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 IPXA2016060504231Skin · corrodedINSPECTION TYPE:3C, MAIN CABIN SUBFLOOR CENTER WING UPPER SKIN CORRODED AT BS XCW106 ALONG S15. REPAIRED NOTED CORROSION IAW EA 011-5730-01-A6269, REV IR AND UPS EO MD11-5730-60878-A.SDR IPXA2016060504230Skin · corrodedINSPECTION TYPE:3C, MAIN CABIN SUBFLOOR CENTER WING UPPER SKIN CORRODED AT BS XCW113 ALONG S10. REPAIRED NOTED CORROSION IAW EA 011-5730-01-A6267, REV. IR AND EO MD11-5730-60880-A.SDR IPXA2016060504229Skin · corrodedINSPECTION TYPE:3C, MAIN CABIN SUBFLOOR CENTER WING UPPER SKIN CORRODED AT XCW-56 ALONG S15. REPAIRED NOTED CORROSION IAW EA 011-5730-01-A6268, REV. IR AND EO MD11-5730-60879-A.SDR IPXA2016060504228Skin · corrodedINSPECTION TYPE:3C, MAIN CABIN SUBFLOOR CENTER WING UPPER SKIN CORRODED BS XCW-30 TO -36 ALONG S15. REPAIRED NOTED CORROSION IAW EA 011-5730-01-A6266, REV. IR AND EO MD11-5730-60881-A.SDR SWAA2016051851890Skin · crackedSKIN CRACKED AT BS 787+4.5, STRINGER 1L. REPAIRED SKIN IAW SRM.SDR CALA2016051600306Skin · dentedFUSELAGE SKIN DENTED STATION 199 - 205, STRINGER 22R - 23R. REPAIR INITIAL INSPECTION IS AT 37,500 AIRFRAME CYCLES & REPEAT HFEC EVERY 3K FLT CYCLES & HFEC EVERY 6K FLT CYCLES. INSTALLED REPAIR DOUBLER & NEW CLIPS IAW SRM 53-00-07 REPAIR 5 FIG 201 DETAIL II.SDR C77A20160514001Skin Panel · damagedDURING THE ACCOMPLISHMENT OF EO E175-5300-163, MX DISCOVERED ELONGATED FASTENER HOLES IN CF III LOWER SKIN PN 170-91883-005 & DOUBLER 170-87558-001. REQUESTED & RECEIVED RELIEF IN THE FORM OF ETD 2016-170-046409 TO REAM THE DAMAGED FASTENER HOLES OVERSIZED. SDR HALA2016051400249Tab · crackedMAIN CABIN TAB CRACKED ON DOOR SURROUNDED INNER SKIN AT STA 210, LONG 15L, CRACK IS 1" LONG. REMOVED DAMAGED TAB ON INNER SKIN AT FS 210 AND REPAIRED IAW SRM 53-10-15-2R-1, REPAIR 1.SDR HALA2016051400248Tab · crackedMAIN CABIN TAB CRACKED ON DOOR SURROUNDED INNER SKIN AT STA 210, LONG 15L, CRACK IS 1" LONG. REMOVED DAMAGED TAB ON INNER SKIN AT FS 210 AND REPAIRED IAW SRM 53-10-15-2R-1, REPAIR 1.SDR SWAA2016060652529Skin · corrodedFUSELAGE SKIN CORRODED AT BS 747, BETWEEN STRINGER 27L - 26L. REPAIRED SKIN IAW SRM.SDR FDEA201605141583Skin · dentedLOWER FUSELAGE, SEVERAL DENTS IN OUTER SKIN LOCATED JUST FWD OF LOWER FWD CARGO DOOR, APPROX STATION 879, BETWEEN LONGERON 35 - 36. INSTALLED REPAIR IAW SRM 53-20-00 FIG 6.SDR DALA2016051503975Skin · damagedCORROSION FOUND ON WING CENTER TANK TOP SKIN EXTERNAL SURFACE BETWEEN FRAME 42 AND STR 16, RIB 1 DATUM AND 1292. PERMANENT