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 SWAA2023101700425Panel · elongatedLEADING EDGE PANEL 521FB HAS ELONGATED FASTENER HOLES<[01] APPLIED PERMANENT REPAIR ON DAMAGE AREA ON PANEL #521FB AS MARKED AS PER B737 SRM 57-41-01-2R-1; B737 SRM 51-70-04-2R-9 PARAG (4-D-M) AND B737 SRM 51-70-04-2R-0 PARAG (4-L-M-N). MATERIAL USED PO#179112SDR FDEA202309131588Doubler · noneEXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 732. EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XOS 732 EVALUATED AND FOUND REPAIRED IAW MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. EO # 1- SDR FDEA202309131587Doubler · crackedEXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XORS 525 EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE BEADED DOUBLER STATION XORS 525 EVALUATED AND FOUND REPAIRED NOT IAW MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. EXISDR DALA2023091407543Unknown · unknownSHIP 3274 CORROSION ON LOWER SURFACE OF UPPER SKIN TRAILING EDGE AT LEVEL RIB 7 LH WING. CORRECTIVE ACTION: COMPLIED WITH ERA 611211-14 REV ORIGINAL. (2967968)SDR JGVR20230913002Unknown · unknownREPAIRED CORRODED AREAS OF THE UPPER INBOARD SKINS OF THE LH & RH WINGS ALONG AND UNDERNEATH THE DRAG ANGLES (WING-TO-FUSELAGE FAIRING ATTACH ANGLES) BY R&R THE DRAG ANGLES, BLENDING CORRODED AREAS, PERFORMING NDT AND REPORTING RESULTS FOR REPAIR DISPOSITION. SDR FDEA202309121582Doubler · crackedLEFT HAND WING LEADING EDGE FIXED PANEL LOWER SKIN BEADED DOUBLER FOUND CRACK AT STATION XOS 663. LEFT HAND WING LEADING EDGE FIXED PANEL LOWER SKIN DOUBLER AT STATION XOS 663 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLSDR FDEA202309121581Doubler · crackedRIGHT HAND WING LEADING EDGE FIXED PANEL LOWER SKIN BEADED DOUBLER FOUND CRACK AT STATION XOS 791. RIGHT HAND WING LEADING EDGE FIXED PANEL LOWER SKIN DOUBLER AT STATION XOS 791 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR SDR FDEA202309121580Doubler · crackedRIGHT HAND WING LEADING EDGE FIXED PANEL LOWER SKIN BEADED DOUBLER FOUND CRACK AT STATION XOS 785. RIGHT HAND WING LEADING EDGE FIXED PANEL LOWER SKIN DOUBLER AT STATION XOS 785 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR SDR FDEA202309121579Doubler · unknownRIGHT HAND WING LEADING EDGE FIXED PANEL LOWER SKIN BEADED DOUBLER FOUND CRACK AT STATION XOS 580. RIGHT HAND WING LEADING EDGE FIXED PANEL LOWER SKIN DOUBLER AT STATION XOS 580 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR SDR FDEA202309121578Doubler · crackedRIGHT HAND WING LEADING EDGE FIXED PANEL LOWER SKIN BEADED DOUBLER FOUND CRACK AT STATION XOS 583. RIGHT HAND WING LEADING EDGE FIXED PANEL LOWER SKIN DOUBLER AT STATION XOS 583 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR SDR FDEA202309121577Doubler · crackedRIGHT HAND WING LEADING EDGE LOWER ACCESS PANEL ATTACHMENT DOUBLER FOUND CRACK AT STATION XOS 994. RIGHT HAND WING LEADING EDGE LOWER ACCESS PANEL ATTACHMENT DOUBLER AT STATION XOS 994 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-03-2R FIGURE 2SDR FDEA202309121576Skin · crackedLEFT WING DROOPED LEADING EDGE FLEX SKIN