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 FDEA202509241786Doubler · damagedLEFT WING - UPPER SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER FOUND DEEP EXISTING BLEND - OUT AND CORROSION ALONG XORS = 264.00 LEFT HAND WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER STATION XORS = 264.00 CORROSION REMOVED AND FOUNSDR FDEA202509241779Skin · chafedRIGHT WING DROOPED LEADING EDGE OUTBOARD SIDE EXISTING DOUBLER FOUND CHAFFED AT STATION XDLE 329.775. REPAIR CARRIED OUT AT RIGHT HAND WING DROOPED LEADING EDGE OUTBOARD SIDE STATION XDLE 329.775 AS PER MD-11 SRM 57-40-01-2R REPAIR 15 FIGURE 202. REPAIR CLSDR FDEA202509241778Skin · chafedRIGHT WING DROOPED LEADING EDGE INBOARD EXISTING DOUBLER FOUND CHAFFED AT STATION XDLE 309.934. REPAIR CARRIED OUT AT RIGHT HAND WING DROOPED LEADING EDGE INBOARD STATION XDLE 309.934 AS PER MD-11 SRM 57-40-01-2R REPAIR 15 FIGURE 202. REPAIR CLASSIFIED AS SDR AALA202510106345Skin · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND WING FIXED LEADING EDGE SKIN WORN AT CONTACT AREA WITH PYLON PANEL 441CL. REMOVED WORN LEADING EDGE WRAP AROUND SKIN AND REPLACED WITH NEW SERVICEABLE WRAP AROUND SKIN. PER SRM 57-41-01SDR IPXA2025092972747Access Panel · crackedLEFT WING, LOWER SURFACE, ACCESS PANEL 575DB, CUT-OUT HAS A CRACK. .ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95281-REQ1 REV. 2 AND VT-MAE EA 300-5751-27-A4155SDR FDEA202509221761Doubler · crackedRIGHT WING - LEADING EDGE LOWER ACCESS PANEL CUTOUT FORWORD EDGE DOUBLER AT STATION XOS 488 FOUND CRACK ABOUT 1 INCH. RIGHT WING LEADING EDGE LOWER ACCESS PANEL CUTOUT FORWORD EDGE CRACKED DOUBLER ABOUT 1 INCH AT STATION XOS 488. FABRICATED DOUBLER PER DOUSDR GTIA2025101439130Panel · corrodedCORROSION UPPER SURFACE LOC. BTW RIB 5 TO RIB 6 REAR SPAR AREA ON RH WING RAF 3525563-02 GENERATED -PERFORMED PERMANENT REPAIR UPPER SURFACE LOC. BTW RIB 6 REAR SPAR AREA ON RH WING I.A.W EA #57-0095-25. THIS REPAIR IS CATEGORY A AND NOT REQUIRED FUTURE INSPECSDR GTIA2025101439129Panel · corrodedCORROSION UPPER SURFACE LOC. BTW RIB 4 TO RIB 6 REAR SPAR AREA ON LH WING RAF 3525563-01 CREATED SEE APPENDIX 3525563-01-PERFORMED PERMANENT REPAIR LOC. ON UPPER SURFACE BTW RIB 4 TO RIB 6 REAR SPAR AREA ON LH WING I.A.W EA # 57-0097-25. THIS REPAIR IS CATEGORSDR GTIA2025101439128Panel · corrodedCORROSION UPPER SURFACE LOC. BTW RIB 4 TO RIB 5 REAR SPAR AREA ON RH WING RAF-01 3525564-01 GENERATED -PERFORMED PERMANENT REPAIR UPPER SURFACE LOC. BTW RIB 4 TO RIB 5 REAR SPAR AREA ON RH WING I.A.W EA #57-0095-25. THIS REPAIR IS CATEGORY A. AND NOT REQUIRED SDR GTIA2025F00008Panel · corrodedCORROSION UPPER SURFACE LOC. BTW RIB 4 TO RIB 6 REAR SPAR AREA ON LH WING RAF 3525563-01 CREATED SEE APPENDIX 3525563-01-PERFORMED PERMANENT REPAIR LOC. ON UPPER SURFACE BTW RIB 4 TO RIB 6 REAR SPAR AREA ON LH WING I.A.W EA # 57-0097-25. THIS REPAIR IS CATEGORSDR GTIA2025F00007Panel · corrodedCORROSION UPPER SURFACE LOC. BTW RIB 4 TO RIB 5 REAR SPAR AREA ON RH WING RAF-01 3525564-01 GENERATED -PERFORMED PERMANENT REPAIR UPPER SURFACE LOC. BTW RIB 4 TO RIB 5 REAR SPAR AREA ON RH WING I.A.W EA #57-0095-25. THIS REPAIR IS CATEGORY A. AND NOT REQUIRED SDR FDEA202509211754Doubler · no discrepancyEXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 785 EXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 785 EVALUATED AND FOUND REPAIRED IAW MD-11 SRM 57-40-02-2R RSDR FDEA202509211752Doubler · no discrepancyEXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 640 EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 640 EVALUATED AND FOUND REPAIRED IAW MD-11 SRM 57-40-02-2R REPSDR FDEA202509211751Doubler · no discrepancyEXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 629. EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 629 EVALUATED AND FOUND REPAIRED IAW MD-11 SRM 57-40-02-2R RESDR FDEA202509211750Doubler · no discrepancyEXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 625. EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 625 EVALUATED AND FOUND REPAIRED IAW MD-11 SRM 57-40-02-2R RESDR VNAA202511250002Access Panel · corrodedCORROSION ON SETTLEMENT AREA OF ACCESS PANEL: 642BZ. CORROSION ON SETTLEMENT AREA OF ACCESS PANEL: 642BZ WAS EVALUATED EXCESSIVE DAMAGE PER SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-700 SRM 51-42-21-001-001-A01.SDR FDEA202509171719Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 792 FOUND CRACK ABOUT 0.8 INCHES.SDR FDEA202509171718Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 792 FOUND CRACK ABOUT 0.8 INCHES. RIGHT WING FIXED LEADINIG EDGE CRACKED BEADED DOUBLER WITH LENGTH OF 0.8 INCHES TRIMMED OUT PER MD11 SRM 57-40-02-2R FIGURE 203 REPAIR 15. FABRICATED REPAIR DOUSDR FDEA202509171716Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 792 FOUND CRACK ABOUT 0.8 INCHES.SDR 2025FA0000649Skin · crackedDURING EXTERIOR INSPECTION ON JANUARY 15 2025 AND AGAIN JULY 2, 2025, MULTIPLE CRACKS WERE OBSERVED IN THE WING UPPER SKIN PANELS OF BOTH THE LEFT AND RIGHT WINGS, AS WELL AS IN THE FUSELAGE STRUCTURE ADJACENT TO THE CABIN ENTRY DOOR. LEFT WING UPPER SURFACE:SDR SWAA2025092415149Panel · crackedPOSSIBLE CRACK ON LOWER SURFACE OF PANEL 671BB. LOWER SURFACE OF PANEL 671BB WAS REPAIRED IAW SRM 51-70-05-2R-2.SDR IPXA2025092036861Skin Panel · crackedRIGHT WING INBD FIXED T/E IS CRACKED AT FASTNER HOLE. INSTALLED SKIN PANEL AT UPEER AND LOWER R/H WING T/E FIXED INBD USING FASTNERS P/N CR3212-4-03 B# 0004279987 150 EA AND P/N MS20426AD4 B# 0004361884 10 EA IAW A300-600-SRM-51-40-21 AND A300-600-IPC-75-51-1SDR FDEA202509161707Skin · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION ON CORNER 11 - FUEL ACCESS DOOR FORWARD INBOARD CORNER ON LEFT HAND FIXED LEADING EDGE SKIN FOUND CRACK APPROXMIMATELY 0.4 INCHES AT STATION XOS 610.844. LEFT HAND WING APPROXMIMATELY STATION 610.844 FIXED LEADING EDGSDR IXXA20250916002Skin · corrodedRIGHT WING UPPER SURFACE SKIN CORRODED AT WSTA 204.5, STR 1 AND STR 3 NR 181429-0600-0047 AND REA 47676REA55SDR IXXA20250916001Skin · corrodedRIGHT WING UPPER SURFACE SKIN CORRODED AT AFT SPAR WSTA 177.5 -231.5SDR IPXA2025100103715Skin · crackedUPON WORKING EO-88069-REQ047 REV1, TASK CARD T3F18E0054EL6, FOUND EVIDENCE OF POSSIBLE CRACK AT HOLE LOCATION NUMBER 10 L/W UPPR SKIN OF #1 ENG. PYLON. ATA-54-00.PERFORMED BLEND-OUT ON CORRODED AREAS LOCATED AT UPPER FACE SURFACES OF INBD AND OUTB DRAG FITTINSDR DALA2025092306962Skin · damagedEXISTING REPAIR FOUND THAT IMPACTS INSPECTION ACCOMPLISHMENT. REPAIR INVESTIGATION REQUIRED BEFORE FURTHER FLIGHT. RH WING XRS 14- XRS 177. REF. EA 619064-14AD REV. B SECT II. DVI OF AFT SIDE OF SPAR CAP AT STOP DRILL SHOWS NO DISCREPANCY. (1199238)SDR SWAA2025102114117Access Panel · crackedCRACK ACCESS PANEL 561CB AT LT WING. REPAIRED ACCESS PANEL 561CB AT LT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10.SDR AALA202509127790Skin · damagedAIRCRAFT IN BASE MAINTENANCE: LEFT WING LOWER SKIN DAMAGED DUE TO TIRE BUST ON TAKEOFF. (SEE AALA202508280585), LOCATED AT WS 156. REPLACED