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 T4OR 4995 70Roller · wornRT OTBD FLAP ATTACH POINT BRACKETS (RIBS) ARE WORN WHERE AFT FLAP TRACK ROLLERS ARE ATTACHED. BRACKETS ARE WORN APPROXIMATELY .015 INCH TO .020 INCH DEEP IN THE BRACKET SIDES FROM THE ROLLER IN THE SHAPE OF THE ROTATING ROLLER ENDS. SUSPECT CAUSE TO BE WORN SDR ASAA0995234Flap Track · corrodedCORROSION ON I/B AFT FLAP I/B TRACK. REMOVED AND REPLACED TRACK.SDR SWAA092653Flap · delaminatedDURING SCHEDULED 2HC1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP ASSY PER MM.SDR SWAA092612Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND LT WING O/B TRAILING EDGE AFT FLAP DELAMINATED AT I/B EDGE. REMOVED AND REPLACED FLAP ASSY PER MM.SDR FDEA200904221381Fitting · crackedLT WING INB FLAP SUPPORT STRUCTURE FOUND FITTING P/N ANB7394-501 WITH CRACK AND FOUR ATTACHMENT HOLES (FOR ANB7118-501 FITTING ) WITH CORROSION ON BORES AND ON LUG FACES. REPAIRED AREA IAW EA NR 8-5340-128563.SDR IPXA09B55781Skin · delaminatedINSPECTION TYPE:D RT WING - I/B FORE FLAP TRAILING EDGE I/B LWR SURFACE DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A FIG 5 REV 11.SDR IPXA09155734Doubler · chafedINSPECTION TYPE:4C LT WING O/B FLAP LEADING EDGE IS CHAFED AT I/B END OF FLAP. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER AND INTERNAL BUTT STRAP IAW A-300-600 SRM 57-50-00 PARA 4 FIG 20B.SDR SWAA092568Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING O/B TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA092571Wedge · corrodedDURING SCHEDULED 20Y CHECK, FOUND RT WING I/B MID FLAP T/E WEDGE CORRODED ON LWR SKIN. REPAIRED WEDGE PER SRM.SDR SWAA092570Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING I/B AFT FLAP UPPER SKIN DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA092569Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING O/B AFT FLAP T/E SKIN DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA092591Rib · corrodedDURING SCHEDULED 20Y CHECK, FOUND LT WING I/B FORE FLAP O/B RIB CORRODED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA092534Flap · delaminatedDURING SCHEDULED 24Y CHECK, FOUND RT WING O/B AFT FLAP I/B END DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA092508Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING O/B AFT FLAP O/B UPPER END DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR IPXA09855653Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 852-W3-20, REPAIR DOUBLER AT LEFT I/B FLAP UPPER SKIN DOES NOT CORRELATE TO SRM. REPAIRED PER DC8 SRM 57-02-01 FIG 002Q SHT 1.SDR IPXA09855641Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQ 852-W3-20 REPAIR DOUBLER AT LT INBD FLAP UPPER SKIN DOES NOT CORRELATE TO SRM. REPAIR ACCOMPLISHED IAW DC8 SRM 57-2-1 FIG 2Q SHT 1.SDR SWAA092484Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING I/B FORE FLAP UPPER SKIN DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA092474Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING I/B FORE FLAP UPPER SKIN DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR FDEA200904161313Rib · dentedDENT IN LEADING EDGE RIB 26-27 NOSE RIB REPLACED BY NEW ONE IAW SRM 57-50-00/201/FIG 208.SDR FDEA200904151303Rib · crackedDEVIATION RT INNER FLAP, ELONGATED AND CRACKED ATTACHMENT HOLES WITH RIB 25A REPLACEMENT. REPAIR PERFORMED IAW EA 6-5750-120193 , TD FOK/001/2009 