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 SWAA2022012673312Rib · elongatedRIGHT WING UPPER SHELF PANEL AT INBOARD DEFLECTION RIB ATTACHMENT HOLES ELONGATED. / REPAIRED BEAM PER SRM 57-51-02-2R-1.SDR SWAA2017071114913Attach Angle · crackedLT WING FIXED TRAILING EDGE PANEL AFT OF PYLON VERTICAL BULB SEAL ATTACH ANGLE CRACKED AT LOWER ATTACH POINT. R&R ANGLE IAW SRM.SDR SWAA2017071715097Plate · crackedLT WING WIGGLE PLATE CRACKED AT ORSS 261. R&R WIGGLE PLATE IAW SRM AND DWG.SDR SWAA2017071014886Support Bracket · crackedRT WING FIXED TRAILING EDGE SUPPORT ANGLE BRACKET CRACKED. R & R THE SUPPORT BRACKET IAW SRM AND DWG.SDR SWAA2017071014828Angle · crackedRIGHT WING DEFLECTOR RIB INTERCOSTAL, L ANGLE CRACKED. R & R THE ANGLE IAW DWG AND SRM.SDR JJBA20170701006Stiffener · crackedTEE INSTL BLEED AIR PIPE HAS STIFFENER ON RT WING FOUND CRACKED IN A COUPLE OF AREAS. R&R STIFFENER.SDR UIEA2017070301099Web · corrodedCORROSION DAMAGES ON THE WEB, UPPER CHORD AND UPPER STRAP OF RT WING LEADING EDGE.. REPAIRED IAW EI T2017A57M-1451 REV.1. CONDITION CHECK NORMAL.</P>)SDR UIEA2017070301101Structure · corrodedCORROSION CHORD OLES 1549, RT WING L/E COMPT UPPER SIDE. RMV DAMAGE DAMAGE IAW SRM 51-10-02 REV 36. WITHIN ALLOWABLE LIMIT IAW SRM 57-20-10-1A-0 REV.36 AND NDT INSP RESULT REF TO JOB CARD ATTACHING SHEET NO. 007754 3. JOB COMPLETED AND CONDITION CHECK NORSDR UIEA2017070301103Web · corrodedWEB CORRODED ON RT WING L/E COMPT FWD SIDE. REMOVED DAMAGE IAW SRM 51-10-02 REV 36. FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-41-13-1A-1, REV 36.SDR SWAA2022012884619Angle · brokenLEFT WING PANEL 551GB OUTBOARD ATTACH ANGLE BROKEN AT FORWARD ATTACH POINT. / REMOVED AND REPLACED LEFT WING PANEL 551GB OUTBOARD ATTACH CNGLE IAW SRM 51-40-02 AND DWG 115A2001 REV -SDR SWAA2022012884621Bracket · crackedRIGHT RING ROOT AT UPPER SUPPORT BRACKET CRACKED AT REAR SPAR ATTACH POINT. / REMOVED + REPLACED SUPPORT BRACKET AT REAR SPUR ATTACH POINT IAW SRM 51-40-02 + DWG#115A2000 REV BSDR A6WA2017071045085Shroud · crackedRIGHT WING OTBD SHROUD CRACKED ON OTBD LEADING EDGE. REPLACED THE SHROUD IAW SRM 51-40-11, AND 51-42-13.SDR SWAA2022012884592Angle · crackedLEFT WING MIDSPAN FIXED UPPER TRAILING EDGE PANEL BULB SEAL ATTACH ANGLE AFT OF LATERAL WEB IS CRACKED / REMOVED AND REPLACED CRACKED UPPER TRAILING EDGE PANEL BULB SEAL ATTACH ANGLE IAW SRM 51-40-02-0G-0 AND BOEING DWG 115A2930 AND APPLIED CIC IAW AMM 51-21-9SDR SWAA2022012886565Beam · elongatedRT WING UPPER TRAILING EDGE SKIN PANEL OB SUPPORT BEAM