FOUND CRACK AROUND FASTENER HOLE AREA AT STATION XDLE 314. LEFT HAND WING DROOPED LEADING EDGE FLEX SKIN AT STATION XDLE 314 REPAIR CARRIED OUT PER MD-11 SRM 57-40-01-2R REPAIR 5 FIGURE 201. REPAIR CLASSIFIED AS MAJSDR SWAA2023102699096Panel · delaminatedLEFT WING L/E PANEL 521KB DELAMINATED AT CUTOUT CORNERS<[01] LEFT WING L/E PANEL 521KB WAS DELAMINATED AT CUTOUT CORNERS AND REPAIRED IAW SRM 51-70-05-2R-6. FINAL FINSIH WILL BE ACCOMPLISHED ON FAULT: TTG8Q00NQTZ;[02] VERIFIED CORRECTIVE ACTION 1.SDR FDEA202309111696Skin · corrodedMAIN CARGO - CTR WING FWD UPPER SKIN PANEL - CORRISION FOUND AT S17, RBL 80-105, DIMENSIONS 13" X 4". COMPLIED WITH EA 958 "WING-PLATES AND SKINS- CENTER WING UPPER FORWARD SKIN - CORROSION REWORK" WORK CARD T 1-5730-T0376479 P1 "MAJOR REPAIR"SDR EE4Y2023091118385Skin Panel · corrodedDURING THE ALLEGIANT WORD CARD ZL-540-01-1-001 ,FOUND AT LH BOTTOM WING SKIN AREA AROUND MANHOLE 540JB WITH CORROSION.DUE REWORKED AREA WAS FOUND OUT LIMITS IAW A320 SRM TASK 57-21-11-283-003 PARAG.2A FLOWCHART FIG 001 (SHEET 1 AND 2). AIRBUS WAS CONTACTED RSDR AWKA202406170001Skin Panel · corrodedCORROSION FOUND ON FUEL PANEL LAND 522DB. ACCOMPLISHED FIELD REPAIR FR-750-0220-11461, REV - "FIELD REPAIR - CORROSION, LH WING, L WR SKIN, PANEL 522DB.SDR AALA202312065920Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL UPPER SURFACE AT WS 6840, RIB 19. REPAIRED SKIN PANEL PER EA 348172.SDR AALA202312066675Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE BETWEEN WS 8483 AND WS 11441, AT RIB 21. REPAIRED SKIN PANEL PER EA 348172.SDR AALA202312063514Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT RIB 14. REPAIRED SKIN PANEL PER EA 348172.SDR SWAA2023102098453Panel · crackedCRACK ACCESS PANEL 661AB TRAILING EDGE AT RT WING 2023-577757<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: A18135081; DUE DATE: 21-JUL-24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18185781 DUE DATE: 24/JAN/24.;[03] TOOL USED HOTBONDER P/N: HCS9200B-AV SDR SWAA2023102098439Panel · crackedCRACK ACCESS PANEL 661CB TRAILING EDGE AT RT WING 2023-577763<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: A18135081; DUE DATE: 21-JUL-24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18185781 DUE DATE: 24/JAN/24.;[03] TOOL USED HOTBONDER P/N: HCS9200B-AV SDR SWAA2023102098455Panel · crackedCRACK ACCESS PANEL 561BB TRAILING EDGE AT LT WING 2023-577759<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: A18135081; DUE DATE: 21-JUL-24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18185781 DUE DATE: 24/JAN/24.;[03] TOOL USED HOTBONDER P/N: HCS9200B-AV SDR SWAA2023100998326Access Panel · crackedCRACK ACCESS PANEL 561BB TRAILING EDGE AROUND HOLES LT WING 2023-575267<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: B20189527 DUE DATE: 26-DEC-23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18185781 DUE DATE: 24-JAN-24.;[03] TOOL USED SCALE P/N: SPX621 SDR DALA2023091507584Unknown · unknownSHIP 197 DURING PDC FOUND ON R/H BOTTOM OUTBOARD ACCESS LUBRICATION PANEL 621AJB MISSING. CORRECTIVE ACTION: REINSTALLED NEW PANEL AS