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 EE4Y2018041906379Skin · corrodedFOUND THE SKIN BETWEEN LBL 45.61 AND LBL 65 AT STRINGER 1C, WITH CORROSION. THE DAMAGED AREA WAS REPAIRED IAW SR 3-4185490079.SDR SWAA2018041721242Skin · corrodedCROWN SKIN AT DORSAL FIN AREA CORRODED BETWEEN BS 887 TO 1007. R & R THE SKIN IAW ER AND EA.SDR ASOA201803215089Doubler · corrodedTCAS ANTENNA DOUBLER CORRODED BETWEEN BS 295 TO 310. REPLACED THE DOUBLER IAW IAW SRM 51-42-06-001-001-A01.SDR ASOA201803215087Butt Joint · corrodedFS 280 CIRCUMFENETIAL JOINT IS CORRODED BETWEEN STRINGER 26L AND 26R. BLENDED THE CORROSION IAW REO 670-53-21-1502, REV -, AND ECTC REO 670-53-21-1502.SDR REXA2018032100226Skin · gougedBS 910, STRINGER 27, SKIN FOUND GOUGED. REPAIRED THE DAMAGE IAW EA 953-06672.SDR DALA2018123197450Skin · corrodedTHE RIGHT HAND FUSELAGE SKIN AT VACUUM WASTE TANK VENT STA 1022-1037 / L28R-29R HAS CORROSION. ER/A 566366-14 ISSUED AND IS CURRENT. SECTION II IS LIMITED TO 12 MONTHS AFTER SECTION I, PENDING DAMAGE TOLERANCE ANALYSIS. ASSOCIATED ER/A 95-566366 ADDED FOR AC 9SDR ABXA2018030330042Skin · crackedCRACK IN SKIN AT THE FASTENER ROW OF STRINGER 14 RIGHT, FUSELAGE STATION 1654.5. THE SKIN WAS REPAIRED. AIRPLANE WAS GROUNDED.SDR VNAA2018032099903Skin · chafedEXTERIOR SKIN JUST AFT OF APU EXHAUST CUTOUT HAS 3 AREAS OF DAMAGE THAT ARE MARKED WITH RED MARKER. RECEIVED ENGINEERING ORDERS AND REPAIRED DAMAGED AREA IAW EA 25-2018-058SDR SWAA2022021028998Skin · dentedTRANSFERRED FROM LOG PAGE 0600956 :'DENT. CREASED AND GOES ACROSS UNDERLYING STRUCTURE ; FUSELAGE SKIN BS 797; 5' BELOW STR 26R / DENT ON FUSELAGE SKIN BS 797 5' BELOW STR 26R FOUND TO BE OUT OF LIMITS PER SRM 53-00-01-1A-5. CUT OUT DAMAGED AREA AND ACCOMPLISHSDR AALA20180323003Skin · crackedCRACKED FUSELAGE SKIN AT LEFT NOSE LANDING GEAR, AFT FOLLOW-UP DOOR, AFT HINGE AT PREVIOUS ROUT-OUT. INSTALLED REPAIR DOUBLER PER SRM 53-05-00-001, FIGURE 158.SDR CALA2018032000951Skin · wornVERTICAL STAB TO FUSELAGE RT SKIN EXTERNAL SURFACE AT BS 2108 TO 2150 WORN. THE SKIN WAS REPAIRED IAW ECRA 5330-06335 REV- ELB.SDR CALA2018032000950Skin · wornVERTICAL STAB TO FUSELAGE LT SKIN AT BS 2108 TO 2150 WORN. THE SKIN WAS REPAIRED IAW ECRA 5330-06335 REV- ELB.SDR 7C7A2018031900373Skin Panel · dentedDENT AND CREASE DAMAGE TO THE RIGHT HAND FUSELAGE SKIN PANEL ASSEMBLY BETWEEN STATION X405.735 TO X424.124 AND STRINGERS 21S TO 22S. RD CALLS FOR A PERMANENT REPAIR FOR THE DENT AND CREASE DAMAGE TO RIGHT SKIN PANEL ASSEMBLY (PART NUMBER 85320266) BETWEEN X40SDR DALA2018031901770Skin · damagedDURING INSPECTION, FOUND A HOLE IN LOWER LEFT FUSELAGE BS 735 BETWEEN STRINGER 25L - 26L. MAINTENANCE REPAIRED IAW 566907-14.SDR TIPR2018031730147Skin · chafedEXTERNAL FUSELAGE SKIN AT FRAME 34 BETWEEN STRINGERS 43L - 43R SHOWS EVIDENCE OF CHAFING.SDR ABXA20180318026Skin · corrodedCORROSION ON THE FUSELAGE SKIN AT BS 756 BETWEEN STRINGERS 34R AND 35R. THE SKIN WAS REPAIRED. AIRPLANE WAS GROUNDED.SDR REXA2018031800225Skin · crackedNOSE HYD BAY UPPER SKIN IS CRACKED AT BS 169. REPAIRED THE SKIN IAW SRM 53-11-43-201-001-A01.SDR