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 SWAA100198Flap · corrodedDURING SCHEDULED SPV CHECK, FOUND LT WING I/B FORE FLAP CORRODED. REMOVED AND REPLACED FORE FLAP PER MM.SDR FDEA201001110079Angle · crackedRT OTBD MID-FLAP AFT UPPER CHORD ANGLE CRACKED WS 470. FLAP REMOVED AND REPLACED DUE TO DAMAGE BEYOND REPAIR LIMITS.SDR A6WA201040153Tube · chafedRT INBD FLAP MIDDLE VANE ACTUATOR INNER TUBE WORN UNDER BOTTOM ROLLER. REPAIRED IAW REO 601R-57-52-1552.SDR A6WA201040152Tube · chafedRT INBD FLAP INBD VANE ACTUATOR INNER TUBE WORN UNDER BOTTOM ROLLER. REPAIRED IAW REO 601R-57-52-1557.SDR CA100127015Bracket · worn(CAN) DURING A ROUTINE INSP OF THE FLAP SYS. DISCOVERED THAT MANY BRGS WERE USED INSIDE THE BRACKETS. EXCESSIVE SIDE PLAY CAUSED WEAR OF FLAP BRACKETS. HAD TO CHANGE THE DAMAGED BRACKETS, ALSO THE BRGS AND THE WASHERS OF TEFLON. A THOROUGH INSP OF OUR FLEETSDR SWAA100119Flap · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR IXXA10SMN010SSkin · dentedDURING ROUTINE C CHECK INSP FOUND RT OTBD FLAP LOWER SKIN DENTED AT STA XF 380.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PSDR IXXA10SMN009SSkin · wornDURING ROUTINE C CHECK INSP FOUND LT INBD FLAP UPPER SKIN WORN AT STA XW 106.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRSDR IXXA10SMN008SSkin · dentedDURING ROUTINE C CHECK INSP FOUND LT OTBD FLAP LOWER SKIN DENTED AT STA XF 104.000-115.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TRSDR IXXA10SMN007SSkin · dentedDURING ROUTINE C CHECK INSP, FOUND LT OTBD FLAP LOWER SKIN DENTED AT STA XF 169.000-213.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TSDR IXXA10SMN006SSkin · wornDURING ROUTINE C CHECK INSP FOUND LT OTBD FLAP UPPER SKIN WORN AT STA XF 211.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRSDR IXXA10SMN005SSkin · dentedDURING ROUTINE C CHECK INSP FOUND LT OTBD FLAP T/E LOWER SKIN HAS SEVERAL DENTS AT STA XF 380.000-404.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSSDR QXEA2010011200034Skin · damagedC5 CHECK -LT INBD FLAP UPPER SURFACE HAS 3 SPOTS OF CHAFE DAMAGE ON THE INBD END APPROX 20' FWD OF THE T/E. BLENDED AFFECTED AREA TO SMOOTH AND REMOVED DAMAGE. HFEC INSP BLENDED AREAS FOR CRACKS IAW NDTM PART 6, 51-00-01-250-801. NO CRACKS NOTED. UT THICKNSDR QXEA2010011200032Flap Track · damagedC5 CHECK - RT NR 4 FLAP TRACK INBD FACE HAS A CHAFE APPROX 5' LONG JUST ABOVE WHERE THE INBD SIDE ROLLER WOULD TRAVEL AND IT STARTS APPROX 21' AFT OF THE WINGS AFT SPAR. MAPPED FOR ENGINEERING. LOCALLY POLISHED AREA TO REMOVE LOOSE MATERIAL AND BREAK SHARP SDR QXEA2010011200031Skin · damagedC5 CHECK -OTBD FLAP UPPER SURFACE HAS LIGHT CHAFE DAMAGE ON PREVIOUS PATCH REPAIR. REMOVED OLD DOUBLER IAW SRM 51-23-00-02-01, HFEC INSPECTED ENTIRE SKIN SURFACE IAW NDTM PART 6,51-00-01, NO CRACKS NOTED. FABRICATED AND INSTALLED NEW DOUBLER, ALL WORK PERFORSDR QXEA2010011200030Skin · damagedC5 CHECK - LT INBD FLAP UPPER SURFACE HAS LIGHT CHAFE DAMAGE AT APPROX STA YW 161.0 AND 20" FWD OF T/E. BLENDED TO REMOVE DAMAGE. HFEC INSP BLENDED AREA FOR CRACKS IAW NDTM PART 6, 51-00-01-0250-801, NO CRACKS NOTED. UT THICKNESS CHECKED BLEND AREA IAW NDTSDR USAA2010020190248Flap · delaminatedSAL - C22 - MAJOR REPAIR - DELAMINATION ON RIGHT INBOARD FORE FLAP BETWEEN WBL 176 TO 182, 284.96 TO 96.96 & WBL 117. REPAIRED RIGHT INBOARD FORE FLAP BETWEEN WBL 176 TO 182, 284.96 TO 96.96 & WBL 117 IAW B737 SRM 51-70-10.SDR SWIA201023419Sealant · out of positionUNCOMMANDED ROLL WHEN FLAPS DEPLOYED TO 45 DEGREES. (FLT 4773) REMOVED PROTRUDING PAINT AND SEALANT ON RIGHT OUTBOARD LEADING EDGE FLAP VANE.SDR IPXA10658082Skin · delaminatedINSPECTION TYPE:SPV-RT WING INBD AFT FLAP LOWER SURFACE INBD T/E FOUND DELAMINATED ON THE EXISTING REPAIR PATCH OTBD EDGE. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10 REPAIR 4, FIG 202, SHEET 1 REV 45.SDR IPXA10658081Support Fitting · crackedINSPECTION TYPE:SPV-RT WING INBD MAIN FLAP, INBD AFT FLAP SUPPORT FITTING FOUND CRACKED. RT INBD MAIN FLAP AFT FLAP SUPPORT FITTING REPAIRED IAW SRM 57-53-02-2R1 FIG201, REV45. INBD FLANGE CRACK LENGTH 1.25". OTBD FLANGE CRACK LENGTH 1.5" BOTH INBD & OTBD CUSDR IPXA10M58247Vane · chafedINSPECTION TYPE:2C LT WING, INBD FLAP VANE, INBD END, TOP SIDE T/E 12" FROM END HAS BEEN CHAFED. REMOVED OLD DAMAGE, FABRICATED AND INSTALLED REPAIR PLIES IAW SRM 57-50-08 REPAIRSDR SWAA100231Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR UIEA201000090Skin · delaminatedRT WING OTBD AFT FLAP L/E MID AREA FOUND DELAMINATED. RT WING - OTBD AFT FLAP REPAIRED IAW SRM 51-70-07 FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU506866-1. EO 4457A224RA, 4457A225RA.SDR USAA2010020490277Flap · delaminatedSAL - MAJOR REPAIR - C22 CHECK - RIGHT WING OUTBOARD AFT FLAP TRAILING EDGE IS DELAMINATED. REPAIRED RIGHT WING OUTBOARD AFT FLAP TRAILING EDGE IAW B737 SRM 51-70-10 REPAIR 4.SDR WRLA20100105330Stop Fitting · crackedDURING 01C CHECK FOUND RIGHT WING OUTBOARD FLAP STOP RIB (P/N:ARC4125-502) CRACKED AT XOF 563.244. NRC U05078 ISSUED. PER EI:W2010A57B-072 REV00 AND AMM REV66, RMV THE FLAP, RPL THE LEADING EDGE RIB, RE-INST THE FLAP. PFM AMM SUBTASK 27-50-30-830-003 TO ADJSDR SWAA100079Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR ASAA1047198Skin · dentedLEFT O/B AFT FLAP LOWER SURFACE HAS A CLUSTER OF DENTS AT REPAIR. INSTALLED FILLER AND DOUBLER AFTER DAMAGED WAS REMOVED.SDR SWIA201023559Support · crackedLEFT ENGINE NACELLE FLAP OUTBOARD SUPPORT CRACKED. (C CHECK) REPLACED PER SRM.SDR ASAA1047194Skin · delaminatedRIGHT I/B FORE FLAP UPPER SURFACE REPAIR 36 INCHES FROM O/B END IS DELAMINATED. INSTALLED DOUBLER.SDR ASAA1047193Skin · chafedLEFT I/B FORE FLAP HAS WORN THROUGH DOUBLER INTO SKIN. INSTALLED CORE AND DOUBLER.SDR UIEA201000095Skin · delaminatedRT WING T/E INBD FORE FLAP L/E FOUND DELAMINATION AS MARKED. RT WING - INBD FORE FLAP REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU 504747-1. EO 4457A224RA, 4457A225RA.SDR UIEA201000091Skin · dentedRT WING T/E OTBD AFT FLAP LWR SURFACE FOUND DENT AS MARKED. RT WING - OTBD AFT FLAP REPAIRED IAW SRM 51-70-10, REPAIR NR 4, FIG 201 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU505223. EO 4457A224RA, 4457A225RA.SDR IPXA10558057Skin · damagedRT INBD AFT FLAP HAS 1/4" HOLE IN LOWER SKIN 8.125 FROM L/E AND 33" FROM INBD END. REMOVED DAMAGE AND REPAIRED IAW EO B757-5750-36155-A.SDR UIEA201000094Skin · delaminatedRT WING INBD AFT FLAP LWR SURFACE 1 LOCATION FOUND DELAMINATED AS MARKED. RT WING - INBD AFT FLAP REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU504176-1. EO 4457A224RA , 4457A225RA.SDR UIEA201000092Skin · delaminatedLT WING T/E OTBD FORE FLAP L/E FOUND DELAMINATION AT SEVERAL LOCATION AS