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 JJBA20230522013Skin · damaged2 INCH HOLE ON RH WING LEADING EDGE 2 FT FROM THE WINGLET. REMOVED AND REPLACED RH #3 LEADING EDGE. OPS AND LEAK CHECK SATSDR 2023F00147Wing · corrodedCORROSION WAS FOUND BETWEEN WING STA 22 TO W ST 49 LEFT AND RIGHT WING LOWER SHEET METAL LAMINATES, ON FWD AND AFT SPARS LOWER RIVET AREASSDR 2023F00146Wing · corrodedCORROSION WAS FOUND ON RIGHT WING STA 22 TO W STA 49 LOWER SHEET METAL LAMINATE ON FWD SIDE UNDER SPAR AREA AND AFT SIDE UNDER SPAR AREASDR FDEA202305170891Skin · damagedRIGHT WING INBOARD LEADING EDGE DAMAGED AT AUX TRACK CUTOUT. PERFORMED PERMANENT REPAIR ON RIGHT WING INBOARD LEADING EDGE AT AUX TRACK CUTOUT IAW DX B757 SRM 57-41-01-2R FIG 201 SHEET 2 AND 51-70-08-0G.SDR DALA2023051904005Unknown · unknownSHIP 6801 AD - AA // DAMAGES WERE FOUND AT RH ENG DRAF FTG CLAM-UP IN HOLES AS FOLLOW: HOLE #1 CORROSION ON SKIN AND FITTING ALL AROUND, HOLE #2 SCRATCHES ON SKIN ALL AROUND AND ELONGATED FITTING, HOLE #3 CORROSION ON SKIN AND FITTING ALL AROUND, HOLE #4 CORROSDR DALA2023051904004Unknown · unknownSHIP 6801 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DRAG BRACE AS FOLLOW: HOLE #1 CORROSION AND SCRATCHES ON SKIN AND FITTING BTW 6 TO 12 O CLOCK POSITION. HOLE #2 CORROSION ON SKIN AND FITTING ALL AROUND HOLE. HOLE #3 CORROSIONSDR CALA2023051701526Skin · cracked2(EA) CRACK INDICATIONS FOUND: L/H UPPER WING SKIN & DRAG FITTIN G FASTENER HOLE #2, IN UPPER LAYER(SKIN) AT 3 & 9 ''OCLOCK POSITI ONS. FLIGHT CYCLES THEREAFTER." REPAIRED #2 HOLE AT L/H WING SKIN & I/B DRAG FITTING PER REO-G24 "ACCOMPLISH INITIAL INSPECTIONSDR DALA2024041704521Skin · crackedSHIP 6801 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING / CRACKS / CORROSION & GOUGES. CORRECTIVE ACTION: REF ERA 608123-14AD.SDR R61A2023060300314Skin · crackedLHW LWR SURFACE SKIN ON RIB 18, INBD OF FLAP TRACK #4 FOUND WITH CRACK APPROX 4" IN LENGTH. L/H WING, LOWER SKIN AT RIB 18 I/B OF FLAP TRACK #4 REPAIRED IAW ETD2023-170-12549 REV A. HFEC ROTOPROBE AND LPI INSPECTION C/OUT. "NO RACKS FOUND"SEE AWS FOR DETAILSDR CALA2023051701551Access Panel · missingLEADING EDGE SLAT MECHANISM LUBRICATION ACCESS DOOR PANEL MISSING AT LEFT HAND WING SLAT #5 ACCESS PANEL AREA CHECKED FOR FURTHER DAMAGE, NO DAMAGE PRESENT. CDL APPLIED CDL COMPLIED WITH. DISPATCH DESK: 63 NAME: AS DATE: 14-MAY-23- EADING EDGE SLAT MECHANISSDR ASAA2023051345989Skin Panel · corrodedR/H WING TOP SKIN PANEL 2 T/E OVERHANG HAS EXTENSIVE CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY B PERMANENT REPAIR OF R/H WING TOP SKIN PANEL 2 TEOH RIBS 9-27 IAW ASA EA A320-57EA-0187 REV 00 AND AIRBUS RDAF 81250074/004/2023 ISSUE A DATED 25-OCT-2023.SDR ASAA2023051345907Skin Panel · corrodedL/H WING/TOP SKIN PANEL 2/TRAILING EDGE OVERHANG BETWEEN RIB 6 AND 27 CORROSION. GROUNDED - YES. REPAIRED L/H WING/TOP SKIN PANEL 2 REAR SPAR AT RIB 15-18 IAW ASA EA A320-57EA-01874 REV 00 AND AIRBUS RDAF 81253170/060/2023 ISSUE A DATED 21-OCT-2023 CATEGORY BSDR AALA202307184242Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING SKIN PANEL AT OVERWING REFUEL CUTOUT HOLE FOR FUEL CAP BETWEEN WS 10204 AND WS 10729, BETWEEN RIBS 19 AND 20. REPAIRED SKIN PANEL PER SRM 57-21-11-300-006.SDR YENA2023051600513Unknown · unknownFLT#2448, SDQ-FLL. 