JASC 5730
Service difficulty reports · 27,262
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 IPXA2024102879210Skin · damaged*SDR FILED OPEN* BIRDSTRIKE ON BASE-TO-FINAL TURN FOR PHL RWY 27R. POST-FLIGHT REVEALED EXTENSIVE DAMAGE TO RH WING LEADING EDGE INBOARD OF #3 ENGINE. REMOVED #2 INBOARD R/H SLAT PER AMM 27-80-20-000-802.SDR IPXA2024103054935Skin · crackedSKIN CRACKED AT NUTPLATE CORNER OF ACCESS PANEL 513AB. MB-60. TREATED AND PRIMED 2 (EA) DOUBLERS WITH ALODINE P/N ALODINE1132, BATCH 0004325097 AND PRIMER P/N 10-P4-2/2TU, BATCH 0004268573, IAW A300-600 SRM 51-21-10.SDR DALA2024102810456Skin · corrodedSHIP 3133 CORROSION ON CUT OUT OF GRAVITY FUEL CAP AT WING TOP SKIN LOC. BTW RIB19 TO RIB20 ON RH WING. CORRECTIVE ACTION: PERFORMED REPAIR AS PER A319 SRM 57-21-11-300-006. (0627762)SDR DALA2024102810455Skin · corrodedSHIP 3133 CORROSION ON CUT OUT OF GRAVITY FUEL CAP AT WING TOP SKIN LOC. BTW RIB19 TO RIB20 ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR AS PER A319 SRM 57-21-11-300-006. (0627753)SDR 2024F00260Skin · corrodedLOWER WING SKIN CORROSION REF (ENGINEERING REPAIR ORDER ERO-979789)SDR SWIA20241115024Access Panel · corrodedFOUND POSSIBLE CORROSION ON THE LEFT WING FUEL ACCESS HOLE 510AB ON THE FWD AND INBOARD LIP. (MARKED WITH TAPE) (FILED CLOSED) REPAIRED CORROSION DAMAGE ON FUEL ACCESS PANEL OPENING 510AB ON THE FWD AND INBOARD LIP WITH REFERENCE TO REO 601R-57-21-030 RSDR SWIA20241108024Skin · corrodedFOUND POSSIBLE CORROSION ON THE LEFT WING FUEL ACCESS HOLE 510AB ON THE FWD AND INBOARD LIP. (MARKED WITH TAPE) (FILED OPEN) REPAIRED CORROSION DAMAGE ON FUEL ACCESS PANEL OPENING 510AB ON THE FWD AND INBOARD LIP WITH REFERENCE TO REO 601R-57-21-030 REVSDR SWI2024F01253Access Panel · corrodedPOSSIBLE CORROSION ON RIGHT WING FUEL ACCESS HOLE 640BB, INBOARD/OUTBOARD/AFT LIP. (MARKED WITH TAPE) (FILED CLOSED) REPAIRED CORROSION DAMAGE ON RH FUEL ACCESS PANEL OPENING 640BB ON THE FWD AND INBOARD LIP WITH REFERENCE TO REO 601R-57-21-030 REV "-L" DSDR SWI2024F01201Skin · corrodedPOSSIBLE CORROSION ON RIGHT WING FUEL ACCESS HOLE 640BB, INBOARD/OUTBOARD/AFT LIP. (MARKED WITH TAPE) (FILED OPEN) REPAIRED CORROSION DAMAGE ON RH FUEL ACCESS PANEL OPENING 640BB ON THE FWD AND INBOARD LIP WITH REFERENCE TO REO 601R-57-21-030 REV "-L" DATSDR DALA2024110710718Skin · corrodedSHIP 3160 CORROSION UPPER SURFACE SKIN LOCATED BETWEEN RIB12 TO RIB13 REAR SPAR ON LH WING. CORRECTIVE ACTION: REMOVED CORROSION BY REWORK AS PER A319 SRM 51-74-00. ( 0624317)SDR CALA2024102302712Skin · crackedRH WING LOWER SKIN, EVIDENCE OF CRACK BETWEEN WSTA 564 AND 591. RII REQUIRED FOR MAJOR REPAIR WORK THAT HAS BEEN ACCOMPLISHED REF EC/RA 5725 01151 AND NON ROUTINE 00225317. SFR HAS BEEN COMPLETED SFR # 1037488.SDR EE4Y2024102221144Skin Panel · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 572112-01-1-002_P1-OP-UP-W , RH WING BOX TOP SKIN TRAILING EDGE OVERHANG WITH CORROSION AT RIB 14 AND RIB 14+415MM LOWER SURFACE AND RIB 14+185MM UPPER SURFACE.THE OEM WAS CONTACTED FOR REPAIR INSTRUCTIONS.