PER B767-300 AMM 57-41. CDL REMOVED. OK FOR SVC. (4570612)SDR DALA2025090206466Skin · dentedER/A 611604-14; WINGS / OUTER WING / L.E. RHS / SKIN XOS 250-260 / DENT. ER/A 611604-14 HAS BEEN REVISED CURRENT STATUS IS REV. A. (2960169)SDR SWIA202311240908Unknown · chafedLH LOWER WING SKIN HAS CHAFING DAMAGE AT APPROX. WS264.00 INBRD AND OUTBRD OF FAIRINGS LOCATION AS MARKED (C-CHECK RO 11/20/2023) REPAIRED LH LWR WING SKIN CHAFFING REF REO 670-57-21-958 REV -- DATED: 2023-10-03. COMPLIED WITH 51-900-1002-SKY.SDR DALA2023091107418Unknown · unknownSHIP 692 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DRAG BRACE AS FOLLOW: HOLE #1 CORROSION ON SKIN BTW 9 O CLOCK POSITION, HOLE #2 CORROSION FITTING BTW 1 TO 2 O CLOCK POSITION, HOLE #3 CORROSION ON SKIN AND FITTING BWT 6 TO 7 OSDR 2023F00271Skin · damagedAIRCRAFT NO. 2 TIRE BLEW OUT ON TAKE-OFF ROLL, CREW ABORTED TAKEOFF AND TAXIIED BACK TO THE FBO WHERE STRUCTURE DAMAGE TO THE WING INBD FIXED T.E. BOX LOWER SKIN WHERE IT LOOKS LIKE A CHUNK OF RUBBER FROM THE TIRE HIT IT WAS DISCOVERED.SDR VNAA202310260003Skin · wornWEAR ON LEADING EDGE PANEL 522AL AT LH WING. WEAR ON LEADING EDGE PANEL 522AL AT LH WING WAS REPAIRED PER EA 23-C9-57-1343 RIV. IR SECTION III - PERMANENT REPAIRSDR VNAA202310260002Skin · wornWEAR ON FIXED LEADING EDGE (622AR,622BR) AT RH WING. WEAR ON FIXED LEADING EDGE (622AR,622BR) AT RH WING WAS REPAIRED PER EA 23-C9-57-1356 REV. IR SECTION III - PERMANENT REPAIRSDR JR2R20230906566Skin · chafedLH WING FIXED LEADING EDGE ABOVE PYLON CHAFEDSDR 2024FA0000124Skin · crackedR/H WING AFT WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH NEWSDR 2024FA0000106Skin · crackedR/H WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH NEWSDR AALA202312062190Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE BETWEEN WS 6840 AND WS 7176, AT RIB 19. REPAIRED SKIN PANEL PER EA 348172.SDR DALA2023090607306Unknown · unknownSHIP 0649 DELAMINATION ON FIXED LEADING EDGE SKIN AT LH WING BTW 155 169 AND 155 213. CORRECTIVE ACTION: DELAMINATION ON FIXED LEADING-EDGE SKIN WAS REPAIRED PER B757- 200 SRM 51-70-17. (4190306)SDR DALA2023090507217Unknown · unknownSHIP 3274 CORROSION ON LOWER SURFACE OF UPPER SKIN TRAILING EDGE AREA AT LEVEL RIB 8 LH WING. CORRECTIVE ACTION: FOUND CORROSION WITHIN LIMITS. (2953223)SDR DALA2023090507242Unknown · unknownSHIP 0669 DAMAGES WERE FOUND IN LH ENG DRAG FTG CLAMP-UP HOLES AS FOLLOW: HOLE #3 CORROSION ON SKIN AND FITTING AT 3 CLOCK POSITION; HOLE #4 CORROSION ON FITTING AT 3 CLOCK POSITION; HOLE #7 CORROSION ON SKIN AT 3 CLOCK POSITION IN REFERENCE TO JOB 080-0001 / SDR DALA2023090507240Unknown · unknownSHIP 0669 AD/AA - DAMAGES WERE FOUND IN LH ENG DRAG FTG CLAMP-UP HOLES AS FOLLOW: HOLE #15 GOUGES ON SKIN BTW 12 TO 2 O CLOCK POSITION IN REFERENCE TO JOB 085-0001 / CARD 5720-01100-05A. CORRECTIVE ACTION: REF ERA 593262-14. (2949787)SDR DALA2023090507231Unknown · unknownSHIP 3411 - MISC - DURING TAXI TO GATE AFTER LANDING, THE RH WINGTIP MADE CONTACT WITH AN OAL AIRCRAFT. CORRECTIVE ACTION: PER ER/A 611768-14, DETAILED INSPECTION VISUAL, EVALUATION AND