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 UIEA2026043000269Skin · crackedRHW L/E SKIN NEAR #4 PYLON O/B AREA FOUND CRACK(<P>L/E SKIN CRACK AREA REPAIRED AS PER RI-57-41-18141 REV B. NO FURTHER DEFECTS NOTED</P>)SDR 1Q2R2026061000002Skin · damagedLEFT-HAND WING LEADING EDGE DAMAGED AT RIB SS64.46, 5TH FASTENER HOLE FROM BOTTOM. PERFORMED REPAIR IN ACCORDANCE WITH MHI RJ REO 670-57-41-695 REV. --, DATED APRIL 27, 2026.SDR 2026FA0000706Skin · crackedR/H WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITHNEWSDR 2026FA0000696Skin · crackedRIGHT WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK CORRUGATED SKIN ASSY WITH NEW.SDR 2026FA0000425Skin · corrodedCORROSION, FORWARD CABIN, RT LOWER SKIN, BFS 125.80 TO 157.00.SDR 1Q2R2026061000003Access Panel · damagedRIGHT HAND INBOARD FLAP INNER UPPER SKIN DAMAGED AT FLS 24.00 AND 2IN FROM VANE CRADLE ACCESS PANEL. PERFORMED REPAIR IN ACCORDANCE WITH MHI RJ REO 670-57-52-352 REV. --, DATED MARCH 28, 2017.SDR 4VAA202605190014Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND ON RIGHT WING TRAILING EDGE TOP SKIN OUTBOARD OF NACELLE. IT WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060668.SDR FXGA2026FA0000409Doubler · corrodedR/H SPAR NEEDS REPAIR DOUBLER AT STA 167 REPLACED DUE TO CORROSION AT MAX LIMIT.SDR 4VAA202605180020Access Panel · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE RIGHT HAND FUEL ACCESS PANEL (624ET) APERTURE FRAME. THE CORROSION WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060718.SDR AALA202605217702Skin Panel · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND WING TRAILING EDGE UPPER SKIN PANEL AT FREEZE PLUG LOCATED BETWEEN WS 470.5 AND WS 442.5. REPAIRED SKIN PANEL PER EA 374710.SDR SWAA2026051903904Access Panel · leakingFUEL LEAK FOUND ON LEFT WING CANOE FAIRING<[01] FOUND FUEL LEAK FROM NR 5 DRIPSTICK ACCESS PANEL. RE-TORQUED PANEL PER AMM 28-11-11. FUEL LEAK NOW CLASSIFIED AS A SEEP PER AMM 28-11-00. RE-INSPECT EVERY 7 DAYS; REPAIR WITHIN 730 DAYS. OK TO CONTINUE ON TLD AUTSDR JR2R20260517033Panel · scratchedRH WING LEADING EDGE HAS SCRATCH FWD OF PANEL 616DB AND ON LANDING OF PANEL 616DB. REPAIRSDR JR2R20260517012Skin · corrodedLH OVER PYLON FIXED LEADING EDGE PANEL IS CHAFED. REPAIRSDR IXXA20260612CC01Skin · corrodedRIGHT WING UPPER SKIN HAS CORROSION AT WBL 109.9 AND 70 INCHES FWD OF REAR SPAR.SDR SWAA2026051803121Skin · pulledRIGHT WING LOWER PANEL (651GB) HAS 5 RIVETS PULLED THROUGH AT FWD O/B WIGGLE PLATE. REMOVED AND REPLACED WIGGLE PLATE ASSY IAW SRM 51-40-02 AND REINSTALLED WING PANEL 651GB IAW AMM 57-05-03SDR ABXA20260515163Skin · ground damageDURING LINE OPS IN CVG, A GROUND CREW TOWED STAIRS UNDER THE RIGHT WING AND SCRAPED THE ENTIRE LOWER WING SKIN FROM FRONT SPAR TO REAR SPAR AT APPROXIMATELY WS 962. THE AIRCRAFT WAS MOVED TO A HANGAR AND IS CURRENTLY IN A-CHK IN CVG. BOEING WAS CONTACTED FOR ASDR EE4Y2026051324476Skin · damagedTHIS JOB WAS PERFORMED BY CUSTOMER REQUEST TO REDO EXISTING REPAIR LOCATED AT WING MAIN BOX - RH WING MAIN BOX LOWER SKIN AT RIB-JACKING FITTING. DUE TO THE REPAIR WAS FOUND WITH MISSING TRACEABILITY, IT WAS REMOVED AND A PERMANENT REPAIR IS PERFORMED AS PER ESDR EE4Y2026051324474Skin · temp repairTHIS JOB IS PERFORMED BY CUSTOMER REQUEST, TO REDO AN EXISTING REPAIR LOCATED AT WING MAIN BOX - CRACK FOUND L/H WING LOWER SKIN AFT EDGE BTW RIB 9-10. DUE TO THE REPAIR WAS FOUND WITH MISSING TRACEABILITY, IT WAS REMOVED AND A PERMANENT REPAIR IS PERFORMED ASSDR 2026F00105Wedge · corrodedDURING SANDING OF THE RH WING FOR PAINT REFURBISHMENT, FOUND CORROSION ON RH WING OUTBOARD TRAILING EDGE STRUCTURE NEAR WS 257.47. AFTER EVALUATION, IT WAS DETERMINED THAT THE RH WING TRAILING EDGE WEDGE IS OUT OF LIMITS AND REQUIRES REPLACEMENT.SDR FDEA202605100579Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285 G P12 STEP3.B & STEP5.A.(2) THEN FOUND 01EA CRACK ON THE RH UPPER WING SKIN FASTENER #5. RH UPPER WING SKIN RIB BAY 10 TRAILING EDGE #5 HOLE REPAIRED AS PER B777 SRM 51-40-05- 0G FIGURE 4 TABLE C,51-40-02-0G,51-40-SDR FDEA202605100578Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285 G P11 STEP3.B & STEP5.A.(2) FOUND TWO CRACKS ON THE LT UPPER WING SKIN FASTENER #5. H WING UPPER SKIN IN RIB BAY 10 TRAILING EDGE #5 HOLE REPAIRED AS PER B777 SRM 51-50- 02-0G FINGURE 1,51-40-02-0G,51-10-01-0G,51-20SDR R61A2026051000121Skin · crackedLH WING MAIN BOX LOWER SKIN CLOSE TO RIB 3A AND SPAR II - CRACK - PERMANENT REINFORCING REPAIRSDR SWAA2026061097046Access Panel · elongatedELONGATED HOLE ON ACCESS PANEL 561AB, LT WING. REPAIRED THE ACCESS PANEL 561AB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026060197185Access Panel · crackedCRACK ANGLE ACCESS PANEL 551GB AT LT WING. REPLACED ANGLE AND FASTENERS LOCATED ACCESS PANEL 551GB AT LT WING IAW SRM B737-700 51-10-02, ITEM 9 AND SRM B737-700 51-40-02. MEASUREMENT OF CRACK: L 1.087.SDR IPXA2026051397715Doubler · crackedCRACK - DOUBLER , RT WING L/E PNL 621HB RIB OSS 514.SDR 2026FA0000727Stiffener · crackedL/H WING FWD LWR I/B SKIN, TOP AFT STIFFENER CRACKED. REPLACED WITH NEWSDR 2026FA0000695Skin · crackedR/H WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK CORRUGATED SKIN ASSY WITH NEWSDR SWAA2026060196747Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 561AB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561AB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-9 REPAIR 9.SDR SWAA2026060196748Access 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 SWAA2026060196749Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661CB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661CB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9.SDR SWAA2026060196750Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661BB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-9 REPAIR 9.SDR SWAA2026060196751Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 561BB AT LT WING. REPAIRED ACCESS PANEL 561BB AT LT WING IAW SRM 51-70-04-2R-9 REPAIR 9.SDR SWAA2026060196752Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 561CB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561CB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-9 REPAIR 9.SDR 2026FA0000453Skin · crackedR/H WING AFT WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITHNEWSDR 2026FA0000452Skin · crackedR/H WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITHNEWSDR 2026FA0000451Skin · crackedR/H WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITHNEWSDR CALA2026051116124Skin · crackedLEFT WING NR 2 SLAT COVE SKIN AROUND INBD MAIN TRACK CRACKED. REMOVED, FABRICATED, REPLACED COVE. SKIN COMMON TO NR 2 SLAT IAW SRM 51-40-02-0G-1 AND REF DWG 114N7076.SDR CALA2026051116122Skin · crackedNUMBER 10 SLAT OTBD COVE SKIN CRACKED NEAR 652BB COVER PANEL. REMOVED, FABRICATED, INSTALLED COVE SKIN COMMON TO NR 10 SLAT OTBD IAW SRM 51-40-02-0G AND DWG 114N4075.SDR CALA2026051116120Skin · crackedRIGHT WING, NR 10 SLAT, INNER SURFACE, CLOSE TO INBD TRACK, SKIN HAS A CRACK. REMOVED, FABRICATED, INSTALLED COVE SKIN COMMON TO NR 10 SLAT IAW SRM 51-40-02-0G AND DWG 114N4075.SDR 2026FA0000341Skin · corrodedCORROSION WAS FOUND ON RIGHT HAND WING UPPER SKIN COMMON TO AFT SPARSDR SWIA2026050777014Skin · corroded640BB WING PLANK HAS CORROSION AROUND ENTIRE OPENING. (C-CHECK RO 08/28/2026)REPAIRED CORROSION DAMAGE AROUND FUEL PANEL 640BB OPENING IAW BOMBARDIER REO 601R-57-21-030, REV -L, DATED 2014-02-05. BOND AND LEAK CHECKS GOOD. COMPLETED AND ATTACHED TASKCARD 51-SDR IPXA2026051439413Skin · cracked- CRACK - SKIN, R/H WING T/E NO.5 FLAP FAIRING (REPAIR). 1. I.A.W. 747-8F SRM 57-53-70-2R-1 REFER TO SRM 51-70-04-2R-1 AND SRM 51-30-10-0G-0 REV. 48 PERFORM REPAIR AS BELOW STEP : REMOVE THE CRACK MATERIALS AND CLEAN. MEASURE THE DAMAGE AREA ( DIA : 1", 32" SDR IPXA2026051439256Skin · debondedDISBOND - SKIN, AFT SIDE OUTBD FACE OF L/H WING NO.1 FLAP TRACK AFT FAIRING (REPAIR). I.A.W. B747 NDT MANUAL PART 1, 51-01-01 AND PART 4, 51-00-05, REV.182 TO PERFORM NDT/UT FOR THE POST REPAIRED AREA INCLUDED THE AREA WAS HOT PLUS WITHIN 6" ALL AROUND. RESULSDR IXXA20260501001Skin · corrodedCORROSION ON THE LOWER SURFACE OF THE RIGHT WING LOWER SKINSDR SWIA2026050577204Skin · chafedRIGHT LOWER WING PLANK AT RBL45 AT THE AFT SPAR HAS CHAFING DAMAGE. REMOVED DAMAGE AND REPAIRED RIGHT LOWER WING PLANK AT RBL 45 AT AFT SPAR IAW REO 601R-57-21-880, REV-D. TASK CARD 51-900-1003-SKY. NO WEIGHT CHANGE.SDR SWIA2026050577156Skin · chafedLEFT LOWER WING PLANK AT LBL 45 AT THE AFT SPAR HAS CHAFE DAMAGE. REPAIRED LT LOWER WING PLANK AT LBL 45 AT THE AFT SPAR CHAFING DAMAGE IAW REO 601R-57-21-880, REV D.SDR DXTR2026050100314Skin · corrodedPOSSIBLE CORROSION ON LOWER LT WING SKIN AT TIP CAP. REMOVED CORROSION FROM SKIN REF SRM 51-10-01. NDT SERVICES PROVIDED BY TOLEDO JET CENTER, CRS 2TJR420B ON WORK ORDER 85280. NO CRACKS NOTED IN THE AREA OF INSPECTION AT THIS TIME. COMPLIED WITH STEPS 1 TSDR 2026FA0000726Stiffener · crackedL/H WING FWD LWR I/B SKIN, TOP AFT STIFFENER CRACKED. REPLACED WITH NEWSDR FDEA202604300524Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285 G P12 STEP 3.B.(1) & STEP 5.A.(2) THEN FOUND 02EA CRACK AT RH WING UPPER WING SKIN COMMON TO FASTENER 5. RT WING UPPER SKIN 5 FASTENER HOLE CRACKED AREA REPAIRED IAW SRM 51-50-02-0G, FIG 1, SRM 51-40-02-0G, FIG 12, SDR FDEA202604300523Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285 G P11 STEP 3.B.(1) & STEP 5.A.(2) THEN FOUND 02EA CRACK AT LT WING UPPER WING SKIN COMMON TO FASTENER 5. LT WING UPPER SKIN NR 5 FASTENER HOLE CRACKED AREA REPAIRED IAW SRM 51-50- 02-0G, FIGURE 1, SRM 51-40-02-0G F
Back to JASC 5730