SKIN PER 367894 AND BOEING WORK ORDER AAL-RE-25000250.SDR IPXA2025100256077Doubler · crackedL/H WING. FIXED L/E INNER SKIN BEADED DOUBLER LOCATED APPROX STA XORS 402 HAS CRACK. VERIFIED STEP 25 VERIFIED REPAIR WAS ACCOMPLISH REPAIR PER MD-11 SRM 57-40-02-2R FIGURE 205 REPAIR 15 REV 72.SDR IPXA2025100255936Doubler · crackedL/H WING. FIXED L/E INNER SKIN BEADED DOUBLER LOCATED APPROX STA XORS 506 HAS CRACK. OUT OF SEQUENCE STEP 3 C/W IAW UPS RII GMM 04-02. ACCOMPLISHED REPAIR PER MD-11 SRM 57-40-02-2R FIGURE 205 REPAIR 15 REV 71SDR 2025F00219Skin · gougedMECHANICALLY BLENDED HIGH SPOTS ON A GOUGE ON THE RH WING LEADING EDGE APPROXIMATELY 3.25 INCHES OTBD OF THE START OF THE LEADING EDGE. POLISHED AND RETURNED AREA TO ORIGINAL SURFACE FINISH IAW CESSNA 680 SPM 51-70-02 AND NETJETS ENGINEERING RFTS-114953 REV. 0SDR IXXA20250911006Skin · corrodedRIGHT WING UPPER SURFACE SKIN CORROSION AT WSTA 681SDR IXXA20250911005Skin · corrodedRIGHT WING UPPER SURFACE AFT SKIN WSTA 550-594 CORROSIONSDR IXXA20250911004Skin · corrodedRIGHT WING UPPER SURFACE AT FWD SPAR WSTA 481. CORROSION.SDR IXXA20250911003Skin · corrodedRIGHT WING UPPER SURFACE AT AFT SPAR WSTA 177.5.SDR IXXA20250911002Skin · corrodedRIGHT WING UPPER SURFACE AT AFT SPAR WSTA 299 CORROSION.SDR IXXA20250911001Skin · corrodedRIGHT WING UPPER SURFACE AT SKIN SPLICE WSTA 320-370 CORRODED.SDR CALA2025091208824Skin · crackedREPAIR AREA AT THE LT SIDE WING FIXED LEADING EDGE UPPER SKIN PA NEL FASTENERS BTW KRAS206.5 TO KRAS220 REF TO EA 5720-02922 REV A OP 001. REPAIRED AREAS AT THE LH WING UPPER FIXED LE SKIN P/N 116A4410-7 IAW ECRA 5741-01665.SDR CALA2025091208823Skin · crackedREPAIR AREA AT THE RH SIDE WING FIXED LEADING EDGE UPPER SKIN PANEL FASTENERS BTW KRAS206.5 TO KRAS220 REF TO EA 5720-02922 REV A OP 002.(1000055151) REPAIRED AREA AT THE RH WING UPPER FIXED LE SKIN P/N 116A4410-8 IAW ECRA 5741-01664SDR IXXA2025091005Skin · corrodedRIGHT WING UPPER SKIN PANEL NO.2 WSTA 565.5-594.5 CORROSION. P.N. 112N3102-14SDR IXXA2025091004Skin · corrodedRIGHT WING UPPER SKIN PANEL NO.1 AT UPPER SKIN REAR SPAR WSTA 264.7 AND 275.5. CORROSIONSDR IXXA2025091003Skin · corrodedRIGHT WING UPPER SKIN PANEL NO.2 FWD SPAR AT STR 20 AND 21, WSTA 226-235. CORROSIONSDR IXXA20250910001Skin · corrodedRIGHT WING UPPER SKIN PANEL NO.2, WSTA 259-313 CORROSIONSDR SWAA2025100113020Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 243, LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 243, LT WING IAW SRM 51-40-02-0G-0; DWG 115A2781 SHEET: 7 REV - AND DWG 115AA2001 SHEET: 87 REV -.SDR IXXA2025090900002Skin · corrodedRIGHT WING UPPER SKIN PANEL NR 1 WSTA 594.5-652.5 CORRODED.SDR IXX2025F00023Skin · corrodedRIGHT WING UPPER SKIN PANEL NO.. 1 WSTA 623.5-652.5 CORRODEDSDR R61A2025100300425Skin · crackedRH WING HAS CRACK ON UNDERSIDE @ RIB 4A SPAR 2 AS MARKED. REPAIRED RH WING CRACK ON UNDERSIDE@ RIB 4A SPAR 2 REF ETD2025-170-928277 REV A.SDR SWAA2025100112828Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 RT WING. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED ORSS 261 AT RT WING IAW SRM 51-40-02, & DWG 115A2714, SHEET 6, REV -. LENGTH OF CRACK IS 0.750 INCH.SDR DALA2025090906656Skin · damagedLEFT WING UPPER SKIN PANEL SUPPORT BEAM AT LWSTA 177.5 REQUIRES INSTALL. REMOVAL AND DAMAGE EVALUATION DOCUMENTED ON ORNRC 184563.0500.0010. INSTALLED SERVICEABLE LEFT WING UPPER SKIN SUPPORT BEAM AT LEFT WING STA 177.5 IAW BOEING 757-200 SRM 51-40-02 PARAGR
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