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 DALA2017071605443Doubler · crackedTHRUST REVERSER HCU ACCESS DOOR INTERNAL DOUBLER CRACKED, BS 1074 LONGERON 22R, . NO WORK ACCOMPLISHED ON THIS NON-ROUTINE CARD. THIS NON-ROUTINE WRITTEN FOR SDR TRACKING ONLY. T/R HCU ACCESS DOOR CUT OUT INTERNAL DOUBLER STA 1074 LONGERON 22RT REPAIRED ON NR-SDR DALA2017072305662Skin · damagedON ARRIVAL, FOUND A DENT AND GOUGES 28 INCHES AFT OF WATER SERVICE PANEL ON ACFT LEFT. REPAIRED IAW ER/A 560289-14.SDR V0XD20170714003Skin · dentedTHREE SCRATCHES AND A DENT BETWEEN BS 549 - 565, STRINGERS 16 - 17L. CUT AWAY DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR IAW REO 670-53-31-415, REV B.SDR AALA20170714004Skin · crackedWHILE ACCOMPLISHING AD 2004-11-07 ON THE R1 DOOR FRAME CORNERS, MAINTENANCE WAS UNABLE TO ACCOMPLISH HFEC INSPECTION ON TWO FASTENER HOLES ALONG THE EDGE OF THE LOWER AFT DOOR CUTOUT. REPAIRED IAW EA 271024.SDR DALA2017081806289Access Panel · crackedCRACK AT LEADING EDGE OF FUEL ACCESS PANEL. REPAIRED PER ERA 560110-14.SDR AALA201707249022Skin · corrodedCORROSION FOUND ON THE LEFT SIDE AFT TOP SKIN PANEL OF CENTER WING BOX, OTBD CORNER UNDER FUEL LINE, Y1292 BETWEEN FRAMES 41 AND 42. REPAIRED THE SKIN PANEL IAW EA 271166.SDR IPXA2017072019562Skin · corrodedINSPECTION TYPE: PE, XTERIOR FUSELAGE SKIN HAS CORROSION AT BS 2139 - 2163, LONGERONS 33 - 35R. REPAIRED THE SKIN IAW EO MD11-5330-64948-A. MAJOR.SDR DALA2017071405471Skin · damagedINSPECTION SHOWS MATERIAL THINNING BS 726 - 727 BETWEEN LONGERON 29L & 30R, .041 REMAINING FROM .063.SDR DALA2017071405468Skin · crackedLOWER AFT SKIN AT STRINGER 17 CRACKED. REPAIRED IAW ER/A 560178-14AD.SDR SWIA201743626Skin · dentedPASSENGER DOOR CUTOUT, FWD SIDE BETWEEN STRINGERS 14L AND 15L, TWO DENTS ON EDGE OF DOOR CUTOUT. COMPLETED ALL APPLICABLE STEPS OF REO.SDR UIEA2017071301194Skin · damagedFUSELAGE SKIN DAMAGED BOTTOM SIDE BS 137 AND RBL 10.5. ACCOMPLISHED A REPAIR IAW EO 6753A513, REV O, PART 1. NO CRACK INDICATIONS NOTED AT THIS TIME IAW NDT M PART 6-51-00-01.SDR QV1Y20170712001Doubler · corrodedCORROSION FOUND ON THE FMU ANTENNA BASE/ DOUBLER DURING MAINTENANCE. STC HOLDER WAS CONTACTED FOR PROVIDING ALLOWABLE LIMITS AND/ OR REPAIR INSTRUCTIONS.SDR SWIA201743618Skin · dentedPROTRUDING DENT 2 INCHES AFT OF BS 672.2 BETWEEN STRINGERS 250R AND 26R, APPROXIMATELY .004 DEEP. REPAIRED IAW REO.SDR SWIA201743617Skin · dentedPROTRUDING DENT 5 INCHES FWD OF BS 672.5 BETWEEN STRINGERS 26 AND 27L APPROXINATELY .014 DEEP. REPAIRED THE DENT IAW REO.SDR SWIA201743604Skin · dentedDENT ON THE LEFT SIDE OUTTER FUSELAGE SKIN BETWEEN FS 682 AND FS700 JUST ABOVE STRINGER 20L. REPAIRED THE SKIN IAW REO.SDR FDEA201707111903Longeron Splice · crackedDURING X-RAY INSPECTION ON THE TRANSVERSE SKIN SPLICE STA 5-0, FOUND A CRACK INDICATION AT LONGERON SPLICE 1L. THE LONGERON SPLICE REPAIRED IAW SRM 53-00-05-2R, FIGURE 202, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707111900Doubler · chafedFWD CARGO, DURING ACCOMPLISHMENT OF AN INSPECTION ON AN EXISTING REPAIR ON THE FWD CARGO DOOR AFT CUTOUT AREA, FOUND THE OUTER DOUBLER CHAFED BS 1002.3, LONGERON 