SIMA20180318001Skin · gougedGOUGE IN THE SKIN AT FRAME 25 BETWEEN STRINGERS 21L AND 21R. CUT OUT THE DAMAGED AREA IAW SRM 53-22-01, REPAIR TYPE A, PERFORMED HFEC INSPECTION, NO DEFECTS NOTED IAW NIM 51-00-00-916-801-A00. FABRICATED A FILLER AND DOUBLER , APPLIED ALODINE AND PRIMER IAWSDR WVER2018031821Skin · corrodedEXTERNAL SKIN IS CORRODED AT FS 280.00 AND STR 27.SDR SWIA2018041044537Skin · dentedEXTERNAL FUSELAGE SKIN DENTED, BS 619, BETWEEN STRINGERS 20R AND 21R. REPAIRED THE SKIN IAW REO.SDR DALA2018031801762Skin Splice · corrodedCORROSION ON SKIN SPLICE BS 898, BETWEEN LONGERONS 26L TO 30L. THE SKIN SPLICE WAS REPLACED IAW SRM 53-20-01-0I-3, FIG 1. UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PAR 5, FIG 3, SHEETS 1 AND 2. FOUND OUT LIMITS IAW SRM 53-00-00-1A, ALLOWABLE DAMAGE PAR 4, FISDR CALA2018031900939Skin · scratchedVERTICAL STAB TO BODY SKIN FOUND SCRATCHED AT BS 1582 - 1625 STRINGER 2L. REPAIRED IAW ECFA 5330 -06344.SDR CALA2018031900938Skin · scratchedVERTICAL STAB TO BODY SKIN FOUND SCRATCHED AT BS 1582 - 1625, STRINGER 2R. BODY SKIN SCRATCH AT RH STA 1582-1625 S2R REPAIRED PER ECRA 5330 -06344 RII INSPECTION APPROVEDSDR IPXA2018031827553Skin · dentedFUSELAGE SKIN DENTED AND GOUGED, FRAMES 85 TO 86 STRINGERS 42 - 43L. REPAIRED IAW EO 5330-67752-B.SDR WVER2018031718Skin · dentedDENT IN FUSELAGE AT FS 485.00 STR 12L. REPAIRED FUSELAGE DENT IAW REO 690-53-31-373, REV-, DATED 2018-03-10.SDR SWAA2022020953288Skin · dented(QC) DENT WITH MECHANICAL DAMAGE AT STA. 196.5 ABOVE STR. 24R LAP (EVIDENCE OF MISSING DENT DOT AT THIS LOCATION) / REPAIRED FUSELAGE SKIN AT BS 196.5 ABOVE STR 24R LAP IAW ER 18-01963 REV IR AND EA 1-753-32431 REV IRSDR SWAA2022020986380Skin · damaged**CUSTOMER REQUEST** INVESTIGATE DAMAGED FASTENER R/H BS 370; STR 21; SKIN. / REPAIRED SKIN AT BS 370; STR 21R IAW SWA EA 1-753-32493 REV IR AND ATS ER 18-02065 REV IRSDR SWAA2022020986379Skin · damaged**CUSTOMER REQUEST** INVESTIGATE DAMAGED FASTENER R/H BS 294; STR 20; SKIN. / REPAIRED DAMAGED SKIN AT FASTENER R/H BS 294 STR 20; IAW SRM 53-00-01-2R-36 APPLIED EXTERIOR FINISH TO REPAIR PER SRM 53-00-01-2R-36; STEP #4.USDR CA180404020Doubler · dented(CAN) DURING HMV VISIT WITH WINDSHIELDS REMOVED TO DVI NODES, DAMAGE WAS NOTED ON THE FORWARD CENTER SKIN DOUBLER. DAMAGE CONSISTED OF 2 DENTS(CENTER AND LT) AT 0.0025 INCHES IN DEPTH AND ALSO THE LT HAD A KINK. DOUBLER REPLACED. (TC# 20180404020).SDR DALA2018031601781Skin · crackedSKIN CRACKED AT BS 1654, STRINGER 13R. REPAIRED IAW SRM 53-00-01.SDR DALA2018031601780Skin · crackedSKIN CRACKED AT BS 1654, STRINGER 13L. REPAIRED IAW SRM 53-80-01.SDR DALA2018031701768Skin · damagedDURING INSPECTION, FOUND DAMAGED EXTERNAL POWER CUTOUT, REPAIRED THE SKIN AT BS 235.8, STRINGER 21R - 22R IAW SRM. 53-10-15, REPAIR 4.SDR DALA2018031701755Skin · crackedCRACKED FUSELAGE SKIN BS 1022, BETWEEN LONGERONS 14R TO 15R. THE SKIN & DOUBLER WERE REPAIRED IAW ETI-17-18-047, REV 3, AND ER/A 566828-14, REV ORIGINAL.SDR DALA2018031701754Skin · crackedCRACKED EXTERNAL FUSELAGE SKIN BS 1133 BETWEEN STRINGERS 2L AND 3L. THE