´PERFORMEDSDR EE4Y2024102221143Skin Panel · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 572112-01-1-002_P1-OP-UP-W , RH WING REAR SPAR TRAILING EDGE OVERHANG TOP SKIN LOWER SURFACE AT WING RIB 10 CORROSION WAS FOUND.THE OEM WAS CONTACTED FOR REPAIR INSTRUCTIONS. ´PERFORMED PERMANENT REPAIR AT RH WING TOSDR EE4Y2024102221142Skin Panel · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 572111-01-1-001_P1-OP-UP-W , LH WING (BETWEEN STA4862/RIB 9 & STA5512/RIB10) FIXED TRAILING EDGE PANEL OVERHANG WITH LOOSE FASTENER AND CORROSION FOUND AT TOP SKIN LOWER SURFACE..THE OEM WAS CONTACTED FOR REPAIR INSTSDR EE4Y2024102221141Skin Panel · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK ZL-500-03-1-001_P1-OP-UP-W , LH WING BETWEEN STA4067/RIB7 & STA4862/RIB 8, UPPER SURFACE, TRAILING EDGE SKIN WITH SPOT CORROSION (2EA) WERE FOUND.THE OEM WAS CONTACTED FOR REPAIR INSTRUCTIONS. ´PERFORMED PERMANENT RESDR I5PA2024102075704Skin · corrodedDURING C CHECK, CORROSION WAS FOUND ON THE RH WING LOWER SKIN AT WS 187-211. CORROSION WAS REPAIRED PER BOEING ENGINEERING INSTRUCTIONS.SDR I5PA2024102075703Skin · corrodedDURING C CHECK, CORROSION WAS FOUND ON THE LH WING LOWER SKIN AT WS 187-213. CORROSION WAS REPAIRED PER BOEING ENGINEERING INSTRUCTIONS.SDR DALA2024102110253Skin · corrodedSHIP 3143 CORROSION WAS FOUND ON THE LOWER SURFACE OF TOP SKIN PANEL 2, BETWEEN WX3494,5 - WX4010,2 AT THE TRAILING EDGE OVERHANG OF THE LEFT-HAND WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 619900-14. (0617492)SDR AALA202410196761Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRALING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 11 PLUS 3.900 INCHES. REPAIRED SKIN PANEL; PER EA 357532.SDR AALA202410190667Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRALING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 17 PLUS 18.856 INCHES. REPAIRED SKIN PANEL; PER EA 357532.SDR YENA2024101701360Skin · corrodedDURING HEAVY MAINTENANCE: RH WING, UPPER SURFACE RIB 18-RIB 19, STGR 14 WITH CORROSION POINTS; REF. MEX WO:1318489,1327754,1328846 N/R S/N: 00337. CORR. POINTS AT RHW TOP SKIN UPPER SURF. BETWEEN RIB 18/ RIB 19 STGR 14 WAS REMOVED. REF MEX EO TRE-2057203, JETBSDR YENA2024101701358Skin · corrodedDURING HEAVY MAINTENANCE: RH WING UPPER SURF. SKIN WITH CORROSION POINTS AT STGR 13 BETWEEN RIB 12/ RIB 13; REF. MEX WO: 1318489,1327754,1328846 N/R S/N: 00101. CORROSION POINTS RHW TOP SKIN UPPER SURF. BETWEEN RIB 12/ RIB 13 STGR 13 WAS REMOVED & REPAIRED. RESDR YENA2024101701357Skin · corrodedDURING HEAVY MAINTENANCE: RH WING UPPER SURFACE SKIN WITH CORROSION AT STGR 15 BETWEEN RIB 14 / RIB 15; REF. MEX WO: 1318489,1327754,1328846 N/R S/N: 00104. : CORROSION POINTS AT RH WING TOP SKIN UPPER SURFACE BETWEEN RIB 14/ RIB 15 STGR 15, WAS REMOVED AND RESDR