JASC 5330
Service difficulty reports · 79,347
Reports filed under 5330 · Fuselage Main, 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 = '5330' 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 = '5330' 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 VNAA2016092500043Skin Panel · crackedNOSE LANDING GEAR CUT-OUT AT FS 235 LBL 26 AND RBL 26 HAS CRACKS IN RADIUS. MAINTENANCE PERFORMED A MAJOR REPAIR TO THE EXTERNAL FUSELAGE SKIN AT FS 235 BETWEEN STR 26L AND 26R AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR FDEA201609253358Skin · damagedFWD LOWER FUSELAGE SKIN BETWEEN FR 0 AND FR 1 .500 RH OF CENTERLINE HAS LIGHTNING STIKE DAMAGE REMOVED DAMAGE ON FWD LWR FUSELAGE SKIN BETWEEN FR 0 AND FR 1, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER PER A300-600 SRM 53-10-12 FIG 202 AND SRM 53-SDR SWAA2016100708545Skin · crackedENTRY DOOR CUTOUT AREA CRACKED ON AFT LOWER REVEAL. R & R CUTOUT IAW SRM & DWG.SDR V0XD201609270001Tripler · gougedAFT LOWER FUSELAGE AT FS 985.00, EXISTING MAJOR REPAIR TRIPPLER IS GOUGED. R & R TRIPPLER IAW REO670-53-00-290, REV D, AND SRM 51-42-21.SDR JR2R20160925255Doubler · corrodedE&E BAY INTERNAL DOUBLER CORRODED. REMOVED AND REPLACED INTERNAL DOUBLER IAW EA 40-2016-292.SDR R61A201609240597Doubler · corrodedWHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE WASTE SERVICE PANEL AND INTERNAL DOUBLER. MAINTENANCE PERFORMED MAJOR REPAIR. REMOVED AND REPLACED THE WASTE SERVICE PANEL (P/N 170-86668-403) DOUBLER (P/N 170-86655-003) ANSDR R61A201609240596Doubler · corrodedWHILE AIRCRAFT WAS IN FOR HEAVY CHECK, MAINTENANCE REPORTED LEVEL 2 CORROSION ON THE WASTE SERVICE PANEL AND INTERNAL DOUBLER. MAINTENANCE PERFORMED MAJOR REPAIR. REMOVED AND REPLACED THE WASTE SERVICE PANEL (P/N 170-86668-403) DOUBLER (P/N 170-86655-003) ANSDR UIEA2016092600774Skin · crackedPRIOR TO SCHEDULED DEPARTURE, ON 24-SEP-2016, THE DATUM AIRPLANE FUSELAGE SKIN WAS FOUND WITH CORROSION CRACKS IN THE VICINITY OF FASTENER LOCATIONS AT BS 1736, ALONG STR 42R, AND AT BS 1731, ALONG STR 42R. SHEET METAL REPAIR EO 4453B268.SDR SWAA2016101408773Skin · crackedR1 DOOR LOWER CORNER SKIN CUTOUT CRACKED BETWEEN BS 312 TO BS 344, BETWEEN STR 15R TO STR 18R. REPAIRED CUTOUT IAW EA.SDR SWAA2016110409395Skin · crackedCENTER WING BOX UPPER SKIN PANEL CRACKED AT BS 540+7, RBL 15.04. REPAIRED SKIN IAW ER AND EA.SDR SWAA2016100708527Skin · crackedLOWER SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW EA.SDR SWAA2016100508465Skin · delaminatedTAIL CONE LOWER FUSELAGE SKIN DELAMINATED AT BS 1156+6, BL 0. REPAIRED THE SKIN IAW SRM.SDR CALA2016092795775Skin · dentedEXTERIOR FUSELAGE SKIN HAS DENT FRAME 7 8.5 INCH ABOVE LOWER LAP SEAM. FOUND TO BE OUT OF LIMITS. CUT OUT THE DAMAGED AREA & FABRICATED A REPAIR DOUBLER AND INSTALLED IAW SRM53-00-11 FIG 239.SDR DALA2016092406808Skin · crackedFUSELAGE SKIN CRACKED AT UPPER FASTENER IN FORMER 1152 BETWEEN L2-L3 LT LOCATION MARKED. REMOVED DAMAGE FROM FUSELAGE SKIN CRACKED AND REPAIRED IAW ER/A 549614-14. REPAIR REQUIRES REPETITIVE INSPECTIONS EVERY 3000 FLIGHT CYCLES.SDR KCSA201609221072Skin · corrodedCORROSION ON SKIN UNDER STRINGER 37L, BS 434 - 456.
