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 UPS08M53852Skin · damagedINSPECTION TYPE:N/A RIVETS PULLED THROUGH UPPER SKIN OF INBOARD FLAP LT WING. REPAIR IAW EO MD11-5750-31055-B.SDR SWIA200820677Fitting · corrodedRIGHT INBOARD FLAP INBOARD HINGE/FLAP ACTUATOR FITTING INBOARD BEARING CORRODED (C-CHECK). REPLACED PER AMM.SDR UPS08854065Doubler · chafedINSPECTION TYPE:SV LEFT OUTBOARD FLAP UPPER SURFACE AT XF333 DOUBLER CHAFED. REPAIRED AS IAW UPS EO DC8 5720 31345.SDR UPS08854064Doubler · gougedINSPECTION TYPE:SV LEFT O/B FLAP TOP SURFACE DOUBLER GOUGED. REPAIRED AS PER UPS EO DC8 5720 31345A.SDR SWAA085985Flap · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FLAP PER SRM.SDR 08FDEA04707Web · crackedLEFT WING INBD FLAP AT RIB 25A, WEB PLATE IS CRACKED. REMOVED AND REPLACED THE -220 WEB PLATE IN REF TO A300-600 SRM 51-40-21; PARA 7; PARA 14 AND FOKKER DWG A57960114, ISSUE E.SDR 08FDEA04706Web · crackedLEFT WING INBD FLAP AT RIB 25A THE WEB PLATE IS CRACKED. REMOVED AND REPLACED -218 WEB PLATE IN REF TO A300-600 SRM 51-40-21, PARA 7, PARA 14 AND FOKKER DWG A57960114, ISSUE E.SDR 08FDEA04648Web · damagedLEFT WING INBD FLAP AT RIB 25A, WEB PLATE IS CRACKED AND MISDRILLED. REMOVED & REPLACED THE WEB PLATE IN REF TO SRM 51-40-21& DWG A57960114.SDR 08FDEA04632Carriage · corrodedLEFT WING CENTER FLAP NR 3 TRACK CARRIAGE UPPER FLANGE ASSY IS CORRODED AT THE LUGS. REMOVED AND REPLACED THE LEFT NR 3 FLAP TRACK FWD CARRIAGE UPPER BRIDGE REF A300-600 AMM 27-54-27-4.SDR SWAA085943Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING I/B FORE FLAP T/E DELAMINATED. REPAIRED FLAP PER SRM.SDR UIEA200800335Fairing · damagedLT WING NR 1 CANOE FAIRING AT WBL 743.828 WAS DAMAGE ON CARGO LOADING. CANOE WAS REMOVED PER ATLAS DMI M08-227. AREAS OF CANOE AT FAIRING STA 147.766 LOWER SIDE, STA 124.5 & 135.5 INSIDE OF CANOE, STA 152.766, 159.766, 167.766 ON OUTBOARD SIDE, SMALL HOLES 3SDR ASAA0843741Skin · chafedRIGHT OUTBOARD FOREFLAP PREVIOUS REPAIR CHAFED ON UPPER SURFACE AT INBOARD END. REMOVED DAMAGED AREA. INSTALLED DOUBLER FILLER AND BOND REPAIR PER SRM 51 70 10.SDR ASAA0843739Skin · dentedRIGHT INBOARD AFT FLAP LOWER SURFACE HAS CLUSTER OF DENTS. BOND REPAIRED DAMAGED AREA PER SRM 51 70 06.SDR ASAA0843736Skin · delaminatedRIGHT INBOARD AFT FLAP UPPER SURFACE DELAMINATED ON OUTBOARD END. REMOVED DAMAGED AREA. BOND REPAIRED WITH REPAIR PARTS PER SRM 51 70 10.SDR 2008FA0000725Rib · corrodedDURING ANNUAL INSPECTION FOUND ALL FLAPS, LEADING EDGE RIBS WERE SEVERELY CORRODED. DETECTION METHOD WAS TO TAKE THE FOREFINGER AND THUMB AND SQUEEZE LEADING EDGE AT THE RIB, GOT A CRUNCHING FEEL AND SOUND.SDR ASAA0843830Skin · dentedRT INBD AFT FLAP UPPER SURFACE HAS DENT. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51 70 10 REPAIR 4.SDR UPS08153886Doubler · chafedINSPECTION TYPE:1C3C LEFT WING T/E CENTER FLAP UPPER SKIN OUTBOARD REPAIR DOUBLER CHAFED. REMOVED, FABRICATED AND REPLACED LEFT WING T/E CENTER FLAP UPPER SKIN OUTBOARD. REPAIR DOUBLER REF A300-600 SRM 57-50-00 PARA 4E AND FIG 205.SDR UPS08153865Doubler · chafedINSPECTION TYPE:1C3C LT WING T/E CTR FLAP UPPER SKIN INBOARD. REPAIR DOUBLER CHAFED AS MARKED. REMOVED, FABRICATED AND REPLACED LEFT WING T/E CENTER FLAP UPPER SKIN I/B REPAIR DOUBLER REF A300-600 SRM 57-50-00 PARA 4E AND FIG 205.SDR ASAA0843740Skin · chafedLEFT INBOARD MIDFLAP UPPER SURFACE CHAFED AT INBOARD END 15 INCHES FORWARD OF TRAILING EDGE. REMOVED DAMAGED AREA. INSTALLED DOUBLER FILLER AND BOND REPAIR PER SRM 57 53 01 AND 51 70 10.SDR ASAA0843738Skin · dentedLEFT INBOARD FOREFLAP HAS CLUSTER OF DENTS ON LOWER SURFACE OUTBOARD OF INBOARD TRACK. REMOVED DAMAGED AREA. REPAIRED WITH DOUBLER FILLER AND BOND REPAIR PER SRM 51 70 10.SDR 08FDEA04586Strap · crackedLEFT WING, OUTBOARD FLAP INBOARD HINGE (WINGSIDE) TENSION STRAP FITTING FOUND CRACKED. R & R AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA04597Angle · crackedLEFT WING OTBD L/E, CRACKS IN INBD AND OTBD REINFORCEMENT ANGLES AT FWD FASTENERS LOCATIONS ABOVE NR 2 SLAT ACTUATOR LWR FAIRING. REMOVED INBD AND OTBD REINFORCEMENT ANGLES, MFG NEW ANGLES REF DWG 65-21672 PGS 1- 3 USING A63549 FOR ANGLE MATERIAL PRIMED AND ISDR ASAA0843828Skin · dentedRT INBD FOREFLAP UPPER SURFACE DENTED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA0843827Skin · chafedRT INBD FOREFLAP UPPER SURFACE CHAFED ON INBD END. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA0843826Skin · dentedRT INBD FOREFLAP UPPER SURFACE DENTED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA0843788Skin · dentedRIGHT INBOARD AFT FLAP LE IS DENTED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER AND SPLICE PLATE PER SRM 57-53-01.SDR UPS08653755Skin · delaminatedINSPECTION TYPE:N/A RT O/B FLAP LWR SKIN DELAMINATION D368856. REPAIRED IAW SRM 51-70-10-2R.SDR IXXA08SMN204SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP LEADING EDGE CORRODED AT STATION XW 2.000-91.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK ASDR UPS08M53982Skin · dentedINSPECTION TYPE:1C RT WING O/B FLAP LOWER SURFACE 22 INCHES O/B OF PANEL 657FB 39 INCHES FROM T/E FOUND DENT. REMOVED DAMAGE AND BONDED REPLIES IAW UPS EO MD11-5750-31266-A AND SAA EA 011-5750-01-A1564.SDR UPS08M53980Skin Panel · dentedINSPECTION TYPE:1C RT WING O/B FLAP LOWER SURFACE 18.5 INCHES O/B OF PANEL 657FB 36 INCHES FROM T/E FOUND DENT. REMOVED DAMAGE AND BONDED REPAIR PLIES IAW UPS EO MD11-5750-31247 -A AND SAA EA 011-5750-01-A1563.SDR 08FDEA04540Skin · chafedRT WING INBD FLAP UPPER SURFACE 12 INCHES AFT OF FWD SPAR AND 1 INCH OTBD OF RIB 12 HAS 2 CHAFED AREA, 2 SQ INCHES CUT OUT DAMAGED AREA AND INSTALLED FLAPS, SKIN PATCH REPAIR DOUBLER ON RT WING INBD FLAP UPPER SKIN AT RIB 12 IAW A300-600 SRM 57-50-00, FIG 205,SDR UALA2008111306273Fitting · crackedLT WING OUTBOARD FLAP, OUTBOARD, AUX TRACK ATTACH FITTING TO RS, IS CRACKED. REPLACED FITTING.SDR ASAA0843796Skin · dentedLT OTBD AFT FLAP DENTED ON LOWER SURFACE. PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2.SDR ASAA0843794Skin · dentedLT OTBD AFT FLAP LOWER SURFACE IS DENTED PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2.SDR ASAA0843785Skin · dentedLEFT INBOARD MID FLAP TE WEDGE UPPER SURFACE IS DENTED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER SRM 51 70 10.SDR