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 DALA2016073105664Doubler · corrodedCORROSION ON INNER PRODUCTION DOUBLER BETWEEN BS 1222 - 1234 AND BS 1205 - 1216, LONGERONS 25 - 26L. THE DOUBLER WAS REPLACED IAW SRM 53-34-0 FIG 3 AND 51-10-1 FIG G.36 (SHEET 6).SDR FDEA201607302674Skin · damagedLIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN FRAME 33 STRINGER 50R. REMOVED DAMAGE IAW SRM 51-73-10. FOUND TO BE WITHIN LIMITS IAW SRM 53-10-12 PAR.4 DIAGRAM 101. HFEC REWORK AREA IAW NTM 51-10-08. NO CRACK INDICATIONS AND NO FURTHER DAMAGE NOTED. MINOR REPASDR FDEA201607302673Skin · damagedLIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN FRAME 37 STRINGER 50R. REMOVED DAMAGE IAW SRM 51-73-10. CHECKED AND FOUND TO BE WITHIN LIMITS IAW SRM 53-10-12 PAR.4 DIAGRAM 101. HFEC REWORK AREA IAW NTM 51-10-08. NO CRACK INDICATIONS AND NO FURTHER DAMAGE NOTED. MSDR FDEA201607302672Skin · damagedLIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN BETWEEN FRAMES 39-40 STRINGER 50R. REMOVED DAMAGE IAW SRM 51-73-10. CHECKED AND FOUND TO BE WITHIN LIMITS IAW SRM 53-10-12 PAR.4 DIAGRAM 101. HFEC REWORK AREA IAW NTM 51-10-08. NO CRACK INDICATIONS AND NO FURTHER DAMASDR DALA2016080405775Skin · corrodedCORROSION ON RIGHT SIDE OF FUSELAGE AFT OF C3 DOOR. REPAIRED IAW ERA 549447-14.SDR FDEA201607302681Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN FRAME 36, S50R. TEMPORARY REPAIR LIGHTNING STRIKE ON FASTENER IAW SRM 53-10-12, FIG 201, SHEET 2, HFEC FASTENER HOLE IAW NTM 51-10-01. NO CRACK INDICATIONS & NO FURTHER DAMAGE NOTED. MINOR REPAIR.SDR 7C7A2016072900252Skin · dentedDENT DAMAGE ON THE LT SIDE AFT CENTER FUSELAGE SKIN PANEL BETWEEN BS 531.5 - 539.5 AND STRINGERS 19 - 20L. REPAIRED IAW RD8-53-117.SDR DALA2016080105710Doubler · corrodedCORROSION ON REPAIR DOUBLER BS 446 - 465 AND X -44 TO -60. AREA WAS REPAIRED IAW SRM 53-05 FIG.131A-11, 51-10-3, 51-30-1, 51-30-2 & 51-30-5.SDR CALA2016080100474Skin · corrodedFUSELAGE SKIN AT LAV EXHAUST BLOWER PORT HAS CORROSION. REPAIRED IAW ECRA 5330-05763 PART 1 .SDR DALA2016073105659Skin · cracked.250 INCH CRACK IN FUSELAGE SKIN BS 1380 BETWEEN LONGERONS 12 - 13L. REPAIRED IAW SRM 53-04 FIG18 SHEET 1,2 AND 53-01 FIG 4 SHEET 4.SDR DALA2016073105658Longeron · crackedCRACKED LONGERON 2R, BS 1418. THE LONGERON WAS REPAIRED IAW SRM 53-02 FIG 18.SDR FDEA201607292659Skin · crackedNR 3 AIR CONDITIONING DOOR AFT UPPER CUT OUT CORNER HAS A .100 INCH CRACK. REPAIRED IAW SRM 53-50-00 FIG 3A VOL I.SDR ASOA20160729047Skin · crackedDURING C-CHECK, THE RT AFT SKIN WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A BUSHING REPAIR IAW EMB 145XR SRM 53-32-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20160729044Skin · crackedDURING C-CHECK, THE RT AFT SKIN WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5330-03109. