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 UALA2010090703291Fitting · failedLT INBD AFT AFT FLAP DRIVE TORQUE TUBE ATTACH FITTING ON LWR SURFACE BEARING RETENTION FAILED, BEARING MIGRATED BUT TRAPPED INSIDE TUBE LUGS AND FITTING. R & R FITTING ASSY.SDR FDEA201009043276Skin · damagedLEFT IB FLAP AFT IS DAMAGED OB TE. REMOVED LT IB AFT FLAP IAW MM 27-51-002-4, AND REMOVED DAMAGE 10" X 3" IAW SRM 51-40-20, AND FABRICATED REPAIR CORE IAW SRM 51-40-20. BONDED CORE IAW SRM 51-40-20 AND FABRICATED DOUBLER 12" X 5" IAW SRM 51-40-20, BONDED DOUSDR FDEA201009043273Skin · gougedLT WING OTBD FLAP INBD L/E GOUGED APPROX 0.500 IN LENGTH X 0.250IN WIDTH BLENDED AREA ON LT OTBD FLAP INBD L/E REF SRM 51-73-00 NDT FOUND NO CRACK REF NTM 51-10-08 BEFORE BLEND 0.053 MAT LOSS 0.017 IN MAT REMAINING 0.036 IN OUT OF LIMITS REF SRM 57-50-00 REMSDR USAA2010090791940Flap Track · corrodedSAL - Q4 - MAJOR REPAIR - CORROSION ON FORE FLAP CENTER TRACK OF INBOARD MIDFLAP LEFT WING AT WBL 117. REPAIRED CENTER FORE FLAP TRACK OF LEFT INBOARD MID FLAP AT WBL 117 IAW B737 CMM 57-53-17 REPAIR 29-1.SDR USAA2010090791939Flap Track · corrodedSAL - Q4 - MAJOR REPAIR - NR # 6255809 - CORROSION ON FORE FLAP INBOARD TRACK OF INBOARD MIDFLAP LEFT HAND WING AT WBL84.96. REPAIRED INBOARD FORE FLAP TRACK AT LEFT HAND INBOARD MID FLAP IAW B737 CMM 57-53-17 REPAIR 28-1.SDR USAA2010093092162Flap Track · corrodedCLT - Q6 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON NR 7 FLAP TRACK AFT PAD. REPLACED NR 7 FLAP TRACK IAW B737 AMM 27-51-49.SDR IPXA10162838Skin · gougedINSPECTION TYPE:10YR, RT CTR FLAP UPPER SKIN REPAIR DOUBLER IS GOUGED IN 5 PLACES. ACCOMPLISHED REPAIR IAW EO A300-5750-39854-A PARA. 6A.SDR IPXA10162753Skin · gougedINSPECTION TYPE:10YR, RT INBD FLAP UPPER SKIN REPAIR DOUBLER HAS 4 SMALL GOUGES AND LOOSE RIVET AT FWD UPPER CORNER. REPAIRED RT INBD FLAP UPPER SKIN BETWEEN RIBS 11-14, STGR 2.1-2.2 IAW EO A300-5750-39726-A AND STA-SA EA 300-5750-01-A2670 I/R.SDR FDEA201009023248Wedge · delaminatedLEFT WING OUTBOARD FLAP TRAILING EDGE WEDGE INBOARD EDGE LOWER SURFACE. FOUND DELAMINATION. REPAIRED AS PER E.A. 1-5750-132474. REPAIR CLASSISIFIED AS MINOR PER GMM 6-2-100, REVISION 111.SDR USAA2010090891959Skin · wornCLT - Q2 - MAJOR REPAIR - DEEP AREA OF WEAR ON UPPER SURFACE OF LEFT OUTBOARD FOREFLAP 48 INCHES FROM INBOARD END. REPLACED LEFT OUTBOARD FOREFLAP IAW B737 AMM 27-51-37.SDR QXEA2010090700523Structure · chafedC-CHECK - LT WING OTBD FLAP, L/E INBD END HAS CHAFING .2500 INCH BY .1250 INCH WIDE. BLENDED DAMAGE IAW SRM 51-14-00, REV 7. MEASURED AFFECTED AREA MIN MATERIAL REMAINING .052" REF HORZ. AIR NTM 4.2.0-1 REV 13.SDR QXEA2010090700522Skin · chafedC-CHECK - LT WING OTBD FLAP, UPPER INBD SKIN HAS 64IN OF CHAFING FROM WING T/E SHROUD. BLENDED FLAP SKIN IAW SRM 57-52-30-02-01, REV 