JASC 5730
Service difficulty reports · 27,254
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 AALA202609092028Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING FUEL ACCESS PANEL 550AB INNER SIDE AROUND FASTENER HOLES - REPLACED FUEL ACCESS PANEL 550AB PER JOB CARD 26C54057020SDR CALA2026090319224Skin · corrodedDURING ZONAL INSPECTIONS OF THE LT WING IAW UAL TC 31-5721-1-2724, EXTENSIVE CORROSION DAMAGE WAS NOTED ON THE LT WING TOP SKIN PANEL NR 2 TRAILING EDGE OVERHANG AT RIBS 11-16. DAMAGE CONSISTS OF EXFOLIATION BEYOND SRM ALLOWABLE DAMAGE LIMITS. PERFORMED INTESDR SWAA2026082765386Panel · crackedL/H WING UPPER TRAILING EDGE SURFACE PANEL AFT RIVET CRACKED OTBD OF PYLON JUST ABOVE DEFLECTION RIB R&R L/H WING UPPER TRAILING EDGE SURFACE PANEL AFT RIVET REF SRM 51-40-02 02 - INSPECTED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMSDR FDEA202608251224Skin Panel · crackedLH WING NR 3 SLAT MAIN TRACK SUPPORT AREA LOWER SURFACE SKIN WITH CRACKED. COVE PANEL WITH CRACK AT LH WING # 3 SLAT MAIN TRACK SUPPORT AREA LOWER SURFACE WAS REMOVED, FABRICATED AND INSTALLED IAW B757 SRM 51-40-02-0G AND B-DWG 114N4077 REV DSDR IPXA2026091394413Panel · delaminatedFAULT: COMP-ZONE 600-RIGHT WING LE BEHIND #7 SLAT IB END HAS DELAMINATION. REMOVED FIXED PANEL DAMAGED R/WING I.A.W B757-200PF SRM 51-40-02-0G. CLEANED AND EVALUATED, ITEM IS REPAIRABLE. REMOVED DAMAGE AND FABRICATED NEW CORE PLUG. P/N HRH-10-1/8-3.0, B/N 000SDR IPXA2026090494430Skin · crackedRIGHT WING FIXED LEADING EDGE BEHIND THE NR 8 SLAT HAS A CRACK. ACOMPLISHED REPAIR IAW SREO-11855-REQ002.SDR CALA2026082518911Skin · crackedRIGHT WING SLAT NR 7. HAS ACTUATOR ATTACHED WITH SMOKING/PULL IN RIVETS. REPAIRED RT WING SLAT NR 7 NOSE SKIN LOWER SURFACE AT THE ACTUATOR RIB IAW SRM 57-42-01-2R-8.SDR REXA2026101601910Access Panel · corrodedCORROSION ON THE ACCESS PANELS 642AZ, 642BZ, 542AZ, & 542BZ. THE ACCESS PANELS WERE REMOVED IAW SRM 51-21-06-001-001-A01, & WERE EVALUATED OUT LIMITS IAW SRM 53-00-00-101-001-A01, & REPLACED.SDR REXA2026101601909Access Panel · corrodedCORROSION ON THE ACCESS PANELS 642AZ, 642BZ, 542AZ, & 542BZ. THE ACCESS PANELS WERE REMOVED IAW SRM 51-21-06-001-001-A01, & WERE EVALUATED OUT LIMITS IAW SRM 53-00-00-101-001-A01, & REPLACED.SDR REXA2026101601908Access Panel · corrodedCORRODED ACCESS PANELS 642AZ, 642BZ, 542AZ, & 542BZ. THE ON ACCESS PANELS WERE REMOVED IAW SRM 51-21-06-001-001-A01 AND WERE EVALUATED OUT LIMITS IAW SRM 53-00-00-101-001-A01, & REPLACED.SDR REXA2026101601907Access Panel · corrodedCORROSION ON THE ACCESS PANELS 642AZ, 642BZ, 542AZ, & 542BZ. THE ACCESS PANELS WERE REMOVED IAW SRM 51-21-06-001-001-A01, AND WERE EVALUATED OUT LIMITS IAW SRM 53-00-00-101-001-A01 & REPLACED.SDR SWAA2026092180434Skin · crackedCRACKED LOWER SKIN OF THE LEFT WINGLET. REPLACED THE LT WINGLET AND INSTALLATION WILL BE ACCOSPLISHED ON TTG8Q00F9LK2.SDR SWAA2026091605216Access Panel · leakingFUEL LEAK ON ACCESS PANEL 632HB AT RT WING. REMOVED AND REINSTALLED