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 IPXA10M59832Vane · damagedINSPECTION TYPE:1C, RT WING AT OTBD FLAP, FLAP VANE OTBD LOWER EDGE IS DAMAGED, HAS CHUNK OF MATERIAL BROKEN OFF. REMOVED DAMAGE AT RT OTBD FLAP VANE OTBD LOWER EDGE AND REPAIRED REF SRM 59-50-80 REPAIR 2 AND UPS RCD 395085.SDR USAA2010050390883Flap · delaminatedMCN - C20 - MAJOR REPAIR - DELAMINATION ON RIGHT OUTBOARD FORE FLAP 40 INCHES FROM INBOARD END. REPLACED RIGHT OUTBOARD FORE FLAP IAW JOB CARDS O3R27002 & C3R27002.SDR FDEA201004301407Wedge · delaminatedLT WING-OTBD FLAP, T/E WEDGE, INBD UPPER SURFACE FOUND DELAMINATED. LT WING - OTBD FLAP T/E WEDGE REPAIRED IAW EA 1-5750-137979, REPAIR CLASSIFIED AS MINOR REPAIR IAW GMM 6-2-100 REV 110.SDR FDEA201004301405Hinge Fitting · corrodedRT OTBD FLAP, OTBD HINGE FLAP SIDE PIVOT BORES HAS PITTING CORROSION. REPAIRED IAW EA 8-5750-139132 WITH REPAIR BUSHINGS, MAJOR REPAIR.SDR ASAA1047766Wedge · damagedRIGHT I/B MID FLAP LOWER T/E WEDGE IS DAMAGED. REPAIRED MID FLAP.SDR ASAA1047765Skin · delaminatedRIGHT I/B MID FLAP DELAMINATED IN SEVERAL AREAS. REPAIRED MID FLAP.SDR ASAA1047947Skin · dentedLEFT I/B AFT FLAP L/E IS DENTED 24 INCHES IN O/B OF I/B END. REMOVED DAMAGED AREA, INSTALLED REPAIR.SDR IPXA10559670Panel · crackedINSPECTION TYPE:C3, LT WING FLAP FAIRING OTBD SIDE PANEL 574DL FOUND CRACK AT ATTACH FASTENER HOLE. REPLACED PANEL IAW MM 27-51-31-2.SDR SWAA102421Flap · delaminatedDURING SCHEDULED 18Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA102417Flap · delaminatedDURING SCHEDULED 10Y CHECK, FOUND RT WING O/B AFT FLAP I/B TRAILING EDGE DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR ASAA1047936Skin · chafedRIGHT O/B FOREFLAP LOWER LEADING SKIN IS CHAFED 6 IN FROM I/B END. REMOVED EXISTING REPAIR DOUBLER, FABRICATED NEW DOUBLER AND INSTALLED.SDR FDEA201004281382Skin · dentedRT WING INBD FLAP UPPER SURFACE AT APPROX XIFH 215 FOUND 1 EACH DENT WITH DEEP NICK DURING BLEND OUT. DENT WITH DEEP NICK AT RT WING INBD FLAP UPPER SURFACE AT APPROX XIFH 215 REPAIRED IAW SRM 57-10-00 FIG 85 VOL I REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM SDR AALA20100427TUL04Flap · wornRIGHT WING WORN AREA OUTBOARD FLAP INBOARD LEADING EDGE. INSTALLED DOUBLER WITH HOT BOND PER SRM 51-70-02.SDR IPXA10159726Skin · gougedINSPECTION TYPE:3/C, REPAIR SURVEY SEQ NR152-W4-03 REPAIR DOUBLER IS GOUGED. REPAIRED IAW EO A300-5750-37699-A AND SAA EA NR 300-5753-01-A2288 REV I/R.SDR IPXA10159697Skin · misrepairedINSPECTION