'WHILE TAXING INTO PARKING POSITION STAIRS SCRAPE UNDER THE NEATH AREA OF THE LEFT WING CLOSET TO WINGTIP AND WINGTIP LIGHTS; ACCOMPLISHED LH WING TIP INSPECTION IAW AMM 05-51-35. FOUND NO MISSING FASTNERS OR DEEP SCRATCHES. PLACED LH WING TSDR AWKA202405310001Skin · corrodedCORROSION FOUND ON FUEL PANEL LAND 611AB. ACCOMPLISHED FIELD REPAIR FR-750-0274-11708 REV. A DATED 01-MAY-23 "FIELD REPAIR- CORROSION, RH WING, LOWER SKIN, 611AB FUEL LAND.SDR DALA2023051603913Unknown · unknownSHIP 660 A.D.//A.A. DAMAGE WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #3 CRACK ON FITTING BTW 5 TO 6 O CLOCK POSITION IN REF. CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00580:[ A.D.//A.A] LH ENG DRAG FTG CLAMP-UP HOLE #3 WASSDR DALA2023051503823Unknown · unknownSHIP 660 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 608209-14AD. CORRECTIVE ACTION: REF ERA 608209-014AD. (2762467)SDR DALA2023051103724Unknown · unknownSHIP 688 [AD//AA DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DRAG BRACE AS FOLLOWS: HOLE #12 CORROSION ON SKIN AND FTG BTW 5 AND 6 CLOCK POS, HOLE #14 CORROSION ON FTG AT 10 CLOCK POS AND GOUGES (02) ON FTG AT 5 AND 7 CLOCK POS, HOLE #15 SCRSDR DALA2023051103723Unknown · unknownSHIP 688 [A.D // A.A DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DRAG BRACE AS FOLLOWS: HOLE #4 CORROSION ON SKIN AND FTG AT 10 CLOCK POS AND GOUGES (02) ON FTG AT 4 AND 6 CLOCK POS, HOLE #5 GOUGES (02) ON FTG LOWER EDGE AT 3 AND 9 CLOCK POSSDR DALA2023051003697Unknown · unknownSHIP 688 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 608185-14AD. CORRECTIVE ACTION: REF ERA 608185-14AD. (2757694)SDR DALA2023051003691Unknown · unknownSHIP 688 IN REF. CARD 5720-01100-05A STEP 13: DAMAGED FASTENERS 13,14 15 AND 18 WERE FOUND. CORRECTIVE ACTION: SUMMARY OF NRC 00340: A.D. // A.A:BOLTS 13,14 15 AND 18 WERE REPLACED PER PRI 608182-14 REV. 2 AND ER/A 608182-14AD REV. ORIG. SEC 1.(2757758)SDR DALA2023050803572Unknown · unknownWEAR AND ELONGATED FASTENER HOLE AT FUEL ACCESS PLATE 520MB LH WING. SUMMARY OF NRC 459: FUEL ACCESS PLATE 520MB WAS NOT POSSIBLE REPAIR AS PER B717-200 SRM-57-10-01-2R-2 PROCEDURE 2 REPAIR 2 PAR 5 B. CONDITION II, AND WAS REPLACED PER B717 AIPC 57-23-01- 01-1SDR DALA2023050803571Unknown · unknownWEAR AND ELONGATED FASTENER HOLE AT FUEL ACCESS PLATE 620PB RH WING. SUMMARY OF NRC 470: FUEL ACCESS PLATE 620PB DUE TO REPAIR OF WAS NOT POSSIBLE AS PER B717-200 SRM-57-10-01-2R-2 PROCEDURE 2 REPAIR 2 PAR. 5 B. CONDITION II AND WAS REPLACED PER B717 AIPC 57-2SDR CALA2023052601672Winglet · damagedEVIDENCE OF LIGHTNING STRIKE RIGHT UPPER WINGLET 2 LOCATIONS DRAWING SHOWS INTERIOR AND EXTERIOR FACING SIDES FOR DAMAGE LOCATION & SIZE. INITIATED DIP FOR 30 DAYS PERFORMED INTERIM REPAIR WITH TYPE 1 SPEED TAPE OF LIGHTNING STRIKES AFTER FINDING DAMAGE WAS WSDR IPXA2023051993272Skin · puncturedINSPECTION TYPE:3C*** MAJOR REPAIR *** R/W FIXED L/E