JASC 5710
Service difficulty reports · 4,456
Reports filed under 5710 · Wing Main, Frame 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 = '5710' 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 = '5710' 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 IPXA2026051938822Former · crackedFORMER, RT WING OUTBD L/E CAVITY CURTAIN SUPPORT NEAR OSS 441. INSTALLED NEW FORMER I.A.W UPS SREO-54290-REQ1 REV.2 AND SRM 51-40-02-0G REV.95 AND BOEING DWG NO.114T2241 SH.4 REV-.SDR IPXA2026051900631Former · crackedCRACKED FORMER , RT WING OUTBD L/E CAVITY CURTAIN SUPPORT, NEAR OSS 499. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 114T2161 SH 6 REV. - AND UPS EO NO: SREO-50900-REQ001 REV2.SDR IPXA2026051800614Former · crackedCRACKED FORMER , FWD SIDE OF L/H WING OUTBD L/E NOSE BEAM , OSS 565.9. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 114T2162 SH 6 REV. - AND UPS EO NO: SREO-50900-REQ001 REV2.SDR IPXA2026051800673Former · crackedCRACK - FORMER , FWD SIDE OF L/H WING OUTBD L/E NOSE BEAM , OSS 499.6 (REPLACE) 1. REMOVE DAMAGE FORMER I.A.W SRM 51-40-02-0G REV.95. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO: 114T2161 SH 6 REV. - AND UPS EO NO: SREO-50900-REQ001 REVSDR AALA202605256190Intercostal · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT WING INTERCOSTAL CRACKED AT UPPER FIXED TRAILING EDGE PANEL JUST INBOARD UNDER #5 SPOILER. INSTALLED SERVICEABLE INTERCOSTAL PER AARD 51-00-05 .SDR AALA202605251532Intercostal · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND WIING, ABOVE AFT END OF ENGINE PYLON, FIXED TRAILING EDGE UPPER PANEL AFT INTERCOSTAL CRACKED AT OUTBOARD RIVET. INSTALLED NEW INTERCOSTAL PER AARD 51-00-05-1.SDR IPXA2026052036566Strut · crackedCRACKED, UPPER AND LOWER CHORD, RT WING OUTBD FXD LE CAVITY RIB, OSS 531.71. INSTALLED NEW CHORD IAW SRM 51-40-02-0G REV.55 AND DWG 114T2206, SH 1, REV B, & DWG 112T2000, SH 1, REV G.SDR SWAA2026060197339Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE IRSS 199 PLUS 30 INCH RT WING. REPLACED ACCESS PANEL 651CT AND FASTENERS LOCATED ON TRAILING EDGE RT WING IAW SRM 51-40-02 AND DRAWING 115A2001 SHEET 30 REV A.SDR SWAA2026060196872Plate · damagedELONGATED HOLE ON CORRUGATED PLATE LOCATED ORSS 261 TRAILING EDGE AT RT WING. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED ORSS 261 TRAILING EDGE AT RT WING IAW SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 PARAGRAPH 9.SDR SWAA2026060196873Plate · damagedELONGATED HOLE ON CORRUGATED PLATE LOCATED ORSS 261 TRAILING EDGE AT LT WING. REPLACED CORRUGATED PLATE LOCATED ORSS 261 TRAILING EDGE AT LT WING IAW SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-03-0G-0 AND DWG: 115A2714 SHEET: 11 REV -.SDR IPXA2026052572301Plate · crackedLH WING, T/E REAR SPAR, LOWER CHORD, BY WS 313.5, SKIN PANEL SPRT IS BROKEN. INSTALLED NEW WIGGLE PLATE ON LH WING, T/E REAR SPAR, I.A.W. 51-40-02-0G-0SDR IPXA2026052572000Plate · crackedRH WING, T/E REAR