ACCESS PANEL 632HB IAW AMM 28-11-11-000-801 AND AMM 28-11-11-400-801.SDR SWAA2026091475041Access Panel · delaminatedACCESS PANEL 192HL - DENTED & DELAMINATED. REPAIRED THE ACCESS PANEL 192HL IAW SRM 51-70-05-2R-2, REPAIR 2.SDR SWAA2026091493968Access Panel · delaminatedACCESS PANEL 551AT DENTED WITH DELAMINATION. REPAIRED ACCESS PANEL 551AT IAW SRM 51-70-05-2R-2 REPAIR 2.SDR SWAA2026092190056Fastener · pulledRIGHT WING LEADING EDGE, JUST INBD OF NR 2 ENGINE HAD THREE FASTENERS PULLING THROUGH SKIN. REMOVED THE THREE PULLING FASTENERS AND OVERSIZED HOLES TO .214 IAW SRM 57-41-01-2R-7. ACCOMPLISHED HFEC HOLE PROBE AND COUNTERSINK INSPECTION IAW NDT PART 6 51-00-00,SDR R61A2026090700253Skin · crackedDURING HEAVY CHECK L/H WING L/E SKIN AT SLAT #2 OB SLAT TRACK CUTOUT FOUND CRACKED. REPAIRED CRACK IAW EMB 170/175 SRM 57-49-01SDR IPXA2026090377741Skin · debondedDEBONDED SKIN, INBD EDGE UPPER FACE OF LT WING T/E OTBD FLAP T/E SKIN , WBL 355. IAW SREO-70175-REQ001, REV 1, REMOVED THE CRACK AND CLEANED. MEASURE THE DAMAGE AREA L : 0.5", W : 0.01", 7" FROM TRAILING EDGE, AT INBD EDGE. BONDED THE REPAIR PLIES WITH RESDR IPXA2026082877721Skin · debondedDEBONDED LOWER SKIN OF LT WING T/E OTBD FLAP T/E SKIN WBL 380. IAW SRM 57-53-01-2R-1, REF SRM 51-70-07-0G-0, REV 132. PERFORMED A REPAIR IAW STEP 1. REMOVED THE DEBOND MATERIALS AND CLEANED. MEASURE THE DAMAGE SIZE AND LOCATION (L:6",W:1", 11" FROM INBD ESDR CALA2026082518890Access Panel · crackedCRACK INDICATION FOUND ON LEFT WING ACCESS PANEL 543BB HOLE #6 AT 12 O' CLOCK POSITION LOOKING. PERMANENT REPAIR FOR L/HWING INTERSPAR LOWER SKIN (P/N 757-3401-1) OUTBOARD OF THE SPLICE AT WSTA 711.50 PER THE LATEST REVISION OFEC/RA 5720-03672.SDR CALA2026082518878Access Panel · crackedCRACK INDICATION FOUND ON LT WING ACCESS PANEL 543BB HOLE #6 AT 12 O' CLOCK POSITION LOOKING. ACCOMPLISHED REPAIR INSTRUCTIONS PER VT MAE EA 757-5720-13-A4564 REV. ORIGINAL WITH NO DEVIATIONS. PER ECRA 5720-03672 FIG. 1-29 FOR REFERENCE. LT WING INTER SPAR LOSDR CALA2026082118798Access Panel · cracked)EA5720-03647 PER FIGURE 1, CRACK INICATION FOUND ON LT WING ACCESS PANEL 543BB, HOLE NR 6 AT THE 12 O'CLOCK POSTION LOOKING FORWARD. A REPAIR WAS PERFORMED ON LT WING SKIN IAW EC/RA 5720 -03672, & EA 757-5720-13-A4564 REV-.SDR FDEA202608201196Panel · delaminatedRIGHT WING UPPER L/E PANEL ABOVE PYLON AT ISS 337.60 HAS EROSION ACROSS L/E, WITH NUMEROUS FASTENER HEADS PULLING THROUGH SKIN. ALSO FOUND SEVERAL DOUBLE DRILLED HOLES ON THE RT WING LEADING EDGE RIBS AND CHORDS BETWEEN WS 337 & 356. THERE ARE NO PUBLISHEDSDR FDEA202608201189Doubler · damagedAGING AIRCRAFT - LEFT WING LEADING EDGE COMPARTMENT FOUND WITH EXISTING BEADED DOUBLER REPAIR BETWEEN STATION XOS 772 TO XOS 776. EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. ENGINEERING ORDER 1-5100- 7-5001SDR FDEA202608201188Doubler · damagedAGING AIRCRAFT - LEFT HAND WING LEADING EDGE COMPARTMENT FOUND WITH EXISTING BEADED DOUBLER REPAIR BETWEEN STATION XOS 759 TO