JASC 5730
Service difficulty reports · 27,255
Reports filed under 5730 · Wing, Plate/Skin, 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 = '5730' 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 = '5730' 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 UIEA2025071200940Skin · damagedLEFT WING L/E FIXED FAIRING BETWEEN INBD ILES 630.46 TO ILES 693.5 SEVERAL FASTENER HOLES FOUND ELONGATED. L/E SKIN REPAIRED AS PER RI-57-41-17749 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR IPXA2025080596626Shear Tie · crackedRIGHT WING, REAR SPAR, BY RIB 10, SKIN SUPPORT IS CRACKED. REMOVED SKIN SUPPORT IAW IAW SRM 51-40-21. FABRICATED NEW SKIN SUPPORT AT RT WING IAW GMM 09-08-01-04, LOCATED AND DRILLED NEW SKIN SUPPORT FOR RT WING REAR SPAR IAW SRM 51-40-21. INSTALLED IAW SRMSDR AALA202507161945Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE UPPER SKIN PANEL UPPER SURFACE AT RIB 3 AT THE INNER REAR SPAR. REPAIRED SKIN PANEL PER EA 363852.SDR VNAA20250715034Skin · gougedGOUGES AT HOLE COUNTERSINK TO LH WING FIXED L/E PANEL AT SLAT STA. 144.94. GOUGES AT HOLE COUNTERSINK TO LH WING FIXED L/E PANEL AT SLAT STA. 144.94 WAS REPAIRED PER REO 690-57-41-522 REV. - - .SDR VNAA20250715027Panel · gougedGOUGES AT HOLE COUNTERSINK TO LH WING FIXED L/E PANEL AT SLAT STA. 144.94. GOUGES AT HOLE COUNTERSINK TO LH WING FIXED L/E PANEL AT SLAT STA. 144.94 WAS REPAIRED PER REO 690-57-41-522 REV. - - .SDR UIEA2025070600836Skin · delaminatedRHW I/B FORE FLAP L/E MID AND O/B AREA FOUND DELAMINATED.(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025070600837Skin · delaminatedLHW I/B MID FLAP L/E MOST I/B AREA FOUND DELAMINATED.(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025070600838Skin · delaminatedLHW I/B FORE FLAP O/B OF MID FORE FLAP TRACK APPROX 9" L/E AREA FOUND DELAMINATED.(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025070600839Skin · delaminatedLHW I/B FORE FLAP L/E MOST I/B AREA FOUND DELAMINATED.(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025070600840Skin · delaminatedLHW I/B FORE FLAP I/B OF FORE FLAP TRACK CUTOUT FOUND DELAMINATED.(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.</P>)SDR DALA2025071405264Fastener · loose(LOG 1075724) LOOSE_ FASTENER ON SKIN_ AND ELONGATED HOLES ON UPPER SURFACE OF TRAILING EDGE BTW WS=278.50 ALSO WS=228.25 TO 204.25 AT RH WING. SKIN UPPER SURFACE OF TRAILING EDGE BTW WS =228.25 TO 204.25 AT RH WING WAS REPAIRED PER ER/A 627456-14.SDR FDEA202507111178Skin · crackedUT AND HFEC OPEN HOLE INSPECTION FOUND TWO CRACKS IN LH WING #5 HOLE. THE LH WING UPPER SKIN #5 HOLE TWO CRACKS REPAIRED AS PER B777 SRM51-20-07-0G REV:47.6 AND EA G-5730-T0384072 P1, TITLE:WING-PLATES AND SKINS-LH WING UPPER SKIN CRACK REPAIR IN RIB BAYSDR R61A2025073100326Skin · crackedLEFT WING LOWER SKIN IS CRACKED AT RIB 4A AND SPAR 2. REPAIRED LH WING LOWER SKIN AT RIB 4A AND SPAR 2 ETD2025-170-924781 REV.: BSDR DALA2025071405255Access Panel · corroded(LOG 1073473) CORROSION IN FUEL ACCESS RING 532AB. CORROSION ON ACCESS RING OF FUEL 532AB WAS REMOVED PER B737-800 SRM -57-20-01-2R-1.SDR DALA2025071405254Landing · corroded(LOG 1073457) CORROSION ON ACCESS PANELS SETTLEMENT AND RING ON 534BB AND 634BB AT DRY BAY WINGS. CORROSION ON ACCESS PANELS RING ON 534BB AND 634BB AT DRY BAY WINGS WAS REMOVED PER B737-800 SRM 51-10-02-0G PAR 15. A. AND SRM 57-20-01-2R PROCEDURE 1 REPAIR 1.SDR ABXA20250710149Skin Panel · corrodedDURING 763CK'S C4 CHECK IN OSC, KALITTA MAINTENANCE