SDR FDEA201609223335Skin · chafedFUSELAGE EXTERNAL SKIN BS 1600 TO 1620, STRINGER 14R. BETWEEN UPPER SKIN PANEL AND LOWER SKIN PANEL. SUSPECT SHIM PRESENT AND MIGRATED. REPAIRED IAW EA F-5330-T0328680. MAJOR REPAIR.SDR FDEA201609223333Skin · scratchedFUSELAGE EXTERNAL SKIN BS 1620 - 1640 , STRINGER 14R. THERE ARE FIVE SCRATCHES FOUND BELOW THE SKIN LAP SPLICE. REPAIRED IAW EA F-5330-T0328680.SDR FDEA201609223332Skin · gougedFUSELAGE EXTERNAL SKIN BS 1600 - 1620, STRINGER 14R, THERE IS A SCRATCH FOUND BELOW THE SKIN LAP SPLICE. REPAIRED IAW EA F-5330-T0328680. REPAIR CLASSIFIED AS MAJOR.SDR KC8A20160922004Skin · crackedCRACKS FOUND ON THE LEFT SIDE OF THE NOSE WHEEL WELL BOX. REMOVED DAMAGED AREA AND INSTALLED PATCH IAW MFG ENGINEERING. NO RECOMMENDATIONS FOR RECURRENCE.SDR ASAA2016092118356Skin · crackedFUSELAGE SKIN CRACKED AT THE R1 DOOR LOWER AFT CORNER. ACFT GROUNDED. REPAIRED THE SKIN IAW SRM 53-10-01-2R 2 REP 2.SDR SWAA2016101208698Skin · crackedSKIN CRACKED BETWEEN BS 663.75+12 TO BS 685+14.5, LBL 5. R&R SKIN IAW EA.SDR SWAA2016101208697Skin · crackedSKIN CRACKED AT BS 663.75+12, LBL 5. R&R SKIN IAW EA.SDR SWAA2016101208667Skin · crackedSKIN CRACKED AT BS 706+2.5, LBL 5. R&R SKIN IAW EA.SDR ASAA2016092118205Skin · crackedCRACK IN FUSELAGE SKIN BS 727E +3 BELOW STRINGER 22L. ACFT GROUNDED. REPAIRED THE SKIN IAW SRM 53-00-01 REP. 31.SDR DALA2016092406809Skin · crackedCRACKS IN FUSELAGE SKIN AROUND RIVET HEAD ABOVE RT PYLON STA 1095.868, JUST ABOVE L14 RT LOCATION MARKED. SKIN CRACKS REMOVED AND REPAIRED IAW ER/A 549613-14 REQUIRES REPETITIVE INSPECTIONS EVERY 3000 FLIGHT CYCLES AFTER REPAIR.SDR YENA20160921842Skin · corrodedCORROSION AFT CARGO DOOR LOWER CUTOUT AT FRAME 77, 6' AFT. REMOVED CORROSION IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.SDR YENA20160921841Skin · corrodedCORROSION AFT CARGO DOOR LOWER CUTOUT AT FRAME 77, 14' AFT. REMOVED CORROSION IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.SDR YENA20160921840Skin · corrodedCORROSION AFT CARGO DOOR LOWER CUTOUT AT FRAME 77, 16' AFT. REMOVED CORROSION IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.SDR YENA20160921839Skin · corrodedCORROSION AFT CARGO DOOR LOWER CUTOUT AT FRAME 78, 5' AFT. REMOVED CORROSION IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.SDR YENA20160921838Skin · corrodedCORROSION AFT CARGO DOOR LOWER CUTOUT AT FRAME 78, 5' AFT. REMOVED CORROSION IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.SDR YENA20160921837Finger Doubler · corrodedCORROSION FWD CARGO DOOR AFT FINGER DOUBLER AT FRAME 26, 1 INCH AFT. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.SDR YENA20160921836Finger Doubler · corrodedCORROSION FWD CARGO DOOR AFT FINGER DOUBLER AT FRAME 27, 1.5 INCHES AFT. REMOVED AND REPLACED THE FINGER DOUBLER. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.SDR YENA20160921835Finger Doubler · corrodedCORROSION FWD CARGO DOOR AFT FINGER DOUBLER AT FRAME 24, 13.5 INCHES AFT. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.SDR YENA20160921834Finger Doubler · corrodedCORROSION FWD CARGO DOOR AFT FINGER DOUBLER AT FRAME 25, 15.5 INCHES AFT. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-23-04, 51-23-05, AND 51-23-06.SDR YENA20160921833Finger Doubler · corrodedCORROSION ON AFT CARGO DOOR FWD FINGER DOUBLER FRAME 78. REMOVED THE CORROSION IAW SRM 51-10-03, AND FOUND OUT OF LIMITS. REPLACED THE FINGER DOUBLER IAW NR00103.SDR YENA20160921832Finger Doubler · corrodedCORROSION ON THE AFT CARGO DOOR FWD LOWER FINGER DOUBLER AT FRAME 77. REMOVED THE CORROSION IAW SRM 51-10-03. FOUND TO BE OUT OF LIMITS. REPLACED THE FINGER DOUBLER.SDR YENA20160921831Finger Doubler · corrodedCORROSION ON AFT CARGO DOOR FWD FINGER DOUBLER AT FRAME 77. REMOVED THE CORROSION, AND FOUND TO BE OUT OF LIMITS IAW SRM 51-75-16.SDR YENA20160921830Finger Doubler · corrodedCORROSION AFT CARGO DOOR FORWARD LOWER FINGER DOUBLER FRAME 77. REPLACED THE FINGER DOUBLER IAW SRM 51-43-03, 51-43-04, AND 51-23-06.SDR YENA20160921829Finger Doubler · corrodedAFT CARGO DOOR AFT LOWER FINGER DOUBLER FRAME 80 CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-10-03. DOUBLER REPLACED.SDR YENA20160921828Finger Doubler · corrodedCORROSION AFT CARGO DOOR AFT LOWER FINGER DOUBLER FRAME 79. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-75-16. REPLACED THE FINGER DOUBLER IAW NR 00105.SDR YENA20160921827Finger Doubler · corrodedCORROSION ON AFT CARGO DOOR AFT LOWER FINGER DOUBLER FRAME 79. REMOVED AND REPLACED THE FINGER DOUBLER IAW SRM 51-43-03, 51-43-04, AND 51-23-06.SDR JR2R20160921506Finger Doubler · corrodedFORWARD CARGO INTERNAL FINGER DOUBLER 100 PERCENT BLOWN OUT. REPAIRED FINGER DOUBLER IAW SRM 53-04, FIG 12D AND 12E.SDR TSAA20161201036Skin · crackedEXISTING REPAIR REMOVED FOR INSPECTION AT BS332.10, R1 DOOR LOWER AFT CORNER. INSPECTED FUSELAGE SKIN AND REPAIRED UNDERLYING DAMAGE IAW SRM REV 111, 53-10-01, FIGURE 201, REPAIR 2.SDR ASOA201609204097Skin · dentedDURING A C-CHECK INSPECTION, DAMAGE TO THE FUSELAGE SKIN WAS FOUND AFT OF THE GROUND AIR DOOR BETWEEN BS 574-605 AND STRINGERS 21-26R. THE SKIN WAS REPAIRED IAW REO 601R-53-61-5820 AND EC/TCREO 601R-53-61-5820, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERSDR SWAA2016092608207Skin · crackedSKIN CRACKED A T EXTERNAL POWER RECEPTICAL. REPAIRED THE SKIN IAW SRM.SDR SWAA2016092208043Skin · crackedEXTERNAL POWER RECEPTACLE SKIN CRACKED. REPAIRED SKIN IAW SRM.SDR ASOA20160920066Skin · crackedDURING A C-CHECK, THE FUSELAGE SKIN WAS FOUND CRACKED AT FRAME 78 STRINGERS 4 - 5L. REPAIRED THE SKIN IAW SRM 53-32-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20160920065Skin · crackedDURING A C-CHECK, THE FUSELAGE SKIN WAS CRACKED AT FRAME 78 STRINGERS 4 - 5R. REPAIRED THE SKIN IAW SRM 53-32-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR FDEA201609203315Skin · dentedFUSELAGE SKIN DENTED AT BS 660 - 680 STRINGERS 26 - 27L. FOUND OUT OF LIMIT AS PER SRM 53-00-01-1A REV 118.0 AND REPAIRED IAW SRM 53-00-01-2R FIG 201 REPAIR 15 REV 119.0. REPAIR CLASSIFIED AS MAJORSDR TSAA20170104047Doubler · corrodedFORWARD WASTE SERVICE PANEL MESH HEATER AND DOUBLER BEHIND VALVE ARE CORRODED. FORWARD WASTE SERVICE PANEL MESH HEATER GASKET BEHIND VALVE REPLACED IAW AMM 38-32-81, REVISION 83. DOUBLER BEHIND VALVE REPLACED IAW SRM 51-40-02, REVISION 111.
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