JASC 5720
Service difficulty reports · 13,629
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 SWIA2026030776834Spar · crackedRIGHT FWD SPAR CRACKED BTWN RIBS 22 & 23. FABRICATED AND INSTALLED RT FWD SPAR DOUBLER (REINFORCEMENT) BETWEEN RIBS 22 AND 23 IAW ETD2026-170-004072 REV-. WEIGHT AND BALANCE HAS BEEN AFFECTED: WEIGHT INCREASE: 5LBS, ARM: 71.51, MOMENTS: 357.55*TEMPORARY REPAISDR SWAA2026040786896Panel · corrodedPANEL 632BB HAS MINOR FRETTING CORROSION ON MESH GASKET SURFACE. CLEANED AND FOUND WITHIN LIMITS IAW SRM 57-20-01-1A-1. REPLACED PANEL 632BB; PANEL TO BE INSTALLED ON TASKCARED TTG8Q019MG2T IAW AMM 28-11-11.SDR SWAA2026040779204Gasket · corrodedPANEL 632BB HAS MINOR FRETTING CORROSION ON MESH GASKET SURFACE. CLEANED AND FOUND WITHIN LIMITS IAW SRM 57-20-01-1A-1. REPLACED PANEL 632BB; PANEL TO BE INSTALLED ON TASKCARED TTG8Q019MG2T IAW AMM 28-11-11.SDR IPXA2026032166896Splice Plate · crackedFAULT - RIGHT WING OUTBOARD L/E CAVITY INSE, PANEL SPLICE PLATE CRACK (REPLACE) INSTALLED FABRICATED FRAME I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO 65B11862 SH2 REV.FSDR SWIA2026030577471Support Fitting · gougedLEFT OTBD FLAP HINGE BOX FWD SUPPORT FITTING AT WS 17800 GOUGED. BLENDED GOUGE AT LT OTBD FLAP HINGE BOX FWD SUPPORT FITTING AT WS 17800 IAW SRM 51-12-00-001-001-A01, AND FOUND OUT OF LIMITS. REPAIRED IAW REO 670-57-21-1130 REV --.SDR SWAA2026040176893Angle · crackedLEFT WING TRANSVERSE ANGLE, JUST ABOVE AFT PYLON WAS CRACKED IN RADIUS. REMOVED AND REPLACED THE LT WING TRANSVERSE ANGLE IAW SRM 51-40-02 AND DWG 115A2512, REV B.SDR SWAA2026030976706Support Angle · crackedLEFT WING TRAILING EDGE WEB SUPPORT ANGLE, ATTACHED TO FLAP DEFLECTION RIB AND AFT OF NR 1 ENGINE PYLON CRACKED IN RADIUS. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02.SDR COEA2026072226803Channel · corrodedRT AILERON, MOVEABLE TRIM TAB CLOSEOUT CHANNEL HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED CHANNEL PER ATR72 SRM 51-25-03 REV. 122.SDR IPXA2026031281768Bracket · crackedLEFT WING, ACCESS PANEL 575AB AREA, INNER TOP BRACKET HAS A CRACK. REMOVED BRACKET AT LT WING, ACCESS PANEL 575AB AREA, INNER TOP. IAW SRM-51-40-21. INSTALLED PLATE MOUNTING USING EXISTING FASTENERS, IAW SRM 51-40-21.SDR IPXA2026031383459Bracket · crackedRIGHT WING LEADING EDGE INSIDE THE ACCES PANEL 675AB HYD LNES SUPPORT BRACKET BROKEN. INSTALLED NEW BRACKET-MOUNTING AT RT WING LEADING EDGE INSIDE THE ACCES PANEL 675AB, IAW SRM 51-40-21.SDR IPXA2026030462840Support Bracket · crackedCRACKED BRACKET, LT WING L/E COMPARTMENT TORQUE TUBE SUPPORT BRACKET. INSTALLED NEW BRCKET I.A.W SRM 51-40-02-0G REV. 94 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.SDR COEA2026072225803Strip · corrodedLEFT WING, REAR SPAR STRIP SLAT UPPER SURFACE BETWEEN RIBS 10-13 HAS LEVEL 2 CORROSION AROUND MULTIPLE FASTENER HOLES. CORRECTIVE ACTION: REPAIR PER SRAS-00026288-01 ISSUE A, DATED 6/8/2026.SDR SWAA2026033174646Support Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE AT ORSS 288 AT RT WING. REPLACED SUPPORT BRACKET TRAILING EDGE AT ORSS288 AT RT WING IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, PARAGRAPH 