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 HYIA20191114001Fitting · corrodedDURING MAINTENANCE AN AREA OF CORROSION WAS VISUALLY IDENTIFIED ON THE TOP FACE OF THE LOWER LEG OF THE FORWARD LEFT HAND LOWER AFT WING FITTING (P/N: 0822550-43) THIS CORROSION MEASURES APPROXIMATELY .600 INCHES LONG, AND .473 INCHES WIDE WITH A MAX DEPTH OF SDR SWAA2022040828737Panel · crackedWING PANEL 621FB I/B FWD CORNER FASTENER HOLE IS CRACKED / WING PANEL 621FB I/B FWD CORNER FASTENER HOLE CRACK REPAIRED IAW SRM 57-41-01-2R-1 TABLE 202 AND IAW SRM 51-70-05-2R-9. DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4A(2)(A). DAMAGE EXCEEDSDR SIMA2019112911006Attach Fitting · crackedLH WINGTIP IS CRACKED SPAR I ATTACHMENT FITTING. INSIDE 551AB-C/A-REMOVED AND REPLACED LH WINGTIP SPAR 1 ATTACHMENT FITTING IAW ENVOY ERS-EJ-57MR-1151 PART ASDR SIMA2019112911005Attach Fitting · crackedRH WINGTIP IS CRACKED SPAR I ATTACHMENT FITTING INSIDE PANEL 651AB-C/A-REMOVED AND REPLACED R/H WINGTIP SPAR1 ATTACHMENT FITTING IAW ENVOY ERS-EJ-57MR-1151 PART B.SDR SWAA2022040566445Panel · crackedRW PANEL 651 GB HAS A CRACK ON FWD O/B SIDE OF BRACKET MARKED IN RED. / DAMAGED BRACKET TO RW PANEL 651GB REMOVED AND REPLACED NEW IAW B-737 SRM 51-40-02-0G-0. NEW PART FASTENER LOCATIONS LOCATED AND DRILLED IAW B-737 SRM 51-40-05-0G-0; SRM 51-40-06-0G-0; & 51SDR SWAA2022040566427Panel · delaminatedRT WING; LWR L/E PANEL 621DB HAS THREE CORNERS DELAMINATED. / VERIFIED NEW PART #116A9110Y30 FOR RIGHT WING; LOWER L/E PANEL 621DB; ATAG# FT2584. LOCATED; DRILLED; COUNTERSUNK NEW FASTENER LOCATIONS IN BLANK PANEL IAW SRM 51-40-05-0G-0 AND SRM 51-40-08-0G-0SDR SWIA2019123147514Bolt · corroded* LEFT WING OUTBOARD GROUND SPOILER PCU ATTACHMENT POINTS HAVE CORRODED / MOUNTING HARDWARE. BOLT, NUT, AND WASHER. (C-CHECK) RO 12/27/2019 REMOVED AND REPLACED LEFT WING OTBD GROUND SPOILER PCU MOUNTING HARDWARE AS REQ REF CRJ200 AMM. RIG CHECK AND OPS CHESDR SWIA2019123147513Nut · corroded* LEFT WING INBOARD GROUND SPOILER PCU ATTACHMENT POINTS HAVE CORRODED / MOUNTING HARDWARE. BOLT, NUT, WASHER. (C-CHECK) RO 12/27/2019 REMOVED AND REPLACED LEFT WING INBD GROUND SPOILER PCU MOUNTING HARDWARE AS REQ REF CRJ200 AMM. RIG CHECK AND OPS CHECK GOOSDR SWIA2019123147512Bolt · corroded* RIGHT WING SPOILERON PCU ATTACHMENT POINTS HAVE CORRODED MOUNTING / HARDWARE. BOLT, NUT, WASHER. (C-CHECK) RO 12/27/2019 REMOVED AND REPLACED R/H SPOLERON PCU HARDWARE REF. CRJ-200 AMM. OP CHECKS GOOD. RIG IS WITHIN LIMITS. SEE ATTACHED CONTINUATION CARD FSDR SWIA2019123147511Washer · corroded* RIGHT WING FLIGHT SPOILER PCU ATTACHMENT POINTS HAVE CORRODED MOUNTING HARDWARE. / BOLT, NUT, WASHER. (C-CHECK) RO 12/27/2019 REMOVED AND REPLACED R/H WING FLIGHT SPOILER PCU UPPER ATTACHMENT POINT HARDWARE REF. CRJ-200 AMM. OP TEST GOOD. SEE ATTACHED CONTSDR SWIA2019123147510Nut · corroded* RIGHT WING OUTBOARD GROUND SPOILER PCU ATTACH POINTS HAVE CORRODED MOUNTING / HARDWARE. BOLT, NUT