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 IPXA2016071906059Skin · dentedINSPECTION TYPE: SEG4, SKIN DENTED BS 360, STRINGERS 15-16L. REPAIRED IAW EA 757-5311-27A2226 AND EO B757-5330-61249-A.SDR SWAA2016071853927Skin · crackedEXTERNAL GROUND ELECTRICAL POWER AFT SIDE AT LOWER FUSELAGE CUTOUT CRACKED. REPAIRED CUTOUT IAW SRM.SDR CALA2016070500403Skin · dentedEXISTING DENT FWD OF L-2 DOOR BETWEEN STA 620 AND STA 640 BETWEEN STR 17L AND STR 18L. INSTALLED FUSELAGE PARTIAL SKIN REPLACEMENT STA 570-661, STR 14L-19L REF RES WI NR 2010609-16 AND ECRA NR 5330-057-36. THIS IS A PERMANENT REPAIR WITH REQUIRED INSPECTIONSSDR CALA2016070500402Skin · damagedLIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT STA 402 AND STA 408 BETWEEN STR 26-27 RT. REMOVED DAMAGED AREA AND INSTALLED REPAIR IN REF TO ECRA 5331-02113. INTIATED 53-DIP CONTROL 99370 TO ACCOMPLISH REPAIR ON/OR BEFORE JULY 1, 2017 IAW PART 3 OF ECRA 5331-021SDR CALA2016070195498Skin · crackedFUSELAGE BUTT JOINT AREA AT FRAME 35 STINGER 30L CRACKED. REPAIRED IAW ECRA 5330-05742 REV- PART 1.SDR CALA2016070100397Skin · damagedLIGHTENING STRIKE ON SKIN AT BS 429 AT S26R. REMOVED DAMAGED AREA AND INSTALLED REPAIR IAW ECRA 5331-02112.SDR FDEA201607012220Skin · crackedTWO CRACK INDICATIONS APPROXIMATE 2.0 INCHES IN LENGTH FOUND DURING X-RAY INSPECTION AT STA 6-0, LONGERON SPLICE 4R AFT SECTION EDGE.SDR COEA2016063058811Skin Panel · corrodedCENTER FUSELAGE LT UPPER SKIN PANEL INNER SURFACE HAS CORROSION, FRAMES 23C-23D, STRINGER 6A-7. REPAIRED IAW SRAS CETS-3143/16..SDR COEA2016063057811Skin Panel · corrodedCENTER FUSELAGE LT UPPER SKIN PANEL INNER SURFACE HAS CORROSION, FRAMES 23C-23D, STRINGER 5A-6. REPAIRED PER SRAS CETS-3143/16.SDR COEA2016063056811Skin · corrodedCENTER FUSELAGE LT UPPER SKIN PANEL INNER SURFACE HAS CORROSION, FRAMES 23B - 23C, STRINGER 7A - 8L. REPAIRED IAW CETS-3143/16.SDR SWAA2016071853971Skin · crackedSKIN CORRODED AT BS 727D+10, BL0. REPAIRED SKIN IAW ER AND EA.SDR AALA20160630018Skin · damagedFUELAGE SKIN IS DAMAGED AT APPROXIMATELY BS 1720, S30R. REPAIRED SKIN IAW SRM 53-00-01, REPAIR 14 AND EA 261141.SDR AALA20160630011Skin · crackedAIRCRAFT WAS IN BASE MAINTENANCE. FUSELAGE SKIN IS CRACKED AT FRAME 1474 AND L22R. REPAIRED SKIN IAW SRM 53-01-00 AND 53-30-00-03.SDR WVER2016062932601Skin · damagedMULTIPLE LIGHTNING STRIKES TO RT SIDE OF FUSELAGE.SDR COEA2016062931811Skin · damagedLIGHTENING STRIKE AT FRAME 8, AFT SKIN EDGE AT BUTT JOINT BETWEEN FWD AND AFT NOSE FUSELAGE CROWN SKIN PANELS. REPAIRED IAW CETS-3232/16.SDR SIMA20160629007Skin · damagedDURING REPAIR, CUT OUTS MADE TOO