SKIN WAS REPAIRED IAW ER/A 566630-14AD, REV ORIG, AND ETI-17-18-029, REV 2.SDR SWAA2022021103952Scuff Plate · crackedNOTED BY RAMP AFT CARGO CENTER SCUFF PLATE HAS A CRACK / R&R AFT CENTER SCUFF PLATE PER AMM 53-11-02SDR SWAA2018031920451Skin · brokenEXTERNAL POWER DOOR MIDDLE LATCH CUTOUT CORNER BROKEN OFF. REPAIRED CUTOUT IAW EA.SDR DALA2018031501796Skin · dentedRIGHT FUSELAGE SKIN FOUND DENTED AT BS 1510 - 1518, STRINGERS 31 - 32R. REPAIRED IAW SRM 53-00-01.SDR DALA2018031501779Skin · crackedHFEC INSPECTION FOUND ONE CRACK, APPROXIMATELY .0-275" IN LENGTH ON THE FUSELAGE SKIN BELOW AT STRINGER 13AR, FROM FWD TO AFT , BETWEEN BS 1654.5 AND 1678. REPAIRED IAW SRM 53-80-01.SDR ASOA201803155072Skin · dentedA DENT WITH A GOUGE WAS FOUND ON FUSELAGE SKIN BETWEEN BS 250 - 265, STRINGERS 18L - 19L. THE SKIN WAS REPAIRED IAW REO 670-53-11-1378, AND EC/TC REO 670-53-11-1378.SDR 7C7A2018031500371Skin · dentedTHREE DENTS IN THE LEFT FUSELAGE SKIN BETWEEN BS 270.5 - 291.4, STRINGERS 8P - 11P. REPAIRED THE SKIIN IAW RD8-53-13551 REVISION 4 AND EC0 008.53-18.08.SDR SWAA2022021153913Scuff Plate · crackedFWD CARGO COMPARTMENT FWD CORNER SCUFF PLATE CRACKED. / REPAIR ACCOMPLISHED IAW EA 1-A53-2076 REV 11 ON B/S W/O 37212-1000-0002 (FWD CORNER SCUFF PLATE FWD CARGO - WELDED)SDR SWAA2022021186359Scuff Plate · crackedAFT CARGO COMPARTMENT FORWARD CORNER SCUFF PLATE CRACKED / LOCATED & DRILLED NEW FWD. CORNER SCUFF PLATE AFT CARGO DOOR IAW SRM 51-40-05 & DWG #146A8341; TO BE INSTALLED ON CUSTOMER CARD #753-140-00-02Y 57171U 06APR18SDR IPXA2018040628277Skin · damagedINSPECTION TYPE: SEG4, RT SIDE FUSELAGE AT BS 231.25 SKIN DAMAGED JUST ABOVE FRAME., CUTOUT THE DAMAGE AND INSTALLED A REPAIR DOUBLER IAW EA 757-5311-27-A2292.SDR SWAA2022021177050Scuff Plate · crackedAFT CARGO CENTER THRESHOLD CRACKED AT SECOND FROM AFT LOWER FASTENER LOCATION / REMOVED AC.B. CENTER THRESHOLD (SCUFF PLATE) IAW AMM 53-11-02-020-801. 56011U. 13-MAR-18 3115C 13MAR18 OK TO INSTALL A.C.B CENTER THRESHOLD 88225C 14MAR18 INSP # 10 14MAR18 INSTALLSDR SWAA2018041021054Skin · corrodedFUSELAGE CROWN SKIN UNDER DORSAL FIN CORRODED BETWEEN BS 1006 TO 897, BETWEEN STRINGERS 3L TO 3R. REPAIRED THE SKIN IAW EA.SDR SWIA2018040544465Skin · dentedFUSELAGE SKIN AT BS 654.5, BETWEEN STRINGERS 20L AND 21L DENTED. REPAIRED THE SKIN IAW REO.SDR GTIA2018031302515Skin · crackedSKIN PANEL CRACKED, FRAME 40, AND 41, STRINGER 20R. REPAIRED IAW EO 5331-1811.SDR AALA20180313011Skin · crackedA VISUAL INDICATION OF A CRACK IN THE FUSELAGE SKIN, RIGHT NOSE LANDING GEAR AFT DOOR AFT HINGE AREA. REPIARED THE SKIN IAW SRM 53-05-00-001, PAR 162, FIG 158.SDR WVER2018031300008Doubler · chafedCHAFED LOWER FUSELAGE DOUBLER AT BS 927, STRINGER 27 ON A PREVIOUSLY REPAIRED AREA.SDR C77A20180313001Doubler · corrodedDURING BASIC CHECK, CORROSION WAS FOUND ON THE CENTER FUSELAGE WASTE BOX SKIN DOUBLER, LOCATED NEAR FRAME 88, STRINGER 28R. THE CORROSION WAS BLENDED AND FOUND TO EXCEED THE ALLOWABLE LIMITS IAW SRM 53-23-60. REMOVED AND REPLACED THE SKIN DOUBLE IAW DRAWING
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