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 SWAA095541Rib · corrodedDURING SCHEDULED 24Y CHECK, FOUND RT WING I/B MID FLAP RIB CORRODED. REMOVED AND REPLACED RIB PER SRM.SDR SWAA095540Rib · corrodedDURING SCHEDULED 24Y CHECK, FOUND LT WING I/B MID FLAP RIB CORRODED. REMOVED AND REPLACED RIB ASSY PER BAC DWG.SDR SWAA095531Wedge · puncturedDURING SCHEDULED 24Y CHECK, FOUND LT WING I/B MIDFLAP T/E WEDGE PUNCTURED. REPAIRED WEDGE PER SRM.SDR FDEA200908263103Skin · crackedRT INBD FOREFLAP WBL 22, CRACK ABOVE CARRIAGE ATTACH FITTING, L/E SKIN. CHEMICALLY REMOVED PAINT IAW MM 51-20-001-7 STOP DRILL CRACK 2 EA DIM: .250 IAW SRM 51-10-1 HFEC SHOW CRACK END ON STOP DRILLS IAW NDTM PT6 51-00-00, FIG 23 FABRICATED DOUBLER REPAIR FRSDR DL76S091399Skin · dentedHAIL DAMAGE DENTS FOUND ON UPPER SKIN OF INBOARD AFT FLAP DURING MTC. DENTS TOO CLOSE TO EXISTING DOUBLERS FOR NEW LOCAL REPAIRS. REPLACEMENT OF UPPER SKIN AND CORE WAS THEREFORE NECESSARY. REPAIRED PER ERA 473815-14.SDR ASAA0946463Skin · chafedLEFT O/B FORE FLAP UPPER SKIN 9 INCHES, 2 INCHES FROM I/B. 4.5 INCHES FROM T/E IS CHAFED AT PREVIOUS REPAIR. REPAIRED FLAP SKIN.SDR ASAA0946462Skin · delaminatedLEFT O/B FORE FLAP LOWER SKIN 1.5 INCHES, 2 INCHES FROM TRAILING EDGE, 2 3 INCHES FROM I/B EDGE IS A DELAMINATED AREA. REPAIRED FLAP SKIN.SDR ASAA0946461Skin · dentedLEFT O/B FORE FLAP LOWER SKIN 20 INCHES FROM I/B EDGE 2 INCHES FROM AFT EDGE IS DENTED. REPAIRED IAW SRM.SDR SWAA095456Flap · delaminatedDURING SCHEDULED 12Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA095455Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA095454Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND RT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA095452Flap · puncturedDURING SCHEDULED 6Y CHECK, FOUND RT WING I/B FORE FLAP LOWER SURFACE PUNCTURED. REPAIRED FORE FLAP PER SRM.SDR USAA2009082492238Skin · delaminatedCLT - Q4 - MAJOR REPAIR - TWO AREAS OF DELAMINATION ON LEFT OUTBOARD FOREFLAP TRAILING EDGE UPPER SURFACE, 36 INCHES FROM INBOARD END. REPLACED LEFT OUTBOARD FOREFLAP IAW JOB CARD 03C30727030.SDR IPXA09657251Wedge · damagedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP T/E WEDGE LOWER SURFACE. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5A (1) FIG 9 REV 44, REPAIR PATCH SIZE 11 X 7 INCHES.SDR IPXA09657194Skin · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP LOWER SURFACE I/B TRAILING EDGE AREA, EXISTING REPAIR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5C FIG 10 REV 44.SDR IPXA09657193Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP TRAILING EDGE WEDGE LOWER SURFACE, EXISTING REPAIR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5A (1) FIG 9 REV 44.SDR IPXA09657192Wedge · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP T/E WEDGE LOWER SURFACE EXISTING REPAIR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5A (1) FIG 9 REV 44.SDR IPXA09657186Fairing · delaminatedINSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP LOWER SURFACE LEADING EDGE FAIRING EXISTING REPAIR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5A (1) FIG 5 REV 44.SDR SWAA095425Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR IPXA09657190Fairing · delaminatedINSPECTION TYPE:C LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 44.SDR IPXA09657189Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 44SDR IPXA09657188Fairing · delaminatedINSPECTION TYPE:C RT WING O/B FLAP MID LEADING EDGE FAIRING FOUND DELAMINATION AT O/B PLACE. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5.SDR IPXA09657187Fairing · delaminatedINSPECTION TYPE:C RT WING O/B TRAILING EDGE FLAP MID LEADING EDGE FAIRING FOUND DELAMINATION AT I/B PLACE. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 44.SDR FDEA200908203060Structure · crackedCRACK LWR CHORD RT WING INBD MIDFLAP OTBD SIDE. REMOVED PANEL AND RETAINER IAW SRM 51-30-2, CUT-OUT DAMAGE SECTION DIM: 40 INCH IAW SRM 51-40-4 FIG 1, FABRICATED SECTION FROM BAC 1503-100046 IAW SRM 57- 50-2 AND 51-40-4 PO NR 2909673 DIM: 40 INCH AND SPLICE SDR FDEA200908203059Structure · damagedCRACK LWR CHORD RT WING INBD MIDFLAP INBD SIDE. REMOVED SEAL RETAINER FOR ACCESS IAW SRM 51-30-2, CUT-OUT DAMAGE ON RT WING INBD MID FLAP INBD SIDE IAW SRM 51-40-4 FIG 1, FABRICATED NEW PARTS IAW SRM 51-40-4. TREATED AND PRIMED NEW PARTS IAW SRM 51-10-2, ISDR USAA2009091592537Flap · debondedCLT - Q4 - MAJOR REPAIR - RIGHT OUTBOARD FORE FLAP DISBONDED ON INBOARD TRAILING EDGE. REPLACED RIGHT OUTBOARD FORE FLAP.SDR IPXA09M57274Wedge · debondedINSPECTION TYPE:2C UPON REMOVAL OF LT WING INBD FLAP INBD TE WEDGE. FOUND INBD UPPER FWD CORNERSKIN LAYERS DISBONDED. REPAIRED LT INBD FLAP INBD TE WEDGE REF EO MD11-5750-34823-A AND EA 011-5750-01-A2007.SDR DL757091367Skin · delaminatedRIGHT WING I/B MAIN FLAP T/E PANEL LOWER SURFACE FOUND AREA DELAMINATED APPROX MF STA 179. C/W AT SAA - SAT ON N/R 138641 JOB 83469790001.SDR DL757091360Skin · crackedAFT FLAP HAS LOWER SKIN CRACK L=0.75 IN AT 54 IN FROM I/B END. C/W AT SAA - SAT ON N/R 143155 JOB 83469420001.SDR IPXA09557199Skin · chafedINSPECTION TYPE:C1 RT WING I/B MAIN FLAP UPPER SURFACE 52 INCHES TO 68 INCHES O/B FROM I/B END, 11 INCHES FWD OF T/E IS CHAFED REPAIRED PER SRM 57-30-01 R1, SRM 51-70-07SDR USAA2009082192196Rib · crackedCLT - Q4 - MAJOR REPAIR - CRACK ON RIGHT WING OUTBOARD MIDFLAP RIB JUST OUTBOARD OF OUTBOARD CARRIAGE SUPPORT. REPLACED RIGHT WING OUTBOARD MIDFLAP IAW JOB CARD 03C40727020 & B737 AMM 27-51-00.SDR SWAA095401Flap · puncturedDURING SCHEDULED 20Y CHECK, FOUND LT WING O/B FORE FLAP L/E PUNCTURED. REMOVED AND REPLACED FORE FLAP PER MM.SDR FDEA200908183045Skin · damagedLT IB MIDFLAP LWR SURFACE WBL 85 HAS ELONGATED FASTENER HOLE. EVALUATED FASTENER HOLE FOUND TO BE OUT OF LIMITS IAW SRM 57-50-01. CUT-OUT DAMAGED AREA APPROX 1 INCH X .5 INCH IAW SRM 57-50-4 FIG 3 FAB REPAIR DOUBLER FROM 2024T3 .125 PO NR 290757Y DIM 13 INSDR FDEA200908183043Structure · crackedLT, IB. MIDFLAP T/E LWR CHORD, WBL 103 IS CRACKED ON IB CORNER. OPENED MID FLAP ACCESS PANEL IAW SRM 51-30-2, REMOVED LWR CHORD PREVIOUS REPAIR IAW SRM 51-30-2 FABRICATED NEW T/E LWR CHORD FROM BAC1503-100046 