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA20160728006Skin · chafedFUSELAGE EXTERNAL SKIN CHAFED INSIDE RT PYLON PANEL 424DB FWD OF CONNECTOR J0816. PERFORMED REPAIR OF THE SKIN AREA IAW SRM 53-31-01.SDR SWIA201642472Skin · chafedEXTERIOR FUSELAGE SKIN CHAFED FROM BODY FAIRING AT BS 980 AND STRINGER 27. REPAIRED IAW REO.SDR UHLA201607280410Skin · corrodedCORROSION ON INTERNAL SKIN PANEL AT FRAMES 83-82, STRINGER 27R. REPAIRED IAW ETD2016-170-071366. MAJOR REPAIR.SDR ASOA2016080115151Skin · burnedONE BURN BETWEEN BS 333 AND 349 BETWEEN STRINGERS 25 - 26L. DRILLED THROUGH SKIN BAY TO REMOVE LIGHTNING BURN IAW EC/TC REO 601R-53-00-115 REV H. FABRICATED INTERNAL REPAIR WASHER. CONTROLLED COUNTERSINK AND INSTALLED NAS1097AD5 SOLID RIVET AND RESTORED FINSDR SWIA201642531Skin · corrodedCORROSION ON FUSELAGE SKIN BELOW AFT CARGO DOOR. COMPLIED WITH REPAIR IAW STS EA AND SRM.SDR Q2SA20160727253Skin · corrodedWHILE WORKING AFT CORNER CORROSION, FOUND ADDITIONAL CORROSION FWD CARGO DOOR FRAME LOWER AFT CUTOUT. AIRCRAFT GROUNDED. REPAIRED THE DOOR FRAME LWR AFT CUTOUT IAW SRM 53-00-01 REPAIR 33, PB 201-245SDR COEA2016072623811Skin · dentedDURING LIGHTENING STRIKE INSPECTION, FOUND A PROTRUDING DENT AT FRAME 14, UNDER STRINGER 14R. REPAIRED THE SKIN IAW SRM 530000-300-808-A01 REV. 95.SDR A6WA201644147Skin · dentedFUSELAGE UPPER SKIN HAS A DENT WITH GOUGE AT FS 636 AND BETWEEN STR 0 AND 1R.SDR DALA2016072705616Skin · crackedCAPTAIN'S SLIDING WINDOW CUTOUT CRACKED. REPLACED IAW DWG 591365.SDR DALA2017041302987Skin · corrodedCORROSION AT THE LOWER EDGE OF THE LEFT SIDE AFT LAVATORY WASTE TANK OVERBOARD VENT, LOCATED AT STA 1574 AND STRINGER S-25L. THE EXPOSED CORROSION IS APPROXIMATELY 3½ FWD/AFT AND CRACKING OCCURRED FROM THE VENT TO TWO FASTENERS WHICH HAVE PULLED THROUGH THE SKSDR IPXA2016073106507Skin · dentedINSPECTION TYPE: C5, DENT DAMAGE ON FUSELAGE SKIN BS 1520, STRINGER 44L. REPAIRED IAW SRID 4-3257425031, AND EO B747-5330-61398-ASDR VGCA20160725001Skin · corrodedSKIN CORRODED AT BS 193-210 STRINGER 7L. REPAIRED THE AREA IAW DWG R508-053-003-001.SDR SWAA2016072654254Skin · corrodedFORWARD CARGO DOOR FRAME CUTOUT ON INNER LOWER SURFACE CORRODED. REPAIRED CUTOUT IAW SRM.SDR CALA2016072595586Skin · gougedRIGHT FUSELAGE BS 660 AFT OF FWD CARGO DOOR HAS SMALL GOUGE IN SKIN. REPAIRED IAW ECRA 5330-05753.SDR SIMA20160724007Skin · crackedLEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2L, CRACK IS APPROX. 3/8" LONG. REPAIRED THE SKIN IAW SRM 53-31-01 REV 54.SDR SIMA20160724005Skin · crackedRIGHT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 AND ABOVE STRINGER 2R, CRACK IS APPROX. 3/8" LONG. REPAIRED THE SKIN IAW SRM 53-31-01 REV 54.SDR SWAA2016082254950Skin · crackedSKIN CRACKED AT BS 540, BETWEEN STRINGER 21 - 23R. REPAIRED THE SKIN IAW EA.SDR DALA2016072405522Skin · crackedTWO CRACKS IN FUSELAGE SKIN BS 1463 -1446. REPAIRED IAW ETI 88-16-255 REV 2 ER/A 547855-14 REV ORG.SDR FOTR20160723001Skin · corrodedNR 1 ATC ANTENNA MOUNT ON THE LOWER FUSELAGE SKIN HAS CORROSION ALONG THE MATING SURFACE OF SKIN.SDR SWAA2016081854904Skin · crackedSKIN SPLICE CRACKED AT BS 540, BETWEEN STRINGERS 22 - 23L. REPAIRED THE SKIN IAW