MARKED. LT WING -OTBD FORE FLAP REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ MO: DJU 503665-1. EO 4457A224RA, 4457A225RA.SDR UIEA201000093Skin · delaminatedEO 4457A224RA, 4457A225RA: RT WING INBD MID FLAP UPPER SURFACE 2 LOCATION FOUND DELAMINATED AS MARKED. RT WING INBD MID FLAP LWR SURFACE OTBD AFT CORNER SCRATCH AS MARKED. RT WING - INBD MID FLAP REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTSDR UIEA201000096Flap Track · erodedNR 7 FIX FLAP TRACK FAIRING L/E AREA ERODED. NR 7 FIX FAIRING RESIN REPAIRED IAW SRM 51-70-06, PARA 5.0, EO 4457A224RA, 4457A225RA.SDR ASAA1047240Skin · delaminatedRIGHT WING I/B AFT FORE FLAP UPPER SURFACE DELAMINATED. REMOVED DAMAGED AREA, FABRICATED REPAIR AND BONDED.SDR ASAA1047239Skin · delaminatedLEFT WING I/B FLAP T/E OUTBOARD END UPPER AND LOWER SURFACE DELAMINATED. REMOVED DAMAGED AREA, FABRICATED REPAIR AND BONDED.SDR IPXA10M58174Skin · canningINSPECTION TYPE:2C, REPAIR SURVEY SEQ NR 290-W4-02 RT WING INBD FLAP UPPER SKIN APPROX BETW EEN STA XIFH 165 TO 177 REPAIR DOUBLER HAS OILCANNING CONDITION. REMOVED EXISTING REPAIR 290-W4-02 RT WING INBD FLAP UPPER SKIN BETWEEN XIFH 165 TO 177. FABRICATED ASDR FDEA200912314576Skin · gougedLT OTBD FOREFLAP L/E IS GOUGED IN 2 PLACES ON PREVIOUS REPAIR- INBD END OF FOREFLAP. REMOVED PREVIOUS REPAIR AT LT OTBD FOREFLAP L/E IAW SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER IAW SRM 57-50-2, FIG 4 AND 51-30-5. TREATED AND PRIMED DOUBLER IAW SRM 51-10SDR ASAA1047238Skin · delaminatedRIGHT WING I/B AFT T/E FLAP UPPER O/B SURFACE AT PREVIOUS REPAIR DELAMINATED. REMOVED DAMAGED DOUBLER, PERFORMED MOISTURE EVACUATION, FABBED REPAIR PARTS AND INSTALLED.SDR ASAA1047232Skin · chafedRIGHT WING O/B TRAILING EDGE FLAP IS CHAFED AT LOWER LEADING EDGE ON I/B END. REMOVED DAMAGED AREA, FABBED REPAIR PARTS AND INSTALLED.SDR ASAA1047231Skin · chafedRIGHT O/B AFT FLAP LOWER SURFACE CHAFED 1 FROM T/E BETWEEN NR 8 TRACK FAIRING CHAFE PAD. REMOVED CHAFED AREA, FABBED REPAIR PARTS AND BONDED.SDR IPXA10M58161Skin · canningINSPECTION TYPE:2C, REPAIR SURVEY SEQ NR 290-W4-01 RT INBD. FLAP UPPER PREVIOUS REPAIR DOUBLER OIL CANNING CONDITION APPROX BETWEEN STA XIFH 133-153. REMOVED EXISTING REPAIR ON RT INBD. FLAP BETWEEN STA XIFH 133-153. CUT OUT DAMAGE SKIN, FABRICATED AND INSSDR IPXA10158105Skin · gougedINSPECTION TYPE:4C RT WING INBD FLAP UPPER SKIN REPAIR DOUBLER GOUGED REPAIR SURVEY SEQ 129-W4-01. INSTALLED REPAIR DOUBLER IAW SRM 57-50-00, PAGE 219, PARA 4E(3) A ND PAGE 220 FIG 205, SRM 51-40-21, PARA 13D, AND EO NR M-5100- 19814 PG. 6 APPX. B.SDR IPXA10158104Skin · gougedINSPECTION TYPE:1C LT INBD FLAP UPPER SKIN IS GOUGED, INBD OF NR 2 FLAP TRACK FWD OF RUB STRIP. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-50-00 PG 218/FIG 205 REF RCD383642.SDR SWIA200923382Flap · defectiveWHEN EXTENDING FLAPS TO 45° AIRCRAFT ROLLED TO THE RIGHT. (FLT 3044) REMOVED EXCESS PAINT BUILDUP ON FLAP.SDR FDEA200912304571Hinge Bracket · corrodedRT INBD FLAP OTBD HINGE (FLAP SIDE) INBD PIVOT HOLE FOUND CORROSION. REWORKED IAW EA NR 1-5750-132282, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 109.SDR ASAA1047250Skin · chafedLEFT WING O/B AFT FLAP DEEP CHAFE BETWEEN RUB STRIPS 2 INCHES O/B OF NR 2 FLAP TRACK. REMOVED DAMAGED AREA, FABBED REPAIR PARTS AND BONDED.
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