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 DALA2015113007254Skin · crackedAIRCRAFT SKIN IS CRACKED AT BS 1418 FROM SKIN EDGE AT LAP ON LONGERON 1 CTR EXTENDING & APPROXIMATELY 3" RBL. ACCOMPLISHED REPAIR IAW PRI 541702-14AD, REV 0 AND 1 AND COMPLIED WITH ER/A 541702-14AD, REV B.SDR SWAA2015120346687Skin · crackedSKIN CRACKED AT BS 908+2, STRINGER 5R. REPAIRED SKIN IAW EA.SDR REXA2015112801108Skin · cracked3"" SCRATCH AFT & ABOVE FWD CARGO DOOR APPROX 18"" FROM THE TOP RT CORNER IN THE 2 O' CLOCK POSITION. DURING ROUTINE LINE MX FOUND THE FUSELAGE SKIN AT FS 541 & 3.25” BELOW STRINGER 16L TO BE DENTED. THE DENT MEASURES 4” X 0.75” X 0.040” DEEP. FOLLOWING RESDR DALA2015112807241Skin · crackedCRACK ON FUSELAGE SKIN BS 1474 LONGERON 15L,. SKIN WAS REPARED IAW SRM 53-01, FIG 4, 51-30-2, AND 51-10-3, PAR 14 AND 21.SDR DALA2015112807719Skin · damagedLIGHTNING STRIKE ON FASTENER HEAD EXTERNAL SKIN AT FRAME 4, 31" ABOVE OF LT SIDE STRINGER AT LOWER FUSELAGE, PERFORMED PERMANENT REPAIR ON FRAME 4 , 31 ABOVE OF LT SIDE STRINGER AT LOWER FUSELAGE IAW SRM 53-11-11.SDR DALA2015112807718Skin · damagedLIGHTNING STRIKE ON FASTENER HEAD EXTERNAL SKIN AT FRAME 3, 23" ABOVE OF LT SIDE STRINGER AT LOWER FUSELAGE, PERFORMED PERMANENT REPAIR ON FRAME 3, 23 ABOVE OF LT SIDE STRINGER AT LOWER FUSELAGE IAW SRM 53-11-11.SDR DALA2015112807717Skin · damagedLIGHTNING STRIKE ON FASTENER HEAD EXTERNAL SKIN AT FRAME 4, 29" ABOVE OF LT SIDE STRINGER AT LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON FRAME 4, 29 ABOVE OF LT SIDE STRINGER AT LOWER FUSELAGE IAW SRM 53-11-11.SDR R61A201511270962Skin · corrodedDURING HEAVY CHECK, BELLY SKIN INTERIOR SIDE FROM 28L-27R BETWEEN FRAMES 90-91 IS CORRODED. MAINTENANCE PERFORMED PERMAMENT REPAIR OF BELLY SKIN INTERIOR SIDE FROM 28L-27R BETWEEN FRAMES 90-91 BY A DOUBLER REPAIR, REF ETD 2015-170-114409.SDR ASAA2015112714054Skin · crackedSKIN IS CRACKED AT BS 945 AT 24L. ACFT GROUNDED. REPAIRED SKIN IAW EA AD20131808-400-53-118 CAT B, STAGE 2 TRACKING UNDER AD20131808-400-53-119.SDR ASAA2015112714045Skin · crackedSKIN IS CRACKED AT BS 727F +1 AT S21R. ACFT GROUNDED. CUTOUT AND REPAIRED DAMAGE TO FUSELAGE SKIN AT BS 727F+1 AND STR 21R IAW SRM 53-00-01, REP 31. THIS IS A CATEGORY B REPAIR WITH AN INSPECTION THRESHOLD OF 66,000 FLT CYCLES REFER TO OPERATORS REPAIR ASSESSDR AALA20151127009Doubler · damagedPSC TIMING, UPPER FUSELAGE ANTENNA DOUBLER DAMAGED OUT OF LIMITS. INSTALLED NEW DOUBLER IAW DWG P131113-01106.SDR AALA20151127006Skin · corrodedLEFT AFT FUSE LAVATORY VENT HAS CORROSION OUT OF LIMITS. INSTALLED PERMANENT FUSELAGE REPAIR IAW EA 256166.SDR KCSA201511271089Skin · corrodedFUSELAGE SKIN IS CORRODED UNDER WATER SERVICE DOUBLER.SDR FOTR20151216065Skin · corrodedFWD CARGO COMPARTMENT BS 550, LT AT ANTENNA CUTOUT INTERIOR SKIN HAS CORROSION. REPAIRED ON FAS EA 15859, REV IR, REF; FAS NR 80287.SDR DALA2015112607328Skin · crackedCRACKS ON FUSELAGE SKIN, BS 1494 BETWEEN LONGERON 2R. REPAIRED IAW ERA 539941-14, REV A.SDR SWAA2015113046493Skin · crackedFUSELAGE SKIN CRACKED AT BS 259.5+5, STRINGER 15R. REPAIRED SKIN IAW EA.SDR KCSA201511251079Skin · corrodedBS 2168 TO 2179, S-34L, EXTERNAL