MEASUREMENT HAS BEEN PERFORMED ON RH WING TIP. NO FURTHER DAMAGE FOUND. PESDR SWIA20231027901Unknown · chafedLH LWR WING PLANK FWD OF THE MLG CUTOUT, W.S. 45.0 TO W.S. 47.61, HAS CHAFFING. (C-CHECK RO 10/29/2023) BLENDED OUT CHAFE ON LH LOWER WING PLANK FWD OF THE MLG CUTOUT, W.S 45.0 T0 47.61. REF CRJ 200 SRM 51-12-00RECEIVED ENGINEERING SUPPORT , FOR CHAFFING BSDR GTIA2023090537458Skin · damagedTOOL MAK ON LH WING LOWER SURFACE FUEL TANK HOLE CUTOUT BTW RIB 17 AND RIB 18 DIMENSION: L=N/A W= N/A D= 0.273 RAF-01-3073925-02 GENERATED-PERFORMED PERMANENT REPAIR ON CUTOUT ON LH WING OF FUEL TANK PANEL IAW A320 SRM 57-21-11-300-002. THIS REPAIR IS CATEGORYSDR GTIA2023090537457Skin · damagedTOOL MARK LOWER SURFACE CUTOUT FUEL TANK BTW RIB 16 AND RIB 17 ON RH WING. RAF-01 3073927-01 GENERATED-PERFORMED PERMANENT REPAIR ON CUTOUT OF RIB 16 AND RIB 17 OF RH WING FUEL TANK PANEL IAW A320 SRM 57-21-11-300-002. THIS REPAIR IS CATEGORY B. REQUIRED INSPESDR GTIA2023090537455Skin · damagedTOOL MARK LOWER SURFACE HOLE CUTOUT FUEL TANK BTW RIB 13 AND RIB 14 ON RH WING. RAF-01 3073926-02 GENERATED-PERFROMED PERMANENT REPAIR ON CUTOUT OF RIB 13 AND RIB 14 ON RH WING OF FUEL PANEL IAW A320 SRM 57-21-11-300-002. THIS REPAIR IS CATEGORY B. REQUIRED INSDR GTIA2023090537454Skin · damagedTOOL MARK LOWER SURFACE HOLE CUTOUT FUEL TANK BTW RIB 18 AND RIB 19 ON RH WING. RAF-01 3073927-02 GENERATED-PERFORMED PERMANENT REPAIR ON CUTOUT OF RIB 18 AND RIB 19 ON RH WING OF FUEL TANK PANEL IAW A320 SRM 57-21-11-300-002. THIS REPAIR IS CATEGORY B. REQUIRSDR GTIA2023090537453Skin · damagedTOOL MARK LOWER SURFACE HOLE FULE TANK BTW RIB 13 AND RIB 14 ON LH WING RAF-01 3073924-02 GENERATED-PERFORMED PERMANENT REPAIR ON CUTOUT OF FUEL TANK PANEL IAW A320 SRM 57-21-11-300-002. THIS REPAIR IS CATEGORY B. REQUIRED INSPECTION THRESHOLD FROM AIRCRAFT FISDR GTIA2023090537452Skin · damagedTOOL MARK ON LH DALING LODNER SRFACE FUEL TANK HOLE CUTOUT BTW RIB 14 AND RIB 15 DIMENSIONS: L=N/A DN=N/A D=0.67" RAF-01 3073929-02 GENERATED -PERFORMED PERMANENT REPAIR ON CUTOUT OF RIB 14 AND RIB 16 IS ON LH WING OF FUEL TANK PANEL IAW A320 SRM 57-21-11-300-SDR JGVR20230901001Unknown · unknownBLENDED TWO AREAS OF CORROSION ON THE UPPER SURFACE OF THE UPPER INBOARD WING SKIN AT THE TRAILING EDGE OF THE LH WING AND TWO ADDITIONAL AREAS ON THE FORWARD EDGE OF THE SAME SKIN PANEL. PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPOSITION. CLEANED, TREASDR IPXA2023092094205Doubler · crackedINSPECTION TYPE:1CRH WING L/E ACCESS PANEL 623MB LANDING HAS A CRACK.FABRICATED REPAIR DOUBLER IAW SRM 53-15-63.SDR DALA2023090107156Unknown · unknownSHIP 5643 RH ENG DRAG FTG CLAMP-UP HOLE #12 HAS GOUGES AND CORROSION NOTED IN SKIN LOCATED AT 7 AND 9 O'CLOCK POSITION. CORRECTIVE ACTION: REAMED HOLE #12 IN THE SKIN CONCENTRICALLY UP TO 0.06557" AND C/ W HFEC OPEN HOLE INSPECTION NO DEFECTS NOTED, ASSET#'S 2SDR AALA202312067785Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING SKIN PANEL UPPER SURFACE AT WS 6401, AT RIB 17. REPAIRED SKIN PANEL PER EA 348172.
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