05, APR 07. MEASURED AFFECTED AREA MIN MATERIAL REMAINING .029 REF HORZ NTM 4.2.0-1.SDR QXEA2010090700504Structure · chafedC-CHECK - FOUND CHAFE DAMAGE TO RT INBD FLAP LOCATED AROUND INBD FLAP HINGE ARM. BLENDED 2 CHAFED AREAS IAW SRM 51-12-00-001-001-A01. ORIGINAL SKIN THICKNESS IS .063, REMAINING MATERIAL IS.055 AND .057. CHAFES ARE WITHIN LIMITS IAW SRM 57-52-01-101-001-A01. SDR DHLA201000114Rib · damagedREMOVE DAMAGED RIB IN RT FLAP WELL STA XW 90 AND REPAIR IAW APPROVED DATA PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATED 10-06-10, EVA D857-00357 REV IR DATED 09-01-10. REMOVED DAMAGED RIB & EXISTING REPAIR IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAMAGED WEB SDR DHLA201000109Skin · nickedRT OTBD FLAP UPPER SKIN NICK, STA XF 227.000 PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 10-04-10 EVA D857-00377 REV IR DATED 09-22-10. REMOVED DAMAGED PLATING AND EXISTING SPLICE IAW SRM 51-1-21, SRM 51-3-0. FABRICATED NEW PLATING SEGMENT (AL2024T3 0.071SDR IPXA10162700Skin · gougedINSPECTION TYPE:10YR LEFT WING CENTER FLAP UPPER SURFACE PREVIOUS REPAIR IS GOUGED. ACCOMPLISHED REPAIR IAW EO A300-5750-39715-A, PARA 6A.SDR USAA2010091692005Support · corrodedCLT - Q2 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON RIGHT INBOARD FOREFLAP SUPPORT TUBE & ARMS. REPLACED RIGHT INBOARD FOREFLAP IAW JOB CARD 03C40927012.SDR UALA2010090203220Skin · damagedTOP OF FLAP HAS SMALL GOUGES APPROX CENTER OF FLAP TOWARD LEADING EDGE RT OUTBOARD TRAILING FLAP. REPAIRED DAMAGE.SDR SWAA105166Skin · delaminatedDURING SCHEDULED 24YCHECK, FOUND LT WING I/B FORE FLAP DELAMINATED LOWER SKIN FROM I/B END. REPAIRED FORE FLAP PER SRM.SDR DHLA201000118Skin · crackedRT INBD FLAP WELL.- WEB CRACKED 1" STA XF 75.000 PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATED 10-04-10, EVA D857-00375 REV IR DATED 09-21-10. CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER REPAIR STRAP IAW DWG ES-D85700375-001-D REV IR DATED 9-21-10.SDR USAA2010090391908Skin · wornCLT - MAJOR REPAIR - Q2 CHECK - WORN AREA OF FLAP SKIN FROM WORKING RIVETS AT LEFT INBOARD FORE FLAP. REPLACED LEFT INBOARD FLAP IAW JOB CARD 03C30927015.SDR FDEA201008313217Angle · crackedRT WING CTR FLAP OTBD EDGE FOUND 1EA ANGLE CRACKED. REMOVED THE CRACKED ANGLE. CLEAN AND INSTALL THE BRAND NEW ANGLE REFER TO AB6F SRM 51-40-21. THE REPAIR WHICH IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201008313216Angle · crackedLT WING T/E CTR FLAP OTBD EDGE 1EA ANGLE CRACKED. REMOVED THE CRACKED ANGLE. FABRICATE A NEW PART IAW DWG NR:A57960402 SH1. INSTALL WITH NEW PART IAW AB6F SRM 51-40-21. REPAIR CLASSFIED AS MINOR IAW GMM6-2-100.SDR QXEA2010090100502Skin · gougedC-CHECK - GOUGE ON INBD FLAP AT TOP CTR OF FLAP BY L/E. BLENDED ON GOUGE ON UPPER SKIN OF RT INBD FLAP LOCATED BETWEEN 2 RIVETS AT FLS 84.20 