TYPE:3/C, REPAIR SURVEY SEQ 152-W4-01 DOES NOT CORRELATE WITH SRM REPAIR. REPAIRED IAW EO A300-5750-37670-A AND EA 300-5750-01-A2284 REV I/R.SDR ASAA1047941Skin · chafedLEFT O/B MIDFLAP RUB STRIP WORN THROUGH JUST O/B OF I/B CARRIAGE FITTING. REMOVED DAMAGED SKIN AND INSTALLED REPAIR.SDR SWAA102378Flap · delaminatedDURING SCHEDULED CV CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR IPXA10M59503Wedge · damagedFLAP T/E WEDGE DAMAGED D422289. REPAIRED IAW MD11-5750-37533-A.SDR WRLA20100426354Panel · gougedDESC - FOUND THE PANEL 657LT 1EA BOLT HOLE SINK INTO PANEL, AT RT OUTBOARD FLAP OUTBOARD SIDE. NRC U05112 ISSUED FOR IT. REMOVED THE DAMAGED PANEL, FABRICATE A NEW IAW EI: W2010P57B-954 REV 00. INSTALLED THE NEW PANEL COND CHECK SATISFACTORY.SDR FDEA201004261360Skin · deformedLT WING INBD FLAP LOWER L/E INBD OF OTBD HINGE, FOUND SKIN DEFORMED. LT WING INBD FLAP LOWER L/E INBD OF OTBD HINGE DEFORMED SKIN EVALUATED AND FOUND WITHIN LIMIT IAW SRM 57-00-01 FIG 1B VOLUME I REVISION 96. DEPTH OF DENT = 0.013", DIAMETER OF DENT = 3.0"SDR ASAA1047972Skin · dentedLEFT I/B AFT FORE FLAP LOWER SURFACE REPAIR DOUBLER DENTED. REMOVED DAMAGED DOUBLER, INSTALLED NEW.SDR A6WA201040328Lug · gougedRT INBD FLAP HINGE BOX AFT LUGS ON WING ARE GOUGED (DWG 601R10315 REF). REPAIRED DAMAGED LUGS ON TR INBD FLAP, INBD HINGE BOX AFT LUGS IAW REO 601R-57-21-1276.SDR SWIA201024097Strip · defectiveAIRCRAFT ROLLED HARD RIGHT WHILE ON FINAL AT 1000FT AGL AND REQUIRED ABOUT HALF CONTROL DEFLECTION TO THE LEFT TO KEEP WINGS LEVEL WITH FLAPS AT 45 DEGREES. (FLT 3075) SANDED LEFT AND RIGHT FLAP TEFLON ABRASION STRIPS DUE TO FINDING LIP ON ABRASION PADS.SDR FDEA201004241347Skin · dentedDENT - RT WING INBD FLAP LOWER SURFACE. REPAIR CARRIED OUT IAW SRM 57-10-00 FIG 3, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.SDR AALA20100422TUL06Wedge · dentedLEFT OUTBOARD FLAP INBOARD WEDGE DENT MEASURED APPROXIMATELY 3 INCHES BY 4 INCHES BY 1/8 INCH DEEP. REMOVED AND REPLACED DENTED SKIN PER ESO 80096 PAGE 01A.SDR A6WA201040306Fitting · chafedLT OTBD FLAP ALIGNMENT ROLLER FITTING ON FLAP IS CHAFED REO 601R-57-53-794.SDR ABXR201006250006Skin · crackedDURING A HEAVY MX, THE LT WING INBD FLAP T/E OTBD END FOUND CRACKED. REPAIRED T/E SRM 57-03. FIG 9, ITEM RETURNED TO SERVICE.
