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 R61A2024051300210Skin · crackedRH WING LOWER SKIN CRACKED BETWEEN FRAMES/RIB 16 AND 17, 31 MM AFT OF FWD SPAR AND 23 MM INBD OF RIB 17 MEASURING 54 MM IN LENGTH. REPAIRED CRACK IAW ETD2024-170-013056, INSTALLED FILLER, DOUBLER AND TRIPLER. ALSO REF VP-014820-2024 N/R #8 FOR WORK ACCOMPLISHESDR DXTA2024050911719Skin · dentedLEFT WING WING LEADING EDGE: LEFT WING, ABOUT MIDWAY OUT, NEAR FUEL CAP. WE HIT A LARGE BIRD IN FLIGHT, AND THERE ARE DENTS RIGHT WHERE IT HIT. REMOVED DENTED LH WING OUTER LEADING EDGE PANEL ASSY P/N: 505-12700-417, S/N: F043017566, REPLACED WITH A CUSTOMESDR SCNA20240604249Skin · crackedRIGHT WING, SLAT #8 ACTUATOR TO SLAT ATTACH POINT SKIN WITH CRACK. REPAIRED RH WING SLAT#8 SKIN SECTION FROM SLAT STA 442.595 TO SLAT STA 460-345 LWL SECTION DUE TO CRACK IAW B737-800 SRM 57-42-01-2R-8 RERPAIR 8 ALTERNATIVE 1 PARA 4.F.FIG 202.SDR UIEA2024050800342Skin · corrodedBULGE - SKIN, LWR FACE OF LH WING T/E INBD FORE FLAP LWR SKIN WBL 395 - WBL 407, FRONT SPAR(<P>1) PERFORM PERMANENT REPAIR OH LH WING T/E INBD FORE FLAP LWR SKIN WBL 395 - WBL 407, FRONT SPAR IAW EGAT EI T2024A57-1049 REV 1. 2) CONDITION CHECK IS GOOD</P>)SDR CNMA2024050001Panel · dentedPANEL 611 FB REMOVED FROM A/C DUE TO BIRDSTRIKESDR IXXA2024050801Panel · wornLEFT WING LE PANEL 521AMB HAS WORN HOLESSDR R61A2024050600195Skin · crackedDURING INSPECTION RH LEADING EDGE SKIN FOUND TO BE CRACKED AT OUTBD CUTOUT FOR SLAT #2. RH WING, L.E. SKIN AT CUTOUT REOAIRED IAW SRM 57-40-01, REPAIR 6. HFEC CUTOUT "NO CRACKS FOUND".SDR IXXA2024050602Skin Panel · crackedLEFT WING FIXED L/E PANEL CRACKED IN 2 PLACES UNDER #5 SLATSDR R61A2024050800204Skin · crackedRH WING LOWER SKIN CRACKED 3 INCHS IN LENGTH ,22 MM INBD OF RIB 17 AND 25 MM AFT OF FWD SPAR. INSTALLED FILLER,DOUBLER AND TRIPLER IAW EDT2024-170-012706. REF VP-014833-2024N/R 1 FOR WORK PERFORMED.SDR YENA2024050700717Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION FLOOR STRUCTURE ON UPPER SKIN CENTER WING BOX LOC, FR,41 TO FR,42 L/H SIDE IN PASSENGER CABIN (REFER TO THE MPD TASK 533135-01); REF AEROMAN WO# 2024 44/1 NR# 2024-149075. ACCOMPLISHED THE REPAIR OF THE CORROSION DAMAGE ON TSDR YENA2024050700716Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE OF TOP SKIN OVERHANG LOC. BTW RIB 8 AND RIB 9 ON RH WING (CPCP RELATED MPD TASK 572178-01); REF AEROMAN WO# 2024 44/1 NR# 2024-148974. ACCOMPLISHED REPAIR OF CORROSION ON THE RH WING TOP SKIN PANEL 2 LOWER SURFSDR YENA2024050700715Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SURFACE OF TOP SKIN OVERHANG BTW RIB 6 AND RIB 7 ON RH WING (CPCP RELATED MPD TASK 572066-01); REF AEROMAN WO# 2024 44/1 NR# 2024-148973. ACCOMPLISHED REPAIR OF CORROSION ON THE RH WING TOP SKIN PANEL 2 LOWER SURFACE TSDR YENA2024050700714Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE OF BOTTOM SKIN FALSE SPAR BOX BTW RIB 5 AND RI B 6 ON RH WING (CPCP RELATED MPD TASK 575167-01); REF AE WO# 2024 44/1 NR# 2024-148982.ACCOMPLISHED REPAIR