9, AND DWG 115A3712, SHEET 7, REV A.SDR AALA202603258367Intercostal · crackedAIRCRAFT IN BASE MAINTENANCE: INTERCOSTAL CRACKED UNDER UPPER FIXED TE PANEL INBOARD OF NUMBER 5 SPOILER. INSTALLED NEW INTERCOSTAL PANEL NUMBER 1. PER SRM 51-40-02SDR SWAA2026032474776Channel · crackedCRACKED GANG CHANNEL ON THE RT WING, BTWN OSS 207.75 - OSS 227.95. REMOVED THE GANG CHANNEL IAW SRM 51-40-02-0G-0, AND FOR INSTALLATION SEE TTG8Q01AVLUQ.SDR SWAA2026032474777Channel · crackedCRACKED GANG CHANNEL ON RT WING, BTWN OSS 240.95 & OSS 259.98. REMOVED GANG CHANNEL IAW SRM 51-40-02-0G-0 INSTALLATION SEE TTG8Q01AVLUQ.SDR REXA2026042800406Channel · corrodedCORROSION ON SEVERAL CHANNEL NUT BTW WS 148.01 TO WS 48.00 LEFT WING FRONT SPART FORWARD, LOWER SECTION. DUE TO EXCESSIVE CORROSION ON SEVERAL CHANNEL NUT BTW WS 148.01 TO WS 48.00 LEFT WING FRONT SPART FORWARD, LOWER SECTION WERE REPLACED PER CRJ900 SRM 51-10SDR REXA2026042800385Channel · corrodedCORROSION ON SEVERAL CHANNEL NUT BTW WS 178.00 TO WS 88.00 RIGHT WING FRONT SPART FORWARD, LOWER SECTION. DUE TO EXCESSIVE CORROSION ON SEVERAL CHANNEL NUTS BTW WS 178.00 TO WS 88.00 RIGHT WING FRONT SPART FORWARD, LOWER SECTION WERE REPLACED PER CRJ 900 SRM SDR SWAA2026031073968Panel · crackedRIGHT WING ANGLE BELOW DEFLECTION RIB PANEL IS CRACKED. REMOVED ANGLE IAW SRM 51-40-02. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-02.SDR REXA2026042800401Angle · crackedCRACK ON ATTACHMENT ANGLE OF ACCESS PANEL 542AZ AT MLG SHOCK STRUT BAY ANGLE ON ACCESS PANEL 542AZ AT MLG SHOCK STRUT BAY WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01SDR SWAA2026033173625Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED AUXILIARY TRACK OF SLAT 8 INBOARD POSITION AT RT WING. REPLACED SUPPORT ANGLE LOCATED AUXILIARY TRACK OF SLAT 8 INBOARD POSITION AT RT WING IAW SRM 51-40-02, AND CMM 57-43-01.SDR AALA202602244331Strap · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND WING FIXED LEADING EDGE LOWER STRAP FORWARD OF FRONT SPAR, INBOARD OF NR 4 KRUGER FLAP ACTUATOR. REPLACED STRAP PER AARD 51-00-05-1.SDR IXXA20260223001Support Bracket · corrodedREAR SPAR HYD BLOCK CLAMP SUPPORT BRACKET CORRODED.PN 271N6114-22SDR IXXA20260222001Support Web · corrodedLW FUEL BOOST PUMP CUTOUT CORROSION IRSS 183SDR IPXA2026032539278Bracket · gougedRIGHT WING T/E SHROUD BOX AREA INBD OF AILERON DROP DOWN PANEL HAS A GOUGED BRACKET. REMOVED THE BRACKET IAW SRM 51-40-21-001. INSTALLED THE BRACKET IAW SRM 51-40-21-001.SDR SWAA2026031972750Bracket · crackedCRACK TRAILING EDGE BRACKET, ORSS 270, LT WING. REPLACED THE BRACKET IAW SRM 51-10-02, PARAGRAPH 9, SRM 51-40-02-0G-0, & DWG 115A2030, SHEET 6, REV-.SDR SWAA2026031972753Bracket · crackedCRACK TRAILING EDGE BRACKET, ORSS 280 INTERNAL CAVITY AT RT WING. REPLACED THE BRACKET IAW SRM 51-10-02, PARA 9, SRM-51-40-02-0G-0, & DWG 115A2930, SHEET 6, REV-.SDR SWAA2026031972754Support Bracket · damagedELONGATED HOLE ON THE RT WING ACCESS PANEL 651GB SUPPORT BRACKET. REPLACED THE SUPPORT BRACKET IAW SRM 51-10-02, SRM 51-40-02, & DWG 115A2714, SHEET 4, REV-.SDR SWAA2026031972751Support Angle · crackedCRACKED TRAILING EDGE SUPPORT ANGLE, LT WING ORSS 269. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02-0G-0, PARAGRAPH 9.SDR SWAA2026031072039Bracket · crackedPANEL 551GB INBD BRACKET CRACKED. THE BRACKET WAS REMOVED FROM PANEL 551GB IAW SRM 51-40-02-0G-0. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G-0.SDR IXXA2026021901Bracket · corrodedLEADING EDGE JUST ABOVE PYLON HAS CORROSION AROUND NUT PLATESDR IPXA2026033182348Web · crackedLEFT WING T/E, RIB 9 INNER UPPER WEB ATTACHED TO SKIN HAD ONE CRACK. INSTALLED, THE WEB IAW SRM 51-40-21-001SDR IPXA2026031782997Angle · crackedLEFT WING OTBD FLAP, INBD EDGE ANGLE BROKEN. REMOVED THE BROKEN ANGLE IAW SRM 51-40-21-001. INSTALLED THE ANGLE IAW SRM 51-40-21-001, & SRM 51-24-00-001.SDR IPXA2026032182096Rub Strip · crackedLEFT WING TRAILING EDGE, OTBD AILERON ACTUATOR AREA, LOWER INBD RUB STRIP HAD ONE HOLE. INSTALLED A NEW RUB STRIP IN LT WING TE, OTBD AILERON ACTUATOR AREA, LOWER INBD IAW SRM 51-40-21-001.SDR IXXA20260218001Bracket · corrodedLEFT LANDING GEAR ELECTICAL CONNECTOR BRACKET CORRODEDSDR 2026FA0000120Stiffener · crackedR/H WING FWD WING WALK CRACKED. REPLACED WITH NEW ASSYSDR 2026FA0000117Stiffener · crackedRIGHT WING AFT WING WALK CRACKED. REPLACED WITH NEW ASSY.SDR 2026FA0000116Stiffener · crackedRIGHT WING FWD WING WALK CRACKED. REPLACED WITH NEW ASSYSDR 2026FA0000115Stiffener · crackedRIGHT WING INBD FWD LWR SKIN, AFT STIFFENER CRACKED, REPLACED WITH NEWSDR 2026FA0000114Stiffener · crackedRT WING INBD FWD LWR SKIN, FWD STIFFENER CRACKED, REPLACED WITH NEWSDR 2026FA0000113Stiffener · crackedLH WING TOP I/B FWD SKIN, AFT STIFFENER CRACKED. REPLACED WITH NEWSDR 2026FA0000112Stiffener · crackedLH WING TOP I/B FWD SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWSDR 2026FA0000111Stiffener · crackedLH WING LWR I/B FWD SKIN, BOTTOM FWD STIFFENER CRACKED. REPLACED WITH NEWSDR 2026FA0000110Stiffener · crackedRIGHT WING LWR INBD FWD SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWSDR 2026FA0000108Stiffener · crackedRIGHT WING LWR INBD FWD SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEWSDR 2026FA0000107Stiffener · crackedRIGHT WING LWR INBD FWD SKIN, FWD STIFFENER CRACKED. REPLACED WITH NEW.SDR SWAA2026031269861Support Angle · crackedCRACKED SUPPORT ANGLE, ACCESS PANEL 551FB, LT WING. REPLACED THE SUPPORT ANGLE FOR ACCESS PANEL 551FB, LT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 115A2710, SHEET 9, REV A.SDR DALA2026083104895Plug · corrodedCORROSION ON FASTENER HOLE C1 OF RT WINGLET ADAPTER PLUG. REPAIRED PER PRI/ER/A 632062-14 (1445360)(AIRCRFT GROUNDED)SDR SWAA2026031669627Nut Plate · corrodedCORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS287 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS287 AT LT WING IAW B737-800 SRM 51-40-02-0G; SRM 51-10-02-0G Ï¿½TEM 9 AND DWG 112A4402 SHEET 40 REV A ; ANSDR SWAA2026031369625Rail · corrodedCORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS411 AT LT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE IAW SRM 51-40-02-0G, SRM 51-10-02-0G, ITEM 9 AND DWG 112A4402, SHEET 40, REV A.
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