SKIN HAS TWO PUNCTURES THROUGH SKIN O/B OF SLAT TRACK BETWEEN STA XIS=250 - XIS=263.REPAIRED SKIN AT THE R/H FIXED L/E O/B OF SLAT TRACK BETWEEN STA XIS=250 - XIS=263 IAW VTSAA EA 011-5730-01-A9957 I/R, UPS SDR DALA2023051003689Unknown · unknownSHIP 688 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DRAG BRACE AS FOLLOW: HOLE #14 CORROSION ON SKIN AND FITTING BTW 2 AND 4 O CLOCK POSITION. HOLE #18 CORROSION ON FITTING BTW 4 AND 5 O CLOCK POSITION. IN REF. CARD. CORRECTIVE ASDR DALA2023050903645Unknown · unknownSHIP 6707 A.D.//A.A. DAMAGES WERE FOUND ON COUNTERSINK HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #3 CORROSION ON COUNTERSINK BTW 4 TO 7 O'CLOCK POSITION, HOLE #4 CORROSION ON COUNTERSINK BTW 3 TO 6 O'CLOCK POSITION, IN REF. CARD. CORRECTIVSDR DALA2023050903644Unknown · unknownSHIP 6707 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #3 CORROSION ON SKIN AND FITTING ALL HOLE, HOLE #4 CORROSION ON SKIN BTW 1 TO 3 O'CLOCK POSITION AND FITTING BTW 7 TO 10 O'CLOCK POSITION, HOLE #5 COSDR DALA2023110909247Unknown · unknownSHIP 688 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 608182-14AD. CORRECTIVE ACTION: RER ERA 608182-14AD. (2752818)SDR VNAA202306220006Skin · corrodedCORROSION ON WING RH BETWEEN WS. 398.93 AND WGLTS 12.5. CORROSION ON WING RH BETWEEN WS. 398.93 AND WGLTS 12.5 WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS REPAIR PER REO 690-57-00-103 REV --SDR VNAA202306220004Skin · corrodedCORROSION ON WING LH BETWEEN WS. 398.93 AND WGLTS 12.53. CORROSION ON WING LH BETWEEN WS. 398.93 AND WGLTS 12.53 WAS REMOVED PER CRJ-900 51-21-06-001-001-A01 AND WAS REPAIR PER REO 690-57-00-104 REV --SDR DALA2023050803599Unknown · unknownSHIP 688 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 608182-14AD. CORRECTIVE ACTION: REF ERA 608182-14AD. (2752815)SDR DALA2023050803596Unknown · unknownSHIP 6707 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #11 CORROSION ON SKIN BTW 10 TO 2 O'CLOCK POSITION, HOLE #13 CORROSION ON SKIN BTW 2 TO 7 O'CLOCK POSITION, HOLE #14 CORROSION ON SKIN BTW 8 TO 3 O'CSDR DALA2023050803595Unknown · unknownSHIP 6707 LOOSE FASTENER NBR 2 ON RH DRAG FITTING. CORRECTIVE ACTION: SUMMARY OF NRC:00125 FASTENER #2 WAS REPLACED PER ERA 576407- 14AD REV D SECTION VI : PERMANET REPAIR.SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. (2753227)SDR DALA2023050803594Unknown · unknownSHIP 6707 AWR AD AA IN REF AMDS 5720-01100-02B: WEAR ON FASTENERS NBR: 1, 3, 4, 5 AND 8 OF RH DRAG FITTING. CORRECTIVE ACTION: SUMMARY OF NRC 00147: FASTENER #1, 3, 4, 5 AND 8 WERE REPLACED PER ERA 576407-14AD REV D SECTION I : PERMANET REPAIR. (2753075)SDR DALA2023050803593Unknown · unknownSHIP 6707 AWR AD AA IN REF AMDS 5720-01100-02A: WEAR ON BOLTS NBR 1, 2, 4, 5, 7 AND 10 AT LH DRAG FITTING. CORRECTIVE ACITON: SUMMARY OF NRC:00209 BOLTS NBR 1, 2, 4, 5, 7 AND 10 AT LH DRAG FITTING WERE REPLACED PER PRI 576482-14 REV 2. PART D STEP 3 TO 4 AND ESDR DALA2023050803592Unknown · unknownSHIP 6707 AWR AD AA, IN REF AMDS 5720-01100-02A: LOOSE FASTENERS NBR 3 AND 9 ON LH DRAG FITTING. CORRECTIVE ACTION: SUMMARY OF NRC:00161: FASTENERS NBR 3 AND 9 ON LH DRAG FITTING WERE REPLACED PER PRI 576482-14 REV 2 PART D STEP 3 TO 4 AND ERA 576482-14AD REV SDR DALA2023050503538Unknown · unknownSHIP 6708 AD RELATED 5720-01100-04A DURING OPEN HOLE INSPECTION HOLE FOUND 2 CRACKED IN THE SKIN LAYER AND FITTING LAYER THE CRACK IN THE SKIN LAYER IS AT THE 10:00 POSITION WITH A LENGTH OF 0.109 THE CRACK IN THE FITTING LAYER IS AT THE 2:00 POSITION WITH A LSDR DALA2025021701171Skin · damagedSHIP 6708 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 608072-14AD. CORRECTIVE ACTION: REF ERA 608072-14AD. (2748108)SDR AALA202307196591Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIBS 10 AND 11. REPAIRED SKIN PANEL PER EA 345131.SDR GTIA2023050437159Access Panel · damagedELONGATED HOLE ON CUT OUT OF ACCESS PNL 540KB FUEL TANK LH WING. RAF-01 3057631-02 GENERATED-PERFORMED PERMANENT REPAIR ON CUTOUT OF ACCESS PANEL 540KB FUEL TANK LH WING IAW A320 SRM 57-21-11-300-002 AND EA# 57-0151-23. THIS REPAIR IS CATEGORY A. REF NR 2023-SDR GTIA2023050437153Panel · corrodedCORROSION FOUND ON LH WING RIB 19-20. RAF01 3117470-02 CREATED.-VERIFIED LTPR J/C # 5001231843-0010 HAS BEEN ACCOMPLISHED AND COMPLIED WITH EA 5721-2330 REV. N/ASDR GTIA2023050437152Panel · corrodedCORROSION FOUND ON RH WING RIB 20-21. RAF01 3117470-01 CREATED.-VERIFIED LTPR J/C # 5001231877-0010 HAS BEEN ACCOMPLISHED AND COMPLIED WITH EA 5721-2329 REV 00SDR DALA2023050403474Unknown · unknownSHIP 6708 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 608072-14AD. CORRECTIVE ACTION: REF ERA 608072-14AD. (2748096)SDR IPXA2023050293095Stringer · crackedINSPECTION TYPE:C3*MAJOR REPAIR* R/H FIXED LE LOWER STRINGER IS CRACKED AT PANEL LANDING 11 IN O/B OFSLAT TRACK 12 , STA XOS=787REPAIRED R/H WING FIXED LE LOWER STRINGER AT STA XOS =787 IAW MD-11 SRM 57-40-03-2R-1 REPAIR 1 , REV 69.01. MAJORSDR FDEA202305020796Bracket · crackedRIGHT WING I/B FIXED L/E CAVITY SUPPORT BRACKET IS CRACKED AT IFSS 283 REMOVED AND REPLACED RIGHT WING INBOARD LEADING EDGE TORQUE TUBE GUIDE BRACKET IAW B767 SRM 51-40-02 AND BAC DWG 114T1240, SHEET 6SDR AALA202307199380Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN UPER SURFACE AT RIB 9. REPAIRED SKIN PANEL PER EA 345131.SDR SWIA2023052211Skin · damagedWHILE DRILLING OUT A STUCK SCREW ON PANEL 672AB MISDRILLED AND DAMAGED UNDERLYING STRUCTURE. (C-CHECK RO 5/18/2023) REPAIRED DAMAGE TO RH WINGLET CLOSING RIB REF MHIRJ EO # CL-600-2C10-57-L07462 DATED 5/2/2023. COMPLIED WITH SKYWEST TASK CARD 51-900-100SDR DALA2023050303451Unknown · unknownSHIP 6707 SECONDARY NRC IN REF NRC 091. A.D: WEAR ON CLIP (1EA) OF SHEAR TIE INBOARD RH AT RH PYLON. CORRECTIVE ACTION: SUMMARY OF NRC 00310. CLIP (1EA) OF SHEAR TIE NBOARD RH AT RH PYLON WAS REPLACED PER B757-200 SRM REF ERA 576407-14SDR DALA2023050203420Unknown · unknownSHIP 6707 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP & DRAG BRACE AS FOLLOW: HOLE NO.12 CORROSION ON SKIN AND FITTING BTW 8 TO 2 O CLOCK POSITION & HOLE NO.17 CORROSION ON SKIN AND FITTING AT 3 O CLOCK POSITION. IN REF. CARD. CORRE
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