JASC 5720
Service difficulty reports · 13,638
Reports filed under 5720 · Wing Miscellaneous Structure, 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 = '5720' 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 = '5720' 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 IPXA09M55750Doubler · gougedINSPECTION TYPE:2C REPAIR SURVEY SEQ 286-W4-11, EXISTING REPAIR DOUBLER ON RT WING FIXED L/E BETWEEN XOS 1164-1171 HAS A GOUGE. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-10-00 FIG 7 SHEET 1-3.SDR IPXA09M55918Doubler · crackedINSPECTION TYPE:2C LT WING L/E BEADED DOUBLER XFS 681 CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, ANGLE AND DOUBLER IAW MD-11 SRM 57-10-00 FIG 27 SHEET 1-4.SDR IPXA09B55834Mount Bracket · crackedINSPECTION TYPE:D RT WING - ILES 344 L/E FAIRING UPPER SUPPORT RIB AFT MOUNT BRACKET FOUND CRACKED. RT WING - ILES 344 L/E FAIRING UPPER SUPPORT RIB AFT MOUNT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 11.SDR IPXA09B55833Support · crackedINSPECTION TYPE:D LT WING - ILES 344 L/E FAIRING UPPER SUPPORT RIB AFT MOUNT BRACKET FOUND CRACKED. LT WING - ILES 344 L/E FAIRING UPPER SUPPORT RIB AFT MOUNT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 11.SDR IPXA09B55832Rib · crackedINSPECTION TYPE:D RT WING GEAR W/W TRIANGLE PANEL I/B RIB FWD BRACKET FOUND CRACKED. RT WING GEAR W/W TRIANGLE PANEL I/B RIB FWD BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 11.SDR 2009FA0000377Angle · crackedRT VERTICAL BREATHER ANGLE CRACKED AFT OF RT MAIN LANDING GEAR. (K)SDR IPXA09M55616Cap · erodedRT UPPER WINGLET CAP HAS EROSION. REPAIRED IAW EO MD11-5720-32859-A.SDR CALA2009042100210Stiffener · gougedLEADING EDGE SUPPORT ANGLE ATTACHED TO FRONT SPAR WORN INTO BY SUPPORT CHANNEL FOR ANTI-ICE DUCT LOCATED BEHIND AUX TRACK FOR NR 5 SLAT. FABRICATED AND REPLACED STIFFENER REF ECRA 5710-02161. ACCOMPLISH A PERMANENT REPAIR WITHIN 12 MONTHS OF 04/13/2009. PLASDR FDEA200904201340Shroud · corrodedCORROSION ON OUTER SHROUD BOX RT REPAIR PERFORMED IAW EA 6-5720-120231 AND RAS/BAE/1009111/2008.SDR FDEA200904201337Shroud · delaminatedDAMAGE ON OUTER SHROUD BOX LT WING REPAIR PERFORMED IAW EA 6-5750-120235 AND RAS/BAE/1009297/2009.SDR UALA2009041501092Doubler · wornWING T/E DOUBLER AT AFT END OF PYLON WHERE HYD LINES GO THRU BOTTOM OF WING, DOUBLER COMPLETELY WORN THRU AT HYD LINE FLANGE ATTACH BOLTS. REPAIR ACP PER EVA 72495.SDR ASAA0995115Bracket · crackedRT WING FIXED T/E AFT AIR DAM BRACKET CRACKED RSS 261. REMOVED CRACKED AND INSTALLED NEW BRACKET PER SRM 51 40 02.SDR WRLA2009116Channel · crackedDURING C-CHK IN TPE INSPECTION FOUND THE RIGHT WING FUEL ACCESS CHANNEL CRACKED AT F/ACCESS PNL 633AT, 634BT, 636AB, 636BB, 636CB, & 638DB (REF EGAT NRC U05081). REPLACED THE DAMAGED CHANNELS AND RUB STRIP AT F/ACCESS PNLS 633AT, 634BT, 636AB, 636BB, 636CB, SDR UALA2009041301057Stiffener · damagedRT WG CTR R SPAR STIFFENER RT. ACP'D COA 930033 ON 4-10-2009. REPAIR NR 3 ACP'D. RPR INSTALLED AND CLEARED COA 930033. REPAIR REQ PERMANENT REPAIR AT OR BEFORE 15000C.SDR UALA2009041301050Stiffener · crackedRT MLG WW FWD BULKHEAD VERT STIFFENER AT 6.15 RBL CRACKED AT WING LOWER CHORD ANGLE. MAJOR REPAIR ACCOMPLISHED: VERTICAL STIFFNER REPAIRED PER MM 57-12-96 FIG 401 RPR 3 AND BOEING DRAWING LOR-760.SDR IPXA09555593Plate · crackedINSPECTION TYPE:C2 CRACKED WIGGLE PLATE STA 330.0 R/W. REPLACED PER B757-5750-5622-A.SDR UALA2009040801019Structure · leakingFUEL LEAKING FROM NR 1 ENGINE PYLON SKATE SUPPORT AREA. FUEL LEAKING IN THE ENCLOSED