REPAIR ON UPPER SKIN BETWEEN FRAME 41 TO FRAME 42 AND 1292 TO 1732 PASSENGER CABIN ON CENTER WING BOX IAW ERA 546005-14AD REVISION ORIGISDR A6WA201643890Skin · dentedPERFORM PERMANENT REPAIR TO FUSELAGE SKIN, 2 OFF DENTS BETWEEN LT FS 409+64 - 409+80, STRINGER 18L - 19L. REPAIRED SKIN IAW SRM 53-00-31 REPAIR NR 1 & SRM 53-00-15.SDR KPVA20160705005Skin · corrodedWHILE UNDERGOING 2 YEAR CHECK INSPECTION, CORROSION WAS FOUND ON FUSELAGE SKIN INTERNAL SURFACE BETWEEN FRAMES 24 AND 25, AND STRINGERS 19 RIGHT AND STRINGER 20 RIGHT. SKIN REPAIRED IAW CETS-2231/16.SDR ASAA2016051316887Skin · crackedCRACK IN FUSELAGE SKIN AT BS 727D+2" BELOW STR 23L AT CHEM MILL STEP. ACFT GROUNDED. REPAIRED FUSELAGE SKIN AT BS 727D+2" IAW SRM 53-00-01, REPAIR 31. THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 66000 FLT. CYCLES, REFER TO OPERATORS REPAIR ASSSDR ASAA2016051316764Skin · crackedCRACK IN FUSELAGE SKIN AT BS 727F+4" BELOW STR 23L AT CHEM MILL STEP. ACFT GROUNDED. REPAIRED SKIN IAW SRM 53-00-01-2R-31, DETAIL VII. THIS IS A CATEGORY B REPAIR. INSPECTION THRESHOLD SET AT 66,000 CYCLES. REFER TO THE OPERATORS REPAIR ASSESSMENT PROGRAM FSDR ASAA2016051316763Skin · crackedCRACK IN FUSELAGE SKIN AT BS 727D+2" BELOW STR 23R AT CHEM MILL STEP. ACFT GROUNDED. REPAIRED SKIN IAW SRM 53-00-01-2R-31, DETAIL VII. THIS IS A CATEGORY B REPAIR. INSPECTION THRESHOLD SET AT 66,000 CYCLES. REFER TO THE OPERATORS REPAIR ASSESSMENT PROGRAM FSDR SWAA2016051851897Skin · damagedSKIN DAMAGED AT BS 802, STRINGER 25R. REPAIRED SKIN IAW EA.SDR ASOA2016051214901Skin · crackedLEFT FWD FUSELAGE SKIN CRACKED BELOW AFT TRU DOOR LATCH AT APPROXIMATELY FS 192.00. REMOVED CRACKED DOOR LAND AND INSTALLED NEW SERVICEABLE DOOR LAND ON LT FWD FUSELAGE BELOW TRU DOOR IAW DWG 600-33052 AND SRM 51-42-06-00 AND 51-42-12-00. LOCATED AND DRILLED SDR SWIA201642176Skin · dentedELONGATED DENT IN EXTERNAL SKIN, BS 256.75 - 258.75, BETWEEN STRINGERS 24 - 25R. COMPLIED WITH EA. ALL STEPS COMPLETED OF PERMANENT REPAIR.SDR DALA2016051303915Skin · crackedSKIN CRACKED AT APPROXIMATELY FS 1095 AND APPROX 6" ABOVE RT PYLON-M. REPAIRED SKIN CRACK AT FS 1095 IAW ER/A 54669-14. SRM 51-40-05, PG 1 IDENTIFY REPAIRED IAW ER/A 54669-14. ASSOCIATED ER/A 54-566914 ADDED FOR AC 9516.SDR DALA2016051303914Skin · corrodedUPPER WING TO CENTER TANK PLANK ON FORWARD BULKHEAD CORRODED FROM BL0 TO RBL 58. REPAIRED UPPER CENTER TANK PLANK SKIN IAW ER/A 545622-14, REV A.SDR KCSA201605121017Skin · crackedCRACKED SKIN BS 1724, STR 22L.SDR