JASC 5740
Service difficulty reports · 3,003
Reports filed under 5740 · Wing, Attach Fittings, 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 = '5740' 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 = '5740' 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 DALA2019083005122Fastener · corrodedSHIP 5647 5 EA CLAMPS - RT WING ROOT ATTACH HARDWARE CORRODED. CORRECTIVE ACTION: REPLACED HARDWARE ON 5EA CLAMPS IN RT WING ROOT AREA. (1247608)SDR SIMA2019083029004Attach Fitting · crackedLEFT ENHANCED WINGTIP SPAR 1 ATTACH FITTING CRACKED. REMOVED AND REPLACED SPAR ATTACH FITTING IAW ERS-EJ-57MR-1151 01, PART A. EASI 8945.SDR SIMA2019083029003Attach Fitting · crackedRT ENHANCED WINGTIP SPAR 1 ATTACHMENT FITTING CRACKED. FOUND ON OPEN UP. REMOVED AND REPLACED THE SPAR ATTACHMENT FITTING IAW ERS-EJ-57MR-1151 01 PART B. EASI 8945.SDR FXGA201908281969Fitting · corrodedREPLACEMENT OF CORRODED FITTING AT STRINGER 17 W/STA 60L OUTBOARD. TO REPLACE CORRODED FITTINGS ON STRINGER 17L, OUTBOARD OF W/STA 60L. ON WING STRINGER 20L, REMOVE OUTBOARD STATION 60L STRINGER FITTINGS AND REPLACE WITH A NEW ONE.SDR FXGA201908281970Tee Fitting · corrodedREPLACEMENT OF TEE ANGLE AT L/H OUTER WING AT W/STA 421. AFTER REMOVAL OF THE L/H OUTER WING THE CENTER SPAR TEE ANGLE (W/STA 421) WAS FOUND CORRODED. ON L/H OUTER WING, REMOVE CENTER SPAR TEE ANGLE AT W/STA 421.SDR FXGA2019082820191Tee Fitting · corrodedREPLACEMENT OF TEE ANGLE AT L/H OUTER WING AT W/STA 421. AFTER REMOVAL OF THE L/H OUTER WING THE CENTER SPAR TEE ANGLE (W/STA 421) WAS FOUND CORRODED. ON L/H OUTER WING, REMOVE CENTER SPAR TEE ANGLE AT W/STA 421.SDR SWAA2022031886912Trunnion · corrodedR/H MLG FWD TRUNNION SUPPORT FITTING UPPER OUTBD LUG HAT FACE EVIDENCE OF CORROSION / REPAIRED PER SRM 57-20-90-2R-2 R-2 REPAIR 2 SEE WO# P26883SDR SWAA2022031886913Trunnion · corrodedR/H MLG FWD TRUNNION SUPPORT FITTING UPPER INBD LUG HAT FACE EVIDENCE OF CORROSION / REPAIRED PER SRM 57-20-90-2R-2 REPAIR 2 SEE WO# 26883SDR SWAA2022031886910Trunnion · corrodedR/H MLG FWD TRUNNION SUPPORT FITTING LOWER OUTBD LUG HAT FACE EVIDENCE OF CORROSION / REPAIRED PER SRM 57-20-90-2R-2 REPAIR 2 SEE WO P26883SDR SWAA2022031886908Trunnion · corrodedL/H MLG FWD TRUNNION SUPPORT FITTING LOWER OUTBD LUG HAT FACE EVIDENCE OF CORROSION / REPAIRED PER SRM 57-20-90-2R-2 REPAIR 2 SEE WO P26883SDR SWAA2022031886909Trunnion · corrodedL/H MLG FWD TRUNNION SUPPORT FITTING LOWER INBD LUG HAT FACE EVIDENCE OF CORROSION / REPAIRED PER SRM 57-20-90-2R-2 REPAIR 2 SEE W/O P26883SDR SWAA2022031886906Trunnion · corrodedL/H MLG FWD TRUNNION SUPPORT FITTING UPPER OUTBD LUG HAT FACE EVIDENCE OF CORROSION / REPAIRED PER SRM 57-20-90-2R-2 REPAIR 2 SEE W/O P26883SDR SWAA2022031886907Trunnion · corrodedL/H MLG FWD TRUNNION SUPPORT FITTING UPPER INBD LUG HAT FACE EVIDENCE OF CORROSION / REPAIRED PER SRM 57-20-90-2R-2 REPAIR 2 SEE W/O 26883SDR SIMA20190811008Attach Fitting · crackedLT ENHACED WINGTIP