OF CORROSION ON THE RH WING BOTTOM SKIN PANEL 2 UPPER SUSDR WX0A2024050632030Screw · displacedSCREW POPPED OUT OF PANEL DIRECTLY ABOVE RT WING EMERGENCY EXIT SLIDE PANEL / TIGHTENED SCREW IAW A320 AMM 20-21-11-911-001-A AIRCRAFT OK FOR SERVICE."SDR IPXA2024052191404Skin Panel · corroded**SUPPLEMENTAL SDR** FAULT - CORROSION - SKIN, L/H WING INBD INSPAR SKIN WBL 97 (EVALUATE) ACCOMPLISHED REPAIR I.A.W EO-90375-REQ1 REV.1 AND BOEING DWG NO. 112T4000 SH 9 REV. B AND NO. 112T4000 SH 8 REV. JOB COMPLETED. PAPER CHECK OK.SDR IPXA2024052191453Skin · corrodedCORROSION - SKIN, R/H WING OUTBD INSPAR LWR SURFACE DRAIN HOLE CUTOUT AREA, WS 852 (EVALUATE) ACCOMPLISHED REPAIR I.A.W EO-90935-REQ1 REV.1. REVIEW COMPLETEDSDR IPXA2024052091487Skin Panel · corroded*** SUPPLEMENTAL SDR *** FAULT - EXISTING BLEND LEFT WING TRAILING EDGE OUTBOARD SKIN WS 1046 (EVALUATE) ACCOMPLISH REPAIR I.A.W EO-90394-REQ1 REV. 1. JOB COMPLETED.SDR IPXA2024051791453Skin · corroded**SDR FILED OPEN**FAULT - CORROSION - SKIN, R/H WING OUTBD INSPAR LWR SURFACE DRAIN HOLE CUTOUT AREA, WS 852 (EVALUATE) REVIEW COMPLETEDSDR IPXA2024051691487Skin Panel · corrodedEXISTING BLEND LEFT WING TRAILING EDGE OUTBOARD SKIN WS 1046 (EVALUATE) REVIEW COMPLETESDR SWAA2024050382050Panel · delaminatedRH PANEL 192BR PANEL DELAMINATED WITH HOLE<[01] C/W EA 24-153-01186SDR FDEA202405030565Doubler · crackedRIGHT WING - FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 789 FOUND CRACK ABOUT 1 INCH. RIGHT WING FIXED LEADING EDGE CRACKED RIB DOUBLER AT STATION XOS 789 REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G . RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWINSDR FDEA202405030564Skin · crackedRIGHT WING, LEADING EDGE NO 14 SLAT TRACK CUTOUT OUTBOARD LOWER CORNER AT STATION XOS 891 FOUND CRACK. RIGHT WING LEADING EDGE NUMBER 14 SLAT TRACK CUT OUT OUTBOARD LOWER CORNER AT STATION XOS 891 CRACKED AREA REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2RSDR FDEA202405030563Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 863 FOUND CRACK ABOUT 0.5 INCHES. RIGHT WING FIXED LEADIING EDGE CRACKED BEADED DOUBLER AT STATION XOS 863 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFISDR FDEA202405030562Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 792 FOUND CRACK ABOUT 0.4 INCHES. RIGHT WING FIXED LEADIING EDGE CRACKED BEADED DOUBLER AT STATION XOS 792 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFISDR FDEA202405030560Doubler · crackedLEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 785 FOUND CRACK ABOUT 0.2 INCHES. LEFT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 785 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203.REPAIR CLASSIFIED ASSDR FDEA202405030559Doubler · crackedLEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 587 FOUND CRACK ABOUT 0.5 INCHES. LEFT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 587 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED ASSDR FDEA202405030558Doubler · crackedLEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 