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 DALA2016012900837Skin · dentedAA WORK CARD 2330-01340-01A. DURING STEP 3 OF TASK CARD, 7 EA DENT DOTS FOUND AT ANTENNA INSTALLATION AREA. CUT OUT AREAS ON FUSELAGE SKIN BETWEEN BS 332 AND BS 351, BETWEEN LONGERONS 29LT AND 29RT. CUTOUT DIMENSIONS: 8.25" X 4.875" AND 1.875" X 1.125". FABRSDR R61A201602030079Skin · dentedDURING MAINTENANCE VISIT, DAMAGE WAS CAUSED TO THE AFT. MAINTENANCE REPAIRED IAW SRM 53-30-33.SDR WX0A2016020373084Skin · crackedFOUND TWO CRACKS ON AFT RT SIDE OF FUSELAGE. MAIN CRACK IS 3.4 INCH LONG. A SPLINTER CRACK OFF THE MAIN CRACK IS 1.9 INCH LONG. BOTH CRACKS ARE JUST AFT OF THE RT ELEVATOR ACCUMULATOR ACCESS PANEL, FS CANT 1474 LONG NR 21. NOTE ALREADY PERFORMED HFEC TO FISDR AALA20160128012Skin · dentedFUSELAGE SKIN DENT ADJACENT TO A FASTENER HOLE ON THE AIR CELL DOUBLER, CTR CROWN SKIN AT STATION 500C +10. ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-00-01-2R & EA 257190 DATED 1 28 16. ACFT IN BASE MX.SDR WX0A2016012973081Skin · crackedRIGHT AFT FUSELAGE SKIN HAS TWO CRACKS AT CANTED STATION 1474, LONGERON 21. REPAIRED SKIN IAW SRM 53-01 FIG 2 SHEET 3. M301 ITEM 3 WO 1012668 3100 0001.SDR DALA2016012900719Finger Doubler · corrodedCORROSION ON INTERNAL FINGER DOUBLER BETWEEN BS 1174-1193 BELOW LONGERON 26L AT AFT CARGO COMPARTMENT C3. FINGER DOUBLER WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 51-10-3 PAR 14, 21 AND 38, AND 53-04-5, FIG 7.SDR DALA2016012900714Skin · crackedCRACK ON FUSELAGE SKIN BS 1309 BETWEEN LONGERONS 6 - 7L. REPAIRED IAW ETI-88-16-035 R2 AND ER/A 541634-14, REV. ORIGINAL.SDR SIMA20160128003Skin · crackedCRACKS AROUND RIVETS ON FRAME 75, BETWEEN STRINGERS 2L - 3L. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE I SKIN IAW ERS-EM-53MR-1899.SDR SIMA20160128002Skin · crackedCRACKS AROUND RIVETS ON FRAME 75, BETWEEN STRINGERS 2R - 3R. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-1899.SDR SWAA2016031749976Window Post · crackedL3 COCKPIT WINDOW POST FRAME CRACKED. REPAIRED POST IAW SI.SDR SWAA2016031749975Window Post · crackedR3 COCKPIT WINDOW POST FRAME CRACKED. REPAIRED POST IAW SI.SDR DALA2016020101435Skin · dentedERA473252-14, REV ORIG FUSELAGE SKIN DENTS AT BS 600 & 640 BETWEEN S-16L & S-18L TIME-LIMITED. ERA INI CYC ACTL/2106 CONVERTED TO SCEPTER ON 08OCT13 09:32 UTC ERA ISSUE DATE 10MAR09 WAS AFTER LAST DEFERED DATE 27JUL89 USED LAST DEFERED DATE AS THE LOG REPORTESDR SWIA201641899Skin · crackedFUSELAGE SKIN AT LT TRU DOOR CUTOUT LOWER AFT CORNER