JASC 5753
Service difficulty reports · 31,513
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 DALA1224811404Fairing · delaminatedRT I/B MAIN FLAP O/B L/E FAIRING IS DELAMINATED IN 3 PLACES. REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 TABLE 1 AND 51-70-05 PAR 5A(1) FIG 5.SDR EE4Y201204180188Trunnion · wornLT WING INBD FLAP INBD TRACK, TRUNNION FITTING WAS FOUND WITH WEAR.SDR SWAA2012051403954Flap · delaminatedLEFT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP IAW AMM.SDR SWAA2012043003557Flap · delaminatedRT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP IAW AMM.SDR SWAA2012042403356Flap · delaminatedRT WING INBD FORE FLAP DELAMINATED. REPAIRED FLAP PER SRM.SDR UIEA2012041800130Panel · deformedLEFT INBD MID FLAP T/E OF COVE PANEL DEFORMED IN FOUR PLACES. OPENSDR SWAA2012051403949Flap · crackedLEFT WING FORE FLAP O/B OF INBOARD LEADING EDGE CRACKED. REMOVED AND REPLACED FORE FLAP IAW AMM.SDR DALA1226926313Skin · damagedDURING INSPECTION FOUND DAMAGE PUNCTURES LOCATED 24 INCHES FROM THE AFT EDGE 65" FROM INBOARD EDGE, AT AFT FLAP SKIN AT RIGHT INBOARD TRAILING EDGE FLAP. MAINTENANCE CUT OUT DAMAGE PER SRM 91-70-10 AND REPAIR COMPLETED PER ERA 502474-14 AND SRM 57-53-01 AND 5SDR USAA2012041900006Skin · delaminatedC1 CHECK - AREA OF DELAMINATION ON LEFT WING OUTBOARD AFT FLAP LOWER SURFACE ADJACENT TO INBOARD END. REPLACED LEFT WING OUTBOARD AFT FLAP IAW B737 AMM 27-51-39.SDR REXA2012041900427Spar · wornLEFT INBOARD FLAP AND CENTER SLIDING BEAMS HAVE WORN SPARS FROM CUTOUT TO ROLLERS. REPAIRED IAW BOMBARDIER REO 601R-57-52-1895.SDR MK9A2012F00075Skin · crackedRT FLAP SKIN CRACKED ON BOTTOM SIDE AT W/S 53.00. THIS IS OCCURING UNDERNEATH THE INBD FLAP TRACK, OTBD CHANNEL. THE CRACKS HAVE BEEN ABOUT 3" IN LENGTH. THE VISIBLE PART OF THE CRACK PROTRUDES APPROX .2500" OTBD OF THE FLAP TRACK CHANNEL AND JUST AFT OF TSDR REXA2012041600074Skin · chafedRIGHT WING INBOARD FLAP VANE LEADING EDGE SKIN CHAFED AT APPROX WS 53. REMOVED AND REPLACED CHAFED SKIN IAW CRG200 SRM 51-42-16. 601R4303-545, B08610, CR3214-5-2, B58337 AAR SM-28.SDR DALA1223181404Fairing · delaminatedLT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING IS DELAMINATED IN 2 PLACES AND HAS BEEN REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 TABLE 1 AND SRM 51-70-05 PAR 5A(1) FIG 5.SDR SWAA2012051403950Skin · crackedLEFT WING MIDFLAP SKIN CRACKED ON INBOARD, UPPER EDGE. REPAIRED SKIN IAW EO AND EA.SDR REXA2012041300072Skin · chafedRIGHT INBOARD FLAP VANE OUTBOARD LEADING EDGE SKIN IS CHAFED AT APPROX WS 139. REMOVED AND REPLACED I/B FLAP VANE O/B LEADING EDGE SKIN IAW CRJ 200 SRM 51-42-13. REF CONTINUATION CARD FOR DETAILS. P/N CR3212-4-3 TAG B12079 P/N 601R14303-44S TAG B19752 AAR SSDR DALA1222771501Skin · delaminatedLT WING, O/B FLAP, LOWER SURFACE DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 57-53-01 REPAIR 1, AND SRM 51-70-06, PAR 5A(1), FIGURE 9.SDR USAA2012042400012Strut · corroded2S CHECK - CORROSION ON LEFT WING INTERCONNECTING STRUT BETWEEN WS 4067 TO WS 4862, RIB 1 OUTB/FLAP. REPLACED LEFT WING INTERCONNECTING STRUT IAW