LARGE FOR REPAIR OF CRACKS AROUND TWO FASTENER HOLES ON FRAME 78 BETWEEN STRINGERS 5L AND 7L, AND AROUND TWO FASTENER HOLES ON FRAME 77 BETWEEN STRINGERS 5 AND 7 LEFT. AIRCRAFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION AND WSDR SIMA20160629009Skin · crackedDURING MBV INSPECTION,QA FOUND A CRACK AT A FASTNER HOLE ON FR 75 BETWEEN STRINGERS 2R AND 3R. AIRCRAFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. -C/A-PERFORMED PERMANENT REPAIR ON CRACK AT FASTNER HOLE OSDR SIMA20160629008Skin · crackedDURING MBV INSPECTION,QA FOUND 1 CRACK AT FASTNER HOLE ON FR 75 BETWEEN STRINGERS 1L AND 2L. AIRCRAFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. -C/A-PERFORMED PERMANENT REPAIR ON CRACKED FASTNER HOLE ONSDR DALA2016063005035Skin · corrodedCORROSION BETWEEN FUSELAGE SKIN AND INTERNAL DOUBLER AT AFT LAV SERVICE PANEL LOWER AREA. FUSELAGE SKIN WAS REPAIRED IAW ETI-88-16-207, REV 1 AND ER/A 547801-14, REV ORIGINAL.SDR DALA2016111108697Skin · corrodedFUSELAGE SKIN & DOUBLER AFT LAV SVC PANEL DOOR CUTOUT CORROSION. REPAIRED PER ER/A 547801-14. ACCOMPLISH SECTION II VISUAL INSPECTION EVERY 8000 FLIGHT CYCLES.SDR SWAA2016080954676Skin Panel · delaminatedLEFT LOWER FUSELAGE SKIN PANEL DELAMINATED BETWEEN BS 663.75 TO BS 727. REPAIRED SKIN IAW SRM.SDR SWAA2016080854637Skin · delaminatedRIGHT EXTERNAL SKIN PANEL DELAMINATED BETWEEN BS 685 - 727, LOWER FUSELAGE. REPAIRED THE SKIN IAW SRM.SDR IPXA2016070905601Skin · gougedINSPECTION TYPE:C-15, UPPER SKIN EXTERNAL CROWN IS GOUGED AT BS 1090 ANTENNA MOUNTING AREA. REPAIRED IAW SRM 53-00-01-2R-3.SDR SWAA2016081054713Skin · delaminatedRIGHT LOWER FUSELAGE SKIN DELAMINATED BETWEEN BS 663.75 - 685. REPAIRED THE SKIN IAW SRM.SDR SWIA201642408Skin · dentedSMALL DENT 6" FWD OF EXTERNAL POWER RECEPTABLE DOOR 1.25" X 1" DIA APPROXIMATELY .005" DEEP LOCATED RT SIDE OF ACFT 6" FWD OF EXTERNAL POWER RECEPTACLE DOOR. REPAIRED DENT IAW STS EA. OPS, RIG CHECKS GOOD.SDR AALA201607299028Skin · corrodedCORROSION ON UPPER SKIN BETWEEN FR 40 AND F R42 AND BETWEEN RIB1 AND Y1292. REPAIRED SKIN IAW EA 261850.SDR UIEA2016062700469Skin · damagedPERFORMED EXTERNAL SKIN DAMAGE REPAIR B/T STA 1197+44 TO STA 1197+66, STR 39R-39L, REF IAI NRC M0548. THE REPAIR PERFORMED WITH DOUBLER AND FILLER IAW SRM 53-00-01, FIG 201, REPAIR 29.SDR UIEA2016062700464Skin · damagedPERFORMED ABRASION DAMAGE REPAIR AT FUSELAGE LOWER SKIN, BS 1423, STR 24R-STR 25R, REF IAI NRC M0076. THE REPAIR PERFORMED WITH REPAIR DOUBLER AND FILLER IAW SRM 53-00-01, FIG 201, REPAIR 14, DETAIL 1.SDR DALA2016062804964Skin · crackedLEFT FUSELAGE SKIN CRACKED APPROXIMATELY .125" AROUND FASTENER HEAD AT STA 1095 JUST ABOVE LONGERON 14L. VERIFIED BY EDDY CURRENT. REPAIR 4H FUSELAGE SKIN CRACK IAW ER/A 545686-14, REV ORIGINAL. ASSOCIATED ER/A 54-568614 ADDED FOR AC 9578.SDR DALA2016062804963Skin · crackedRIGHT FUSELAGE SKIN CRACKED AT FASTENER HEAD AND BETWEEN 2 FASTENERS, STA 1095 JUST ABOVE LONGERON 14R. VERIFIED BY EDDY CURRENT.