SPAR 1 ATTACHMENT FITTING CRACKED. TRANSFERRED TO NRTC E732621. C/A-R&R LT ENHANCED WINGTIP SPAR 1 ATTACHMENT FITTING IAW ERS-EJ-57MR-1151 01 PART A.SDR SIMA20190811007Attach Fitting · crackedRT ENHANCED WINGTIP SPAR 1 ATTACHMENT FITTING CRACKED. TRANSFERRED TO NRTC E732622 C.OAKLEY 657866. C/A-REMOIVED AND REPLACED RT ENHANCED WINGTIP SPAR 1 ATTACHMENT FITTING IAW ERS-EJ-57MR-1151 01 PART B. EASI# 8945. SEE NRTC E732622 FOR DETAILS.SDR MK1Y20190903001Bushing · corrodedUPON PYLON REMOVAL FOUND CORROSION DAMAGE IN THE BUSHING COMMON TO LT WING FRONT SPAR OUTBD AND INBD PITCH LOAD FITTING, BOTH FITTINGS BORE DIAMETER EXCEED PRODUCTION LIMITS.SDR A6WA2019080946785Bracket · crackedRIGHT WING I/B LEADING EDGE ATTACH BRACKET IS CRACKED. REPLACED BRACKET IAW SRM 51-41-02.SDR HYIA20190731001Fitting · corrodedDURING MAINTENANCE, TWO AREAS OF CORROSION WERE DISCOVERED ON THE HORIZONTAL FLANGE OF THE UPPER LEFT HAND AFT WING FITTING (P/N 0822550-45.) THESE AREAS OF CORROSION MEASURED .750 BY .250 WITH A DEPTH OF .042, AND .400 BY .250 WITH A DEPTH OF .031. THIS FITTISDR LR7A2019080232141Fitting · crackedDURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5711, FOUND THE LH OUTER WING OWS241.6L FLAP TRACK-TO-AFT SPAR LOWER ATTACHED FITTING CRACKED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70.SDR SWAA2019071634845Attach Angle · crackedLT WING TRAILING EDGE FOUND CRACKED ATTACH ANGLE UNDER FIXED TRAILING EDGE PANEL JUST AFT OF THE #1 PYLON ORSS. 277. R&R ANGLE IAW SRM.SDR U2RA201908090004Attach Angle · crackedFOUND ONE EACH BREATHER ANGLE P/N 69B13824-11 CRACKED COMMON TO LEFT WING FIXED TRAILING EDGE PANEL OUTBOARD SIDE BETWEEN INBOARD AILERON AND NUMBER FIVE SPOILER. REMOVED AND REPALCED BREATHER ANGLE PER SRM 51-40-02.SDR SCNA20190627076Support Rod · wornRT LOWER TRAILING EDGE PNL SUPPORT ROD ATTACH POINTS WORN, ROD IS LOOSE. (AT WS 317, MARKED WITH STREAMER). REMOVED RT TE PNL SUPPORT ROD. REPLACED BUSHINGS AND INSTALLED ROD.SDR LR7A2019062401951Cap · crackedDURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER WING REAR SPAR WEB CWS192L FLAP ATTACHMENT VERTICAL CAP CRACKED; FS597. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6249.SDR LR7A2019062401950Cap · crackedDURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER WING REAR SPAR WEB CWS192R FLAP ATTACHMENT VERTICAL CAP CRACKED; FS597. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6248.SDR LR7A2019062401931Attach Angle · corrodedDURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT OUTER WING FLAPWELL L-ANGLE ATTACH TO REAR WEB CORRODED ON TOP POSITION, OWS142L, FS597, WL260-280. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6208.SDR LR7A2019062401770Attach Angle · crackedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND CTR WING LT FWD BEAM WING ATTACH ANGLE TO LEADING EDGE RIB CRACKED AT LOWER BEND RADIUS 1.5" AT FS517, WL260-285, AND CWS174. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2469.SDR LR7A2019062401735Fitting · corrodedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD WING TIP ATTACHMENT POINT, AFT ATTACHMENT POINT UPPER AND LOWER FITTING CORRODED AT FS580, OWS563, AND WL256-280. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 235SDR REXA2019062101084Canister · crackedINITIAL INSPECTION: CRACK IN CANISTER, WELDED NR 3 IN STA. WS148 AT RT MAIN FUEL TANK. (AD) CANISTER, WELDED NR 3 IN STA WS148 AT RT MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV.-- AND SRM 51-42-20-001-001-A01 PAR. 6.SDR REXA2019062101083Canister · crackedINITIAL INSPECTION : CRACK IN CANISTER, WELDED NR 3 IN STA WS148 AT LT MAIN FUEL TANK. (AI) CANISTER, WELDED NR 3 IN STA WS148 AT LT MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV.-- AND SRM 51-42-20-001-001-A01 PAR. 6SDR SWAA2022031040626Trunnion · corrodedRT MLG FORWARD TRUNNION LOCATION #1 UPPER O/B INNER FACE SHOWS EVIDENCE OF CORROSION. DOT 82-057. / AT RIGHT MLG FWD TRUNNION FITTIN G LOCATION #1 UPPER O/B INNER FACE SPOT FACED TO A DEPTH OF 0.035' AND DIAMETER OF 2.750' N SIGN OF CORROSION REMAIN PER B737-7SDR SWAA2022031040628Trunnion · corrodedRT MLG FWD TRUNNION LOCATION # 3 LOWER O/B INNER FACE SHOWS EVIDENCE OF COROSION. DOT 82-059. / AT RIGHT MLG FWD TRUNNION LOCATION #3 LOWER O/B R INNER FACE; SPOT-FACED INNER SURFACE TO A DEPTH OF 0.055' AND A DIAMETER OF 2.750' NO SIGN OF ON CORROSION REMAIN SDR SWAA2022031040629Trunnion · corrodedRT MLG FWD TRUNNION LOCATION #4 LOWER I/B INNER FACE SHOWS EVIDENCE OF CORROSION. DOT 82-060. / AT RIGHT MLG FWD TRUNNION FITTING LOCATION #4 LOWER I/B INNER FACE; SPOT FACE INNER SURFACE TO A DEPTH OF 0.041' AND A DIAMETER OF 2.750' NO SIGNS OF CORROSION REMASDR SWAA2022031040630Trunnion · corrodedRT MLG FWD TRUNNION LOCATION #1 O/B UPPER OUTER FACE SHOWS EVIDENCE OF CORROSION. DOT 82-061. / AT RIGHT MLG FWD TRUNNION FITTING LOCATION #1 O/B UPPER OUTER FACE; SPOT-FACED OUTER SURFACE TO A DEPTH OF 0.158' AND A DIAMETER OF 3.00' REAMED UPPER O/B BORE TO ASDR SWAA2022031040631Trunnion · corrodedRT MLG FWD TRUNNION LOCATION #2 UPPER I/B OUTER FACE SHOWS EVIDENCE OF CORROSION. DOT 82-062. / AT RIGHT MLG FWD TRUNNION FITTING LOCATION #2 UPPER I/B OUTER FACE; SPOT-FACED OUTER SURFACE A DEPTH OF 0.185' AND DIAMETER OF 3.00' AND REAMED UPPER I/B BORE TO A SDR SWAA2022031040639Trunnion · corrodedLT MLG FWD TRUNNION LOCATION #2 UPPER I/B OUTER FACE AND BORE SHOWS EVIDENCE OF CORROSION. DOT 82-070 / AT LEFT MLG TRUNNION FIITTING LOCATION#2 I/B OUTER FACE SPOT-FACED AREA DEPTH OF 0.210' AND DIAMETER OF 3.00' AND REAMED UPPER I/B BORE TO A BORE DIAMETEROFSDR SWAA2022031040640Trunnion · corrodedLT MLG FWD TRUNNION LOCATION #3 LOWER O/B OUTER FACE SHOWS EVIDENCE OF CORROSION. DOT 82-071. / AT LEFT MLG FWD TRUNNION FITTING LOCATION #3 LOWER O/B OUTER FACE; SPOT-FACED AREA DEPTH 0.193' AND DIAMETER OF 2.250' AND REAMED LOWER O/B BORE TO A BORE DIAMETER SDR SWAA2022031040641Trunnion · corrodedLT