JR2R05122016004Skin · crackedEXTERNAL POWER RECEPTICAL DOOR CUTOUT SKIN CRACKED .5" IN LENGTH. REPAIRED IAW STS EA 30-2016-141, DOCUMENTED ON WO 00298720, M301, 004.SDR KC8A20160510003Skin · crackedDURING ROUTINE INSPECTION, A CRACK WAS FOUND ON THE LOWER FUSELAGE SKIN AT THE FORWARD LOWER CORNER OF THE MAIN ENTRY DOOR. CRACK TO BE REPAIRED IAW FIELD SERVICE ENGINEERING.SDR EE4Y2016051200022Skin · dentedLOWER FUSELAGE SKIN FROM FRAME 85 TO 86 BETWEEN STRINGERS 22 & 23R FOUND DENTED. REPAIRED IAW ETD2016-190-044552.SDR SWAA2016062753238Skin · crackedR1 DOOR FUSELAGE SKIN LOWER AFT CORNER CRACKED. REPAIRED SKIN IAW SRM.SDR SWAA2016060652539Skin · corrodedSKIN CORRODED AT BS 500+10.5, BL 0. REPAIRED SKIN IAW ER & EA.SDR SWAA2016060652538Skin · corrodedSKIN CORRODED AT BS 500+10.5, BL 0. REPAIRED SKIN IAW ER & EA.SDR ASAA2016051116890Skin · crackedR1 DOOR CUTOUT LOWER AFT CORNER IS CRACKED. ACFT GROUNDED. REPAIRED DAMAGE TO LOWER AFTER CORNER OF R1 DOOR CUTOUT IAW SRM 53-10-01-2R-19, REPAIR 19. THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 60,000 TOTAL FLIGHT CYCLES REFER TO THE REPAIR SDR SIMA20160511015Skin · crackedLEFT UPPER FUSELAGE SKIN CRACKED 2 PLACES. CRACK 1 IS JUST FWD OF FRAME 75 & JUST ABOVE STRINGER 2L, CRACK IS APPROX 1.25" LONG. CRACK 2 IS AT THE FIRST FASTENER BELOW STRINGER 2L ON FRAME 75, CRACK IS 1/4" LONG. PERFORMED REPAIR AT LT UPPER FUSELAGE SKIN CRSDR DALA2016051203888Skin · canningDENT WITH OIL CAN EFFECT ON EXTERNAL FUSELAGE, SKIN BS 1189 CANT TO 1200 CANT BETWEEN 6-7 O'CLOCK POSITION, SM, FS. FUSELAGE SKIN WAS REPAIRED IAW ER/A 545165-14, REV ORIGINAL.SDR GLBA2016051200586Skin · corrodedMAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND BELLY CORROSION AT FS 213.35 & STRINGER 14L, JUST AFT OF ADF ANTENNA. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR & RETENTION OF THE PAPERWORK.SDR EE4Y2016051100020Skin · dentedUPPER FUSELAGE AT FRAME 20+75 MM AND FRAME 20+107 MM AND 67MM ABOVE STRINGER 12L SKIN DENTED. DAMAGE HAS BEEN REPORTED UNDER NON ROUTINE ITEM A1E143, 2-112. REPAIR HAS BEEN ACCOMPLISHED UNDER ETD2016-190-044555, INSTRUCTIONS AND APPROVED.SDR SWAA2016070853631Post · crackedRT 3 WINDOW E-F POST CRACKED AT 2ND FASTENER HOLE FROM BOTTOM. REPAIRED POST IAW ACO.SDR HALA2016051000248Doubler · crackedCRACK ON GROUND CONDITION AIR ACCESS DOOR LANDING, FWD INBD CORNER AND AFT INBD CORNER. R & R CRACKED DOUBLER AT GROUND CONDITIONED AIR ACCESS DOOR LANDING IAW DWG 5911429, REV 02 AND SRM 51-41-02, LEAK CHECK GOOD IAW AMM 21-22-07.SDR