A319 AMM 27-51-44-400-001-A.SDR SWAA2012041603121Flap · damagedLT WING O/B FORE FLAP DAMAGED. REMOVED AND REPLACED FORE FLAP PER MM.SDR REXA2012041200423Vane · chafedRIGHT INBOARD FLAP VANE LEADING EDGE CHAFED IN 3 LOCATIONS. OUTBOARD AND CENTER WITHIN ALLOWABLE LIMITS, BUT INBOARD OUT OF LIMITS. REPAIRED IAW REO 601R-57-52-004.SDR UALA2012041302226Trunnion · wornRIGHT INBOARD FLAP TRUNNION WORN TO MAX LIMIT. REPLACED TRUNNION PER MT57-019.SDR IPXA12673052Hinge Fitting · crackedINSPECTION TYPE: 8C, RT WING INBD MAIN FLAP, INBD HINGE ARM FITTING FOUND CRACKED. RT WING INBD MAIN FLAP INBD HINGE ARM FITTING REPAIRED IAW SRM 57-53-02-2 REPAIR 1 FIG 201, REV 52.SDR USAA2012041900011Strut · corroded2S CHECK - DURING DISASSEMBLY OF THE RIGHT WING INTERCONNECTING STRUT CORROSION WAS FOUND IN IMMER HOUSING BETWEEN WS 4067 TO WS 4862, RIB 1 O/B FLAP. REPLACED RIGHT WING INTERCONNECTING STRUT IAW A318 AMM 27-51-44-400-001.SDR USAA2012041600008Flap · delaminatedC5 CHECK - DELAMINATION ON LEFT OUTBOARD FOREFLAP APPROX 108 INCHES INBOARD OF OUTBOARD EDGE ALONG THE UPPER TRAILING EDGE SURFACE. REPAIRED LEFT OUTBOARD FOREFLAP UPPER TRAILING EDGE SURFACE IAW B737 51-70-10 & 51-21-00.SDR DALA1222231501Skin · delaminatedLEFT WING, O/B FLAP LOWER SURFACE DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 57-53-01, REPAIR 1 AND SRM 51-70-06, PAR 5A(1), FIGURE 9.SDR DALA1222201501Fairing · delaminatedRIGHT WING, O/B FLAP, O/B FWD FAIRING DELAMINATED. COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT AS PER SRM 57-53-01, REPAIR 1 AND SRM 51-07-05 PAR 5A(1), FIGURE 5.SDR DALA1222191501Fairing · delaminatedLEFT WING, O/B FLAP, O/B FWD FAIRING DELAMINATED. COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT AS PER SRM 57-53-01, REPAIR 1 AND SRM 51-07-05 PAR 5A(1), FIGURE 5.SDR SWAA2012041102983Flap · delaminatedLT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR FDEA201204101335Skin · misrepairedRT WING INBD FLAP UPPER SURFACE MISREPAIRED. REPAIRED IAW SRM 57-00-01, FIG 201, REPAIR 1, REV 49.SDR SWAA2012041303114Skin · delaminatedLEFT WING INBOARD AFT FLAP TRAILING EDGE DELAMINATED AT INBOARD END. REMOVED AND REPLACED AFT FLAP IAW AMM.SDR DALA1222221501Skin · delaminatedRIGHT WING O/B FLAP UPPER SURFACE DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 57-53-01 REPAIR 1 AND SRM 51-70-06, PAR 5A(1), FIGURE 9.SDR DALA1222211501Fairing · delaminatedRIGHT WING, I/B FLAP, O/B FWD FAIRING DELAMINATED. COMPOSITE PREPREG REPAIR CARRIED OUT AS PER SRM 57-53-01, REPAIR 1 AND SRM 51-07-05 PAR 5A(1), FIGURE 5.SDR A6WA201240523Vane · chafedLEFT INBD FLAP VANE EDGE IS CRACKED IN 3 PLACES. REPAIRED OTBD AND MID CHAFED AREAS IAW REO 601R-57-52-004, REV C. REMOVED UNSERVICEABLE INBD SKIN AND INSTALLED SERVICEABLE INBD SKIN IAW SRM 51-42-13.SDR WX0A071150Skin · dentedLEFT INBOARD FLAP VANE LOWER SURFACE XW 138.053 - 7.000. PERMANENT REPAIR WITH 4X4 DOUBLER AND 1" DIA FILLER IAW MD80 SRM 51-70-02 SECTION 18 PARA B.SDR IPXA2672830Wedge · dentedLEFT WING INBD FLAP T/E WEDGE DENTED UPPER AND LWR SURFACE. REPAIRED REF EO B767-5750-46365-B.SDR FDEA201204091324Bushing · wornRT WING (FLAP SIDE) OTBD FLAP, OTBD HINGE, OTBD PIVOT HOLE BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.152" AND FOUND EXCEED LIMIT IAW CMM 57-52-04, REV 72. MAXIMUM ALLOWABLE DIAMETER 1.150". REPAIR ACCOMPLISHEDSDR FDEA201204091301Hinge Fitting · damagedLEFT WING (FLAP SIDE), INBD FLAP OTBD HINGE, OTBD PIVOT HOLE, FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED, OTBD LUG DIAMETER 1.254", OTBD STRAP DIAMETER 1.190" AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DSDR FDEA201204091300Hinge Fitting · damagedLEFT WING (FLAP SIDE) INBD FLAP, OTBD HINGE, INBD PIVOT HOLE, FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURE, INBD LUG, DIAMETER 1.283", INBD STRAP DIAMETER 1.217" AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DISDR FDEA201204091299Hinge Fitting · damagedRT WING (FLAP SIDE) INBD FLAP, OTBD HINGE, OTBD PIVOT HOLE, FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED, OTBD LUG DIAMETER 1.250", OTBD STRAP DIAMETER 1.21" AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DIAMSDR FDEA201204091298Hinge Fitting · damagedRT WING (FLAP SIDE) INBD FLAP, OTBD HINGE, INBD PIVOT HOLE FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURE, INBD LUG DIAMETER 1.252 IN, INBD STRAP DIAMETER 1.218" AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DIASDR DALA1223753722Attach Fitting · crackedLEFT WING T/E CAVITY BETWEEN INBD AND OUTBD FLAPS DEFLECTOR RIB UPPER PANEL ATTACHMENT FLANGE BROKEN. REPAIRED PER ERA 501412-14.SDR IPXA2572794Skin · dentedINSPECTION TYPE:C10, RT WING INBD MAIN FLAP INBD LOWER SKIN HAS DENTED AREA. REPAIRED FLAP IAW SRM 57-53-01 AND 51-70-102R FIG 203.SDR SWAA2012042503383Skin · puncturedLT WING INBD FORE FLAP LOWER SURFACE PUNCTURED. REPAIRED FLAP PER SRM.SDR SWAA2012041903242Skin · delaminatedLEFT WING I/B FOREFLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.SDR SWAA2012041703175Skin · puncturedLEFT WING I/B FORE FLAP LOWER SURFACE PUNCTURED. REPAIRED FORE FLAP IAW SRM.SDR FDEA201204051256Vane · delaminatedLEFT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. R & R IAW AMM 27-50-22-4, REV 72.0. ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-22-5 REV 72.0. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.SDR A6WA201240501Vane · dentedRT OTBD FLAP VANE HAS A DENT INBD ON VANE AT WS 162.49. REPAIRED RT OTBD FLAP VANE IAW REO 601R-57-53-041, REV B.SDR SWAA2012040902915Flap · delaminatedRT WING O/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER AMM.SDR CA120404011Cable · cracked(CAN) DURING A SCHEDULED INSPECTION AN ITEM CALLED FOR THE REMOVAL, CLEANING AND LUBRICATION OF FLAP DRIVE CABLES. DURING THE INSPECTION 8 OUT OF 12 FLAP DRIVE CABLE ENDS WERE FOUND WITH CRACKS. THE ACFT MFG WAS CONTACTED AND INDICATED THAT THE ARE AWARE OF CSDR AALA20120420011Skin · dentedHAIL DAMAGE TO THE RIGHT OUTBOARD AFT FLAP UPPER SKIN. ACCOMPLISHED BONDED REPAIR PER EA B757-51-023001.SDR AALA20120420010Flap · dentedHAIL DAMAGE TO THE INBOARD AFT FLAP. ACCOMPLISHED BONDED REPAIR PER EA B757-51-023001.
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