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 SPUY201403310012Skin · corrodedRIGHT WING LOWER OUTER SKIN SHOWS CORROSION BETWEEN WS 198 AND 224.5.SDR SPUY201403310011Skin · corrodedRIGHT WING LOWER OUTER SKIN SHOWS CORROSION BETWEEN WS 357- 330.5.SDR ASOA2014042910419Skin · crackedLOWER WING PLANK AT RT BOOST PUMP LANDING FOR PANEL 610CB HAS MULTIPLE INDICATIONS. NOTED ON HORIZONTAL AND VERTICAL SURFACES GREATER THAN 50 PERCENT FSH AROUND ENTIRE CIRCUMERENCE. FAILED NDT INSP. COMPLIED WITH EA 26-2014-038. PERFORMED ROTO PEEN IAW SRM 5SDR SPUY201403280010Skin · corrodedRIGHT WING LOWER OUTER SKIN SHOWS CORROSION AT WS 436.5.SDR SPUY201403280009Skin · corrodedRIGHT WING LOWER OUTER SKIN SHOWS CORROSION BETWEEN WS 574-546.5.SDR SPUY201403280007Access Panel · corrodedRIGHT WING, ACCESS PANEL LOWER SKIN SHOWS CORROSION AROUND FASTENERS.SDR SPUY201403280006Skin · crackedLEFT WING L/E UPPER SKIN CRACKED .5 INCH AT WS 325.SDR SPUY201403280005Skin · crackedLEFT WING L/E UPPER SKIN CRACKED .7500 INCH AT WS 410.0, REF NR 0171.SDR SPUY201403280004Skin · crackedLEFT WING L/E UPPER SKIN CRACKED ONE INCH AT WS 457.5.SDR SPUY201403280003Skin · crackedLEFT WING L/E UPPER SKIN CRACKED ONE INCH AT WS 450.5.SDR SPUY201403280002Skin · crackedLEFT WING L/E UPPER SKIN CRACKED ONE INCH AT WS 443.5.SDR GTIA2014032701235Skin · corrodedCORROSION DETECTED FROM PHASED ARRAY INSPECTION ON LT WING SKIN PANEL NR 2 OVERHANG BETWEEN RIBS 17 AND 18. REF NRI 7337N00136 ER SRM 51-74-00. REMOVED CORROSION TOP SKIN AND RE-MEASURED WITHIN ALLOWABLE SRM 57-21-1 LIMITS. TREATED, PREPPED, PRIMED AND PAINTSDR GTIA2014032701234Skin · corrodedCORROSION DETECTED FROM PHASED ARRAY INSPECTION ON LT WING SKIN PANEL NR 2 OVERHANG AT RIB 17. REF NRI 7337N00135 IAW SRM 51-74-00. REMOVED CORROSION TOP SKIN AND RE-MEASURED WITHIN ALLOWABLE SRM 57-21-1 LIMITS. TREATED, PREPPED, PRIMED AND PAINTED IAW SRM.SDR GTIA2014032701233Skin · corrodedCORROSION DETECTED FROM PHASED ARRAY INSPECTION ON LT WING SKIN PANEL NR 2 OVERHANG BETWEEN RIBS 15 AND 16. REMOVED CORROSIONIAW SRM 57-21-1. TREATED, PREPPED AND TOP COATED IAW SRM.SDR GTIA2014032701232Skin · corrodedCORROSION DETECTED FROM PHASED ARRAY INSPECTION ON LT WING SKIN PANEL NR 2 OVERHANG BETWEEN RIBS 14 AND 15. REF NRI 7337N00132 IAW SRM 51-74-00. REMOVED CORROSION TOP SKIN AND RE-MEASURED WITHIN ALLOWABLE SRM 57-21-1 LIMITS. TREATED, PREPPED AND TOP COATED SDR GTIA2014032701231Skin · corrodedCORROSION DETECTED FROM PHASED ARRAY INSPECTION ON LT WING SKIN PANEL NR 2 OVERHANG BETWEEN RIBS 10 AND 11. REF NRI 7337N00131 IAW SRM 51-74-00. REMOVED CORROSION TOP SKIN AND RE-MEASURED WITHIN ALLOWABLE SRM 57-21-1 LIMITS. TREATED, PREPPED AND TOP COATED SDR GTIA2014032701230Skin · corrodedCORROSION DETECTED FROM PHASED ARRAY INSPECTION ON LT WING SKIN PANEL NR 2 OVERHANG BETWEEN RIBS 16 AND 17.SDR IPXA2014090284126Skin · gougedINSPECTION 3C, RT WING OTBD L/E REPAIR DOUBLER IS GOUGED AT XORS 1170. REPAIRED IAW EA 011-5754-01-A5241, REV I/R AND EO 5730-55400-A.SDR IPXA2014062383373Skin · gouged3C INSPECTION, EXTERIOR SURFACE OF LT WING PANEL, 518GB GOUGED. FABRICATED AND INSTALLED