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 DALA2015111707069Skin · damagedACFT EXPERENCED LIGHTNING STRIKE AT BS 480 BETWEEN STR 3R AND 4R. MAINTENANCE ACCOMPLISHED REPAIRS IAW ERA 541376-14.SDR ASOA20151116088HSkin · dentedA DENT WAS DISCOVERED BEHIND THE CARGO DOOR BETWEEN FRAMES 73-74 STRINGERS 12L-13L. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW SRM 53-31-01 AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR DALA2015111707009Skin · damagedFUSE CROWN-BS 1130 DAMAGE 6" BELOW S-1R, MARKED.SDR SWAA2015120746759Skin · crackedSKIN CRACKED AT BS 787+3, STRINGER 17L. REPAIRED SKIN IAW ER & EA.SDR DALA2015111607068Skin · damagedLIGHTNING STRIKE AT BS 500C AT STR 3R ON FASTNER. MAINTENANCE CUT OUT DAMAGE, TREATED AND PRIMED. LOCATED REPAIR DOUBLER .063, 2024T3, DRILLED AND COUNTERSUNK. TRIMMED DOUBLER TO SIZE AND CHAMFERED EDGES IAW SRM 53-00-01, FIG 201. TREATED AND PRIMED DOUBLERSDR DALA2015111606978Skin · damagedDURING INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO THE CROWN SKIN AT FS 500, BETWEEN S-3R AND S-4R. MAINTENANCE REPAIRED IAW ERA 541374.SDR DALA2015111606977Skin · damagedDURING INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO THE CROWN SKIN AT FS 480, BETWEEN S-3R AND S-4R. MAINTENANCE REPAIRED IAW ERA 541376.SDR DALA2015111606970Skin · damagedER/A 532116-14, REV A SECTION II WAS ACCOMPLISHED DURING C-CK IN MSP TO ADDRESS GROUND DAMAGE TO FUSELAGE SKIN JUST BELOW AND AFT OF L1 DOOR, PREVIOUSLY REPAIRED IAW SECTION I.SDR ASOA20151115192VSkin · crackedDURING C-CHECK, THE LT AFT SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FRAME 76, STRINGER 6L. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5330-03071. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR 33AY2016FA0000056Skin · corrodedINSPECTION FOUND CORROSION ON UPPER SKIN FAYING SURFACE AT LAP JOINT STR 26R BETWEEN BS 500 TO BS 500A. THE CORRODED UPPER SKIN SECTION WAS TRIMMED OUT AND EXTERNAL REPAIR DOUBLER WAS INSTALLED. REPAIR WAS DONE IAW SRM 53-30-3, REV 108.SDR 33AY2016FA0000054Skin · corrodedINSPECTION FOUND CORROSION ON UPPER SKIN FAYING SURFACE AT LAP JOINT STR 26R BETWEEN BS 370 TO BS 400. THE CORRODED UPPER SKIN SECTION WAS TRIMMED OUT AND EXTERNAL REPAIR DOUBLER WAS INSTALLED. REPAIR WAS DONE IAW SRM 53-30-3, REV 108.SDR SWAA2015120746758Skin · crackedSKIN CRACKED AT BS 360+2, STRINGER 5R. REPAIRED SKIN IAW EA.SDR SWAA2015120746757Skin · crackedSKIN CRACKED, BETWEEN BS 892.5 - 894, STRINGER 2L. REPAIRED SKIN IAW ER & EA.SDR SWAA2015120746756Skin · crackedSKIN CRACKED, BETWEEN BS 346 - 347, STRINGER 