655 FOUND CRACK ABOUT 0.2 INCHES. LEFT WING FIXED LEADIING EDGE CRACKED BEADED DOUBLER AT STATION XOS 655 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED SDR FDEA202405030557Doubler · crackedLEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 640 FOUND CRACK ABOUT 0.3 INCHES. LEFT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 640 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS SDR FDEA202405030556Doubler · crackedLEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 631 FOUND CRACK ABOUT 0.3 INCHES. LEFT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 631 REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED ASDR FDEA202405030555Skin · corrodedRIGHT WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN AUXILLARY SPAR AND YW 467 FOUND CORROSION. RIGHT HAND WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN AUXILLARY SPAR AND YW 467 CORROSION REMOVED AND SDR FDEA202405030554Skin · corrodedLEFT WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN AUXILLARY SPAR AND YW 467 FOUND CORROSION. LEFT HAND WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN AUXILLARY SPAR AND YW 467 CORROSION REMOVED AND FOSDR SWAA2024052182019Skin · corrodedL/H WINGLET TIP HAS CORROSION AT THE TOP.<[01] REMOVED DAMAGE ON L/H WINGLET TIP IAW B737-800 SRM 57-30-01 REPAIR 6;[02] REMOVED DAMAGE ON L/H WINGLET TIP IAW B737-800 SRM 57-30-01 REPAIR 6SDR IPXA2024052076482Skin Panel · corrodedCORROSION - SKIN, L/H WING OUTBD VORTEX GENERATORS AREA, WS720 TO WS772. (EVALUATE) ACCOMPLISHED REPAIR I.A.W EO-90376-REQ1 REV.1 AND BOEING DWG NO. 112T3000 SH 16 REV. -.SDR IPXA2024052073956Skin Panel · corroded*** SUPPLEMENTAL SDR *** FAULT - CORROSION - SKIN, L/H WING TO BODY SPLICE LOWER SKIN LOWER SURFACE, STA 792, WBL 97.5. (EVALUATE) ACCOMPLISHED REPAIR I.A.W EO-90393-REQ1 REV.1 AND SRM 51-40-04-0G REV. 49 AND BOEING DWG NO. 112T4323 SH5 REV. C; NO. 112T5000 SHSDR IPXA2024051673956Skin Panel · corrodedCORROSION - SKIN, L/H WING TO BODY SPLICE LOWER SKIN LOWER SURFACE, STA 792, WBL 97.5. (EVALUATE) ACCOMPLISH REPAIR PER EO-90393-REQ1 AND EGAT EI F2024A57M-1171, REV. 4 (REF. T3F18E004H051) PRIOR TO FURTHER FLIGHT.SDR KKVA20240506002Skin Panel · corrodedCORROSION FOUND ON CENTER WING, RH INNER SKIN FS 410 AND RBL 32.SDR KKVA20240506001Skin Panel · corrodedCORROSION IDENTIFIED ON L/H UPPER WING SKIN LWS 37 STRINGER # 2 TO CENTER SPARSDR GSAA2024050101Skin · dentedAIRCRAFT SUFFERED A BIRDSTRIKE ON CLIMB OUT FROM KCXY. ACFT CLIMBING THRU 2000 FT MSL WITH AUTOPILOT ENGAGED. CLIMB SPEED 140 KTS INDICATED CLIMB RATE APPROX 1700 FPM. ACFT ON AN APPROX HEADING OF 260 WHEN ATC ASSIGNED A LT TURN TO 180 FOR OUR CLIMB TO 8000 FSDR WX0A2024052432055Skin · damagedDISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 6000-0033: 1205-15 RH WING BOTTOM SKIN LOWER SURFACE, PREVIOUS BLEND FOUND AT RIB 25 APPROX 6 INCHES FROM T/E. / RH WING BOTTOM SKIN PANEL #2 LOWER SURFACE BTW RIB 25-26 AND STGR11 REPAIRED PER AIRBUS DOSSIER #813SDR