YENA2024101701356Skin · corrodedDURING HEAVY MAINTENANCE: RH WING UPPER SURFACE SKIN WITH CORROSION POINTS AT STGR 13 BETWEEN RIB 11 / RIB 12; REF. MEX WO. 1318489,1327754,1328846 N/R S/N : 00091 - CORROSION POINTS AT RH WING TOP SKIN UPPER SURFACE BETWEEN RIB 11/ RIB 12 STGR 13, WAS REMOVEDSDR FDEA202410171532Doubler · crackedLEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 1047. LEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT STATION XOS 1047 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. SDR FDEA202410171531Doubler · crackedLEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 561. LEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT STATION XOS 561 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. RESDR FDEA202410171530Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 696. RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT STATION XOS 696 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. SDR VNAA202411240006Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (686AB, 692AB, 697AB) AT RH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (686AB, 692AB, 697AB) AT RH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-495 REV.--SDR VNAA202411240005Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-494 REV.--SDR QXEA2024101800243Access Panel · leakingNOTED FUEL DRIPPING FROM R/H WING STUB AFT END IN WING TO FUSELAGE PANEL. REMOVED FROM SERVICE. C/W T/C E-28-0031 ITEMS 1-4 ONLY. C/W STEPS 5 AND 6 OF TASKCARD E-28-0031 LEAKAGE WAS IN EXCESS OF ALLOWABLE LIMITS IN STEP 5. UNABLE TO FERRY A/C REF LP 1085371 FOSDR FDEA202410161522Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 990. RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT STATION XOS 990 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. SDR FDEA202410161521Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 628. RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT STATION XOS 628 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. SDR FDEA202410161520Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACKED AT STATION XOS 614. RIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER AT STATION XOS 614 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. SDR S9BA20240005Doubler · corrodedCORROSION FOUND BEYOND MFR LIMITS ON LH WING WS310.O FORE FLAP HINGE SKIN DOUBLERS. FOLLOWING PART NUMBERS WERE REMOVED AND REPLACED IAW DHC SRM. 969401-7 AND 969401-9.SDR SWAA2024112149225Panel · pulledL/W T/E PANEL 561BB HAS SEVERAL PULLED FASTENER HOLES ON T/E. (MARKED)<[01] USED TINNERMAN WASHERS UNDER SCREW HEADS ON 6 EA PULLED FASTENER HOLES ON T/E OF L/W T/E PANEL 561BB PER AMM 20-60-11-201 STEP A. (6). PANEL WAS INSTALLED ON CARD TTG8Q00VTYLU.;[02] VESDR SWAA2024112149226Panel · pulledR/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES ON T/E. (MARKED)<[01] USED WASHERS UNDER SCREW HEADS ON SEVERAL PULLED FASTENER HOLES ON T/E OF R/W T/E PANEL 