40 TO 42R. THE DOUBLER WAS REMOVED IAW SRM 51-33-01-0G, AND A NEW DOUBLER INSTALLED IAW EA 1-5SDR AALA20170711009Skin · crackedCRACKS ON TWO FASTENERS ON THE R1 DOOR UPPER FORWARD DOOR FRAME RADIUS. REPAIRED IAW SRM 53-05-00-001, 53-01-00 AND EA 271277.SDR DALA2017071205363Skin · crackedSKIN CRACK AT FASTENER AT STA 1095, 4" ABOVE L14R ABOVE RT PYLON. REPAIRED SKIN REF PRI 560007-14 REV 0 AND 1 AND ER/A 560007-14 REV ORIGINAL.SDR DALA2017071205361Skin · cracked2 SKIN CRACKS AT FASTENERS AT STA 1095, 4" ABOVE L14R ABOVE LT PYLON. REPAIRED SKIN REF PRI 560007-14 REV 0 AND 1 AND ER/A 560007-14 REV ORIGINAL.SDR CALA2017081402663Skin · corrodedRIGHT FUSELAGE EXT SKIN AROUND LAVATORY E, EXHAUST HAS CORROSION. BLENDED CORROSION AROUND LAVATORY EXHAUST VENT, FOUND TO BE OUT OF LIMITS ORIGINAL .063 REMAINING .052 LOSS OF .011. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-41-11-300-004, PG 1-6, SDR IPXA2017071019106Skin · dentedFUSELAGE SKIN DENTED AT FRAME 85 BETWEEN STRINGERS 44-45L. REPAIRED IAW EO A300-5330-62584-BSDR FDEA201707092138Skin · crackedEXTERIOR SKIN SURFACE, BS 859 LONGERON 43R HAS CORROSION AROUND FASTENERS CUT OUT DAMAGED SKIN AND INSTALLED CLASS II REPAIR IAW SRM 53-20-00, FIG 6, SHEETS 16 & 17, & EA 8-5330-T0334722, PT 1SDR FDEA201707092099Skin · crackedEXTERIOR SKIN SURFACE APPROXIMATELY BS 897, LONGERON 45R HAS A POSSIBLE CRACK. REPAIRED THE SKIN IAW SRM 53-20-00, VOL 1, FIG 6, SHT 17-19.SDR SWAA2017080115386Skin · corrodedAFT POTABLE WATER DRAIN MAST CUTOUT CORRODED. R&R CUTOUT PER SRM AND DWG.SDR FDEA201707091888Skin · chafedCENTER CARGO, WHILE ACCOMPLISHING INSPECTION ON EXISTING REPAIR ON CTR CARGO AFT CUTOUT AREA, FOUND THE OUTER DOUBLER CHAFED BS 1781, LONGERON 40-42R. REMOVED IAW SRM 51-33-01-0G AND NEW REPAIR DOUBLERS INSTALLED AS PER EA# 1-5330-T0302103 A PART 5 TITLE: SDR FQAR20170708064Stiffener · crackedDURING INSPECTION, A THIN STIFFENER RIVETED TO THE BELLY SKIN BELOW THE BAGGAGE AREA WAS FOUND CRACKED. IT APPEARS THAT OIL CANNING OF THE SKIN CAUSES THE STIFFENERS TO CRACK.SDR JR2R201707080005Skin · crackedL1 DOOR HOLD OPEN HOOK CUP AND SURROUNDING SKIN IS DAMAGED. REPAIRED IAW EA 20-2017-130.SDR SWAA2017082815924Skin · crackedFUSELAGE SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED THE SKIN IAW EA.SDR SWAA2017082415902Skin · crackedFUSELAGE SKIN CRACKED AT BS 540, STRINGER 22L. REPAIRED THE SKIN IAW ER AND EA.SDR DALA2017070805283Skin · crackedCRACK ON FUSELAGE SKIN BS 1076 BETWEEN LONGERONS 15 - 13L. REPAIRED IAW ETI-17-17-082, REV 2, AND ER/A 559501-14, REV ORIG.SDR DALA2017070805282Skin · crackedCRACK ON FUSELAGE SKIN BS 1087 BETWEEN LONGERONS 13 - 15L. REPAIRED IAW ETI-17-17-082, REV 2, AND ER/A 559501-14, REV ORIG.SDR DALA2021122908130Skin · crackedTWO CRACKS WERE NOTED ON THE FUSELAGE SKIN, BETWEEN 1076 AND 1087, L-14L. ER/A 559501-14 SECTION I REPAIR WAS ACCOMPLISHED. FOLLOW ON ACTION FOR SECTION II IS REQUIRED. ACCOMPLISH ER/A 559501-14 SECTION II INSPECTION AT C-CHECK INTERVALS FROM SECTION I, NOT TOSDR AALA20170706010Skin · corrodedAIRCRAFT WAS IN BASE MAINTENANCE. CORROSION ON FUSELAGE SKIN LAP SEAM AT THE 5:00 POSITION BEHIND