDED REPAIR, NSDR C8GA20090095Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RT OTBD MID FLAP TRAILING EDGE DELAMINATED AT WBL 442. REMOVED DAMAGED AREA DIM 43 INCH BY 3 INCH. FABRICATED FILLER 2024 T3 .016 INCH DIM 43 INCH BY 3 INCHES AND 2 EA DOUBLERS 3 INCH BSDR C8GA20090094Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RT INBD AFT FLAP TRAILING EDGE DELAMINATED AT WBL 230. DAMAGED OUTER SKIN WAS REMOVED DIM 23.25 INCH BY 2 INCH AND REMOVED DAMAGED CORE 5 INCH BY 2 INCH. FABRICATED NEW CORE FROM 5052-4-SDR SWAA091907Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING TRAILING EDGE O/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA091906Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING TRAILING EDGE I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR ASAA0944857Flap Track · corrodedCORROSION ON NR 4 FLAP TRACK. REMOVED AND REPLACED FLAP TRACK.SDR UIEA201000175Linkage · damagedRT OTBD MID TO AFT FLAP SUPPORT LINKAGE STRUCTURE PN 65B39149-19/21 WAS FOUND DAMAGED, WITH A GOUGE/DENT. "AFTER BLEND OUT THE REWORKED AREA MEASURED 0.500 IN WITH A 0.013 IN DEPTH. IN ADDITION, INSPECTION OF THE DAMAGE WAS PERFORMED AS DESCRIVED IN THE PART 1SDR TAMF20090017SSkin · corrodedDURING C3 INSP CHECK FOUND LT WING OTBD FLAP AT UPPER SKIN STA 83.73 HAS LIGHT CORROSION. REPAIR ACCOMPLISHED IAW EWO 767 57-052 AND SR 1-1247041324.SDR TAMF20090026SSkin · corrodedDURING C3 CHECK INSPECTION, FOUND RT WING OTBD T/E FLAP LWR SURFACE AT STA OTEF 119 AND BETWEEN STA OTEF 265.69 TO OTEF 371.88 HAS CORROSION. REPAIR ACCOMPLISHED IAW EWO 767 57-054 AND SR 1-1247041324.SDR WRLA2009068Vane · debondedDURING C3 CHECK IN TPE INSPECTION FOUND LT INBOARD FLAP VANE HAS DISBOND AT XIFH196 AND XIFH249. PER AMM 27-50-22-000-081 & 27-50-24-000-081 REV 63. REMOVED THIS DISBONED FLAP VANE, REPAIRED THE FLAP VANE AS JOB CARD ATTACHMENT SHEET 079554, PER AMM 27-50-22SDR IPXA09855118Skin · dentedINSPECTION TYPE:N/A LEFT O/B FLAP UPPER SKIN XF225 CIRCULAR DOUBLER REFERENCE K142525 AND SURVEY SEQ 702-W3-13. REMOVED AND REPLACED REPAIR IAW EO DC8-5750-32751-A AND SRM 51-1-21A.SDR IPXA09855116Attach Angle · crackedINSPECTION TYPE:SV LEFT I/B FLAP SURFBOARD ATTACH ANGLE HAS TWO ADJACENT HOLES CRACKED OUT. ACCOMPLISHED REPAIR PER DC8 SRM 57-2-0 FIG 2A SHT 1 AND 57-2-0 SHT 2.SDR UALA2009032300855Skin · chafedLT INBOARD FLAP UPPER SURFACE CHAFED NEAR OUTBOARD END. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLAP.SDR IPXA09855111Skin · dentedINSPECTION TYPE:N/A REFERENCE K142531 RT I/B FLAP UPPER SKIN REPAIR BETWEEN XW=38.488 AND XW42.674 SURVEY SEQ 702-W4-32. REMOVED AND REPLACED DOUBLER IAW EO DC8-5750-32749-A.SDR IPXA09655142Fairing · delaminatedINSPECTION TYPE:C LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PARA 5A (1) FIG 5 REV 43.SDR ASAA0944844Skin · wornLEFT I/B EXHAUST GATE UPPER SKIN IS WORN BEYOND REPAIR. REMOVED AND REPLACED LEFT I/B EXHAUST GATE UPPER SKIN PER SRM 51 40 02.SDR FDEA200903190971Skin · dentedDENT, RT WING INBD FLAP LEADING EDGE AT XIFH167. MINOR REPAIR AS PER EA 1-5750-127809.SDR FDEA200903190960Skin · dentedFOUND DENTS ON LT CENTER FLAP LEADING EDGE REPAIR PERFORMED BY CUT OUT THE STRAP AND IAW SRM 57-50-00 FIG 208 WITH ONE FASTENER OMIT IAW RAS/FOK/006/2009 ISS A, APPROVED BY EA 6-5750-120226.SDR IPXA09655138Panel · delaminatedINSPECTION TYPE:C LT WING I/B MAIN FLAP LWR PNL 555EB FOUND DELAMINATED. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REPAIR 4 FIG 201 REV 43.SDR SWAA091831Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING I/B TRAILING EDGE FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR SWAA091830Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING I/B TRAILING EDGE FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.SDR UALA2009031900845Flap Track · out of adjustPER EG CREW, AIRCRAFT FLOWN ON DIAGNOSTIC FOR AP DISCONNECT TRANSIENT. RESULT: AIRCRAFT ROLLED APPROX 3-5 DEG LEFT AFTER DISCONNECT FROM EITHER AP USING EITHER SIDE-STICK DISCONNECT OR FCU SWITCH. THIS TRANSIENT IS NOTICEABLE ABOVE 260KC AS. ISOLATION INCLSDR ASAA0944843Skin · corrodedCORROSION ON RIGHT I/B FLAP LEADING EDGE. REPAIRED LEADING EDGE.SDR ASAA0944800Skin · debondedLEFT O/B AFT FLAP LOWER AFT SKIN IS DISBONDED AT I/B AFT CORNER. LEFT O/B AFT FLAP LWR AFT SKIN DISBOND WAS REPAIRED PER SRM.SDR DL75E090458Fitting · gougedLEFT WING INBD AFT FLAP INBD PROGRAMMER FITTING IS GOUGED. C/W AT SAA - SAT ON N/R 118711 SAA JOB 82298770001.
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