FOUND CORROSION ON THE UPPER SKIN PANEL #1 (P/N 112T3301-1) UNDER PANEL #9 (P/N 113T1609-1), AFT OF THE REAR SPAR, WSTA 349.7 - 359. THE CORROSION WAS BLENDED AND FOUND OUT OF LIMITS PER SRM 57-20-01, ALLOWABSDR ABXA20250710147Skin Panel · corrodedDURING 763CK'S C4 CHECK AT KALITTA, CORROSION WAS FOUND ON THE LH WING, LOWER SKIN PANEL #3 BETWEEN WING STATION 668.2 - 694.2, RIB 19 - 20 AND A BLENDOUT WAS ACCOMPLISHED. BLENDOUT WAS BEYOND ALLOWABLE LIMITS STATED IN REF /A/. FVCI WAS CONTACTED TO PROVIDE ASDR JR2R20250710997Skin · chafedL/H WING FIXED LEADING EDGE PANEL HAS CHAFE MARKS.SDR JR2R20250710187Skin · chafedR/H WING FIXED LEADING EDGE OVER PYLON HAS CHAFE MARKS.SDR JR2R20250710860Access Panel · chafedL/H LOWER WING PLANK AT FUEL ACCESS CUTOUT 521EB DOORLAND SHOWS SIGNS OF CHAFING.SDR SWAA2025071489335Panel · crackedRIGHT WING LOWER MIDSPAN FIXED TRAILING EDGE PANEL 661AB TURN BARREL CRACKED ON SUPPORT ROD<[01] REMOVED AND REPLACED RIGHT WING LOWER MIDSPAN FIXED TRAILING EDGE PANEL 661AB TURN BARREL SUPPORT ROD PER AMM 20-50-11SDR 2025FA0000492Skin · crackedRIGHT WING AFT WING WALK CORRUGATED SKIN CRACKED, REPLACED SKIN ASSY WITH NEW.SDR 2025FA0000491Skin · crackedRIGHT WING FWD WING WALK CORRUGATED SKIN CRACKED, REPLACED SKIN ASSY WITH NEW.SDR DALA2025070805106Skin · not reportedSHIP 663 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 627081-14AD. CORRECTIVE ACTION: REF ERA 627081-14. (1069558)SDR DALA2025070805099Skin · damagedSHIP 663 AD // AA SCRATCHES AND CORROSION BTW 5-6 HRS SKIN AT DRAG FITTING HOLE #2, SCRATCHES ON DRAG FITTING HOLE #3 AT 12 HRS ON SKIN AND SCRATCHES ON DRAG FITTING HOLE #8 6:00 HRS AT SKIN LH WING(REF: CARD 5720-01100-04A). CORRECTIVE ACTION: SUMMARY OF NRC SDR DALA2025070805097Fastener · looseSHIP 6711 A.A. IN REF TO AMDS: 5720-01100-02A, STEP 12 D. LOOSE FASTENER NO. 3 WAS FOUND AT LH ENG DRAG FITTING. CORRECTIVE ACTION: SUMMARY OF NRC 00396: HOLES 3, 14, 16 & 18 WERE REPAIRED PER PRI 580219-14 REV. 6 & ER/A 580219-14AD, REV. D SECTION I. (1066274SDR AALA202507089730Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL LOWER SURFACE AT RIB 11 AND 1 INCH FROM THE REAR SPAR. REPAIRED SKIN PANEL PER EA 364989.SDR AALA202507085372Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL LOWER SURFACE BETWEEN RIBS 10 AND RIB 11 AT 1 INCH FROM THE REAR SPAR. REPAIRED SKIN PANEL PER EA 364980SDR AALA202507089333Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL LOWER SURFACE AT RIB 19 AND 1 INCH FROM THE REAR SPAR. REPAIRED SKIN PANEL PER EA 364980.SDR AALA202507081427Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL LOWER SURFACE BETWEEN RIB 15 AND RIB 16 AT 1 INCH FROM THE REAR SPAR. REPAIRED SKIN PANEL PER EA 364980.SDR EE4Y2025070622641Skin · crackedDURING THE ACCOMPLISHMENT OF SB190-57-0056, TWO CRACKS WERE DISCOVER COMING FROM THE PREVIOUS REPAIR TRIM OUTS, AND ONE ADDITIONAL CRACK WAS FOUND CLOSE TO RIB 11. CRACKED AREAS WERE REMOVED BY SKIN TRIM OUTS. THIS SITUATION WAS REPORTED TO EMB ASKING FOR REPASDR SWAA2025081188575Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661AB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661AB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-9 REPAIR 9.SDR SWAA2025081188576Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661BB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9.SDR SWAA2025081188577Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 