REPLACEMENT SKIN IAW SRM 51-35- 01, 51-31-01, AND DWG ARB2956.SDR SWAA2014041627174Panel · crackedLEFT WING LOWER TE PANEL JUST OTBD NR 1 ENG PYLON CRACKED. R & R PYLON IAW MM.SDR CALA2014032790702Skin · damagedLEFT WING FUEL TANK LANDING 540PB OTBD OF RIB 19 HAS DAMAGE AT HOLE N & F. REAMED BOTH HOLES TO 0.297 IAW SRM 57-21-11 PGS 201 - 220, FIG 202. FABRICATED NEW BUSHINGS & INSTALLED IN HOLES N & F IAW SRM 51-72-12 PGS 1-8, FIG 2. TSDR SWAA2014032726570Panel · crackedRIGHT WING LE COVE PANEL CRACKED. R & R PANEL IAW DWG & SRM.SDR SWAA2014033126666Panel · crackedRIGHT LE PANEL CRACKED. R & R PANEL IAW DWG & SRM.SDR DALA14018566302Skin · corrodedDURING A NON ROUTINE CHECK, LT WING LOWER SURFACE, WS 1430 FRONT SPAR LOWER RABBIT AREA FOUND BULGING. PERFORMED REPAIR IAW ERA522150-14, REV 0 PERFORMED HFEC INSPECTION TO REWORK AREA IAW NDT MANUAL PART 6 51-00-00 PROCEDURE 4 OR 23.SDR ABXA20140324142Skin Panel · corrodedAFTER REMOVAL OF LOWER LE SPLICE PLATE, FOUND LE OF LOWER WING SKIN CORRODED, UPPER SURFACE AT SS 410 - 418. REPAIRED DAMAGE IAW B657-60879-MR & B65760916. LEVEL 2 CORRODED, PN 112T4101-5, SN NA, PART NAME WING SKIN PANEL NR 4, EXACT STRINGER & WS LOCATION OSDR FDEA201403240567Access Panel · crackedACCESS PANEL FOUND TO HAVE CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION BETWEEN XORS = 683.4 & XORS = 713.6. REPAIRED IAW SRM 57-20-02 FIGURE 201 REPAIR 5 REVISION 55. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 120.SDR GLBA2014032400406Skin · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE LOWER WING SKIN FROM SKIN FASTENERS FWD TO EDGE OF SKIN AT DRY BAY ACCESS PANEL LOCATED AT WS 1359, .2 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-120-57SDR SWAA2014051327898Skin · crackedRIGHT WING FIXED LE SKIN CRACKED AT NR 4 LE SLAT ACTUATOR CUT OUT. REPAIRED SKIN IAW EA.SDR DALA14017900616Skin · delaminatedWING PANEL INSPECTION, FOUND RT PANEL HAS ELEVEN FASTENERS PULLING THROUGH AND APPROXIMATELY 16 INCHES OF DELAMINATION LOCATED ON FWD EDGE 8TH FASTENER FROM INBD EDGE. REMOVED RT WING PANEL FOR REPAIR OF DELAMINATION. DRILLED UP NEW PANEL. COMPLETED NEW PASDR CHQA20140322107Skin · gougedDURING INSPECTION, A GOUGE WAS FOUND ON THE RT NR 2 WING LE UPPER NOSE SKIN. THE RT NR 2 WING LE UPPER NOSE SKIN WAS REPAIRED IAW SRM 57-40-00.SDR GLBA2014032100405Skin · crackedDURING A SCHEDULED INSPECTION WHILE INVESTIGATING A FUEL LEAK ON THE RT LOWER WING, REMOVED EXISTING REPAIR AT WING STATION YA-4533.5 TO FIND CRACK PAST REPAIR STOP DRILL. NEW CRACK APPROXIMATELY 1 INCH THAT REACHES TO THE END OF THE SKIN. REPAIRED THE AFFESDR DALA14017815649Skin · corrodedRT WING UPPER SKIN - BETWEEN FRONT SPAR AND REAR SPAR, RWS 95 - 204, THE EMERGENCY SCAPE PATH HAS CORROSION. BLENDED OUT CORRODED IAW SRM 51-10-02. NDT AREAS AND HOLES IAW NDTM 51-00-19 AND 51-00-16, NO CRACKS NOTED. FLAP PEENED REWORKED AREA IAW SOPM 20-1SDR DALA14017675649Skin · corrodedLEFT WING UPPER SKIN, BETWEEN FRONT SPAR AND REAR SPAR AT STA WS 95 AND WS 204 APPROXIMATELY AT THE EMERGENCY ESCAPE PATH HAS CORROSION. REMOVED CORROSION ON LT WING UPPER SKIN SURFACE FROM WS 95 AND 204 APPROX IAW SRM 