AND WASHER. (C-CHECK) RO 12/27/2019 REMOVED AND REPLACED R/H WING OTBD GROUND SPOILER PCU MOUNTING HARDWARE REF. CRJ-200 AMM. RIG IS WITHIN LIMITS AND OP TESTSDR SWIA2019123147509Bolt · corroded* RIGHT WING INBD GROUND SPOILER , PCU ATTACH POINTS HAVE CORRODED MOUNTING / HARDWARE. BOLT, WASHER , NUT. (C-CHECK) RO 12/27/2019 REMOVED AND REPLACED R/H WING INBD GROUND SPOILER PCU ATTACH POINT HARDWARE REF. CRJ-200 AMM. OP TEST GOOD.SDR SWIA2019122747303Attach Bracket · chafedR/H WING INBD WING TRAILING EDGE STUB FAIRING ATTACH BRACKET IS CHAFED/WORN BEYOND LIMITS AT WS 48. (C-CHECK) RO:12/24/2019REMOVED AND REPLACED R/H STUB FAIRING BRACKET P/N 6701R10371-2 IAW CRJ SRMSDR SWIA2019122747390Link · corrodedR/H OUTBD. GROUND SPOILER ACTUATOR LINK (LWR.) AND BOLT RUSTED AND WORN. INSTALLED NEW GRND ACTUATOR LINK AND ATTACHING HARDWARE FOR R/H OTBD GRND SPOILER ACTUATOR REF CRJ-200 AMM OPS CHECK GOOD.SDR SWIA2019122747389Link · corrodedR/H INBD GROUND SPOILER ACTUATOR LINK (LWR.) AND BOLT RUSTED AND WORN (C-CHECK) RO:12/24/2019 INSTALLED NEW GRND ACTUATOR LINK AND ATTACHING HARDWARE FOR R/H INBD GRND SPOILER ACTUATOR REF CRJ-200 AMM OPS CHECK GOOD.SDR SWIA2019122747388Fitting · dentedOUTBD. OF R/H W.S. 148.019 FLAPGUIDE FITTING AT REAR SPAR DETENTED FROM - ALSO WORN FLAP GUIDE BEARING. REMOVED DAMAGED GUIDE FITTING AND INSTALLED NEW FITTING P/N 601R10156-2 PO: T52766 AND FLAP CAM FOLLOWER AT R/H OUTBOARD FLAP W.S 148.019. REF. SRM.SDR SWIA2019122747386Link · corrodedL/H OUTBD. GROUND SPOILER ACTUATOR LINK (LWR) AND BOLT RUSTED AND WORN (C-CHECK) RO:12/24/2019 INSTALLED NEW GRND ACTUATOR LINK AND ATTACHING HARDWARE FOR L/H OTBD GRND SPOILER ACTUATOR REF CRJ-200 AMM, OPS CHECK GOOD.SDR SWIA2019122747385Link · corrodedL/H INBD GROUND SPOILER ACTUATOR LINK(LWR.) AND BOLT RUSTED AND WORN ATTACHING TO SPOILER (C-CHECK) RO:12/24/2019 REMOVED AND INSTALLED NEW L/H INBD GROUND SPOILER ACTUATOR LINK WITH NEW HARDWARE REF CRJ-200-AMM AND CRJ-200-AMM OP CHECKS GOOD AND SEESDR SWAA2019111438825Attach Angle · crackedINBOARD OF L/H WING DEFLECTION RIB BULKHEAD ATTACH ANGLE CRACKED. / R&R ATTACH ANGLE PER SRM AND DWG.SDR REXA2019112601665Canister · crackedINITIAL INSPECTION. CRACK ON SLAT TRACK CANISTER 1-3 INSIDE LH WING MAIN FUEL TANK WS 148. (SM)(AD).
SUMMARY: SLAT TRACK CANISTER 1-3 INSIDE LH WING MAIN FUEL TANK WS 148 WAS REPAIRED PER REO 670-57-42-577 REV.-SDR V0XD20191103005Mount · crackedLEFT WING 1-3 SLAT TRACK CANISTER AFT MOUNT BRACKETS CRACKED AT BASE, REPAIRED THE MOUNT IAW REO 670-57-42-577.SDR SWAA2019102838259Attach Angle · crackedR/H WING TRAILING EDGE PANEL 651FB, 28" FROM OUTBOARD END ATTACH ANGLE CRACKED COMMON TO FORWARD BULB SEAL RETAINER. / R&R ANGLE IAW / MR.SDR HKGA20191022010Shear Tie · crackedFOUND CRACKED SHEAR TIE WHILE INSTALLING DOUBLER AT LH WING FUEL TANK RIB 21 FWD OF THE AFT STIFFENER. INSTALLED NEW SHEAR TIE (REF EMB120 SRM 51-40-02 REV 58)SDR HKGA20191022009Shear Tie · crackedLH