IAW SRM 51-12-00-001-001-A01. SCRATCH MEASURES 0.5"L X .050W X .0025"D. GOUGE IS WITHIN LIMITS OF SRM 57-52-01-101-SDR FDEA201008313204Skin · wornLT WING- INBD MAIN FLAP L/E, OTBD SIDE HAS 3 WORN SECTIONS WITH TOTAL LENGTH APPROX 20 INCHES. COMPLIED WITH EA F-5750-141199, CLEANED AREAS IAW SRM 51-10-02, OUT OF LIMITS, IAW SRM 57-53-01, FIG 101, SHEET 6. DAMAGE REPAIRED IAW SRM 57-53-01, LOCATED & DRILLSDR IPXA10562771Skin Panel · gougedINSPECTION TYPE:C3, L/W INBD MAIN FLAP L/E EXTERNAL SURFACE IS GOUGED JUST AFT OF TRUNNION FAIRING DOOR. R & R FLAP L/E SKIN PANEL IAW SRM 51-40-02-0G & SOPM 20-50-01.SDR FDEA201008303202Skin · dentedRT WING - INBD FLAP LOWER SURFACE FOUND DENT AT XIFH 198. DENT AREA TRIMMED OUT AND FABRICATED NEW SKIN AND DOUBLER AS PER SRM 57-50-01, FIGURE 201 REPAIR 2, REVISION 44. NEW SKIN AND DOUBLER INSTALLED AS PER SRM 57-50-01 FIGURE 201, REVISION 44. REPAIRSDR IPXA10162287Skin · dentedRT INBD FLAP DENTED WITH GOUGE. REPAIRED IAW EO A300-5750-35971-C.SDR FDEA201008303194Skin · dentedRT WING INBD FLAP DENTED AT APPROX WS 369.5 LOWER SURFACE EVALUATED DENT ON RT WING INBD FLAP LOWER SURFACE WS 369.5 A=1.187 Y=.062 A/Y RATIO 19.1 FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01, FIG 101, DETAIL VII. REPAIRED FLAP IAW SRM 57-53-01. CLASSIFIED CATSDR DHLA201000125Skin · dentedRT INBD FLAP UPPER PLATING DENTED STA XW 68. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED DENTED PANEL PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING (AL2024T3 0.025") & BONDED DOUBLER (AL2024T3 0.020") IAW SRM 57-7-1 FIG 1 ITEM "A" & "L"SDR IPXA10B63093Skin · dentedINSPECTION TYPE:C, DMI D433270 - LT WING OTBD AFT FLAP DENT OTBD OF INBD CANOE FAIRING. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 2, FIG 203, REV 16.SDR DHLA201000101Skin · dentedRT INBD FLAP UPPER PLATING DENTED STA XW 68 PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED DENTED PANEL PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING & BONDED DOUBLER IAW SRM 57-7-1 FIG 1, ITEM "A" & "L". BONDED BOTH PARTS WITH HYSOL IAW SDR USAA2010090391907Skin · wornCLT - MAJOR REPAIR - Q2 CHECK - AREA OF HEAVY WEAR ON LEFT OUTBOARD FLAP, INBOARD LEADING EDGE SKIN AT EXTREME INBOARD END. REPAIRED LEFT OUTBOARD FLAP, INBOARD LEADING EDGE SKIN AT EXTREME INBOARD END IAW B737-300 SRM 57-53-010.SDR SWAA105139Flap · puncturedDURING SCHEDULED OTS CHECK, FOUND LT WING AFT I/B FLAP PUNCTURED. REMOVED AND REPLACED AFT FLAP PER MM.SDR IPXA10B62723Wedge · damagedINSPECTION TYPE:C, RT WING INBD AFT FLAP T/E WEDGE LWR SURFACE HOLED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 5, REV 57.SDR USAA2010083091869Flap · delaminatedCLT - Q2 - MAJOR REPAIR - DELAMINATION ON LEFT INBOARD FLAP UPPER OUTBOARD CORNER. REPAIRED LEFT INBOARD FLAP UPPER OUTBOARD CORNER IAW B737 SRM 51-70-10.SDR SWAA104997Flap · delaminatedDURING SCHEDULED 12Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER MM.SDR IPXA10B62670Wedge · misrepairedINSPECTION TYPE:C, LT WING INBD AFT FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR (REDO) NON-STANDARD REPAIR. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 57.SDR IPXA10B62658Fairing · misrepairedINSPECTION TYPE:C, RT WING OTBD FORE FLAP L/E FAIRING EXISTING REPAIR (REDO) NON STANDARD REPAIR. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR. 5A(1) FIG 5, REV 57.SDR IPXA10B62657Wedge · misrepairedINSPECTION TYPE:C, RT WING OTBD FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR (REDO) NON STANDARD REPAIR. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR. 5C FIG 2, REV 57.SDR IPXA10B62652Wedge · misrepairedINSPECTION TYPE:C, RT WING OTBD FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR (REDO) NON-STANDARD REPAIR. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM51-70-07 PAR 5A(1) FIG 5, REV 57.SDR USAA2010091491990Skin · crackedMCN - C4 - MAJOR REPAIR - LEFT WING OUTBOARD AFT FLAP HAS A CRACK IN LOWER SKIN AT NR 1 FLAP TRACK AREA AT WBL 483.69 TO WBL 484.89. REPAIRED LEFT WING OUTBOARD AFT FLAP LOWER SKIN AT NR 1 FLAP TRACK AREA AT WBL 483.69 TO WBL 484.89 IAW B757 51-70-04 REPAIR 5SDR IPXA10662348Flap · misrepairedINSPECTION TYPE:C, RT WING INBD AFT FLAP INBD FWD CORNER NON-STANDARD REPAIR DOUBLER. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R. REPAIR 4, FIG 202, SHEET 1, REV 47.SDR IPXA10662346Fairing · delaminatedINSPECTION TYPE:C, RT WING OTBD T/E FLAP L/E FAIRING FOUND DELAMINATION. HOT BOND REPAIR PERFORMED IAW SRM 51-70-05 PAR 5A (1) FIG 5, REV 47.SDR IPXA10B62543Wedge · delaminatedINSPECTION TYPE:C, LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1), FIG 5, REV. 57.SDR USAA2010082591796Bolt · corrodedSAL - Q4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON CARRIAGE 3 RETAINING BOLTS OF INBOARD MID FLAP LEFT (6EA). REPLACED NR 3 CARRIAGE RETAINING BOLTS OF LEFT INBOARD MID FLAP IAW JOB CARD 03C30927014.SDR IPXA10B62553Fairing · delaminatedINSPECTION TYPE:C, LT WING OTBD FORE FLAP L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1), FIG 5, REV 57.SDR SWAA104971Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING I/B AFT FLAP O/B END TRAILING EDGE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA104926Skin · puncturedDURING SCHEDULED 10Y CHECK, FOUND LT WING I/B AFT FLAP LOWER SKIN PUNCTURED. REPAIRED AFT FLAP PER EA.SDR IPXA10662084Skin · dentedFOUND ON WALKAROUND, RT OTBD FLAP BOTTOM HAS A DENT 7.5" X 4.5" IN DEEP AND A 3 IN DIAMETER BUBBLE. TEMPORARY REPAIR C/O IAW EO B767-5750-39284. REPETITIVE INSP REQUIRED AT (7) DAY INTERVALS UNTIL PERMANENT REPAIR OR PART REPLACEMENT IS ACCOMPLISHED WITHIN 60
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