661CB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661CB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-9 REPAIR 9. SSDR SWAA2025081188578Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 561BB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9.SDR SWAA2025081188468Panel · delaminatedLEFT ING L/E PANEL 521KB DELAMINATED AT CORNERS OF CUTOUT. LEFT WING L/E PANEL 521KB WITH DELAMINATIONS AT CORNERS OF CUTOUTS WAS REPAIRED PER SRM 51-70-05-2R-6.SDR SWAA2025081188467Panel · delaminatedLEFT WING L/E PANEL 521DB DELAMINATED AT CUTOUT CORNERS. REPAIRED PER SRM 51-70-05-2R-6-A00737 REPAIR 6 - REPAIR OF DAMAGE TO THE EDGEBAND OF A HONEYCOMB PANEL.SDR SWAA2025081188470Panel · delaminatedRIGHT WING L/E PANEL 621JB DELAMINATED AT CUTOUT FWD CORNERS. RIGHT WING L/E PANEL 621JB DELAMINATED AT CUTOUT FWD CORNERS; WAS REPAIRED IAW SRM 51-70-05-2R-6.SDR SWAA2025081188472Panel · delaminatedRIGHT WING L/E PANEL 621QB DELAMINATED AT FWD I/B CORNER. RIGHT WING L/E PANEL 621QB DELAMINATED AT FWD I/B CORNER; WAS REPAIRED IAW SRM 51-70-05-2R-6.SDR DALA2025070805107Skin · not reportedSHIP 663 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 627083-14AD WINGS / OUTER WING / LHS UPPER SKIN & DRAG FITTINGS / HOLES #2, #3, #8 & #18 / CORROSION & CRACK. CORRECTIVE ACTION: REF ERA 627083-14SDR AALA202507084119Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL LOWER SURFACE AT RIB 8 AND 1 INCH FROM THE REAR SPAR. REPAIRED SKIN PANEL PER EA 364771.SDR AALA202507088489Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL LOWER SURFACE AT RIB 10 AND 1 INCH FROM THE REAR SPAR. REPAIRED SKIN PANEL PER EA 364771.SDR AALA202507089692Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL LOWER SURFACE BETWEEN RIB 17 AND RIB 18 AT 1 INCH FROM THE REAR SPAR. REPAIRED SKIN PANEL PER EA 364771.SDR YENA2025070800687Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION LEADING EDGE UPPER SURFACE LOC. BTW RIB1 TO RIB 2 ON LH WING; ACCOMPLISHED REPAIR OF CORROSION DAMAGE ON THE LH WING TOP SKIN PANEL UPPER SURFACE AT LEVEL OF RIB 1-2 AND STRG 4 IAW AEROMAN EA 57-0048-25 REV 0 (COVER PLUS P-1SDR YENA2025070800686Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE ON TOP SKIN LOWER SURFACE OVERHANG AT LEVEL R IB 6 TO RIB 7 ON RH WING (CPCP FINDING ). REPAIR OF CORROSION ON THE RH WING TOP SKIN PANEL 2, LOWER SURFACE TEOH FALSE REAR SPAR BETWEEN WX3494.5 - WX4010.2 IN SDR EE4Y2025070422633Skin · damagedDURING THE ACCOMPLISHMENT OF SB190-57-0056, WERE FOUND 5 EXISTING FASTENER HOLES WITH OVERSIZED DIAMETER (LOCATED AT SPAR I AND RIBS 8 AND 9). THIS CONDITION WAS REPORTED TO EMB FOR REPAIR INSTRUCTIONS. THIS CONDITION WAS REPAIRED PER ETD2025-190-922232 AND DOSDR EE4Y2025070422627Skin · damagedDURING THIS PROCESS, WERE IDENTIFIED ( 1EA) EXISTING FASTENER HOLE WITH OVERSIZED DIAMETER COMMON TO LOWER SKIN, SPAR I, AND RIB 8 AND WITHIN THE AREA COVERED BY THE REF. EMBRAER SB 190-57-0056 AND FAA AD2020-04-16. THIS CONDITION WAS REPORTED TO EMB AND REPAISDR CALA2025071506574Skin · crackedTWO CRACK INDICATIONS LT WING LOWER LE SKIN SURFACE BETWEEN WSTA 564.5 AND WSTA 591.5, NR 1 EMANATING FROM LOWER FWD SPAR CHORD FASTENER, THRU FWD ROW O/B S-9 FASTENER MARKED 5,500"L. NR 2 EMANATING FROM OB AFT S-9 ROW FASTENER .150"L.SDR 2025FA0000490Skin · crackedRIGHT WING AFT WING WALK CORRUGATED SKIN CRACKED, REPLACED SKIN ASSY WITH NEW.SDR 2025FA0000489Skin · crackedRIGHT WING FWD WING WALK CORRUGATED SKIN CRACKED, REPLACED SKIN ASSY WITH NEW.
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