CRACKED. REMOVED AND INSTALLED SERVICEABLE LT SIDE FUSELAGE SKIN AT THE TRU DOOR CUTOUT IAW SRM.SDR SWAA2016020248580Skin · crackedFUSELAGE CROWN SKIN CRACKED AT BS 536, BETWEEN STRINGER 5R - 6R. REPAIRED SKIN IAW EA.SDR DALA2016012800688Doubler · corrodedCORROSION ON INNER PRODUCTION DOUBLER AT AFT LAVATORY PANEL BS 1287-1309. REPAIR WAS ACCOMPLISHED IAW ERA 541618-14, REV ORIG SECTION I.SDR UHLA201601260090Skin · crackedUPPER FUSELAGE SKIN CRACKED AND HAS A HOLE THROUGH IT LOCATED BETWEEN FRAMES 14 AND 15, AND STR 2R/3R. CUT OUT DAMAGED AREA AT FR 14-15, STR 2R-3R, REF SRM 53-10-01. FABRICATED, LOCATED, DRILLED, ALODINED, AND PRIMED DOUBLER AND FILLER FOR DAMAGED AREA. INSTSDR SIMA20160126005Skin · crackedRIGHT UPPER FUSELAGE SKIN CRACKED 2 PLACES, CRACK 1 IS JUST AFT OF FRAME 75, JUST ABOVE STRINGER 2R, CRACK IS APPROX 3/8" IN LENGTH. CRACK 2 IS ON FRAME 75, AT THE FIRST FASTENER BELOW STRINGER 2R, CRACK IS APPROX 1/4". EASI 8071 USED, 100-500 KHZ PROBE, FRESDR SIMA20160126004Skin · crackedLEFT UPPER FUSELAGE SKIN CRACKED AT FRAME 75, JUST ABOVE STRINGER 2L, CRACK IS APPROX 1" IN LENGTH. EASI 8071 USED, 100-500 KHZ PROBE, FREQ=400 KHZ, V-GAIN=77.0, H-GAIN=64.0, LPF=100. ACCOMPLISHED REPAIR OF LT UPPER FUSELAGE SKIN AT FRAME 75, JUST ABOVE 2L ISDR KO0R201601260039Skin · corrodedMAIN DECK CENTER SKIN HAS CORROSION AT WING TANK STR 8, BS 1281.0, LBL 103.5 AND 110.5.SDR KO0R201601260038Skin · corrodedMAIN DECK CTR WING, UPPER SKIN HAS CORROSION AT WING TANK STRINGER 19, STATION 1197.0, LBL 110.0.SDR KO0R201601260037Skin · corrodedMAIN DECK CTR WING, UPPER SKIN HAS CORROSION AT WING TANK, STRINGER 20, STATION 1189.0, LBL 112.0.SDR DALA2016012700673Skin · damagedSKIN DAMAGED BETWEEN BS 620 AND 640 AND STRINERS 17 - 18L.SDR DALA2016012600668Skin · damagedER/A 479548-14AD, REV A, FUSELAGE, SKIN, BS 1282 NEAR STRINGER 4R LIGHTNING STRIKE.SDR DALA2016012600667Skin · damagedER/A 479548-14AD, REV A, FUSELAGE,SKIN, BS 1282 NEAR STRINGER 4R, LIGHTNING STRIKE.SDR DALA2016012600622Skin · damagedLIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN, BS 927 BETWEEN LONGERON 1 AND LONGERON 2 RT. LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN BS 927 BETWEEN LONGERON 1 AND 2 RT WAS REPAIRED IAW ETI-88-15-444, REV 2 AND ER/A 541593-14AD, REV ORIGINAL. REPAIR IS APPROVASDR CALA2016012500068Skin · damagedNICK WAS FOUND ON INTERNAL SURFACE OF FWD CARGO COMPARTMENT DOOR CUTOUT, FWD LOWER CORNER, STATION 442, RBL 35 8=0.4" X 0 .4". PERFORMED REPAIR IAW ECRA 5311-01671 & 737EN-53-024 0, INITIATED A DIP