EA.SDR IPXA2016080206600Skin · corrodedINSPECTION TYPE: C09. BULGE DAMAGE ON EXTERNAL SKIN OF FUSELAGE TAIL SEC 48, AT BS 1857. REPAIRED IAW SRID 4-3263483125 AND EO B767-5330-61376-A.SDR DALA2016072905687Skin · corrodedDURING A MAINTENANCE, CORROSION WAS FOUND ON THE LOWER SKIN AT THE LAP SPLICE, STRINGER 19R BETWEEN BS 740 - 760. REPAIRED IAW ERA 548015-14.SDR CALA2016072200439Skin · damagedLIGHTNING STRIKE BS 380 BETWEEN STRINGERS 6 & 7R. 1/4" DIA 1 PLY DEEP (0.009) WITHIN LIMITS IAW SRM 53-10-01-02A-661A-A TABLE 1.SDR CALA2016072200438Skin · damagedLIGHTNING STRIKE ON SKIN BS 500 1/4 DIA 1 PLY DEEP (0.009") 2 " ABOVE STRINGER 15R. WITHIN LIMITS IAW SRM 53-10-01-02A-661A-A TABLE 1.SDR CALA2016072200437Skin · damagedLIGHTNING STRIKE ON SKIN BS 237 1/4" DIA 1 PLY DEEP (0.009") 6 " ABOVE STRINGER 23R. WITHIN LIMITS IAW SRM B787-A-53-10-01-02A-661A-A TABLE 1.SDR CALA2016072200436Skin · damagedLIGHTNING STRIKE ON SKIN BS 143 3/8" DIA 1 PLY DEEP (0.009") 2 0"BELOW STRINGER 23R. WITHIN LIMITS IAW SRM B787-A-53-10-01-02A-661A-A TABLE 1.SDR ASAA2016072117650Skin · crackedR1 DOOR CUTOUT LOWER AFT CORNER CRACKED. ACFT GROUNDED. REPAIRED IAW SRM 53-10-01-2R-19.SDR DALA2016072205586Skin · crackedAIRCRAFT SKIN HAS 3 SMALL CRACKS NEAR BS 1437, L13L. COMPLIED WITH PRI/ERA 548968-14. REV O.SDR DALA2017021301663Skin · dentedRAMP REPORTS A DENT FWD OF L2 DOOR 2 FT BELOW 11 LEFT PAX WINDOWS AND 5 INS AFT OF WINDOW REAR VERTICAL EDGE. INSP AND DENT IS NOT WITHIN LIMITS REF SRM. ACCOMPLISHED PERMANENT REPAIR ON FUSELAGE SKIN FWD OF L2 DOOR 2FT BELOW 11 LEFT PAX WINDOW AT STA 620 BET SDR K11A2016110291517Skin · corrodedFUSELAGE EXTERIOR CORROSION JUST AFT OF THE AFT CARGO DOOR.SDR ABXA20170720121Skin · crackedCRACK INDICATION FOUND L-1 DOOR CUTOUT LOWER FORWARD CORNER. REPAIRED FUSELAGE SKIN STA 287 TO STA 347, S18L TO S24L BELOW L-1 DOOR IAW REO-G20052, REV B AND NR-B653-62038MR. SDR INFO: PART NAME: FUSELAGE SKIN, PN: 141T3331-5, SN: NSN, STA 287-347, LT BELOWSDR ASAA2016072017664Skin · crackedVHF NR 2 INTERNAL PAN CRACKED. ACFT GROUNDED. ACCOMPLISHED REPAIRS TO INTERNAL SUPPORT PAN AND FUSELAGE SKIN IAW T/C AD2016-1004-53-3 AND EA AD20161004-400-53-102. THIS IS A CATEGORY B REPAIR WITH 1ST AND 2ND STAGE APPROVAL DTE. STAGE 3 APPROVAL IS REQUIRESDR SWAA2016080554586Skin · crackedNR 3 VHF ANTENNA FASTENER HOLES COMMON TO FUSELAGE SKIN CRACKED, SECOND FROM AFT ANTENNA ATTACH FASTENER HOLE. REPAIRED SKIN IAW EA AND DWG.SDR SIMA20160720010Skin · damagedDAMAGED SKIN PANEL. REMOVED AND REPLACED DAMAGED THE SKIN PANEL IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201607202634Skin · damagedUPPER FUSELAGE, EXTERIOR SKIN, 6 EACH RIVET HEADS BURNED/MELTED. LOCATED BETWEEN BS 1621-1721 AT LONGERON 1L. POSSIBLE LIGHTNING EXIT POINTS. REMOVED RIVETS BURNISHED MINOR DAMAGE PER SRM 51--00-01 VOL1. REAMED RIVET HOLES TO .245 AND COMPLIED WITH NDT. ISDR DALA2016072105571Skin · crackedLEFT AFT SKIN BS 1437, L13L IS CRACKED.
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