WING RIB 15 2ND FROM THE FWD SHEAR TIE IS CRACKED. INSTALLED NEW SHEAR TIE (REF EMB120 SRM 51-40-02 REV 58)SDR HKGA20191022008Shear Tie · crackedLH WING RIB 15 2ND FROM THE AFT SHEAR TIE IS CRACKED. INSTALLED NEW SHEAR TIE (REF EMB120 SRM 51-40-02 REV 58).SDR HKGA20191022007Shear Tie · crackedLH WING RIB 16 2ND FROM THE AFT SHEAR TIE IS CRACKED. INSTALLED NEW SHEAR TIE (REF EMB120 SRM 51-40-02 REV 58)SDR HKGA20191022005Shear Tie · crackedLH WING INTERNAL RIB 19 AFT MOST UPPER SKIN TO RIB SHEAR CLIP IS CRACKED. INSTALLED NEW SHEAR TIE (REF EMB120 SRM 51-40-02 REV 58)SDR HKGA20191022004Shear Tie · crackedLH WING INTERNAL RIB 19, 3RD UPPER SKIN TO RIB SHEAR CLIP FROM FRONT SPAR IS CRACKED. INSTALLED NEW SHEAR CLIP (REF EMB120 SRM 51-40-02 REV 58).SDR HKGA20191022003Shear Tie · crackedLH WING INTERNAL RIB 19 FWD MOST UPPER SKIN TO RIB SHEAR CLIP IS CRACKED. INSTALLED NEW SHEAR CLIP (REF EMB120 SRM 51-40-02 REV 58)SDR IPXA2019102308072Tee Fitting · corrodedINSPECTION TYPE:N/A**SDR FILED OPEN** RIGHT WING AUX SPAR UPPER T-CHORD WBL 235.2 CORRODED AT INBD END. REPAIRED IAW EO B747-5710-74368-A. DEFERRED DUE TO PERMANENT REPAIR BY NEXT C CHECK NOT TO EXCEED 24 MONTHS.SDR FDEA2019101762670Support · corrodedRIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING C MOUNT HOLE FOUND WITH CORROSION RIGHT HAND OUTBOARD FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50- 32-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-32-5. REFER SNRM N005SDR FDEA201910162669Fitting · corrodedRIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING E MOUNT HOLE FOUND WITH CORROSION RIGHT HAND OUTBOARD FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50- 32-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-32-5. REFER SNRM N005SDR FDEA2019101762668Fitting · corrodedRIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING B MOUNT HOLE FOUND WITH CORROSION RIGHT HAND OUTBOARD FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50- 32-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-32-5. REFER SNRM N005SDR FDEA201910162667Fitting · corrodedLEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'F' MOUNT HOLE FOUND WITH CORROSION CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING 'F' MOUNT HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-20-02-2R REPAIR 5 FIGURE 201. OSDR SWAA2022040593431Panel · crackedFOUND WING PANEL 621YB WITH A CRACK ON FWD O/B EDGE AROX 1IN. LING ON EDGE OF COUNTERSINK APROX .350 FROM END OF PANEL / (PER CLOSING DMA 0088116) CLEARING #98045 REMOVED AND REPLACED PANEL 621YB IAW M/M 57-41-02.SDR HYIA20191014001Fitting · corrodedWHILE PERFORMING SPECIAL INSPECTION 402-22 IAW INSPECTION PROGRAM MANUAL, AND MM 5-20-01, CORROSION WAS VISUALLY IDENTIFIED ON THE LEFT WING'S, FORWARD SPAR'S, UPPER, AFT, WING FITTING (P/N 082255-45). THIS CORROSION IS ON THE UPPER HORIZONTAL FLANGE OF THE FISDR SWAA2022040594407Panel · crackedR/H WING L/E PANEL 621PB (116A9110Y40) HAS A CRACK AT L/E FASTENER HOLE GOING 1.75' ALONG FORWARD EDGE OF PANEL. / CLOSING DMA # 0506509 R+R L/E PANEL 621PB PER SMM 51-40-02 CL# 96984SDR FDEA2019101102584Attach Angle · corrodedL/W L/E PNL ATTACH STRUCTURE AT STA 532 HAS INTERGRANULAR CORROSION REMOVED AND REPLACED ANGLE PER B757 SRM 51-40-02 AND DWG #114N2151SDR FDEA2019101102583Attach Angle · corrodedLEFT WING L/E PANEL ATTACH ANGLE AT WS 478 HAD INTERGRANULAR CORROSION. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-40-02, AND DWG 114N2151.SDR HKGA201910108023Attach Angle · chafedRH WING LEADING EDGE ATTACH ANGLE RIB AT INBOARD SIDE OF NACELLE IS CHAFED IN MULTIPLE AREAS. LOCATED AND DRILLED NEW ATTACH ANGLE AND INSTALLED NUTPLATES (IAW EMB120 SRM 51-40-02 REV 58). INSTALLED NEW L/E ATTACH ANGLE (IAW EMB120 SRM 51-40-02 REV 58).SDR DALA2019100905813Bracket · crackedCRACK BRACKET TELESCOPIC DUCT OB FIXED LEADING EDGE ON LH WING ( 1EA). REPLACED BRACKET TELESCOPIC DUCT OB FIXED LEADING EDGE ON LH WING AS PER A319 SRM 51-42-11 AND DWG D57449202 ISSUE F RELEASE DATE:11-SEP-18 AND ENGINEERING REPAIR AUTORIZATION NO.530598-14 SDR DALA2019100905812Bracket · crackedCRACK BRACKET TELECOPIC DUCT IB SIDE FIXED LEADING EDGE RH WING. REPLACED BRACKET TELESCOPIC DUCT IB SIDE FIXED LEADING EDGE RH WING AS PER A319 SRM 51-42-11 AND ERA 530598-14MA.SDR IPXA2019102104877Skin · crackedINSPECTION TYPE:2CL/H WING L/E LOWER SKIN IS CRACKED AT STA. XOS.=717.REPAIRED CRACKED L/H WING L/E SKIN AT STA. XOS.=717 IAW SRM 57-40-02 REPAIR 7 FIG. 201. (MAJOR)SDR IPXA2019100747634Attach Bracket · crackedWHILE REMOVING FUEL VENT LINE IN ACCESS HOLE 560AB, FOUND ATTACH BRACKET CRACKED. REMOVED AND REPLACED THE ATTACH ANGLE IAW DWG A57140632 & SRM 51-40-21.SDR SWAA2019100837613Trunnion · corrodedR/H MAIN LANDING GEAR FORWARD TRUNNION FITTING LOWER INBOARD LUG OUTER FACE CORRODED. REPAIRED LUG PER EA.SDR IPXA2019103098458Bracket · crackedINSPECTION TYPE:SEGL/WING REAR SPAR AREA, INBD & BELOW #3 SPOILER, L-BRACKET CRACKEDREMOVED, FABRICATED ON MAE TRAVELER T19/1450716, INSTALLED IAW SRM 51-40-21SDR EBV220191002001Attach Fitting · crackedFOUND CRACK IN RH AUXILIARY WING SPAR INBOARD ATTACH FITTING. LOCATED ON AFT CLOSEOUT OF RH MLG WHEEL WELL AT FS446.38. CRACK EXTENDS FROM BOLT HOLE TO BOLT HOLE THROUGH WEB IN FITTING. FOUND BY VISUAL INSPECTION DURING SCHEDULED MAINTENANCE.SDR SWIA2019101846530Bracket · crackedL/H WHEEL WELL FWD HYD FUSE BRACKET IS CRACKED. (C-CHECK) RO: 10/16/2019 RREMOVED UNSERVICEABLE L/H WHEEL WELL FWD HYD FUSE BRACKET IAW SRM. INSTALLED NEW SERVICEABLE L/H WHEEL WELL FWD HYD FUSE BRACKET IAW SRM.SDR SWIA2019101846529Rib · crackedL/H MLG BATT RIB IS CRACKED AT W.S. 53.60. (C-CHECK) RO: 10/16/2019 REPAIRED LH MLG BATT RIB AT WS 53.6 IAW REO.SDR SWIA2019101846527Bracket · crackedR/H MLG WHEEL WELL AFT HYD FUSE BRACKET IS CRACKED. (C-CHECK) RO: 10/16/2019REMOVED AND REPLACED BRACKET IAW SRM.
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