SDR A6WA201040307Skin · chafedRT WING INBD FLAP VANE SKIN CHAFED FROM 11B STRAP R & R INBD FLAP SKIN IAW SRM 51-42-10.SDR SWAA102257Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED AT T/E. REMOVED AND REPLACED FLAP PER MM.SDR AALA20100420TUL04Flap · puncturedINBOARD AFT FLAP LOWER ONE PUNCTURE. INSTALLED DOUBLER PER SRM 51-70-10-2R2 AND AARD 57-50-1.SDR AALA20100420TUL05Skin · corrodedINBOARD AFT FLAP OUTER SKIN HAS AREAS OF CORROSION ALONG TRAILING EDGE OF FLAP. HOT BONDED REPAIR PER SRM 51-70-10-2R-4 FIGURE 202.SDR A6WA201040296Skin · chafedRT WING INBD FLAP VANE SKIN HAS CHAFING FROM OTBD STOP REPAIRED DAMAGE IAW REO 601R-51-52-004, REV C.SDR A6WA201040294Skin · chafedRT WING INBD FLAP VANE SKIN CHAFING FROM CENTER STOP. REMOVED DAMAGE WITH MATERIAL LOSS OF .006" WITHIN LIMITS IAW REO 601R-57-52-004, REV C.SDR A6WA201040293Skin · chafedLT INBD FLAP VANE CHAFED IN 3 AREAS ON L/E VANE REPAIRED DAMAGE IAW REO 601R-57-52-004, REV C.SDR FDEA201004201259Hinge Fitting · corrodedRT WING OTBD FLAP; OTBD HINGE AT LOCATION NR 8 INBD LUG FACE IS CORRODED. REMOVED CORROSION IAW CMM 57-44-09. ACCOMPLISHED HFEC IAW NTW 51-00-17. ETCHED, ROTO-PEENED, CLEANED, CALCULATED AMP HRS, CAD PLATED AND ADHESION TESTED IAW BSOPM 20-10-02. PRIMED ISDR FDEA201004201258Hinge Fitting · corrodedRT WING OTBD FLAP; OTBD HINGE AT LOCATION NR 8 INBD LUG FACE IS CORRODED. REMOVED CORROSION IAW CMM 57-44-09. ACCOMPLISHED HFEC IAW NTW 51-00-17. ETCHED, ROTO-PEENED, CLEANED, CALCULATED AMP HRS, CAD PLATED AND ADHESION TESTED IAW BSOPM 20-10-02. PRIMED ISDR FDEA201004191249Fitting · corrodedRT OTBD FLAP; OTBD HINGE LOCATION NR 5 OTBD LUG FACE IS CORRODED. REMOVED CORROSION IAW 57-44-09. ACOMPLISHED HFEC IAW NTW 51-00-17. ETCHED; ROTO- PEENED; CLEANED; CALCULATED AMP-HRS; CAD PLATED AND ADHESION TESTED IAW BSOPM 20-10-02. PRIMED IAW CMM 57-SDR FDEA201004191251Fitting · corrodedLT WING OTBD FLAP; OTBD HINGE LOCATION NR 7 BORES (2 EA) ARE CORRODED INSIDE. REMOVED CORROSION FROM BORES. BORE FOUND TO BE WITHIN LIMITS. ETCHED BORES. CAD PLATED BORES. PRIMED BORES IAW CMM 57-44-09.SDR FDEA201004191250Fitting · crackedRT OTBD FLAP; OTBD HINGE LOCATION NR 2 BORE HAS CRACK INDICATION. REMOVED CRACK INDICATION IAW CMM 57-44-09. ACCOMPLISHED HFEC IAW NTW 51-00-17. ETCHED AND ROTO-PEENED BORE; CALCULATED AMP-HRS; CAD PLATED AND ADHESION TESTED BORE IAW BSOPM 20-10-01. PRIMSDR FDEA201004191248Fitting · corrodedRT OTBD FLAP; INBD LOCATION NR 4 INBD LUG FACE IS CORRODED. VERIFIED LUG THICKNESS AND REMOVED CORROSION IAW BAC CMM 57-44-08. ETCHED; ROTO- PEENED; CLEANED; CALCULATED AMP-HRS; PREPPED; CAD PLATED AND ADHESION TESTED IAW BSOPM 20-10-02. PRIMED IAW CMSDR