2L. REPAIRED SKIN IAW SRM.SDR SWAA2015120746755Skin · crackedSKIN CRACKED, BETWEEN BS 482A+4.5 - 482A+5.5, STRINGER 26L. REPAIRED SKIN IAW EA.SDR SWAA2015112546455Skin · crackedSKIN CRACKED AT BS 360+2, STRINGER 6R. REPAIRED SKIN IAW SRM.SDR SIMA20151114006Skin Panel · damagedHAIL DAMAGE EVENT. REPLACE REAR FUSELAGE I TOP SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R REAR FUSELAGE I TOP SKIN PANEL IAW SRM 53-22-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40SDR DALA2015111506976Skin · gougedDURING INSPECTION FOUND SKIN GOUGED APPROXIMATELY 4" AFT OF 727H 3" BELOW STR 4L. MAINTENANCE REPAIRED IAW ERA 540727.SDR DALA2015111506966Skin · dentedDENT ON PREVIOUS DOUBLER REPAIR, BS 238 BETWEEN LONG 17 - 18L ON OUTER FUSELAGE SKIN. REPAIRED IAW ER/A 273447-14, REV E.SDR JJBA20151113004Skin Panel · dentedDISCOVERED ACFT DAMAGE NEAR LOWER FUSELAGE ON RT SIDE, DENT, DURING L CHECK. TWO DENTS & SCRATCH BETWEEN X219.0 - X232.5 & BETWEEN STRINGERS 27S - 29S. REPAIRED DAMAGE IAW RD 8-53-14442.SDR DALA2015111406964Skin · damagedELONGATED HOLE ON INTERNAL FUSELAGE SKIN, BELLY DRAIN HOLE, BS 1210 BETWEEN LONGERONS 29 - 30L. REPAIRED IAW ETI-88-15-373, REV 1 AND ER/A 539904-14, REV ORIG.SDR HNAA2015111300337Skin · debondedDISBOND DISCOVERED AT BS 467 TO 488, STR 32S TO STR 32P. PREVIOUS REPAIRED USING EO8-53-11-0651. REMOVED BOTTOM SKIN SECTION BS X424 TO BS X488.50, STR 32S TO STR 32P. INSTALLED NEW SKIN IAW DWG 85330022. SEALED, PRIMED AND PAINTED AS NEEDED.SDR COEA2015111221923Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. CTR FUSELAGE CROWN PANEL, BETWEEN FRAMES 23 - 24, INTERNAL SKIN HAS LEVEL 2 CORROSION. REPAIR IAW SRAS CE 5362 15 9696 DATED 10 23 15.SDR SIMA20151112009Skin · chafedFUSELAGE SKIN CHAFED UNDER PANEL 424DB. REPAIRED FUSELAGE SKIN CHAFE UNDER PANEL 424DB IAW ERS-EM-53MR-1779.SDR SIMA20151112010Skin · chafedFUSELAGE SKIN CHAFED UNDER PANEL 414DB. REPAIRED FUSELAGE SKIN CHAFE UNDER PANEL 414DB IAW ERS-EM-53MR-1778.SDR UIEA2015111600657Skin · damagedDAMAGE FOUND TO FUSELAGE SKIN AT STATION 1925, AFT CARGO DOOR AREA, A =1.5", Y =1/16". VISUAL INSPECTION EVERY 250 FLIGHT CYCLES. REMOVED DAMAGE & REPAIRED IAW SRM 53-00-01-2R-1 REPAIR 1.SDR DALA2015111306981Skin · damagedLIGHTNING STRIKE ON FASTENER AT STA 263 BETWEEN L24R-L25R. REMOVED FASTENER, HFEC IAW NDT 51-00-19, NDT 51-00-16. OK TO TREAT, PRIME, AND INSTALL FASTENER. INSTALLED SOLID FASTENER, TREATED, PRIME AND PAINTED WORKED AREA. CATEGORY A REPAIR NO FURTHER ACTIOSDR DALA2015111306980Skin · damagedLIGHTNING STRIKE ON FASTENER AT BS 263 AT L27L. REMOVED