XOS 763. EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. ENGINEERING ORDER 1-5100- 7SDR FDEA202608201187Doubler · damagedAGING AIRCRAFT - LEFT HAND WING LEADING EDGE COMPARTMENT FOUND WITH EXISTING BEADED DOUBLER REPAIR BETWEEN STATION XOS 625 TO XOS 629. EVALUATED AND FOUND REPAIRED IN ACCORDANCE WITH MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. ENGINEERING ORDER 1-5100- 7SDR FDEA202608201186Doubler · damagedAGING AIRCRAFT - LEFT WING LEADING EDGE COMPART FOUND WITH EXISTING BEADED DOUBLER REPAIR BETWEEN STATION XOS 616 TO XOS 621. LEFT WING LEADING EDGE COMPARTMENT FOUND WITH EXISTING BEADED DOUBLER REPAIR BETWEEN STATION XOS 616 TO XOS 621 EVALUATED AND FOUSDR FDEA202608201173Doubler · crackedLEFT WING- LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 745 FOUND CRACK ABOUT 0.2 INCH. LEFT WING LEADING EDGE COMPARTMENT CRACKED BEADED DOUBLER AT XOS 745. CARRIED OUT REPAIR IAW SRM 57-40-02-2R, REPAIR 15, FIGURE 203. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-SDR SWAA2026092451667Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 561BB, LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026092472212Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661CB T / E, RT WING. REMOVED AND REPLACED THE ACCESS PANEL 661CB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026091483813Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 671CB TRAILING EDGE, RT WING. PERFORMED VISUAL INSPECTION ON REPORTED AREA AND NOT FOUND ELONGATED HOLE ONLY FOUND BURN PAINT AROUND THE HOLE IAW SRM 51-00-06-OG-0. RESTORED PAINT IAW AMM 51-21-99-300-801.SDR SWAA2026091465029Access Panel · elongatedELONGATED HOLE ACCESS PANEL 561BB ON LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026091482156Access Panel · elongatedELONGATED HOLE ACCESS PANEL 561CB AT LT WING. REPAIRED ACCESS PANEL 561CB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR CALA2026082518876Skin Panel · crackedACCOMP ALPHA INSPECT OF EXTERNAL DOUBLER/TR IPLER INTERIM REPAIR ON THE LT WING OTBD LWR SKIN PANEL BETWEEN WSTA 564.5 & 591.5 AT STR L9 PER PART 2, TABLE 1 OF ECRA 5725-01 158. INITIALSDR CALA2026082418831Access Panel · crackedGOUGED NOTED POSSIBLY CRACK AT HOLE #6 LOWER ACCESS PANEL 543BB, LT WING AT 12 OCLOCK LOOKING UP AND FWD. REPAIR ACCOMPLISHED IAW EA 757-5720-13-A4547.SDR CALA2026082018758Access Panel · misinstalledDURING TOWING, LT FUEL LEAKAGE FROM LT SURGE TANK, ACCESS PANEL 541XB. FOUND PANEL HAD BEEN INSTALLED 180 DEGREES OUT OF ALIGNMENT, WITH MISPOSITIONED ALIGNMENT DOWEL THE LIKELY CAUSE FOR FUEL LEAK. FOD CHECK BEFORE PANEL. NO FOD NOTED. INSTALLED THE TANKSDR JR2R20260819263Skin · gougedFOUND GOUGE IN METAL ON LWER SURFACE OF UPPER SKIN OTBD SIDE OF 23 AT WING ACCESS PANEL 541CB. REPAIREDSDR VNAA202610280007Skin Panel · damagedLIGHTNING STRIKE DAMAGE TO RHS WING UPPER FWD AND AFT PLANKS AT WS88 & WS128 BETWEEN STR19 AND STR20. LIGHTNING STRIKE DAMAGE TO RHS WING UPPER FWD AND AFT PLANKS AT WS88 & WS128 BETWEEN STR19 AND STR20 WAS REPAIRED PER REO 690-57-21-573 REV -.SDR SWAA2026091837614Access Panel · crackedCRACKED FLOAT ACCESS PANEL 532QB FUEL TANK AT LT WING. REPLACED FLOAT ACCESS PANEL 532QB FUEL TANK AT LT WING IAW CMM 28-40-11 TASK 28-40-11-000-801-A01 DISASSEMBLY PROCEDURES PAG 3002 AND 3003 STEP 3.A.