REPAIRED RT FUSELAGE SKIN CRACK IAW ER/A 545686-14, REV ORIGINAL. ASSOCIATED ER/A 54-568614 ADDED FOR AC 9578.SDR FDEA201606252140Skin · crackedNR 3 A/C COMPARTMENT CUTOUT AFT UPPER CORNER SKIN HAS A .75" CRACK FROM SKIN EDGE THRU 1 FASTENER. REPAIRED A/C COMPARTMENT IAW SRM 53-50-00, FIG 3A, VOL 1.SDR FDEA201606242135Skin · damagedSCRIBE LINE DAMAGE FOUND AT LAP SEAM S-14R, BS 777 TO BS 779. COMPLIED WITH EA F-5330-T0325500, PT 1: FUSELAGE, PLATES AND SKINS, SECTION 43- SCRIBE LINE INSPECTIONS, STR S-14R, BS 777.032 TO BS 778.99, 1.65" LG. CLASSIFIED AS A CAT B MAJOR REPAIR.SDR CALA2016062700386Skin · damagedLIGHTNING STRIKE DAMAGE OUT LIMITS FROM STA 807 TO STA 847, STR 25L TO STR 27R. REPAIRED IAW ECRA 5331-02109, INITIATED A DIP IAW SAME ECRA PART 1 STEP D-9. ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE JUNE 24, 2018. PLANNING TO CONTACT ENGINEERING AFTER APRISDR SIMA20160623007Skin · crackedRT AFT FUSELAGE, FRAME 75 SKIN CRACKED BELOW STR 2R. REPAIRED THE SKIN IAW ERS-EM-53MR-2162SDR FDEA201606232128Skin · dentedFUSELAGE DENT AT APPROXIMATELY STA 412, 5.5" JUST BELOW STR 31L. EVALUATED DENT AT STA 417 STR 31L, AY=17.46 IS OUT OF LIMITS. REPAIRED DENT BY REMOVING DAMAGE (2"X2.5"), FABRICATED & INSTALLED REPAIR FILLER AND DOUBLER FROM 2024T3-.063 PO ST00006329 IAW SSDR CALA2016062700383Skin · damagedLIGHTNING STRIKE FOUND AT STA 471, STR 23L TO STR 24L. ACCOMPLISHED REPAIR OF FUSELAGE SKIN AT STA 471, STR 23L TO STR 24L IAW EC/RA 5331-02104.SDR CALA2016062700382Skin · crackedREF AD 2013-19-04, EA 5310-05878, REV D, OP-5 STE 7.1 LOWER FUSELAGE STA 540, STR-22, AMP 23, RT SIDE THERE IS A CRACK INDICATION IN THE SKIN AT THE 2 PLACES IN THE FWD FASTENER .2500 HOLE JUST BELOW THE DRAG LINK COMMON TO THE CHORD AREA. FUSELAGE AT STA 540SDR CALA2016062700381Skin · crackedPERFORMED HFEC IAW NDT PART 6, 51-00-00 PROCEDURE 23 AND EA 530-05878, REV D, STEP 4, 2. FOUND CRACKS ON RT SKIN, STA 540 BETWEEN STR S-22R AND S-23R. CRACK NOTED AT FWD ROW, 2ND HOLE AND CRACK NOTED ON AFT ROW 2ND HOLE. REF FIG 2, SHEET 2 OF 2 OF THE EA NOSDR DALA2016062404913Skin · damagedFUSELAGE SKIN DAMAGE BETWEEN STA 1095 AND STA 1116, L-21L AND L-23L REF EMPOWER NR 35, RII ENTRY, REF NR 35 REPAIRS MADE IAW ER/A 547473-14, REV A. ASSOCIATED