FASTENERS, HFEC NDT 51-00-19, NDT 51-00-16. OK TO TREAT, PRIME, AND INSTALL SOLID FASTENER. INSTALLED SOLID FASTER, TREAT AND PRIMED & PAINTED WORKED AREA IAW SRM 53-00-01, FIG 201. CATEGORY A REPAIR NOSDR DALA2015111306979Skin · damagedLIGHTNING STRIKE ON FASTENER AT BS 215 BETWEEN L 24-25 R. REMOVED FASTENER, HFEC NDT 51-00-19, NDT 51-00-16. OK TO TREAT, PRIME AND INSTALL FASTENER. INSTALLED SOLID FASTENER, TREATED, PRIMED, AND PAINTED WORKED AREA. CATEGORY A REPAIR NO FURTHER ACTION REQSDR DALA2015111306946Skin · damagedLIGHTNING STRIKE IN NOSE AREA. FOUND EVIDENCE OF DISCHARGE APPROXIMATELY 3" AFT OF DOOR 1R, 12" FROM TOP EDGE. REF SRM 53-00-01, REPAIR 6 + 53-00-01, REMOVED FASTENER + CLEANED UP AREA. NEEDS NDT EDDY CURRENT, WIP 715288, MEASURED BLEND TO BE WITHIN ACCEPTASDR SIMA20151112002Skin · damagedLEFT AFT FUSELAGE SKIN SHOWS ADVERSE SCREEN INDICATIONS DURING HFEC. THREE PLACES AT FRAME 75, BETWEEN STRINGERS 1L & 3L. REPAIRED LT AFT FUSELAGE SKIN IAW ERS-EM-53MR-1751.SDR SIMA20151112003Skin Panel · damagedHAIL DAMAGE EVENT. REPLACE FWD FUSELAGE II CROWN SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R FWD FUSELAGE II CROWN SKIN PANEL IAW SRM 53-12-01 SI, 51-20-01, 51-20-03, 51-40-06, 5SDR DALA2015111206909Skin · damagedWEAR ON RECEIVER OF L1 DOOR HOOK AT EXTERNAL FUSELAGE SKIN BETWEEN LONGERON 15LT AND 14LT, BS 160 TO 148. NEW DOUBLER WAS FABRICATED, DRILLED, PAINTED, AND INSTALLED IAW SRM 53-04, FIG 24, SHEET 2, 51-10-4, 51-10-3 PAR 14, 51-30-2, AND 51-30-5, 51-10-2. PISDR CA151111002Skin · corroded(CAN) DURING C CHECK, CORROSION FOUND ON FUSELAGE SKIN BS 559+32 TO 559+112 STRINGER 27. NO DAMAGE IS ALLOWED IN THIS AREA IAW SRM 53-00-31. MINIMUM REMAINING THICKNESS IS 0.057", ORIGINAL THICKNESS IS 0.063".SDR SWAA2015123147561Skin · crackedFUSELAGE SKIN CRACKED AT STATION 344, STRINGER 17R. REPAIRED SKIN IAW EA.SDR CALA2015111300913Skin · dentedSMALL DENT IN FUSELAGE ON ACFT RIGHT BELOW R1 DOOR, AT STATION 380, STRINGER 26 - 27R. PERFORMED INTERIM REPAIR, REF ECRA 5330 - 05444, PART 1. INSPECT AS PER PART 2. DIP 53-DIP 38338. ACCOMPLISH A PERMANENT REPAIR WITHIN 50,000 TOTAL FLIGHT CYCLES. PLANNSDR DALA2015111206952Skin · corrodedCORROSION ON INSIDE SURFACE OF SKIN OTBD OF STR 42L BETWEEN FRAMES 56-57. PRI 541258-14AD, REV O,1,2. C/W PRI 541258-14AD, REV 2, STEP 9.SDR DALA2015111206951Skin · corrodedCORROSION ON SKIN UNDER STR 43L BETWEEN FRAME 56 & 57, PRI 541258-14AD, REV 0, 1, 2 AND ER/A 541258-14AD. BLENDED OUT CORROSION UNDER SKIN IAW 51-74-00, MININUM REMAINING THICKNESS .148.SDR DALA2015111206902Skin · crackedCORROSION