SKIN HAS EVIDENCE OF CORROSION.SDR KCSA201511251078Skin · corrodedBS 1966 TO 2062, S-12L EXTERNAL SKIN HAS EVIDENCE OF CORROSION.SDR KCSA201511251077Skin · corrodedBS 2120 TO 2177, S-19L EXTERNAL SKIN HAS EVIDENCE OF CORROSION.SDR KCSA201511251076Skin · corrodedBS 2140 TO BS 2160, S-12L EXTERNAL SKIN HAS EVIDENCE OF CORROSION.SDR KCSA201511251075Skin · corrodedBS 2235 TO 2184, S19L EXTERNAL SKIN HAS EVIDENCE OF CORROSION.SDR UHLA201511240857Skin · corrodedCORROSION ON SKIN CORRODED UNDER SHEAR TIE REMOVED AT FRAME 82, STR 28-27R. REPAIRED SKIN IAW SRM 53-23-01. MAJOR REPAIR.SDR ASOA2015112414223Skin · crackedFUSELAGE SKIN IS CRACKED AT FS 235.00 S26R. RECIEVED AND COMPLIED WITH REO 601R-53-11-2844. COMPLIED WITH EC/TC REO 601R-53-11-0048 IAW REO 601R-53-11-0048, REV C.SDR SWIA201541676Frame · corrodedBS 310 FRAME AT STRINGER 26R - 26L CORRODED OUT OF LIMITS. REPAIRED THE FRAME IAW REO.SDR DALA2015112507296Skin · corrodedLOWER EXTERIOR FUSELAGE SKIN, CORROSION FROM BS 433-440, LONGERON 26R TO 26L, AFT OF LAV PAN & AT SPLICE. REMOVED CORROSION FROM FUSELAGE EXTERIOR SKIN 430-440, STR 28 LT IAW ERA 536298-14, REV O AND RESTORED AREA.SDR KCSA201511241072Skin · corrodedBS 2235, S18-19L, EXTERNAL SKIN HAS EVIDENCE OF CORROSION.SDR EE4Y2015112400419Skin · bulgedTAIL CONE AT X34707 RT SIDE LOWER SKIN BULGED. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER A NON ROUTINE ITEM A1D208,1-40. REPAIR HAS BEEN ACCOMPLISHED UNDER ETD2015-190-103976, INSTRUCTIONS AND APPROVED.SDR EE4Y2015112400418Skin · bulgedTAIL CONE AT X34707 LT SIDE LOWER SKIN BULGED. DAMAGE HAS BEEN REPORTED AND MANAGED UNDER NON ROUTINE ITEM A1D208,1-39. REPAIR HAS BEEN ACCOMPLISHED UNDER ETD2015-190-103976, INSTRUCTIONS AND APPROVED.SDR DALA2015112407162Doubler · corrodedCORROSION ON PRODUCTION DOUBLER BS 584 BETWEEN LONGERONS 28 - 29L. PRODUCTION DOUBLER WAS REPAIRED IAW ER/A 539957-14, REV ORIGINAL EQUIPMENT, PANAMETRICS NDT35DL. TRANSDUCER SON OPEN V260SM.SDR DALA2016102607655Doubler · corrodedAIRCELL ANTENNA ATTACH STRUCTURE HAS CORROSION. REMOVED CORROSION AND CHECKED LIMITS PER SRM 53-00-00 FIG 103. FOUND OUT OF LIMITS. REPLACED THE DOUBLER PER DWG D12441-2005.SDR SIMA20151123007Skin · crackedLEFT UPPER FUSELAGE SKIN HAS 2 CRACKS, CRACK 1 IS AT FRAME 75 & ABOVE STRINGER 2L, CRACK IS 1" LONG. CRACK 2 IS AT FRAME 75 OFF OF THE FIRST FASTENER BELOW STRINGER 2L, CRACK IS APPROX 1/4" LONG, EASI 8071 USED, 100-500 KHZ PROBE, FREQ= 400KHZ, V-GAIN= 77.0, SDR SIMA20151123003Skin · crackedPOSSIBLE CRACKS ON LT REAR FUSELAGE RIVETS FRAMES 77 - 79. REPAIRED LT UPPER FUSELAGE SKIN CRACK AT FRAME 77 & STRINGER 06L IAW ERS-EM-53MR-1795.SDR CALA2015112300945Skin · crackedSUPPORT TASK, CRACK FOUND AROUND ONE EACH FASTENER IN THE SKIN COMMON TO THE STATION CGO BULK CHORDS, BETWEEN STRINGER 22R - 23R. REFER ATTACHED RECORD FOR DETAILS FX SKIN STATION 540, STRINGER 21R - 24R. SKIN REPAIRED IAW ECRA 5310-05878 REV C PART 1 & EA 5SDR IPXA2015112396036Doubler · damagedDAMAGE TO FUSELAGE SKIN DOUBLER LOCATED AT FR 85 BETWEEN S44L TO S44R, REF EO A300-5330-58946A FOR DETAILS REPLACED SKIN DOUBLER IAW EO A300-5330-58946A.SDR CALA2015112394854Skin · scratchedUPON