ER/A 14-547473 ADDED FOR AC 9562.SDR DALA2016062404909Doubler · corrodedCORROSION ON INTERNAL DOUBLER OF RADIO ALTIMETER CUTOUT ANTENNA LOCATED FROM STA Y=674-693 BETWEEN LONGERONS 30 AND 29LT. REMOVED FASTENERS STA Y=660 TO Y=693, LONG 30 AND LONG 29 LT IAW SRM 51-30-2 DOUBLER INTERNAL WAS REMOVED IAW SRM 51-30-2 DOUBLER INTERNASDR DALA2016062304895Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON EXTERNAL SKIN PASSENGER CREW DOOR LOCATED BETWEEN BEAM 3 TO BEAM 4 AND XP297 TO XP453 AT FORWARD GALLEY AREA. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN PASSENGER CREW DOOR LOCATED BETWEEN BEAM 3 TO BEAM 4 ANDSDR DALA2016062304894Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON EXTERNAL SKIN, LOCATED 6" ABOVE RT SIDE STR AT FRAME 9 AT LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED 6" ABOVE OF LOWER STR RT AND FRAME 9 IAW ER/A 547910-14AD, REV ORIGINAL AND PRI 5479SDR DALA2016062304893Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON EXTERNAL SKIN LOCATED 6" ABOVE RT SIDE STR AT FR 11 AT LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED "6" ABOVE OF LOWER STR RT SIDE AND FRAME 11 IAW ER/A N547910-14 AD REV ORIGINAL AND PRISDR FDEA201606232111Skin · crackedNLG EXTERIOR SKIN RT FWD CORNER AT STA 306 HAS A CRACK. REPAIRED DAMAGED IAW SRM 53-50-00, FIG 25, SHEET 3.SDR ASOA2016062215093Doubler · corrodedTCAS DOUBLER CORRODED AT STRINGER 27 BETWEEN BS 295 & 310. REMOVED AND REPLACED TCAS DOUBLER IAW SRM 51-42-06-001-001-A01.SDR A6WA201644030Skin · crackedSKIN CRACKED RT AFT NLG SPADE DOOR CUTOUT AT FS 235.00, STR 26R. REPAIRED RT AFT NLG SPADE DOOR CUTOUT AT FS 235.00, STR 26R IAW GREO 601R-53-11-048, REV-D, DATED 06/10/2015.SDR DALA2016062304892Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON EXTERNAL SKIN ON UPPER FUSELAGE FROM FRAME 56 TO FRAME 57 AND STR 1L. PERFORMED TIME LIMITED REPAIR ON EXTERNAL SKIN ON UPPER FUSELAGE FROM FRAME 56 TO FRAME 57 AND STR 2LT TO 2RT IAW ER/A 546749-14, REV ORIGINSDR DALA2016062304891Skin · dentedDENT ON EXTERNAL SKIN, ON UPPER FUSELAGE STR 23L BETWEEN FRAME 64 TO FRAME 65. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN, ON UPPER FUSELAGE STR 23L BETWEEN FRAME 64 TO FRAME 65 IAW ER/A 546748-14.SDR DALA2016062304872Skin · crackedCRACKED SKIN ON ELEVATOR ACCUMULATOR ACCESS CUTOUT, AFT UPPER CORNER LOCATED BETWEEN STA 1463 CANT AND 1474 CANT RT SIDE. SKIN DOUBLER WAS REPLACED IAW DWG 5917686-7, REV AA, SRM 51-30-5 AND 51-30-2.SDR DALA2016062304868Skin · puncturedPUNCTURE ON AFT VENTRAL STAIR OUTER SKIN, STA Y=1474, CANT. DAMAGE WAS REPAIRED IAW SRM 53-04-2 FIG1.
Back to JASC 5330