SPAR, LOWER CHORD, BY WS 313.5, SKIN PANEL SPRT IS BROKEN. INSTALLED NEW WIGGLE PLATE ON RH WING, T/E REAR SPAR, I.A.W. 51-40-02-0G-0.SDR UATA2870513265701Stiffener · crackedFOUND A CRACK IN STIFFENER ON THE LH WING FALSE SPAR AT W.S. 4900. THE CRACKED STIFFENER WAS R&R WITH NEW, FABRICATED STIFFENER MADE FROM 2024-T3 ALUMINUM .032" THICK, THE PRE-EXISTING SPACER HAD NO DAMAGE AND WAS REUSED. THE NEW STIFFENER WAS PRIMED WITH SUPESDR IPXA2026051184334Landing · crackedLEFT WING T/E PANEL 575DB SUPPORT STRUCTURE CRACKED. ACCOMPLISH PERMANENT REPAIR PER EO-97380-REQ1.SDR IPXA2026050566722Former · crackedCRACKED FORMER, FWD SIDE OF LT WING OTBD L/E NOSE BEAM, OSS 499.6. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G, REV 95. INSTALLED NEW FORMER IAW SRM 51-40-02-0G, REV 95, DWG 114T2161, SH 6, REV - , & EO SREO-50900-REQ001, REV 2.SDR SWAA2026052694432Plate · crackedCRACKED CORRUGATED PLATE TRAILING EDGE AT ORSS294 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE AT ORSS294 AT LT WING IAW SRM 51-40-02 SRM 51-10-02 ITEM 9. MEASURE OF CRACK IS L=0.890 INCH.SDR SWAA2026052294431Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE AT IRSS217 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE AT IRSS217 AT RT WING IAW SRM 51-40-02 AND DWG 115A2713 SHEET 6 REV A.SDR SWAA2026052294433Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE AT ORSS304 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE AT ORSS304 AT LT WING IAW B737-800 SRM 51-40-02 SRM 51-10-02 ITEM 9. MEASURE OF CRACK IS L=0.565 INCH.SDR SWAA2026051394194Plate · crackedWIGGLE PLATE ON LT WING REAR SPAR AT ORSS 434 CRACKED. REMOVED AND REPLACED WIGGLE PLATE ON LT WING REAR SPAR AT ORSS 434 IAW SRM 51-40-02-0G-0, AND AIPC 57-50-00-19.SDR SWAA2026051394287Fitting · crackedLEFT WING INBD FIXED TE SEAL BULKHEAD FITTING CRACKED. REMOVED AND REPLACED THE LT WING INBD FIXED TE SEAL BULKHEAD FITTING IAW SRM 51-40-02, AND DWG 115A2930, REV E.SDR CALA2026050415956Frame · crackedFOUND CRACK L/W FRONT SPAR INB END TO BODY FAIRING "U" ANGLE CRACKED ATTACHED TO FIXED L/E FAIRING - MKD DOT 002 REF. AAR N/R:100024822 STEP CREATED TO DOCUMENT CORRECTIVE ACTION,REMOVED AND REPLACED L/W FRONT SPAR INB END TO BODY FAIRING FRAME REF SRM 51-4-02SDR SWAA2026052793221Rail · corrodedCORROSION ON RAIL NUT AT LEVEL ORSS 449 LEADING EDGE AT RT WING. REPLACED RAIL NUT AT LEVEL ORSS 449 LEADING EDGE AT RT WING IAW SRM: 51-40-02-0G-0 AND DWG: 112A4402 SHEET 40 REV. A.SDR SWAA2026052793220Plate · crackedCRACK ON CORRUGATED PLATE LOCATED AT LEVEL IRSS 210 TRAILING EDGE RT WING. REPLACED CORRUGATED PLATE LOCATED AT LEVEL OF IRSS 210 TRAILING EDGE RT WING IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02-0G-0.SDR IPXA2026042665993Panel · crackedDURING OK TO INSTALL PANEL 623BB, FOUND CRACK AT THE FWD UPPER RADIUS OF PANEL CUTOUT, DOT 55-006. INSTALLED REFORCING PLATE IAW SRM 57-41-12-227.SDR IPXA2026051748003Fitting · damagedWHILE ACCOMPLISHING EO#7219-REQ001 REV1, HOLE "A", HOLE DIAMETER WAS FOUND OUT OF TOLERANCES, DWG MAPPING ATTACHED WITH DETAILS OF TOLERANCE. RECEIVED AND ACCOMPLISHED THE REPAIR EO-97617-REQ1 WITH EA# 300-5710-27-A4469 REV.