(3)(A) AND CMM 28-40-11 TASK 28-40-11-400-001-A01 ASSEMBSDR DALA2026081804710Skin · damagedELONGATED HOLES ON CUT OUT LOC BTW RIB14 AND RIB15 FUEL TANK ON RH WING, REPAIRED CUT OUT HOLES PER SRM 57 -21-11-300-002 AND REPLACED GANG CHANNEL AS PER A320 SRM 51-72- 11. (1762554) (AIRCRAFT GROUNDED).SDR VNAA202610280006Skin Panel · damagedLIGHTNING STRIKE DAMAGE TO WING RH UPPER FWD PLANK BETWEEN WS29.76-WS68.00 AND BETWEEN STR19R-STR21R. LIGHTNING STRIKE DAMAGE TO WING RH UPPER FWD PLANK BETWEEN WS29.76-WS68.00 AND BETWEEN STR19R-STR21R WAS REPAIRED PER 690-57-21-576 REV. - -SDR EE4Y2026081724876Skin Panel · corrodedDURING ACCOMPLISHMENT AS PER ALLEGIANT WORK CARD A32X-ZL-500-02-1-002 GENERAL VISUAL INSPECTION OF WING LOWER SURFACE INCLUDING UPPER AND LOWER SURFACES OF SLATS AND FLAPS (EWIS) RELATED TO MPD TASK ZL-500-02, IT WAS FOUND AT RH WING AT MLG SKIN DOUBLER O/B SESDR EE4Y2026081724875Skin Panel · corrodedDURING ACCOMPLISHMENT AS PER ALLEGIANT WORK CARD A32X-ZL-500-02-1-002 GENERAL VISUAL INSPECTION OF WING LOWER SURFACE INCLUDING UPPER AND LOWER SURFACES OF SLATS AND FLAPS (EWIS) RELATED TO MPD TASK ZL-500-02, IT WAS FOUND AT RT WING AT MLG SKIN DOUBLER O/B SESDR R61A2026081700228Skin Panel · damagedWING LEADING EDGE - RH FIXED LE SKIN #4 SLAT TRACK CUTOUT TOP SIDE - CRACK - PERMANENT REPAIR-SDR SWAA2026081997745Panel · delaminatedRIGHT WING UPPER INBOARD FIXED TRAILING EDGE SURFACE PANEL 651AT HAS A 6 INCH CUT WITH A 13" X 17". DELAMINATED AREA REMOVED AND REPLACED RIGHT WING TRAILING EDGE PANEL 651AT IAW AMM 32-11-00.SDR FDEA202608141126Skin · crackedRIGHT WING - NO. 15 LEADING EDGE SLAT TRACK CUT OUT LOWER SURFACE OUT BOARD CORNER FOUND CRACK AT STATION XOS 950 APPROX 0.35" REPAIR CARRIED OUT AT RIGHT WING - NO. 15 LEADING EDGE SLAT TRACK CUT OUT LOWER SURFACE OUT BOARD CORNER AS PER MD-11 SRM 57-40-0SDR U2RA2026091000057Skin · damagedRT WINGLET TIP BROKEN, SUSPECTED LIGHTNING STRIKE. RT WINGLET REPAIRED VIA FLIGHT VEHICLES CONSULTING INC. EO CONTROL NR 26123-1.SDR CALA2026081918729Skin · damagedRIGHT WING FUEL TANK PANEL 640JB LANDING HAS 1 HOLE OUT OF ROUND.PERFORMED REPAIR OF HOLE ON THE LANDING OF PANEL 640JB IAW SRM 57-21-11-300-002. HOLE REAMED TO 0.433 IN., COLD WORKED AND BUSH REPAIR INSTALLED IAW SRM 57-21-11-300-002, 51-44-11/001, 51-48-00/0SDR CALA2026081718648Plate · crackedLOWER LT WING FASTENER HOLE NR 370 HAS A CRACK INDICATION (1E A) INSIDE THE 1ST LAYER OF THE HOLE AT THE 6 O'CLOCK POSITION, REMOVED AND REPLACED PLATE ASSY AF LWR LT WING SKIN IAW SRM 51-40-02-0G-0 AND DWG 757-3400.SDR JR2R20260813858Skin · chafedLH WING LEADING EDGE PANEL ABOVE PYLON CHAFED. REPAIR
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