ISSUE "C" AND RAS/FOK/001/2009 ISSUE "A" .SDR FDEA200904151302Rib · damagedDEVIATION LT INNER FLAP, ELONGATED AND CRACKED ATTACHMENT HOLES WITH RIB 25A REPLACEMENT. REPAIR PERFORMED BY REPLACEMENT OF RIB 25A AND MODIFICATION IAW OF RIB AS PER SB A300-57-6098. INSTALLED IAW SRM 51-72-10 AND TD FOK/359/2008 ISSUE "C" .SDR CA090415009Rib · cracked(CAN) RT OTBD FLAP L/E RIB ALSO FOUND CRACKED AT SAME LOCATION. THIS PROBLEM COMMON ON 200 SERIES AIRCRAFT. ON 200 SERIES PLANES THE PROBLEM IS DEALT WITH BY A SB. THE SB DOES NOT APPLY TO 300 SERIES PLANES. IT SHOULD. THE REPAIR KIT CALLED OUT BY THE 200 SERISDR IPXA09555724Flap · chafedINSPECTION TYPE:C4 RT I/B MAIN FLAP LEADING EDGE IS CHAFED I/B AND O/B OF FAIRING 671BB. FLAP WAS REPAIRED PER ATS ENGINEERING REPAIR 09-2394.SDR IPXA09555723Flap · gougedINSPECTION TYPE:C4 RT O/B MAIN FLAP L/E IS GOUGED 2 INCHES FROM O/B END. FLAP WAS REPAIRED PER ATS ENGINEERING REPAIR 09-2392 DATED 29 APR 09.SDR IPXA09555696Flap · chafedINSPECTION TYPE:C4 RIGHT I/B MAIN FLAP LWR T/E IS CHAFED 64 INCHES FROM O/B END. REPAIRED AREA PER SRM 51-70-10-2R3.SDR IPXA09555609Plate · crackedINSPECTION TYPE:C4 RT WING LWR T/E PANEL SUPPORT FASTENERS PULLING THROUGH WIGGLE PLATE FWD OF NR 8 SPOILER ACTUATOR INBD EDGE. REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02.SDR IPXA09B55577Wedge · delaminatedINSPECTION TYPE:C LHW, INBD T/E AFT FLAP LWR SURFACE MID AREA DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A FIG 5 REV 52.SDR SWAA092444Flap · delaminatedDURING SCHEDULED 24Y CHECK, FOUND LT WING O/B AFT FLAP I/B END DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR UIEA201000116Skin · delaminatedACCOMPLISH REPAIR TO THE LT INBD AFT FLAP, LOWER SURFACE INBD FWD AREA OF DELAMINATION IAW SRM 57-53-01 FIG 201,SRM 51-70-07 (REF FIG 1). ACCOMPLISH REPAIR TO THE RT INBD FORE FLAP, INBD T/E LOWER SURFACE DAMAGE IAW SRM 57-53-01, FIG 201, RPR 1 TABLE I AND THESDR AALA20090512TUL52Cover · damagedSCREW MISDRILLED INTO CASTING ON BOTTOM O/B SIDE NIPPLE FLAP HINGE COVER. INSTALLED REPAIR BUSHING PER EA MD8057-005935.SDR IPXA09155623Skin · gougedINSPECTION TYPE:4C SURVEY SEQ NR 122-W4-02 R/W INBD FLAP UPPER SKIN BETWEEN RIBS 11-12 AND STR 2.1-2.4 DOUBLER GOUGED. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW A300 SRM 57-50-00 PG 218, 57-50-00 FIG 205.SDR IPXA09155622Skin · gougedINSPECTION TYPE:4C SURVEY NR 122-W3-02 LW CENTER FLAP UPPER SKIN BETWEEN STR 2.6-2.8 AND RIBS 13-15 DOUBLER GOUGED. REMOVED FABRICATED AND INSTALLED REPAIR DOUBLER IAW A300 SRM 57-50-00, PG 218, 57-50-00, FIG 205.SDR IPXA09155621Skin · gougedINSPECTION TYPE:4C SURVEY SEQ NR 122 L/WD INBD FLAP UPPER SKIN BETWEEN RIBS 11-12 AND STR 2.1-2.2 REPAIR DOUBLER GOUGED. REMOVED, FABRICATED AND INSTALLED REPAIR DOUBLER IAW A300 SRM 57-50-00, FIG 205 AND 51-21-10, PG 1.SDR FDEA200904131281Skin · dentedLT WING INBD FLAP LOWER SURFACE LOWER OUTBD SEGMENT FOUND SEVERAL DENTS AT XIFH 243 TO XIFH 255 EXCEED LIMIT. REPAIRED AS PER SRM 57-10-00 FIG. 3 VOL. I REV. 40. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.SDR SWAA092345Skin · delaminatedDURING SCHEDULED 10Y CHECK, FOUND LT WING O/B AFT FLAP I/B UPPER SURFACE DELAMINATED. REPAIRED AFT FLAP PER AAR EA.SDR UIEA200900025Skin · puncturedLT WING INBOARD MID FLAP LOWER SKIN HAS ONE 0.500 INCH PUNCTURE AT WBL 198.55. PERMANENT REPAIRED AS PER N747-400 SRM 57-53-01-2R-1 AND 51-70-10-2R-1. REF: ATLAS AIR EO 4457A184.SDR UIEA200900024Skin · puncturedLT WING INBOARD AFT FLAP LOWER SKIN HAS ONE 0.750 INCH PUNCTURE AT WBL 243.30 AND ONE 0.250 INCH PUNCTURE AT WBL 251.30. PERMANENT REPAIRED AS PER B747-400 SRM 57-53-01-2R-1 AND 51-70-10-2R-1, REF, ATLAS AIR EO 4457A184.SDR 2009FA0000453Bearing · failedLT OTBD AFT FLAP BEARING FAILURE. THIS CAUSED FLAP TO SEIZE ON OTBD TRACK ON FLAP RETRACTION, WHICH DISTORTED FLAP AND CAUSED RETRACTION CABLE TO BREAK. CAREFUL INSPECTION OF FLAP TRACKS FOR ABNORMAL WEAR AND INSPECTION OF ROLLERS COULD PREVENT RECURRENCE. SDR IPXA09555686Carriage · chafedINSPECTION TYPE:C2 OUTBOARD MAIN FLAP NR 1 FLAP CARRIAGE FWD PANEL 666BR IS CHAFED ON INNER SURFACE. REMOVED CHAFING DAMAGE AND COMPLIED WITH ALL STEPS IN ER 09-2305 DATED 4-21-09 AND SRM 57-53-01-1-A1.SDR WRLA2009097Rib · crackedDURING C-CHK IN TPE INSPECTION FOUND RT O/B TRAILING EDGE FLAP STOP RIB CRACKED AT XW486. REPAIRED RT O/B FLAP LEADING EDGE RIB IAW EGAT EI W2009A57B-504 REV 00. CONDITION CHECK NORMAL & JOB COMPLETE.SDR WRLA2009096Rib · crackedDURING C-CHK IN TPE INSPECTION, FOUND LEFT O/B TRAILING EDGE FLAP STOP RIB CRACKED AT XW486. REPAIRED LT O/B FLAP LEADING EDGE RIB IAW EGAT EI W2009A57B-503 REV 00. CONDITION CHECK NORMAL & JOB COMPLETE.SDR USAA2009041390878Support Fitting · crackedCLT - B13 - MAJOR REPAIR - CRACK ON RIGHT OUTBOARD MAIN FLAP AFT FLAP ROLLER SUPPORT FITTING ASSEMBLY. REPLACED RIGHT OUTBOARD MAIN FLAP AFT FLAP ROLLER SUPPORT FITTING ASSEMBLY IAW US AIRWAYS EA 101063 & BOEING DWG 113N3330.SDR SWAA092390Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR WRLA2009104Support Bracket · crackedDURING C-CHECK IN TPE INSPECTION FOUND LEFT WING O/B TRAILING EDGE FLAP I/B FAIRING STRUCTURE HAS TWO BRACKETS CRACKED AT STA YW490.55 (REF EGAT NRC U05071). REPLACED THE TWO BRACKETS ON LEFT WING O/B TRAILING EDGE FLAP I/B FAIRING STRUCTURE IAW MD-11F SRM VOSDR IPXA09M55657Web · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQ W4-05, RT WING I/B FLAP, O/B CLOSING WEB AT XIFH 311.851 EXISTING REPAIR HAS DELTA ERA ASSIGNED TO IT, BUT DATA NOT RETRIEVABLE. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW IPXA EO MD11-5750-33241-SDR WRLA2009093Vane · debondedDURING C2-CHK IN TPE INSPECTION FOUND THE RT I/B FLAP VANE DISBONDED 13X20 INCHES AT STA XW188. PER AMM 27-50-22-000-801 REV 63 REMOVED RIGHT I/B FLAP VANE. PER ATTACHED SHEET 078656 TO REPAIR DISBONDED AREA. PER AMM 27-50-22-830-80V REV 63 ADJUSTMENT OF ISDR FDEA200904091257Support Fitting · corrodedCORROSION FOUND ON INBD FLAP INBD TRACK NR 4 SUPPORT FITTING LOWER FWD HOLE. REPAIRED AS PER EA 1-5750-127817. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091256Support Fitting · corrodedCORROSION FOUND ON INBD FLAP INBD TRACK NR 4 SUPPORT FITTING LOWER AFT HOLE. REPAIRED AS PER EA 1-5750-127817. CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091255Support Fitting · corrodedCORROSION-INBD FLAP INBD TRACK NR 4 SUPPORT FITTING UPPER AFT HOLE. REPAIRED AS PER EA 1-5750-127817. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200904091254Support Fitting · corrodedCORROSION-INBD FLAP INBD TRACK NR 4 SUPPORT FITTING UPP FWD HOLE. REPAIRED AS PER EA 1-5750-127817. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.
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