ASAA0843784Skin · dentedRIGHT OUTBOARD AFT FLAP LOWER SURFACE DENTED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER SRM 51 70 10.SDR ASAA0843783Skin · puncturedRIGHT INBOARD FOREFLAP DENTED AND PUNCTURED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER SRM 51 70 10.SDR 08FDEA04517Bracket · corrodedLEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE BRACKET AFT LOWER ATTACH OUTBOARD HOLE FOUND WITH CORROSION. CORROSION AT LEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE BRACKET AFT LOWER ATTACH OUTBOARD HOLE REWORKED AND CORROSION REMOVED AS PER EA NR 1-5750-1SDR 08FDEA04516Bracket · corrodedLEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE BRACKET AFT LOWER ATTACH INBOARD HOLE FOUND WITH CORROSION. CORROSION AT LEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE AFT LOWER ATTACH INBOARD HOLE REWORKED AND CORROSION REMOVED AS PER EA NR 1-5750-122606. TISDR ASAA0843716Skin · puncturedRT WING I/B FORE FLAP LOWER SURFACE HAS VARIOUS DENTS WBL 73-93. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW B737 400 SRM 51 70 10.SDR UPS08853833Doubler · gougedINSPECTION TYPE:SV APPENDIX D SURVEY SEQUENCE 715-W4-02 EXTERNAL DOUBLER ON RT WING FLAP UPPER SURFACE AT STA XF 255 IS GOUGED. INSTALLED DOUBLER IAW DC8 SRM 51-1-21.SDR UPS08853832Skin · gougedINSPECTION TYPE:SV APPENDIX D SURVEY SEQ 715-W4-03 EXTERNAL DOUBLER AT STA XF 240 RT WING FLAP UPPER SURFACE IS GOUGED. INSTALLED DOUBLER IAW DC8 SRM 51-1-21.SDR UPS08853768Skin · damagedINSPECTION TYPE:SV REF UPS EO APPENDIX H STEP A (7) REPAIR FAILS. SURVEY SEQUENCE 715-W3-27. INSTALLED DOUBLER IAW DC8 SRM 57-02-01-0.SDR 2008UALA06273Attach Fitting · crackedLT WING OUTBOARD FLAP, OUTBOARD, AUX TRACK ATTACH FITTING TO RS, IS CRACKED. REPLACED FITTING.SDR USAA920081967Skin · wornCLT Q3 MAJOR REPAIR NR 03C40727023/007 AND LOG NR 5030908 RT OTBD FOREFLAP HAS NUMEROUS WORKING FASTENERS ALONG LEADING EDGE. REPLACED RT OTBD FOREFLAP.SDR 08FDEA04495Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER ATTACH OUTBOARD HOLE AFT MATING SURFACE FOUND WITH CORROSION. CORROSION REPAIRED IAW EA 1-5750-122600. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA04492Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER ATTACH INBOARD HOLE FORWARD MATING SURFACE FOUND WITH CORROSION. CORROSION REPAIRED IAW EA 1-5750-122600. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA04491Hinge Bracket · chafedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT UPPER ATTACH OUTBOARD HOLE FOUND WITH SCORING MARK. SCORING REPAIRED IAW EA 1-5750-122600. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA04490Hinge · chafedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT UPPER ATTACH INBOARD HOLE FOUND WITH SCORING MARK. SCORING REPAIRED IAW EA 1-5750-122600. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR ASM2008F00007Hinge · corrodedAFTER REWORK OF RT OB FLAP, IB AFT HINGE PN ARC 1984-502, OB PIVOT LUG BORE HAS BEEN FOUND OUT OF LIMITS PER CMM 57-52-04 PAGE 624 AND 625. FOUND 1.162" INSTEAD OF 1.150". NR 1-1032193304-2 APPROVE TO INSTALL AN OS BUSHING.
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