THAT STATES THE REPAIR IAW ECRA 5311-016 71 HAS ONLY FIRST STSDR CALA2016012500067Skin · dentedDURING AGEING ACFT INSPECTION, DENT WAS FOUND ON A PREVIOUS CATEGORY B REPAIR & TOP FASTENER IN LOWER CTR SHEAR TIE AT STATION 620, BETWEEN STRINGER 15L & 16L, NO DOCUMENTATION COULD BE LOCATED ON THIS REPAIR FROM RECORDS REPORT. CUT OUT DAMAGED AREA OF SKIN SDR SWAA2016012748404Skin · crackedFUSELAGE SKIN CRACKED AT BS 500B+3, STRINGER 2R. REPAIRED SKIN IAW SRM.SDR FDEA201601240311Skin · dentedLEFT FUSELAGE, APPROX STATION 766.5, HAS A DENT OUT OF LIMITS. REPAIRED IAW SRM 53-00-01 REPAIR 12 EA H-5330-T0321872 A.SDR DALA2016012500559Skin · damagedSCRATCH ON RT WINDOW BELT BETWEEN BS 1155 - 1174 UPPER SURFACE. SCRATCHES WERE BLEND OUT FOUND WITHIN LIMITS IAW SRM 53-05, FIG 111 AND ER/A 543131.14, REV ORIGINAL. AREAS WERE TREATED IAW SRM 51-10-03, PAR 21.SDR DALA2016012500558Skin · wornWORN PREVIOUS REPAIR DOUBLER ON HOLD OPEN HOOK AREA AT PASSENGER ENTRANCE DOOR L1. REPAIR DOUBLER WAS REPLACED IAW ERA 486216-14 MA, REV A.SDR R61A201602030078Skin · dentedMAINTENANCE FOUND 5 DENTS PROTRUDING FROM INSIDE BELLY AT AFT SERVICE DOOR. MAINTENANCE REPAIRED IAW RD 8/4 53-7285.SDR R61A201602030077Skin · dentedMAINTENANCE FOUND DENT ON FUSELAGE 10" INBD OF EXTERNAL AIR CONDITIONING DOOR. MAINTENANCE COMPLIED WITH RD 8/4-55-1242. ACFT REMAINS FOR HEAVY CHECK COMPLETION.SDR UHLA201601230004Skin · damagedDAMAGE TO FUSELAGE SKIN BETWEEN FRAMES 91 AND 92 STRINGERS 28L. REPAIRED IAW ETD2016-170-003505.SDR DALA2016012700671Stringer · damagedTWO LIGHTNING STRIKES ON CROWN OF FUSELAGE BETWEEN BS 720 AND 760. DRILLED OUT DAMAGE IAW SRM 53-00-01. REPAIR 6, SECTION 1, PARA 3. PERFORMED BHEC INSPECTION IAW SRM 53-00-01 REPAIR 6. NO DEFECTS NOTED. INSTALLED RIVETS IAW SRM 53-00-01, REPAIR 6, SEC 1 PSDR DALA2016012600669Skin · damagedTWO LIGHTNING STRIKES ON CROWN OF FUSELAGE BETWEEN BS 720 AND 760. DRILLED OUT DAMAGE IAW SRM 53-00-01, REPAIR 6, SECTION 1. PARAGRAPH 3, PERFORMED BHEC INSPECTION IAW SRM 53-00-01, REPAIR 6. NO DEFECTS NOTED. INSTALLED BLIND RIVETS, 2 EA IAW SRM 53-00-01SDR SWAA2016012548339Skin · damagedSKIN DAMAGED AT BS 1130, STRINGER 4L. REPAIRED SKIN IAW EA.SDR DALA2016012400551Skin · corrodedCORROSION ON FUSELAGE SKIN AND INNER PRODUCTION DOUBLER AROUND AFT LAV SERVICE PANEL. ALSO CORROSION IS RUNNING UNDER SKIN, PANEL AND DOUBLERS. DUE TO EXCESSIVE CORROSION AREA WAS REPAIRED IAW ERA 541624-14, REV ORIG.SDR R61A201601220201Skin · gougedDURING HEAVY CHECK, FOUND INTERNAL FUSELAGE SKIN AT BS 234 AND STR 