-. MAJOR REPAIR.SDR 1Q2R2026042700001Fitting · temp repair2-OFF AREAS OF BLENDED CHAFE DAMAGE TO MAIN LANDING GEAR SIDE STAY FITTING (DWG: CC690-10608, AL ALY 7050-T7452, 0.310" +/- 0.010" NOMINAL THICKNESS, REF), RHS. TEMPORARY REPAIR PREVIOUSLY PERFORMED UNDER PSA AIRLINES EA NO: 57-2025-0371 REV --, DATED 2025-03-SDR SWAA2026051191824Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT RT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT RT WING IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 115A2001; SHEET: 30; REV A .SDR SWAA2026051191951Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE OFSS241 AT RT WING . PERFORMED DETAIL VISUAL INSPECTION ON CORRUGATED PLATE LOCATED TRAILING EDGE OFSS241 AT RT WING IAW SRM 51-10-02 AND NOT FOUND CRACK ONLY FOUND DIRTY AND CONTAMINATION; AND PERFORMED CLEAN ASDR SWAA2026051191955Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE ORSS261 AT RT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE ORSS261 AT RT WING IAW SRM 51-10-02-0G-0 ITEM 9 SRM 51-40-02-0G-0.SDR SWAA2026051191624Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT LT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT LT WING IAW SRM 51-10-02 SRM 51-40-02 AND DWG 115A2001 SHEET 30 REV A.SDR IPXA2026050202306Splice Plate · deformedLEFT WING AT LEADING EDGE SPAR AREA LWR PANEL ATTACH STRUCTURE AT NR 1 SLAT INBD DRIVE MOTOR LINK IS DEFORMED. REPAIR DAMAGE AREA IAW SRM 57-41-01-2R-4, REPAIR 4, REV 95, AND WORK SHEET 60290.SDR IPXA2026050202373Splice Plate · deformedLEFT WING AT LEADING EDGE SPAR AREA LWR PANEL ATTACH STRUCTURE AT NR 2 SLAT OUTBD DRIVE MOTOR LINK IS DEFORMED. REPAIR DAMAGE AREA IAW SRM 57-41-01-2R-4, REPAIR 4, REV.95 AND WORK SHEET 60291.SDR 2026F00077Pulley Bracket · corrodedFOUND 2 AREAS OF CORROSION ON SPOILER PULLEY BRACKET ON LH WING INBD, AFT SPAR. MECHANICALLY REMOVED 2 AREAS OF CORROSION LOCATED ON LH WING SPOILER PULLEY BRACKET, INSIDE INBD FLAP WELL, AFT SPAR IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYONDSDR SWAA2026042290500Fairing · crackedRIGHT WING INBD TE BUMP FAIRING DAMAGED AND CRACKED 3.6". REPLACED THE DAMAGED FAIRING IAW AMM 57-50-02 & AMM 20-50-11.SDR IPXA2026042657472Retainer · brokenFAULT-STR-ZONE 500. AFTER REMOVAL OF LH WING PANEL 572PB, (2EA) CRACKS FOUND AT INNER PANEL SEAL RETAINER. INSTALLED NEW PANEL IAW SRM 51-40-21-001.SDR CALA2026042015536Bracket · crackedRIGHT WNG TRAILING EDGE UPPER FIXED PANEL, ONE BRACKET CRACKED ABOVE PANEL 651GB APPROX. 