MLG FWD TRUNNION LOCATION #4 LOWER I/B INNER FACE SHOWS EVIDENCE OF CORROSION. DOT 82-072. / AT LEFT MLG TRUNNION FIITTING LOCATION #4 LOWER I/B INNER FACE SPOT FACED AREA TO A DEPTH OF 0.060' AND DIAMETER OF 2.750' NO SIGNS OF CORROSION REMAIN PER B737-700SDR HYIA20190621001Attach Fitting · corrodedWHILE PERFORMING SPECIAL INSPECTION 402-22 PER INSPECTION PROGRAM MANUAL, AND MAINTENANCE MANUAL 5-20-01, CORROSION WAS VISUALLY IDENTIFIED ON THE LEFT WING'S, FORWARD SPAR'S, LOWER, AFT, WING FITTING. THIS CORROSION IS ON THE LOWER HORIZONTAL FLANGE OF THE FSDR A6WA2019062646678Bracket · crackedBRACKET BETWEEN TH INBD LE AND CENTER LE CRACKED. REPLACEDSDR CA190603010Attach Angle · cracked(CAN) UPPER ATTACH ANGLE FOR BATT RIB RHS AT WS48.30 WAS FOUND TO BE CRACKED. (TC# 20190603010)SDR FDEA2019060311196Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM 57-44-08 AND FOUND LOWER BARREL NUT FACE EXCEED LSDR FDEA2019060311195Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE BARREL NUT HOLE SURFACE REWORKED AS PER MD-11 CMM 57-44-08 AND FOUND LOWER AND UPPER BARREL NUT FACESDR DALA2019053103334Bracket · crackedCRACK BRACKET TELECOPIC DUCT OB FIXED LEADING EDGE INBOARD POSITION RT WING (1 EA). REPLACED BRACKET TELESCOPIC DUCT OB FIXED LEADING EDGE INBOARD POSITION RT WING (1E/A) AS PER SRM 51-72-11 AND DRAWING #D57449202000 AND ER/A NO530598 -14MA.SDR SWAA2019060763415Attach Angle · crackedL/H FIXED WING TRAILING EDGE PANEL, BETWEEN #5 AND #6 SPOILERS, LOWER CENTER BULB SEAL ATTACH ANGLE CRACKED. / R&R SEAL RETAINER FITTINGS PER SRM.SDR SWAA2019061333702Stiffener · crackedL/H WING INBOARD FIXED LEADING EDGE UPPER SKIN PANEL STIFFENER CRACKED. / R&R STIFFENER PER SRM.SDR REXA2019051900738Canister · crackedINITIAL INSPECTION : CRACK IN CANISTER, WELDED NR 3 IN STA. WS=148 AT LT MAIN FUEL TANK. (AI) SUMMARY OF NRC 00188: CANISTER WELDED NR 3 IN STA. WS=148 AT LT MAIN FUEL TANK. WAS REPAIRED PER REO 670-57-42-577 REV. --.SDR SIMA20190516005Attach Angle · crackedLEFT UPPER WING TO FUSELAGE FAIRING, LOWER ATTACH ANGLE ON WING JUST FWD OF SPAR 3 HAS A 3/4' CRACK. C/A-REMOVED AND FABRICATED NEW SECTION OF DAMAGED LT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE ON WING JUST FWD OF SPAR III IAW ETN-EM-53-142. 53-142.SDR SIMA20190516004Attach Angle · crackedRIGHT UPPER WING TO FUSELAGE FAIRING, LOWER ATTACH ANGLE ON WING JUST FWD OF SPAR 3 HAS 2 CRACKS. (APPROX. 1" AND 2" IN LENGTH). C/A-RAR DAMAGED SECTION RT UPPER WING TO FUSELAGE FAIRING LOWER ATTACH ANGLE ON WING JUST FWD OF SPAR III IAW ETN-EM-53-142.SDR SWAA2019053133210Support Rod · corrodedRT WING FORWARD ATTACH SUPPORT ROD JUST OUTBOARD OF MAIN LANDING GEAR BEAM FITTING CLEVISES CORRODED. R&R SUPPORT ROD IAW SOPM.SDR SWAA2019053133209Support Rod · corrodedRT WING AFT ATTACH SUPPORT ROD JUST OUTBOARD OF MAIN LANDING GEAR BEAM FITTING CLEVISES CORRODED. R&R SUPPORT ROD IAW SOPM.
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