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 REXA2026030900223Canister · crackedCRACK ON SLAT TRACK CANISTER 1-3 AT RH WING MAIN FUEL TANK WS 148 CRACK ON SLAT TRACK CANISTER 1-3 AT RH WING MAIN FUEL TANK WS 148 WAS REPAIRED PER REO 670-57-42-577 REV --SDR SWIA2026011775820Hinge Fitting · gougedRIGHT WING FWD HINGE BOX FITTING AT WS127.25 GOUGED. REPAIRED RT WING FWD HINGE BOX FITTING AT WS127 PER REO 601R-57-21-4040 REV -. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.SDR REXA2026030900205Seal · crackedBROKEN SEAL NEXT TO ACCESS PANEL 591JB UPPER, LH WING BROKEN SEAL NEXT TO ACCESS PANEL 591JB UPPER, LH WING WAS REPLACED PER CRJ 900 SRM 51-42-10-001-001-A07SDR SWAA2026021262340Web · corrodedCORROSION WEB INTERNAL CAVITY LEADING EDGE LOCATED OFSS276, RT WING. PERFORMED PERMANENT REPAIR ON WEB IN THE INTERNAL CAVITY LEADING EDGE IAW SRM 51-70-11-2R-0, REPAIR GENERAL, PARAGRAPH 4.SDR DALA2026011200256Strut · corrodedCORROSION ON INTERCONNECTING STRUT ON RT WING (REFERS TO AMDS CARD 275 1-9202 FOR RII). REMOVED INTERCONNECTING STRUT OF RH WING ON UNSERVICEABLE CONDITION P/N D5757032201100, S/N 985, IAW AMM 27- 51-44-000-001-A, STEP 1 THRU 3.C AND 4.A. REPLACED INTERCONNECSDR VNAA202601090006Washer · crackedREQUEST, SUBMIT RFTS FOR AN EA TO FABRICATE PN CC670-10635-7 FOR , HR00572741 SO# 400416899 AND FABRICATE AS INSTRUCTED. (THIS CARD IS FOR RFTS SUBMITTAL AND FABRICATION OF QTY 1 PN CC670-10635-7SDR VNAA202601090005Washer · crackedSUBMIT RFTS FOR AN EA TO FABRICATE PN CC670-10635-7 FOR HR00572740, SO 400416898 AND FABRICATE AS INSTRUCTED. (THIS CARD IS FOR RFTS SUBMITTAL AND FABRICATION OF QTY 1 PN CC670-10635-7) RETENTION WASHERSDR SWAA2026012859175Plate · crackedCRACKED CORRUGATED PLATE ORSS 261, RT WING T/E. REPLACED THE CORRUGATED PLATE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 115A2001, SHEET 29, REV -.SDR SWAA2026012859176Plate · crackedCRACKED CORRUGATED PLATE ORSS 241, RT WING T/E. REPLACED THE CORRUGATED PLATE IAW SRM 51-40-02-0G, & DWG 115A2001, SHEET 30, REV A.SDR 2026FA0000001Strut · crackedCRACK ON WING SIDE OF RH STRUT. AIRFRAME TOTAL TIME IS 10298.9. CRACK WAS FOUND DURING ROUTINE 100/HR INSPECTION. AIRPLANE DOES PIPELINE PATROL.SDR CALA2026010412640Door · missingUPON ARRIVAL, FOUND THE RIGHT WING THERMAL ANTI-ICING DUCT SEAL DOOR ASSEMBLY MISSING.SDR SWAA2026012657685Plate · crackedCRACKED WIGGLE PLATE ASSY, IRSS 199+13, LT WING REAR SPAR. REMOVED THE WIGGLE PLATE IAW SRM 51-40-02-0G-0. RECEIVED A NEW WIGGLE PLATE, AND INSTALLED IAW SRM 51-40-02-0G-0.SDR DXTA2026010506406Wing · ground damageJUST AS WE GOT TO THE AIRPORT AND BEFORE WE GOT TO THE PLANE A EXECUJET VAN STRUCK THE LEFT WING OF N341QS AT 8:56. THE DAMAGE TO THE WING SEEMS MINIMAL BUT THE VAN HAS A BIG DENT. CORRECTIVE ACTION: GAINED ACCESS TO THE AIRCRAFT AND INSPECTED THE DAMAGED AREASDR U2RA2025123100028Wedge · damagedDURING SHEDULED C-CHECK VISIT, FOUND LT WINGLET T/E WEDGE LIGHTNING STRIKE DAMAGE. REPAIR HAS BEEN C/W IAW EO 25197-2.SDR SWAA2026012056575Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE ORSS261 AT RT WING. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED TRAILING EDGE ORSS261 AT RT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2001, SHEET 29, REV-.SDR SWAA2026012056583Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT LT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT LT WING IAW SRM 51-0-02, ITEM 9, SRM 51-40-02, AND DWG 115A2001, SHEET 29, REV- .SDR SWAA2026012056587Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE ORSS261 AT LT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE ORSS261 AT LT WING IAW SRM 51-0-02, ITEM 9, SRM 51-40-02 AND DWG 115A2001, SHEET 29, REV- .SDR SWAA2026012056580Plate · crackedCRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT RT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2001, SHEET 30, REV A.SDR SWAA2026012056586Plate · crackedCRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT LT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02 AND DWG 115A2001, SHEET 30, REV A.SDR SWAA2026011956589Beam · crackedCRACKED BEAM LOCATED TRAILING EDGE ORSS285 AT LT WING. REPLACED BEAM AND FASTENERS LOCATED TRAILING EDGE ORSS285 AT LT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 115A3700; SHEET 31, REV -, AND DRAWING 115A3712, SHEET 5, REV -.SDR CALA2026010212636Diaphragm · damagedLEFT WING DRY BAY STRUCTURE, RIB 6 - 6B, CLOSING PANEL AND DIAPHRAGM WERE REPLACED AT MLB. REPAIR IS EXPECTED TO BECOME A PERMANENT SOLUTION WITH NO SUPPLEMENTAL INSPECTION REQUIREMENTS. ACCOMPLISH PERMANENT REPAIR ACTION IAW PART 3 OF THE LATEST REVISION OF ESDR SWAA2026011555699Plate · noneCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT LT WING. PERFORMED VISUAL INSPECTION ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT LT WING AND NOT FOUND CRACK PAINT MARKET ONLY; PERFORMED CLEAN IAW SRM 51-10-04.SDR SWAA2026011555700Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE, ORSS 261 LT WING IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, & DWG 115A2001, SHEET 29, REV-.SDR CALA2026010612696Control Panel · corrodedRIGHT WING FUELING STATION, THE CON TROL PANEL HAS CORRODED. REMOVED AND REPLACED FUELING CONTROL PANEL (P28) IAW AM M 28-21-08-004-001 AND AMM 28-21-08-404-031 TEST PASS AND SEVERA L SWITCHES WERE REPLACED IAW SWPM 20-83-11 AND SWPM 20- 84-20.SDR VNAA20260201013Web · crackedCRACK ON WEB OF INBD AUXILIARY SPAR FWD FACE (MLG SHOCK STRUT BAY AREA) WS 24.50 APPROX AT LT WING. CRACKED WEB OF INBD AUXILIARY SPAR FWD FACE (MLG SHOCK STRUT BAY AREA) WS 24.50 APPROX AT LT WING WERE REPAIRED PER REO 690-57-21-550 REV-.SDR VNAA20260201010Angle · crackedCRACKED ANGLE ON WING FIXED T.E. WS= 168.07 ON REAR SPAR AREA AT RT WING. CRACKED ANGLE ON WING FIXED T.E. WS= 168.07 ON REAR SPAR AREA AT RH WING WAS REPAIRED PER REO 690-57-51-503 REV.- -SDR VNAA20260201009Angle · crackedCRACKED ANGLE ON WING FIXED T.E. WS= 168.07 ON REAR SPAR AREA AT LT WING. CRACKED ANGLE ON WING FIXED T.E. WS= 168.07 ON REAR SPAR AREA AT LH WING WAS REPAIRED PER REO 690-57-51-504 REV. - -SDR SWAA2026012654818Plate · crackedCRACKED CORRUGATED PLATE, IRSSS216, LT WING T/E. REPLACED THE CORRUGATED PLATE IAW SRM 51-40-02-0G-0, AND DWG 115A2713, SHEET 6, REV A.SDR SWAA2025123054882Panel · crackedPANEL 621YB CRACKED ON THE CORNER. DRILLED REPLACEMENT PANEL PER SRM 51-40-05. APPLIED TOP COAT PER AMM 51-21-00. INSPECTED WORK ACCOMPLISHED DRILLED REPLACEMENT PANEL PER SRM 51-40-05. APPLIED TOP COAT PER AMM 51-21-00.SDR CALA2025121912259Seal · missingRIGHT WING INBD AILERON BOTTOM SEAL MISSING.SDR VNAA20251216022Canister · crackedCRACK ON CANISTER WELDED NO.3, ON WS148.01 OF INTERNAL RH MAIN FUEL TANK. CRACK ON CANISTER WELDED NO.3, ON WS148.01 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV - -SDR CALA2025121612141Structure · damagedLEFT WING CENTER TANK LOWER CHORD AND WEB DAMAGE LOCATED AT LBL 62.05 FROM BSS 785.9 TO BSS 955.1 BTW STRINGER L-4 TO L-6. THIS LP WAS CLASSIFIED AS RII IAW GMM 03-20-20. QC AWARE. REMOVED FASTENERS, PERFORMED TRIMMED THE DAMAGED AREA AND PERFORMED NDT INSPECTSDR SWAA2026010551585Plate · crackedCRACK ON CORRUGATED PLATE LOCATED AT LEVEL ORSS 261 TRAILING EDGE RT WING. REPLACED CORRUGATED PLATE LOCATED AT LEVEL ORSS 261 TRAILING EDGE RT WING IAW SRM 51-10-02 ITEM 9; SRM 51-40-02; DRAWING 115A2001; REV-, SHEET 29.SDR SWAA2026010251588Angle · crackedCRACK ANGLE AT ACCESS PANEL 651GB, RT WING. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0, AND DWG 115A2714, SHEET 14, REV-. MEASUREMENT OF CRACK: L= 0.440.SDR SWAA2026010551438Plate · crackedCRACK ON CORRUGATED PLATE LOCATED AT LEVEL IRSS 227 TRAILING EDGE AT RT WING. REPLACED CORRUGATED PLATE LOCATED AT LEVEL IRSS 227 TRAILING EDGE AT RT WING IAW SRM 51-10-02 ITEM 9. AND SRM 51-40-02 AND DRAWING 115A2781 SHEET 7 REV -.SDR SWAA2026010251446Plate · crackedCRACKED CORRUGATED PLATE, TRAILING EDGE AT IRSS 217, RT WING. REPLACED THE CORRUGATED PLATE IAW SRM 51-40-02-0G-0, AND 51-10-02-0G-0, STEP 9.SDR SWAA2025123051312Panel · delaminatedRIGHT WING LEADING EDGE PANEL 621VB HAS DELAMINATED AT INBD CORNER. RT WING LE PANEL 621VB WAS REPAIRED IAW SRM 51-70-05-2R-6, & SRM 57-41-01-2R-1.SDR JGVR20251209001Drag Angle · corrodedBLENDED AREAS OF CORROSION ON THE LOWER AFT DRAG ANGLE, LEFT WING INBD OF FLAP, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPLACED BLENDED FASTENERS WITH NEW, CLEANED, TREATED AND PRIMED AREAS PER REQUEST FOR TECHNICAL SERVICES REPORT.SDR SWAA2026011447658Angle · crackedRIGHT WING T/E ORSS 280 L ANGLE COMMON TO DEFLECTION CONTROL RIB AND T/E UPPER SURFACE PANEL IS CRACKED. REMOVED AND INSTALLED WITH A NEW L ANGLE IAW SRM 51-40-02-0G.SDR SWAA2026011343160Plate · crackedCRACKED CORRUGATED PLATE TRAILING EDGE LOCATED BETWEEN ORSS290 TO ORSS297, LT WING. REPLACED CORRUGATED PLATE AND FASTENERS TRAILING EDGE, LT WING IAW SRM 51-40-02, DWG 115A3700, SHEET 81, REV A, AND DWT 115A3712, SHEET 5, REV -.SDR SWAA2026011343149Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 297 RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 297 RT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG 115A3712, SHEET 7, REV A, AND DWG 115A3700, SHEET 41, REV - .SDR SWAA2026011343150Plate · crackedCRACK CORRUGATED PLATE T/E IRSS 215 ON RT WING. REPLACED CORRUGATED PLATE LOCATED ON RT WING TRAILING EDGE IAW SRM 51-40-02, AND DWG 115A2001, SHEET 67, AND REV -.SDR SWAA2026010242837Tee Fitting · corrodedLEFT-WING LEADING-EDGE STRUCTURE: LEADING EDGE 'T' EXTRUSION HAS CORROSION ON THE VERTICAL LEG. LOCATED OUTBOARD OF THE #3 SLAT ANTI-ICE TUBE. CORROSION ON T FITTING BEYOND LIMITS. REMOVED LOWER LEADING EDGE RIB T FITTING FOR REPLACEMENT. DRILLED A REPLACEMENSDR CALA2025120811871Drag Fitting · crackedRIGHT UPPER WING SKIN AND DRAG FITTING HAD A CRACK INDICATION, NOTED IN HOLE NR 4 IN ALL LAYERS. ACCOMPLISHED ECRA 5720-03589 AND VT MAE EA 757-5720-13-A4212 REV-.SDR SWAA2025122954889Fitting · wornLEFT WING TRAILING EDGE DEFLECTION RIB FITTING UPPER ATTACH POINTS HAS EXCESSIVE WARE AT BOLT HOLES. INSPECTED DEFLECTION CONTROL RIB UPPER TAB AND FOUND TO BE OUT-OF-LIMITS. CUT AND REMOVED DAMAGE ALL WORK IAW PER SRM 57-51-02-1A-1. NO CRACK INDICATIONS FSDR SWAA2025121942038Plate · crackedCRACK CORRUGATED PLATE ON TRAILING EDGE, ORSS 261, LT WING. REPLACED THE CORRUGATED PLATE IAW SRM 51-40-02, AND DWG 115A2001, SHEET 29, AND REV-.SDR SWAA2025121641447Plate · crackedLEFT WING REAR SPAR, IRSS 215 WIGGLE PLATE IS CRACKED, AND NOT SECURE. REMOVED AND REPLACED IAW SRM 51-40-02-0G-0-B00069,SDR IXXA20251202003Former · crackedRIGHT WING LE NOSE FORMER AT 0SS 441 IS CRACKED.SDR IXXA20251202002Former · crackedRIGHT WING LE NOSE FORMER AT 0SS 430 CRACKED.SDR CALA2025120311729Cover · missingRIGHT WING 1ST FLAP TRACK PIVOT COVER MISSING. REPLACED MISSING COVER REF AMM 57-55-11 PARTS USED: D5754052520200A,QTY :1
Back to JASC 5710