AREA OF PYLON ABOVE THE AFT SUPPORT STRUT. APPEARS TO BE COMING FROM FASTENERS THRU THE STRUT SUPPORT STRUCTURE INTO THE WING. LOCATED LEAK. SEALED WITH A1-2 AND B1-2 AT 1SDR ASOA200900393Intercostal · crackedINTERCOSTAL AT WS 130 ON LT WING HAS A CRACK.SDR FDEA200904061203Support · crackedRIGHT WING T/E SUPPORT IS CRACKED ABOVE RIB 9. REMOVED FASTENERS AND BUTT STRAP IAW SRM 51-40-21; PG 22. LOCATED AND DRILLED NEW BUTT STRAP IAW SRM 51-40-21; PARA 7 AND SRM 51-40-44; PARA 3. INSTALLED BUTT STRAP IAW SRM 51-40-21; PARA 7. OPENED AND CLOSED SDR FDEA200904061202Support · crackedRIGHT WING T/E UPPER PANEL SUPPORT PLATE IS CRACKED AT RIB 9. REMOVED SUPPORT PLATE IAW SRM 51-40-21; PG 22. FORMED A NEW SUPPORT PLATE IAW DWG A57242294; MOD "B". HEAT TREATED NEW SUPPORT PLATE IAW TPS 1003, REV "A". ALODINED, PRIMED AND PAINTED NEW SDR FDEA200904061201Intercostal · crackedRIGHT WING T/E SUPPORT INTERCOSTAL IS CRACKED ABOVE THE NR 4 FLAP BEAM; RIB 16. REMOVED PANEL SUPPORT IAW SRM 51-40-21; PARA 6 AND 7. FORMED A NEW SUPPORT REF DWG A57240194; ISSUE "A". ALODINED AND PRIMED IAW SRM 51-2110 PARA 2-B AND SRM 51-23-20; PG 23. SDR WRLA2009090Doubler · crackedDURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON THE DB DOUBLER FASTENER AREA OF THE LEFT WING OUTBOARD FIXED CAVITY AT STA XOS627 (REF EGAT N/R U05035). REPAIR THIS CRACKED AREA B PER MD-11 SRM 57-00-01 VOL 1 FIG 10 REV 40. PERFORM ET INSPECTION FOR CUTOUSDR SWIA200922018Web · crackedLEADING EDGE AT 630KL INNER WEB CRACKED. (C CHECK) REPAIRED PER REO.SDR WRLA2009087Stiffener · crackedDURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON ZEE STIFFENERS OF LT WING FIXED L/E UPPER PNL 516ET (REF EGAT N/R U05031). REMOVED THE DAMAGED STIFFENERS (ARB2440-503/503) 2EA PER MD-11 SRM 51-35-01 VOL 2 REV 40. STOP DRILLED WITH 0.25 INCH DIA HOLE AT ENSDR WRLA2009086Stiffener · crackedDURING C3 CHECK IN TPE INSPECTION FOUND: CRACK ON ZEE STIFFENERS OF RT WING FIXED L/E UPPER PNL 616ET (REF EGAT N/R U05027). REMOVED THE DAMAGED STIFFENERS (ARB2440-504/506) 2EA PER MD-11 SRM 51-35-01 VOL 2 REV 40. STOP DRILLED WITH 0.25 INCH DIA HOLE AT ENSDR ASAA0944948Support Angle · crackedLT WING I/B TRAILING NO STEP PANEL O/B SUPPORT ANGLE IS CRACKED. REPLACED SUPPORT ANGLE (FITTING) PER SRM 51 40 02.SDR ASOA200900340Structure · crackedSUSPECT CRACK AT WS 127.25 WHILE C/W TASK CARD 000-57-540-604.SDR ASAA0944897Support Angle · damagedLT WING T/E CAVITY NO STEP PANEL I/B ANGLE AFT FASTENER HOLE IS OUT OF ROUND. REPLACED SUPPORT ANGLE.SDR C8GA20090134ASupport Angle · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE # 6 SLAT I/B & O/B ROD END SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED I/B & O/B RIBS AT # 6 SLAT WS 530. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.SDR AALA20090324TUL02Stiffener · crackedFORWARD END OF RIGHT FOD PANEL ABOVE RIGHT MAIN LANDING GEAR, INBOARD END VERTICAL STIFFENER CRACKED. INSTALLED NEW VERTICAL STIFFENER PER SRM 51-10-01.SDR IPXA09555314Bracket · damagedINSPECTION TYPE:C3 RT WING LOWER T/E PANEL TRUNNION FAIRING HAS 2 FASTENERS LOOSE ON THE I/B EDGE. REMOVED, FABRICATED AND INSTALLED REPLACEMENT BRACKET PER SRM 51-40-02.SDR WRLA2009080Support Bracket · deformedDURING C3 CHECK IN TPE INSPECTION FOUND DEFORM ON THE GND JACKS SUPPORT BRACKET INSIDE OF RT WING FUELING STATION (REF EGAT N/R U05025). REMOVED BRACKET IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED SUPPORT BRACKET IAW EGAT EI W2009P57B-350 REV 00, INSTALLED THISDR WRLA2009079Support Bracket · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON LWR PANEL SUPPORT BRACKET OF RIGHT WING T/E AT STA XOSP465.027 (REF EGAT N/R U05023). REMOVED SUPPORT BRACKET IAW SRM 51-35-01 VOL 2 REV 40, FABRICATED SUPPORT BRACKET IAW EGAT EI W2009P57B-350 REV 00, INSTALLESDR WRLA2009071Seal · crackedDURING C3 CHECK IN TPE INSPECTION FOUND CRACK ON LEFT WING T/E BEAM SEAL LAND Y=1474 Z=-100. REPLACE THIS CRACK SEAL LAND IAW SRM 51-35-01 AND 51-33-01 VOL 2 REV 40, JOB COMPLETED AND CONDITION CHECK NORMAL.SDR DL75E090460Structure · crackedLT DRY BAY HAS 1 INCH CRACK AT TOP CORNER OF BARRIER AND WS 285.65 RIN INBD OF INNER DOOR 532HZ, FOUND DURING DRY BAY LEAK CHECK. C/W AT SAA - SAT ON N/R 119332 JOB 82305140001.SDR IPXA09655176Fitting · crackedINSPECTION TYPE:C LT WING - L/E LES 675 FIXED FAIRING SUPPORT AFT FRONT SPAR CLIP FOUND CRACK. CRACK 0.75 INCH LENGTH. LT WING - L/E LES 675 FIXED FAIRING SUPPORT AFT FRONT SPAR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 43.SDR ASAA0944745Panel · gougedRIGHT WING O/B OF PYLON FAIRING T/E DOGHOUSE HAS DEEP GOUGE AND CHAFING. FABRICATED A REPLACEMENT PANEL AND INSTALLED PER SRM 51 10 02.SDR ASAA0944701Stiffener · crackedSTIFFENER CRACKED AT RT WING IFOT I/B SIDE. REMOVED AND REPLACED STIFFENER.SDR ASAA0944700Stiffener · crackedLT WING AFT INBOARD NO STEP PANEL LWR SURFACE OUTBOARD STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER PER SRM 51 40 02.SDR C2XA09IA072Structure · leakingDURING CRUISE A REPORT OF FUEL LEAKING FROM THE LEFT WING WAS MADE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FULLY FUELED THE WING TANKS HOWEVER A LEAK COULD NOT BE CONFIRMED. THE AIRCRAFT WAS THEN RETURNED TO SERVSDR ASAA0944693Angle · tornANGLE AT RSS 272 WBL 201 IS TORN LT WING. REPLACED ANGLE.SDR XV6A2009030600001Structure · crackedREPETITIVE EDDY CURRENT INSPECTION IAW RAS-328-57-3051 AND AD 2008-10-15.SDR AALA20090317TUL10Attach Fitting · crackedCABLE PULLEY BRACKET ATTACH FITTING CRACKED ON LEFT WING INBOARD OF NR 8 SLAT TRACK. REMOVED AND REPLACED FITTING PER AARD 51-00-00-012.SDR ASAA0954618Retainer · crackedLT WING T/E SEAL RETAINER SUPPORT ANGLE CRACKED. REMOVED AND REPLACED LT WING T/E SEAL RETAINER SUPPORT ANGLE.SDR ASAA0954570Retainer · crackedRIGHT WING TRAILING EDGE BULB SEAL RETAINER CRACKED. REMOVED AND REPLACED RT WING T/E BULB RETAINER.SDR TAMF20090004SSplice Plate · corrodedDURING C3 CHECK INSPECTION, FOUND CORROSION ON THE LOWER SURFACE OF THE UPPER SPLICE PLATE AT STA OSS 460 RH. CORROSION REMOVED AND REPAIRED IAW EWO 767 57-051 AND SR 1-1230329934.SDR FDEA200902270760Angle · crackedLEFT WING T/E BELOW NR 7 SPOILER HAS CRACKED ANGLE AT FALSE SPAR LOWER CHORD. REPAIRED IAW STANDARD REWORK DRAWING SR27-57-038 REV. C.SDR FDEA200902250705Stiffener · crackedFOUND CRACK IN CENTER SPAR CUTOUT IN STIFFENER, C 44, IN HOLE NR 3 REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL AND PERFORMING NDT IAW RAS 70517477/009/2009 ISS A, APPROVED BY EA 6-5710-120225.SDR 2009FA0000117Attach Fitting · misrepairedPREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE RT WING LWR FWD ATTACH FITTING PN 0822550-50 HAD UNAPPROVED STEEL BUSHING INSTALLED UNABLE TO PERFORM NDT INSPECTION. REPLACED WINGSDR 2009FA0000115Attach Fitting · corrodedPREVIOUSLY REPORTED IAW INSTRUCTIONS BY MFG SUPPLEMENTAL INSPECTION DOCUMENTS FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. THE RT WING LWR AFT ATTACH FITTING PN 5011024-2 FAILED NDT INSPECTION. REPLACED WING FITTING.
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