SWIA201642231Skin · dentedDENT APPROXIMATELY AT BS 625 AT STRG 20L. REPAIRED IAW EA.SDR FDEA201605101523Skin · unknownFUSELAGE EXTERIOR SKIN THERE IS A RIVET THAT IS NOT FLUSH AT BS 1520, BETWEEN STRINGER 29 LT & 29 RT. REPAIR CARRIED OUT IAW EA F-5330-T0324711B PART 1. REPAIR CLASSIFIED AS MAJOR.SDR FDEA201605101522Skin · damagedFUSELAGE EXTERIOR SKIN THERE IS A RIVET WITH AN ELONGATED HOLE AT BS 1600 - 1620, BETWEEN STRINGER 29 LT & 29 RT. REPAIR CARRIED OUT IAW EA F-5330-T0325043A PART 1. REPAIR CLASSIFIED AS MAJOR.SDR DALA2016051103865Skin · damagedDAMAGE TO FUSELAGE SKIN BS 1520, BETWEEN STR 15 - 16L. REPAIRED IAW ERA 546898-14AD.SDR DALA2016051103858Skin · crackedSKIN IS CRACKED JUST ABOVE THE PYLON. FWD OF AFT ENGINE MOUNT. ACCOMPLISHED HFEC TO IDENTIFY ENDS OF CRACKS IAW NDTSPM 06-10-01.00. ACCOMPLISHED SECTION 1 OF ER/A 546967-14.SDR SWIA201642171Skin · dentedDENT APPROXIMATELY BS 589 AT STR 22 - 23L. DENT OUT OF LIMITS IAW SRM. COMPLIED WITH ALL STEPS OF EA.SDR DALA2016051003862Skin · dentedDENT ON FUSELAGE SKIN FWD AND AFT SIDE OF FRAME AT BS 640, BELOW SKIN LAP STR 14L. FOUND DENT TO BE OUT OF LIMITS REF SRM. COMPLIED WITH ER/A 544731-14 REV ORIGINAL. REF NRC.SDR DALA2016051003861Skin · damagedLOWER FUSELAGE SKIN BS 740-760, STR 18-20L DAMAGED. FOUND OUT OF LIMITS IAW SRM. TRIMMED OUT DAMAGE. REPAIRED IAW SRM.SDR DALA2016051003860Skin · dentedFUSELAGE SKIN BS 600-640, STR 15-19L, DENTED AND SCRATCHED. REPAIRED THE SKIN IAW ER/A 544731-14, REV ORIGINAL.SDR DALA2016050903836Skin · damagedDUE PRI 546901-14: FOUND 2 PULLED FASTENERS AT BS 229 BETWEEN 29RT AND 30RT. C/W PRI 546901-14, REV 0,1, 2, 3. C/W PRI 546901-14, REV 4, 8 MAY 16 AT 2230E. VERIFIED ERA 546901-14, REV ORIGINAL MATCHES PRI 546901-14, REV 0,1,2,3,4 8TH MAY 16 AT 2230E.SDR DALA2016111108699Splice Strap · corrodedER/A 546901-14 WAS ISSUED TO ADDRESS CORROSION TO THE SPLICE STRAP COMMON TO THE FUSELAGE BUTT SPLICE AT STA 229.SDR AALA201606249016Skin Panel · crackedAIRCRAFT IN BASE MAINTENANCE, CRACK INDICATION IN SKIN PANEL FASTENER HOLE AT FRAME 35 AND STR 30 LT. REPAIRED SKIN PANEL IAW EA 260369.SDR SIMA20160508010Skin · crackedINVESTIGATE POSSIBLE SKIN CRACK AT FRAME 77, BETWEEN STRINGER 5L - 7L, ONE EACH. REPAIRED SKIN CRACK IAW ERS-EM-53MR-2107.SDR SIMA20160508009Skin · crackedINVESTIGATE POSSIBLE SKIN CRACK AT FRAME 79, BETWEEN STRINGERS 4L - 6L, ONE EACH. REPAIRED SKIN CRACK AT FRAME 79, BETWEEN STRINGERS 4L - 6L IAW ERS-EM-53MR-2107.
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