THE RIGHT MAIN LANDING GEAR WHEEL WELL, FUSELAGE STATION 1197+44 TO 1197+70, STRINGER 36R. REPAIRED PER SRM 53-00-01-2R-12.SDR SWAA2017071715048Skin · delaminatedSKIN DELAMINATED AT BS 1100, AT APU COWL DOOR RIGHT HAND SIDE. REPAIRED SKIN PER SRM.SDR DALA2017070705276Skin · corrodedCORROSION ON WING BOX UPPER SKIN BETWEEN BS 737 - 751 RBL 22 - 60. REPAIRED IAW ETI-17-17-079, REV 1 AND ER/A 559498-14, REV ORIGINAL.SDR SWAA2022012640881Scuff Plate · crackedAFT CARGO DOOR; CENTER BULLNOSE SCUFF PLATE CRACKED. / REPAIRED AFT CARGO DOOR CENTER BULLNOSE SCUFF PLATE PER EA 1-A53-2076 REV 11SDR ABXA20170705074Skin · crackedCRACK IN FUSELAGE SKIN AROUND A FASTENER AT BS 1678. SKIN WAS REPAIRED. ACFT WAS GROUNDED.SDR ABXA20170705073Skin · dentedDENT IN FUSELAGE SKIN BS 325-347. THE FUSELAGE SKIN WAS REPAIRED. THE ACFT WAS GROUNDED.SDR FDEA201707051852Skin · corrodedFWD TOILET SERVICE PANEL LOWER CUTOUT SKIN DELAMINATED. INSPECTED FOUND SKIN INNER STIFFENER CORRODED AND OUT OF LIMITS IAW SRM 51-40-21, & SRM 53-12-18, FIG 2, SHEET 3, ITEM 205, REPLACEED THE STIFFENER. . MAJOR REPAIR IAW GMM 6-2-100.SDR SWIA2017072543563Doubler · corrodedAVIONICS BAY TCAS DOUBLER BETWEEN FRAMES 295 - 310 CORRODED. INSTALLED A NEW TCAS ANTENNA DOUBLER IAW SRM. PRESSURE CHECKED GOOD.SDR DALA2017070505260Skin · crackedCRACKED FUSELAGE SKIN STA 1531.604 CANT BETWEEN LONGERONS 22R-23R. REPAIRED IAW SRM 53-00-01.SDR SWAA2022012618291Scuff Plate · crackedAFT CARGO DOORWAY AFT CORNER SCUFF PLATE IS CRACKED / REPLACED AFT CARGO DOORWAY AFT CORNER SCUFF PLATE PER CUSTOMER AND 753-721-10-01 P/N 146A8341-9SDR SWAA2022012618292Scuff Plate · crackedAFT CARGO DOORWAY FWD CORNER SCUFF PLATE IS CRACKED / REPLACED AFT CARGO DOORWAY FWD CORNER SCUFF PLATE PER CUSTOMER CARD. 753-721-10-01 P/N 146A8341-7.SDR SWIA201743619Skin · dentedMULTIPLE DENTS AFT OF GROUND AC DOOR BS 589 - 605. REPAIRED THE DENTS IAW REO.SDR SIMA20170703001Skin · dentedSKIN DENTED AFT OF FRAME 23 BETWEEN STRINGERS 9 - 10R. ACCOMPLISHED A REPAIR IAW ERS-EM-53MR-2796.SDR IPXA2017070318853Skin · gougedFUSELAGE SKIN DOUBLER DAMAGED AT FRAMES 84 TO 85, STRINGER 45 - 44R AT THE TAIL STAND BALL AREA. REPAIRED IAW EO A300-5330-63531-E.SDR FDEA201707031840Skin Splice · crackedDURING AN X-RAY INSPECTION ON TRANSVERSE SKIN SPLICE AT STA 5-0, FOUND ONE CRACK APPROX 5 INCHES ON SPLICE LONGERON 7L AT EDGE OF 3 - 7 FASTENERS. REPAIRED IAW SRM 53-00-05 REPAIR 1 AND EA 1-5310-T0334128 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100SDR FDEA201707031838Longeron Splice · crackedDURING X-RAY INSPECTION ON TRANSVERSE SKIN SPLICE AT STA 5-0, FOUND ONE CRACK APPROXIMATELY 1 INCH ON LONGERON SPLICE 3L. A NEW LONGERON SPLICE WAS FABRICATED IAW DRAWING AEA7634, REVISION B. REMOVED AND REPLACED AS PER MD-11 SRM 51-33-01-0G. REPAIR CLASDR FDEA201707031837Longeron Splice · crackedDURING X-RAY INSPECTION ON TRANSVERSE SKIN SPLICE AT STA 5-0, FOUND ONE CRACK APPROXIMATELY 1 INCH ON LONGERON SPLICE 2L. REMOVED AND REPLACED AS IAW SRM 51-33-01-0G. A NEW LONGERON SPLICE FABRICATED IAW DRAWING AEA7634, REVISION B. REPAIR CLASSIFIED AS MA
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