FDEA201004191247Fitting · corrodedRT OTBD FLAP; INBD LOCATION NR 2 MOUNTING SURFACE IS CORRODED. REMOVED CORROSION AND SOLD LIMITS IAW CMM 57-44-08. ETCHED; FLAP-PEENED; CLEANED; CAD PLATED AND ADHESION TESTED IAW BSOPM 20-11-01 AND BSOPM 20-10-02. PRIMED SURFACE; MATERIAL ID FOR SHIM; FSDR FDEA201004191246Fitting · corrodedRT OTBD FLAP; INBD LOCATION NR 3 MOUNTING SURFACE IS CORRODED. REMOVED CORROSION AND SOLD LIMITS IAW CMM 57-44-08. ETCHED; FLAP-PEENED; CLEANED; CAD PLATED AND ADHESION TESTED IAW BSOPM 20-11-01 AND BSOPM 20-10-02. PRIMED SURFACE; MATERIAL ID FOR SHIMSSDR FDEA201004191245Structure · corrodedRT OTBD FLAP; INBD HINGE BARREL NUT HOLE IS CORRODED. REPAIRED BARREL NUT HOLE IAW CMM 57-44-08.SDR FDEA201004191244Fitting · corrodedRT OTBD FLAP; INBD HINGE LOCATION NR 4 OTBD LUG FACE IS CORRODED. VERIFIED THICKNESS AND REMOVED CORROSION IAW CMM 57-44-08. ETCHED; CLEANED; CALCULATED AMP-HRS; PREPPED; CAD PLATED AND ADHESION TESTED IAW BSOPM 20-10- 02. PRIMED IAW CMM 57-44-08.SDR FDEA201004191242Fitting · corrodedRT OTBD FLAP; INBD HINGE FITTINGS AND LUGS HAVE SEVERAL AREAS OF BARE METAL IS CORRODED. PRIMED BARE AREAS IAW SOPM 20-11-02.SDR FDEA201004191241Fitting · corrodedRT OTBD FLAP; OTBD HINGE LOCATION NR 3 OTBD LUG FITTING IS CORRODED. REMOVED COROSION AND ACID ETCHED IAW CMM 57-44-09. ROTO-PEENED; CLEANED; CALCULATED AMP-HRS; CAD PLATED AND ADHESION TESTED IAW BSOP 20-10-02. PRIMED SURFACE IAW CMM 57-44-09.SDR FDEA201004191240Fitting · corrodedRT OTBD FLAP; OTBD HINGE LOCATION NR 7 SIDE LOAD FITTING MOUNTING SURFACE IS CORRODED. REPAIRED IAW CMM 57-44-09. VERIFIED LUG THICKNESS. REMOVED CORROSION. ETCHED SURFACE. ROTO-PEENED SURFACE. CAD PLATED SURFACE. PRIMED SURFACE. MATERIAL ID FOR SHIMSDR FDEA201004191239Fitting · corrodedRT OTBD FLAP; OTBD HINGE LOCATION NR 3 MOUNTING SURFACE IS CORRODED. REPAIRD IAW CMM 57-44-09. VERIFIED LUG THICKNESS. REMOVED CORROSION. ETCHED SURFACE. ROTO-PEENED SURFACE. FLAP PEENED SURFACE. CAD PLATED SURFACE. MATERIAL ID FOR SHIM. MACHINED SHISDR FDEA201004191238Fitting · corrodedRT OTBD FLAP; OTBD HINGE LOCATION NR 2 JUST AFT OF MOUNTING SURFACE IS CORRODED. REMOVED CORROSION AND ETCHED IAW BAC CMM 57-44-09. FLAP-PEENED; CALCULATED AMP-HRS; CAD PLATED AND ADHESION TESTED IAW BSOP 20-10-02. PRIMED IAW CMM 57- 44-09.SDR FDEA201004191237Fitting · corrodedLT OTBD FLAP; INBD HINGE; INBD BARREL NUT HOLE IS CORRODED. REPAIRED BARREL NUT HOLE IAW CMM 57-44-08.
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