7075 PO NR 29057145 DIM: 49 INCHES IAW SRM 57-50-2SDR ASAA0946409Flap Track · corrodedNR 8 FLAP TRACK AFT ATTACH POINT RUSTY AT SHIMS. REMOVED AND REPLACED THE NR 8 FLAP TRACK.SDR A6WA200940498Plate · gougedRT WING INBD FLAP, INBD AFT HINGE LUG PLATES FOUND GOUGED (INBD .014 INCH DEEP, OTBD .007 INCH DEEP) LUG PLATES REPAIRED IAW REO 601R-57-52-1488. (K)SDR ASAA0946410Flap Track · corrodedNR 6 FLAP TRACK IS CORRODED ON BEARING WEAR SURFACES. REMOVED AND REPLACED NR 6 FLAP TRACK.SDR SROM20090013Fitting · chafedREPAIRED WORN FITTING P/N 65-50750-12 INSIDE RT INBOARD CANOE FAIRING RT WING IN ACCORDANCE WITH FAA DER APPROVED FORM 8110-3 ASI SOLUTIONS, INC 208-1226-09-683, DATED JULY 27, 2009. REFERENCE KELOWNA FLIGHTCRAFT NON-ROUTINE 325, DATED JULY 29, 2009.SDR IPXA09557233Fitting · gougedINSPECTION TYPE:C2 LT WING I/B FLAP O/B FLAP TRACK FWD FITTING I/B SIDE IS GOUGED 3 EA LOCATION. FITTING WAS REPAIRED PER ATS ENGINEERING 09-4267, DATED 27AUG09.SDR IPXA09557231Skin · gougedINSPECTION TYPE:C2 PREVIOUS REPAIR ON RT WING O/B MAIN FLAP UPPER I/B SKIN PANEL WBL 361.0 - 374.0 GOUGED IN TWO PLACES (W4-01). REPAIRED PER ATS ENGINEERING REPAIR 09-4250 DATED 27AUG09.SDR SWAA095342Flap · puncturedDURING SCHEDULED MV4 CHECK, FOUND RT WING I/B AFT FLAP PUNCTURED. REMOVED AND REPLACED AFT FLAP EPR MM.SDR ASAA0946408Flap Track · corrodedNR 1 FLAP TRACK AT AFT O/B MOUNT BOLT HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED NR 1 FLAP TRACK.SDR ASAA0946407Flap Track · corrodedNR 2 FLAP TRACK HAS EVIDENCE OF CORROSION ON ALL ROLLER SURFACES. REMOVED AND REPLACED NR 2 FLAP TRACK.SDR DLM88091562Skin · puncturedINBOARD FLAP LOWER SKIN REPAIRED IAW SRM 57-03D FIGURE 8.SDR FDEA200908122995Skin · misrepairedEXISTING EXTERNAL REPAIR DOUBLER FOUND AT LT WING INBD FLAP LWR SKIN BETWEEN STA (XIFH 153.300) AND (XIFH 159.300). EXISTING EXTERNAL REPAIR DOUBLER AT LT WING INBD FLAP LWR SKIN BETWEEN STA (XIFH 153.300) AND (XIFH 159.300) EVALUATED AND FOUND NOT IAW SRM RESDR IPXA09157180Skin · chafedINSPECTION TYPE:4C LT WING CENTER FLAP UPPER SURFACE IS CHAFED ABOVE NR 4 FLAP TRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER PER E0 A300-5750-34744-A AND EA 300-5753-01-A1987.SDR IPXA09157178Skin · gougedINSPECTION TYPE:4C LT WING CENTER FLAP UPPER SKIN GOUGED IN 8 PLACES, OUTBOARD OF NR 3 FLAP TRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER PER EO A300-5750-34743-B AND EA 300-5753-01-A1982 REV A.SDR SWAA095225Flap · puncturedDURING SCHEDULED MV2 CHECK, FOUND RT WING I/B AFT FLAP PUNCTURED. REMOVED AND REPLACED AFT FLAP PER MM.SDR FDEA200908112972Bellcrank · damagedRT INBOARD TRAILING EDGE FLAP, MAIN FLAP O/B CARRIAGE AREA FAIRING BELLCRANK FORK END (LONGER SIDE) WITH ONE NICK. NICK ON RT INBD TRAILING EDGE FLAP OUTB CARRIAGE FAIRING BELLCRANK FORK END REPAIRED IAW E.A. F-5740-131082. REPAIR IS CLASSIFIED AS MAJOR PERSDR SWAA095166Flap · delaminatedDURING SCHEDULED SPV CHECK, FOUND RT WING I/B MID FLAP T/E PANEL O/B END DELAMINATED. REMOVED AND REPLACED INBOARD FLAP PER MM.
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