BOLT HOLES TO DEFLECTION CONTROL TAB ARE ELONGATED. / REPAIRED PER SRM.57-51-02SDR SWIA201743595Channel · corrodedCHANNEL ALONG THE LT WING AFT SPAR CORRODED. REMOVED AND REPLACED THE CHANNEL IAW SRM.SDR SWIA201743594Channel · corrodedCHANNEL ALONG THE RT WING AFT SPAR CORRODED. REMOVED AND REPLACED THE CHANNEL IAW SRM.SDR FQAR20170628062Channel · crackedA CHANNEL IN THE LEFT WING WAS FOUND CRACKED. THE CHANNEL IS LOCATED INBOARD ON THE WING'S LOWER SURFACE AND IS RIVETED TO SKIN PANEL.SDR FDEA201706271774Angle · crackedRIGHT WING SLAT DRIVE PANEL OTBD ANGLE IS CRACKED IN 2 PLACES. REMOVED AND REPLACED IAW SRM 51-31-01,VOL 2, AND DWG ARB2918.SDR DALA2017062805059Web · crackedDURING INSPECTION, FOUND THE LEFT WING AFT TRAILING EDGE PANEL, AFT OF PYLON, SUPPORT WEB CRACKED AT THE OTBD UPPER ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE LT WING T/E PANEL SUPPORT WEB IAW DWG 115A2156, REV D, AND 115A2512, REV B.SDR FQAR20170626059Stiffener · crackedDURING ROUTINE INSPECTION A STIFFENER ON THE LEFT WING UPPER AFT SKIN NEAR ROOT WAS FOUND CRACKED THROUGH INBOARD MOST RIVET HOLE.SDR FQAR20170626058Channel · crackedA CHANNEL IN RIGHT WING WAS FOUND CRACKED. THE CHANNEL IS LOCATED ON LOWER WING SKIN EXTENDING FROM ROOT TO APPROX WS 48 AND IS PART OF THE WING SKIN ASSY. CRACKS WERE LOCATED ON THE OTBD END OF CHANNEL AROUND RIVET HOLE.SDR SWAA2017071715071Fitting · crackedRT WING UPPER AFT WING TO BODY PANEL SUPPORT BEAM FORWARD CLIP CRACKED. R&R CLIP IAW SRM.SDR SWAA2017071214968Fitting · crackedLT WING UPPER AFT WING TO BODY PANEL SUPPORT BEAM FORWARD CLIP CRACKED. R&R CLIP IAW SRM.SDR FQAR20170623055Channel · crackedA CHANNEL IN RIGHT WING WAS FOUND CRACKED. CHANNEL IS LOCATED ON LOWER WING SKIN EXTENDING FROM ROOT TO APPROX WS 48. CRACKS WERE LOCATED ON THE OTBD END OF CHANNEL AROUND RIVET HOLE.SDR SWAA2022012782909Fairing · elongatedFWD FLAP FAIRINGS 544AB; 543AB; AND 644AB HAS EXPOSED COMPOSITES AND ELONGATED FASTENER HOLES AS MARKED. / REPAIRED FWD FLAP FAIRINGS 544AB; 543AB AND 644 IAW SRM 51-70-081 PAR R3 (C-F) REV 61 AND AMM 51-21-99-300-801 PAR E (6) REV 62.07SDR SWAA2017071715070Angle · crackedRT WING UPPER FIXED TRAILING EDGE PANEL ANGLE CRACKED. R&R ANGLE IAW SRM.SDR IPXA2017063018786Stiffener · crackedINSPECTION TYPE: 3C, RT WING FUEL ACCESS PANEL 634CT INTERNAL STIFFNER ANGLE IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE STIFFNER ANGLE IAW DWG ARB0358, SRM 51-35-01, AND 51-33-01.SDR SWAA2022012708184Bracket · crackedRT WING-FIXED UPPER TRAILING EDGE PANEL (BETWEEN