23S HAS GOUGE IN SKIN AT PREVIOUS REPAIR. MAINTENANCE DID PERMANENT REPAIR TO SKIN, PN 85360122 BETWEEN FRAME BS X236.0-BS X258.5 AND STR 23S-24S IAW RD 8/4-53-4897, ISSUE 2 DATED 8 FEB 2016. SDR SWAA2016022949529Skin · crackedL1 DOOR THE LOWER AFT CORNER SKIN CUT OUT CRACKED. REPAIRED CUT OUT IAW SRM & EA.SDR FDEA201601220284Skin · dentedINCOMING, DENT IN FUSELAGE EXTERIOR SKIN, 18" FWD OF THE E & E BAY ENTRANCE WAY. ACCOMPLISHED EA F-5330-T0322892 PT 1. FUSELAGE PLATES & SKINS, FUSELAGE SKIN. REPAIR STATION 439 - 446, STRINGER 27L - 28L. THIS IS A CAT B REPAIR. REFERENCE FAA FORM 8100-9 SDR DALA2016012300536Skin · damagedLIGHTNING STRIKES ON LT WINDOW BELT CUTOUT BETWEEN BS 617 TO 636. LIGHTNING STRIKE ON LT WINDOW BELT CUT OUT BS 617 TO 636 WAS REPAIRED BY BLEND OUT AND ITS WITHIN LIMITS IAW ER/A 541610-14, REV ORIGINAL AND ETI-88-16-012, REV 2.SDR DALA2016012200731Skin · corrodedCORROSION ON EXTERNAL SKIN AT LOWER FUSELAGE ON FRAME 71 BETWEEN STR 28R TO STR 30R. PERFORMED TIME LIMITED REPAIR ON EXTERNAL SKIN AT LOWER FUSELAGE ON FRAME 71 BETWEEN STR 28R TO STR 30R IAW ER/A 542037-14, REV ORIGINAL.SDR DALA2016012300537Skin · corrodedEXFOLIATION CORROSION BS 674 BETWEEN LONGERON 30 RT AND 29 RT AT FUSELAGE SKIN. REPAIR FUSELAGE SKIN AT BS 674 BETWEEN LONGERON 30 RT AND 29 RT WAS ACCOMPLISHED IAW ER/A 541626-14, REV ORIGINAL.SDR SIMA20160121002Skin · crackedFUSELAGE SKIN CRACK ON FRAME 78, BETWEEN STRINGERS 6R - 7R. FABRICATED & INSTALLED DOUBLER AT FRAME 78, BETWEEN STRINGER 6R & 7R IAW SRM 53-32-01.SDR FDEA201601210273Skin · puncturedFORWARD LOWER FUSELAGE SKIN AT STATION 630, BETWEEN STRINGER 34R - 35R, FOUND A 2" PUNCTURE HOLE. REPAIR IDENTIFIED AS MAJOR REPAIR BY ENGINEERING. EA G-5330-T0322852A WAS COMPLIED WITH.SDR RAIA201601200002Skin · dentedTHIS ITEM HAS BEEN RECLASSIFIED AS A MAJOR REPAIR. ORIGINAL DISCREPANCY: TWO DENTS PROTRUDING FROM CENTER FUSELAGE SKIN BETWEEN FRAMES 22 AND 23, STRINGER 17L AND 18L. FWD DENT EVALUATED AND FOUND TO BE WITHIN LIMITS. AFT DENT REPAIRED IAW SRM. WHEN AVAILABLE,SDR SWAA2016030749706Skin · crackedFORWARD ENTRY DOOR CUT OUT UPPER FWD CORNER CRACKED AT BS 312. REPAIRED CUT OUT IAW EA.SDR SWAA2016021148953Skin · brokenEXTERNAL GND ELEC POWER SKIN CUT OUT BROKEN AT BS 235, ON LOWER FUSELAGE. R & R SKIN IAW SRM & DWG.SDR AALA20160120004Skin · crackedAIRCRAFT WAS IN BASE MX. FUSELAGE SKIN IS CRACKED AT STATION 1437 & L4R. REPAIRED SKIN IAW SRM 53-04-00-001, SRM 53-34-00-001 & SRM 51-00-00-001.
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