661BB PER AMM 20-60-11-201 STEP A. (6). PANEL WAS INSTALLED ON CARD TTG8Q00VTYC6.;[02] VERIFIED SDR DALA2024101610134Skin · ground damageSHIP 3148 LH WING BOTTOM SKIN PANEL #3 WAS INADVERTENTLY DAMAGED. CORRECTIVE ACTION: COMPLIED WITH ER/A 568357-14. (0611142)SDR DALA2024101610132Skin · damagedSHIP 3148 LH WING BOTTOM SKIN PANEL #3 WAS INADVERTENTLY DAMAGED. CORRECTIVE ACTION: COMPLIED WITH ER/A 568357-14. (0611151)SDR IXXA20241115002Access Panel · corrodedLW FUEL BOOST PUMP PANELS 531AB AND 532AB ARE WORN AND CORRODED. HAECO WO 320009 NON ROUTINE 46434SDR JR2R20241012335Skin · gougedLH WINGLET LEADING EDGE GOUGEDSDR JR2R20241012972Panel · chafedLH WING FIXED LE PANEL ABOVE PYLON CHAFED. REPAIRED.SDR A6WA202410108842Skin · corrodedFOUND EROSION DAMAGE TO THE RIGHT WING LEDAING EDGE SKIN BETWEEN WS350.348 AND WS386.348. THE DAMAGE IS REMOVED MEASURING A MATERIAL LOSS OF UP TO 0.018". THE SKIN IS FORMED FROM 0.080" 6013-T6 AL ALLOY LOCALLY CHEM-MILLED TO 0.042". MAINTENANCE CONTACTED ENGISDR GTIA2024101238435Skin Panel · corrodedLEFT WING CORROSION ON WING BOTTOM SURFACE BETWEEN RIBS 21-22 REAR SPAR PANEL 2. RAF-01 AND SDR CREATED -REPAIRED ACCOMPLISHED REF HAECO S.O. 122204 OPS 34308 CAT B REPAIR REQUIRES INSP AT 4100FC 8200 FROM EMBODIMENT AT INTERVALS OF 4100FC 8200FH PER RDAF 81SDR GTIA2024101238434Skin Panel · corrodedLH WING CORROSION ON WING LOWER SKIN PANEL 1 RIBS 18-19 RAF-01 AND SDR CREATED -ACCOMPLISHED REPAIR ON HAECO S.O. 122204 OPS 34313PERMANET CAT B REPAIR. POST REPAIR INSP AT 114700 FC 229500 FH PER RDAF 81464650/003/2024/B REF EA 5721-2447SDR GTIA2024101238432Skin · gougedGOUGE FOUND ON LH WING LE PANEL 522QB LANDING ASSY MEASURING .3770" L X .3770" W. RAF 01 CREATED. SDR SUBMITTED-FABRICATED AND INSTALLED LH WING LWR LE PANEL 522QB LANDING REF EA 5741-2454 & HAECO S.O 122204 OPS 34413 CAT A REPAIR NO REINSPECT REQUIRED PER RDASDR QXEA2024101000236Access Panel · leakingSUSPECTED FUEL LEAK, RH CENTER TANK. REMOVED FROM SERVICE. FOUND FUEL SEEPING FROM COLLECTOR TANK (RH) ACCESS PANEL 144BR. RE-TORQUED ACCESS PANEL REF E175 AMM 28-11-03-400-801-A. SEEP CEASED, NO LEAKS NOTED. AIRCAFT OK FOR SERVICE. NO PARTS REPLACED. RETURNEDSDR 2024FA0000888Skin · crackedR/H WING AFT WING WALK SKIN CRACKED AT CORRUGATED SKIN. REPLACED ASSEMBLY WITH NEWSDR 2024FA0000880Skin · crackedR/H WING FWD WING WALK SKIN CRACKED AT CORRUGATED SKIN. REPLACED ASSEMBLY WITH NEWSDR DALA2024101009963Access Panel · corrodedSHIP 3143 CORROSION ACCESS PANEL 631CB BONDING STRAP ON RH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FLAP TRACK FAIRING 631CB AS PER ER/A 620280-14. (0601048)SDR DALA2024101009933Skin · damagedSHIP 5808 A/C SUFFERED HEAT DAMAGE TO THE L/H OUTER WING LOWER SKIN AND L/H MLG SURROND STRUCTURE. CORRECTIVE ACTION: C/W ERA 621235-14 REV. ORIG COMPAIRED TO PRI 621235-14 REVS 0, 1 , & 2 AND VERRIFIED ALL REVS MATCH ERA 621235-14 REV. ORIG. (0601084)
Back to JASC 5730