51-10-02. HFEC INSP REWORKED AREA IAW NDSDR DALA14017600675Panel · departedF/A ADVISED A PANEL WAS MISSING FROM RT WING. HAD LT HYDRAULIC SYSTEM PRESSURE LOSS FOLLOWED BY TOTAL LT HYD FAILURE. RAN CHECKLIST AND LANDED WITH MANUAL FLAP AND GEAR EXTENSION. COMPLIED WITH PARTS DEPART ACFT INSPECTION IAW AMM 05-51. COMPLIED WITH TAP TSDR CALA2014032090649Skin · damagedRT WING FUEL TANK PANEL 640MB LANDING HAS ONE HOLE DAMAGED. REWORKED HOLES & INSTALLED BUSHINGS IAW SRM 57-27-11 FIG 102 & 57-21-11 FG 201.SDR CALA2014032090648Skin · damagedLT WING FUEL PANEL LANDING 540MB HAS FOUR EACH SCREW HOLES GOUGED. REWORKED HOLES & INSTALLED BUSHINGS IAW SRM 57-27-11 FIG 102 & 57-21-11 FG 201.SDR DALA14017320675Panel · damagedCOMPOSITE PANEL DAMAGED JUST FWD OF INBD SPOILER ON TOP OF RT WING. REPAIRED IAW ERA 524217-14, REV ORIGINAL.SDR SWAA2014032126308Skin · crackedLT WING LE SKIN CRACKED AT WS 564.50. REPAIRED LE IAW SRM.SDR SWIA201436867Skin · corrodedRIGHT LOWER WING PLANK ACCESS ORIFICE 640BB HAS LIGHT CORROSION. C-CHECK, REMOVED CORROSION IAW REO.SDR SWIA201436866Skin · corrodedLEFT LOWER WING PLANK ACCESS 540BB ORIFICE HAS LIGHT CORROSION. C-CHECK, REMOVED CORROSION FROM LT LOWER WING PLANK ACCESS ORIFICE IAW REO.SDR SWIA201436865Skin · corrodedLEFT LOWER WING PLANK ACCESS PANEL 510AB ORIFICE HAS LIGHT CORROSION. C-CHECK, REMOVED CORROSION FROM LT LOWER WING PLANK ACCESS PANEL ORIFICE 510AB IAW REO.SDR SWIA201436817Skin · crackedCRACK NOTED AT RT LOWER WING PLANK FASTENER. C-CHECK, REPAIRED RT WING PLANK AT WS 48.95 BETWEEN REAR SPAR AND AUXILIARY SPAR IAW REO.SDR DALA14017033155Skin · corrodedCORROSION ON WING TOP SKIN BETWEEN RIBS 19 & 20. REWORKED AND FOUND WITHIN LIMITS IAW SRM 57-21-11.SDR C77A20140313004Skin · gougedON THE LT WING, THE SKIN MATING FLANGE ON WING FUEL PANEL 521AB IS GOUGED IN 3 PLACES. BLENDED GOUGES IAW SRM 51-10-03 & 51-12-01 ON WORK ORDER 736922-543 IAW 2014-170-019684 & EA 175-57-187 REV IR WORK ORDER 1413297.SDR TIMA20140312017Skin · crackedSEVERAL CRACKS DEVELOPED IN THE SKIN OTBD OF THE LT NACELLE & AFT OF THE MAIN SPAR ORIGINATING FROM VARIOUS RIVETS.SDR TIMA20140312016Skin · debondedLEFT WING DEBOND. UPPER SKIN OF BONDED PANEL IN AREA AROUND FUEL BAY ACCESS OVAL PANEL DEBONDED FROM FUEL ACCESS DISH & HONEYCOMB CORE.SDR TIMA20140312015Skin · debondedRIGHT WING DEBOND. UPPER SKIN OF BONDED PANEL IN AREA AROUND FUEL BAY ACCESS OVAL PANEL DEBONDED FROM FUEL ACCESS DISH & HONEYCOMB CORE.SDR DALA14025309212Skin · gougedLEFT WING EXISTING REPAIR DOUBLER HAS DEEP GOUGES BETWEEN NR 10 AND NR 11 SLAT TRACK. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED NEW EXTERNAL REPAIR IAW SRM 57-20-01, PARA 21 AND ERA 522710-14.SDR R61A201403120360Access Panel · corrodedDURING HEAVY CHECK, CORROSION WAS FOUND ON FUEL ACCESS PANEL 622BT. MAINTENANCE R & R ACCESS PANEL IAW AMM 57-11-01-400-801.SDR FDEA201403110483Skin · crackedDURING INSPECTION, FOUND RIGHT WING XOS 995 FIXED LE NOSE SKIN FOUND CRACKED. REPAIRED IAW SRM 57-40-01 REPAIR 9 FIGURE 201 REVISION 55. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 120.
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