ARRIVAL, FOUND A SCRATCH APPROX 4 X 2 INCHES NEAR FWD CARGO DOOR LT SIDE. BLENDED AREA & PERFORMED EDDY CURRENT INSPECTION. PRIMED & PAINTED AREA.SDR SWAA2015121147036Skin · crackedFUSELAGE SKIN CRACKED, BETWEEN BS 799.5 - 801.0, STRINGER 19L. REPAIRED SKIN IAW ER & EA.SDR SWAA2015121147035Skin · crackedFUSELAGE SKIN CRACKED, BETWEEN BS 782.5 - 783, STRINGER 22L. REPAIRED SKIN IAW ER.SDR SWAA2015113046573Post · crackedFLIGHT DECK RT NR 3 WINDOW FRAME E - F POST, 2ND FROM BOTTOM WINDOW PANE ATTACH FASTENER HOLE CRACKED. REPAIRED POST IAW ACO.SDR SWAA2015113046572Post · crackedFLIGHT DECK LT NR 3 WINDOW FRAME E - F POST, 2ND FROM BOTTOM WINDOW PANE ATTACH FASTENER CRACKED. REPAIRED POST IAW AMM.SDR DALA2015112107204Skin · damagedPREVIOUS LIGHTNING STRIKE REPAIR, PERFORM SRM 53-00-01, REPAIR 3-ZONE A, ALTERNATIVE REPAIR IAW ER/A 518351-14B. STR 1L-2R, REMOVED AND NEW REPAIR ACCOMPLISHED IAW PRI 518351-14B.SDR SIMA20151121007Skin · crackedRIGHT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 & ABOVE STRINGER 2R, CRACK IS APPROX 3/8" LONG. REPAIRED IAW ERS-EM-53MR-1793.SDR DALA2015112207185Skin · damagedAFTER REMOVAL OF ANTENNA MOUNT, FOUND SCRIBE MARKS AT ANTENNA MOUNT AREA, LWR EXT FUSELAGE SKIN BETW BS 1460 -1480, STR 29R-30. ACCOMPLISHED PERMANENT REPAIR ON FUSELAGE SKIN ANTENNA MOUNT AREA BS 1459-1480 BETWEEN STR 29R-30, REF ER/A 541036-14, REVISION ORISDR A6WA201543277Skin · crackedLOWER FWD FUSELAGE SKIN AT NLG AFT DOOR CUT OUT, AFT RT RADIUS IS CRACKED. REPAIRED DAMAGED FUSELAGE SKIN CRACK AT NLG CUT OUT, AFT RADIUS RT SIDE IAW REO 601R-53-11-048 REV D.SDR A6WA201543269Skin · chafedFUSELAGE SKIN IS CHAFED NEXT TO PREVIOUS REPAIR CUT OUT, JUST FWD OF PAX DOOR OPENING & JUST ABOVE WL 79.50. REPAIRED FUSELAGE SKIN JUST FWD OF PAX DOOR OPENING & JUST ABOVE WL 79.50 IAW REO 601R-53-21-180 REV A.SDR CALA2015112300941Skin · chafedVERTICAL STAB PANEL 322AR TO FUSELAGE AREA, FOUND SEVERAL AREAS OF CHAFING, INTERIM REPAIR DOUBLER INSTALLED STATION 2108 - 2150, STRINGER 1L - 4R IAW ECRA 5300-02264.SDR CALA2015112300940Skin · chafedVERTICAL STAB PANEL 322AL TO FUSELAGE AREA, FOUND SEVERAL AREAS OF CHAFING. INTERIM REPAIR DOUBLER INSTALLED, STATION 2108 - 2150, STRINGER 1R - 4L IAW ECRA 5300-02264.SDR CALA2015112300939Skin · dentedDENT FROM BIRD STRIKE, JUST ABOVE CAPTAINS EYEBROW PLUGS, WINDOWS. ACCOMPLISHED INTERIM REPAIR IAW ECRA 5331-02064 PT 1. DIP ISSUED TO ACCOMPLISH INSPECTION REQUIREMENTS ON OR BEFORE THE ACFT REACHES 50,000 TOTAL FLIGHT CYCLES. PLANNING TO CONTACT ENGINEERISDR SIMA20151121005Skin Panel · damagedHAIL DAMAGE EVENT. REPLACE CTR FUSELAGE I RT SKIN PANEL. ACFT WAS REMOVED FROM SERVICE FOR SKIN REPLACEMENT & WILL BE RETURNED TO SERVICE AFTER SKIN REPLACEMENT. R & R CTR FUSELAGE I RT SKIN PANEL IAW SRM 53-21-01 SI, 51-20-01, 51-20-03, 51-40-06, 51-40-02,SDR DALA2016110908360Skin · damagedSKIN DAMAGED. REPAIRED IAW ER/A 533202-14 SECTION II. MAJOR REPAIR.SDR ASAA2015112017447Skin · dentedVERTICAL CREASE LEFT SIDE RVSM AREA. ACFT GROUNDED. ACCOMPLISHED CATEGORY "B" REPAIR TO THE RVSM AREA IAW EA 800-53EA-17465 REV 00 AND REO G20089 REV A.
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