INBOARD GROUND SPOILER CUTOUT AND FLIGHT SPOILER PANEL CUTOUT) HAS AFT WEB SEAL ASSY BRACKET CRACKED AT FASTENER HOLE. / REMOVED AND REPLACED AFT WEB SEAL BRACKET ASSY PER SRM 51-40-02.SDR SWAA2022012718252Retainer Seal · crackedLT WING FIXED TE; UPPER PANEL AFT BULB SEAL RETAINER ANGLE CRACKED; JUST AFT OF PYLON APPROX. ORSS 270; MARKED / REMOVED AND REPLACED LT WING FIXED TE; UPPER PANEL AFT BULB SEAL RETAINER ANGLE; JUST AFT OF PYLON APPROX. ORSS 270; ITEM 115A2930-7 PO# 635993 IAWSDR SWAA2017072515267Plate · crackedLT WING FIXED TRAILING EDGE LOWER WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM.SDR SWAA2022012782792Bracket · crackedLEFT WING; SUPPORT BRACKET FOR UPPER WING TO BODY FAIRING PANEL 195AL; IS CRACKED AT LOWER FASTENER.(STREAMERED) / REMOVED AND REPLACED SUPPORT BRACKET ON LEFT WING; UPPER WING TO BODY FAIRING PANEL 195AL IAW BAC DRAWING 116A3118; REV B AND B737 SRM 51-40-02-0SDR SWAA2022012783587Web · cracked(RIGHT WING) TRANSVERSE WEB IS CRACKED AT O/B END UPPER LEG JUST I/B OF PROGRAM ROLLER SUPPORT ARM ATTACH POINT / REMOVED AND REPLACED TRANSVERSE WEB FITTING OF O/B END AND I/B OF PROGRAM ROLLER ARM SUPPORT IAW SOPM 20-50-01 84036 22JUN17SDR SWAA2022012783588Angle · cracked(RIGHT WING) UPPER T/E SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT ABOVE #2 PYLON AFT TIP / REMOVED AND REPLACED UPPER T/E SUPPORT ANGLE AT THE TRANSVERSE WEB ABOVE #2 PYLON IAW SOPM 20-50-01 84036 24JUN17SDR SWAA2022012783589Angle · cracked(RIGHT WING) T/E COVE SEAL SUPPORT ANGLE CRACKED ABOVE #2 PYLON AFT TIP / REMOVED AND REPLACED T/E CORE SEAL SUPPORT ANGLE ABOVE #2 PYLON AFT TIP IAW SRM 51-40-02-0G-0 84036_24JUN17SDR SWAA2022012783590Angle · cracked(RIGHT WING) UPPER T/E PANEL U SUPPORT BEAM TO REAR SPAR ATTACH ANGLE IS CRACKED; RSS80 / REMOVED RT WING UPPER TE PANEL U SUPPORT BEAM TO SPAR ATTACH CLIP IAW SRM 51-40-02 56790 06/21/17 3074 C 21JUN17 INSTALLED A NEW T/E PANEL U SUPPORT BEAM TO SPAR ATTACH CSDR SWAA2022012701236Beam · elongatedTOP OF WING T/E PANEL ATTACH POINT TO GUIDE ARM HAS ELONGATED MOUNT BOLT HOLES; R/H WING APPROX. RSS 284; AFT OF R/H ENG PYLON SAIL FIN / REPAIRED TOP OF WING T/E PANEL ATTACH POINT TO GUIDE ARM ELONGATED MOUNT BOLT HOLES. RIGHT WING RSS289; AFT OF R/H ENG PYLSDR SWAA2022012701241Bracket · crackedI/B ATTACH BRACKET CRACKED; FOR I/B AUX TRACK ON #8 L/E SLAT; WHERE TRACK ATTACHES TO LOWER SEAL PLATE / REMOVED AND REPLACED #8 L/E SLAT; I/B AUX TRACK LOWER SEAL PLATE I/B ATTACH BRACKET IAW SOPM 20-50-01SDR IPXA2017071319258Tee Fitting · crackedINSPECTION TYPE: 3C, RIGHT WING T/E SUPPORT TEE CRACKED NEAR OPENING FOR PANEL 641BB. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT TEE IAW DWG ARC0341, AND SRM 51-33-01.SDR SWAA2017071014834Angle · crackedLEFT WING UPPER TRAILING EDGE PANEL LOWER SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT. R & R THE ANGLE IAW SRM.SDR SWAA2017070514765Plate · crackedLT WING LOWER TRAILING EDGE SKIN AT AFT SPAR WIGGLE PLATE ABOVE NR 3 FLAP TRACK CRACKED. R&R WIGGLE PLATE IAW SRM.SDR SWAA2017070514764Plate · crackedLT WING LOWER TRAILING EDGE SKIN AT AFT SPAR WIGGLE PLATE INBOARD OF NR 3 FLAP TRACK CRACKED. R&R WIGGLE PLATE IAW SRM.SDR SWAA2022012640188Panel · delaminatedLEFT WING PANEL 551FB HAS AREA OF DELAMINATION (MARKED) / REPAIRED AREA OF DELAMINATION ON LEFT WING PANEL 551FB IAW SRM 57-51-01-2R-1 AND IAW SRM 51-70-05-2R-2.SDR SWAA2022012612852Web · crackedL/W DEFLECTION RIB PANEL TRANSVERSE WEB IS CRACK. INSUFFICIENT REFERENCE USED TO INSTALL WEB ATS377INSP 01JUL17 / REMOVED AND REPLACED TRANSVERSE WEB L/W DEFLECTION RIB PANEL TRANSVERSE WEB. PER SRM 51-40-02-0G 898134 07-01-17 PER DRAWING 115A2156 PER SRM 51-2SDR FQAR20170619049Angle · crackedDURING A ROUTINE INSPECTION, AN ANGLE IN THE RIGHT WING THAT IS CO-LOCATED WITH THE OUTBOARD FLAP MOUNTING BRACKET WAS FOUND TO BE CRACKED THROUGH THE RIVETS.SDR SWAA2022012640185Bracket · brokenLEFT WING PANEL 551FB ATTACH BRACKET BROKEN (MARKED) / INSTALLED NEW BRACKET ON 551FB PANEL IAW SRM 51-40-02 80116U 6-23-17SDR SWAA2022012601184Bracket · elongatedTOP OF L/H WING T/E PANEL ATTACH BRACKET MOUNT HOLES ARE ELONGATED; RSS 272; JUST I/B OF #5 SPOILER / REPAIRED TOP OF L/H WING T/E PANEL ATTACH BRACKET MOUNT HOLES AT RSS 272 JUST I/B OF #5 SPOILER IAW SRM 57-51-02-2R-4 REPAIR 4.SDR FQAR20170615048Angle · crackedDURING A ROUTINE INSPECTION, AN ANGLE IN THE RIGHT WING THAT IS CO-LOCATED WITH THE OUTBOARD FLAP MOUNTING BRACKET WAS FOUND TO BE CRACKED THROUGH THE RIVETS.SDR SWAA2022012646283Bracket · crackedSUPPORT BRACKET IN RWW JUST I/B AND ABOVE OF THE #2 TANK AFT BOOST PUMP IS CRACKED. / R&R'ED BRACKET IAW SRM 51-40-02SDR FDEA201706141639Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 789 DOUBLER FOUND CRACKED. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G, DRAWING ARB3954, REV K, AND SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR KO0R201706140030Support · corrodedLEFT WING LEADING EDGE PANEL SUPPORT HAS CORROSION AT WING STATION 445 LEADING EDGE UPPER
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