ON FUSELAGE SKIN INTERNAL DOUBLER BETWEEN BS 1309-1322 AND LONGERONS 20-23L. REPAIRED IAW ER/A 508134-14, REV B.SDR DALA2015111206901Skin · crackedCRACK OF 0.150" LENGTH ON FUSELAGE SKIN, BS 1418 BETWEEN LONGERON 2-3 LT, SM, CARD 2, ZONE 65. DAMAGE WAS REPAIRED IAW ER/A 539886-14, AD REV: ORIGINAL. REPAIR APPROVAL IS LIMITED TO 75,000 TOTAL CYCLES ONLY. ADDITIONAL E/A, ER/A REVISION, IS REQUIRED FOR SDR ASAA2015111017348Skin · damagedLIGHTNING STRIKE AT BS 502 ADJACENT TO RIVET HEAD 1.7" ABOVE STRINGER 4R. ACFT GROUNDED. ACCOMPLISHED PERMANENT CATEGORY B REPAIR IAW EA 900ER-53EA-17423 REV 00 AND REO-G20079 REV A.SDR SWAA2015112346253Window Post · crackedLEFT NR 3 WINDOW POST NR 3 HOLE FROM BOTTOM CRACKED. REPAIRED WINDOW POST IAW EA.SDR CALA2015111794817Skin · crackedTHREE EACH HOLES WERE FOUND CRACKED, R5 DOOR CUT OUT AFT UPPER CORNER. EA 5331-01798 OP 10 WAS ACCOMPLISHED FOR REPAIR, BUT HAD DEVIATIONS THAT WERE ADDRESSED ON ECRA 5330-05433. NR 5R DOOR AFT UPPER CORNER SKIN REPAIRED IAW ECRA 5330-05433.SDR FDEA201511103548Skin · crackedRIGHT FUSELAGE UPPER AFT CORNER OF NR 3 A/C COMPARTMENT. DOOR CUT OUT HAS A .200 INCH CRACK EXTENDING OUT OF FASTENERS HOLE, END OF CRACKED CRACK, REPAIR COMPLIED WITH IAW SRM 53-50-00 FIG 3 A SHEET 3.SDR CALA2015111300912Skin · chafedSUPPORT TASK VERTICAL STAB TO FUSELAGE SKIN, LT STATION 2110 - 2195 FOUND CHAFING MARK. REPAIRED IAW ECRA 5330-05449 REV PART 1 ITEM 1 & REPAIR PARTS WEIGHT 6.1 LB ATTACH MX WORK SHEET FORM 44.0008 ITEM 1 TO ITEM 40. ACCOMPLISHED INTERIM REPAIR. REF LOG PAGSDR CALA2015111300911Skin · chafedSUPPORT TASK, VERTICAL STABILIZER LOWER TO FUSELAGE SKIN RT STATION 2110 - 2195 FOUND CHAFING. REPAIRED IAW ECRA 5330-05449 REV PART 1 ITEM 1 & REPAIR PARTS WEIGHT 6.1 LB. ATTACH MX WORK SHEET FORM 44.0008 ITEM 1 - 40 ACCOMPLISHED, INTERIM REPAIR. REF LOG PSDR DALA2015111106924Skin · dentedLT EXTERNAL FUSELAGE, DENT ON SKIN AT BS 620, 4 INCHES ABOVE STRINGER 17LT.SDR DALA2015111106923Skin · dentedLT EXTERNAL FUSELAGE, DENT ON SKIN AT BS 620, 4 INCHES ABOVE STR 17L.SDR DALA2015110906918Skin · dentedUPPER FUSELAGE SKIN HAS DENT AT BS 760- 800, S8R TO S9R. INSPECTED AND MEASURED DENT ON EXTERIOR FUSELAGE BS 760 TO 800, STR 8R-9R A/Y=100, FOUND WITH IN LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III.SDR FDEA201511103551Skin · dentedPROTRUDING DENT BS 1543 IN FUSELAGE SKIN, 2.5" ABOVE STRINGER 27L. REPAIRED SKIN AT BS 1540, BETWEEN STRINGER 26L - 27L IAW-SRM-53-00-01 FIG 201 REPAIR 16. THIS IS CATEGORY B REPAIR, MAJOR.
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