260. REPLACED THE BRACKET ON RT WING T/E UPPER FIXED PANEL IAW AMM 20-50-11-910-801, & SRM 51-40-02.SDR DALA2026041602420Sealant · misinstalledPOOR SEALANT ON INNER REAR SPAR CORNER OF THE NEWLY REPLACED LHW RIB 6 FITTING ASSY. RE-WORKED SEALANT PER ERA 633297-14AD REV ORIGINAL. (1547040) AIRCRAFT WAS GROUNDED.SDR IPXA2026060480423Fitting · damagedLEFT WING, FR 47 LOWER JUNCTION, HOLE S HAS A VISUAL DAMAGE. ACCOMPLISHED THE REPAIR PER EA 300-5710-27-A4437.SDR IPXA2026041371289Fitting · noneNR 2 WING STRUT SUPPORT CLEVIS FITTING FREEZE PLUG - PERMANENT REPAIR. CONDITION CHECK NORMAL. PAPER FINAL CHECK OK.SDR IPXA2026041649774Scoop · damagedENLARGED HOLE, LT WING OUTBD LOWER FUEL VENT SCOOP PANEL FWD FASTENER HOLE. IAW DWG 112U0700, SHEET 01, REV D. REMOVED LT WING FUEL VENT SCOOP PANEL IAW DWG 112U0700, SHEET 01, REV. D. INSTALLED LT WING FUEL VENT SCOOP PANEL.SDR SWAA2026041488202Support Bracket · crackedRIGHT WING UPPER T/E PANEL SUPPORT Z BRACKET CRACKED. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-02-0G-0-A00729.SDR IPXA2026050544443Bracket · crackedRIGHT WING ROOT, MLG DOOR CUTOUT AFT INNER SKIN PANEL, CURVED SUPPORT BRACKET HAS (1EA) CRACK. REMOVED CURVED SUPPORT BRACKET FROM RH WING ROOT, MLG DOOR CUTOUT AFT INNER SKIN PANEL IAW SRM 51-40-21-001. INSTALLED NEW SUPPORT BRACKET IAW SRM 51-40-21-001.SDR CALA2026050415935Vent · crackedRIGHT WING INSPECTION OF LOWER WING SKIN AND ACCESS PANEL 643BB PERIPHERY - DISCOVERED CRACK AFT OF FUEL VENT DURING NDT INSPECTION OF LOWER WING SKIN ACCESS PANEL 643BB 10 INCH IN LENGTH. FUEL IS PRESENT AND FORMS A DROP OUT OF THE CRACK AT A SLOW RATE OF APPSDR IPXA2026041113551Splice Strap · crackedCRACKED SPLICE STRAP, LT WING INBD T/E FWD LOWER RIB SUPPORT, WS 298. INSTALLED A NEW STRAP IAW SRM 51-40-02-0G, REV 94, AND DWG 113T1639, SHT 1, REV G.SDR IPXA2026041094116Former · crackedCRACKED FORMER, FWD SIDE OF LT WING OTBD L/E NOSE BEAM, OSS 499.6. INSTALL NEW FORMER IAW SRM 51-40-02-0G REV.95 AND DWG 114T2511 SH 1 REV: DSDR IPXA2026041094070Former · crackedCRACKED FORMER, FWD SIDE OF LT WING OTBD L/E NOSE BEAM, OSS 441.6. INSTALLED NEW FORMER I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO. 114T2241 SH 4 REV - AND UPS SREO-54290-REQ1 REV2SDR IPXA2026041094681Former · crackedCRACKED FORMER, RT WING OTBD LE WS 510. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO. 114T2161 SH 6 REV - AND UPS SREO-50900-REQ001 REV2.SDR IPXA2026041590371Beam · crackedDURING PERFORMANCE OF EO-63801-JIC001, FOUND LEFT WING TRAILING EDGE SUPPORT BEAM CRACKED AT WS 1079.95. INSTALLED A NEW BEAM IAW SRM 51-40-02-0G, REV.94 AND DWG 113T1913, SHT 1, REV A, DWG 113T1657, SHT 1, REV C, AND DWG 113T1676, SHT 2, REV -.SDR SWAA2026050686906Plate · crackedLEFT WING WAFFLE PLATE IS CRACKED UNDER DEFLECTION RIB FIXED TRAILING EDGE PANEL; I/B SIDE OF ENGINE PYLON. ACCOMPLISHED INSPECTION PER NDT PART 6 CH51-00-00 PROCEDURE 23 WITH NO DEFECTS NOTED. REMOVED WAFFLE PLATE FOR NDT PER SRM 51-40-02.. INSTALLED WAFFSDR IPXA2026041575356Bushing · migratedMIGRATED BUSHING, RT WING T/E NR 8 SPOILER MID LWR. IAW CMM:57-70-11, REV 42, REPAIR 2-1, PAGE 601 - 602 STEP 3, COMPLETED THE REPLACEMENT OF BUSHING.
Back to JASC 5710