ASAA2024043049467Skin · chafedCUSTOMER REQUEST:DB #28, RH WING LEADING EDGE SLAT #3 CHAFFING MARKS- REINSPECT TO VALIDATE DAMAGE RECORDED ON NRC 39664 FROM W/O 375225 AND NRC:27505 SO:536489 GROUNDED - YES. CUT OUT DAMAGED AREA, FABRICATED EXTERNAL PLATE AND INSERT IAW A320 SRM 57-44-21-30SDR DATA20240503001Skin · corrodedRIGHT HAND INBOARD WING LEADING EDGE HAS SEVERE CORROSION. RESKINNED RIGHT HAND LEADING EDGE SPANNING ONE NOSE RIB BETWEEN RW535.00 TO RW568.00 IN ACCORDANCE WITH SRM 57-23-00.SDR EE4Y2024042820032Skin Panel · corrodedDURING THE ACCOMPLISHMENT OF ALLEGIANT TASK 572112-01-1 , LH WING TEOH AREA BETWEEN RIB 14 AND 15 CORROSION WAS FOUND. AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS AND REPAIR WAS ´PERFORMED IAW COOPESA ENGINEERING ORSDR SWIA20240522427Skin · damagedDAMAGE TO RIGHT WING LOWER SURFACE DURING CROSSWIND LANDING. (FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28155864 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED DAMAGED PANELS 672AB AND 672BB. SEE CP 2816+3762 FOR REPLACEMENT OF DAMAGED RIB. SESDR UIEA2024042500316Skin · corrodedRH WING, TOP SURFACE,BTW WB 289.45 AND WBL 97.9566, DURING REMOVAL OF ACCESS SPOILER HINGE PANEL, CORROSION WAS FOUND ON THE SPOILER BEAM(<P>CORROSION RH WING TRAILING EDGE STRUCTURE INBOARD SPOILER SUPPORT BEAM UPPER CHORDS WERE REPAIRED PER SRM 57-51-02-2R-2SDR DALA2024042904777Skin · damagedSHIP 6809 DTE, ERA 616812-14, LHS UPPER SKIN &FITTING AT FWD DRAG FITTINGS HOLES CORROSION. CORRECTIVE ACTION: REF ERA 616812-14AD.SDR DALA2024042804742Skin · damagedAIRCRAFT 6809, LOOSE FASTENER NBR 3 BY CRACKED PAINT ALL THE WAY AROUND THE FASTENER HEAD AT LH WING UPPER SKIN DRAG FITTING. (IN REF AMDS 5720-01100-02A STEP 12). CORRECTIVE ACTION: LH WING UPPER SKIN DRAG FITTING HOLE #3 WAS REPAIRED PER ER/A 616812-14AD REVSDR DALA2024042804741Skin · damagedAIRCRAFT 6809, LOOSE FASTENERS NBR 13 BY CRACKED PAINT ALL THE WAY AROUND THE FASTENER HEAD AT LH WING UPPER SKIN DRAG FITTING. (IN REF AMDS 5720-01100-02A STEP 13). CORRECTIVE ACTION: LH WING UPPER SKIN DRAG FITTING HOLE #13 WAS REPAIRED PER ER/A 616812-14AD SDR DALA2024042604723Panel · damagedAIRCRAFT 0686, DURING THE ONGOING MAINTENANCE CHECK OF THE DATUM AIRCRAFT, LH WING, DRY BAY PANEL, P/N: 112N8003-1, WAS FOUND WITH A TOOL MARK AFFECTING FLAME SPRAY COATING AND 1 EA. PLY AROUND THE DRY BAY DOOR LOCATED BETWEEN WSTA 231.5 WSTA 258.5. CORRECTISDR VNAA20240531007Skin · wornWEAR ON SETTLEMENT AREA OF FAIRINGS (683AB, 686AB, 692AB, 695AB AND 697AB) AT RH WING LOWER SKIN. WEAR ON SETTLEMENT AREA OF FAIRINGS (683AB, 686AB, 692AB, 695AB AND 697AB) AT RH WING LOWER SKIN. WERE REPAIRED PER REO 690-57-21-466 REV. --SDR VNAA20240531006Skin · wornIN REFERENCE TO RC TRFKE001HT5B: WEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB AND 597AB) AT LH WING LOWER SKIN.
AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB AND 597AB) AT LH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21
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