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 DALA2016062304865Skin · dentedFUSELAGE DENT ON LT SIDE, STA 1087 AT L-20L. CW ER/A 547473-14, REV A, FINAL ER/A MATCHES ALL PRI REVISIONS.SDR DALA2016062304863Skin · damagedDAMAGE TO EMPENNAGE SKIN STA 1178-1144 FROM LONGERON 3R-9R MULTIPLE LOCATIONS. REPAIRED SKIN IAW ER/A 547582-14, REV ORIGINAL ER/A MATCHES ALL PRIS.SDR 4AER20161103003Doubler · corrodedEXTERNAL DOUBLER AT BS 800 & STRINGER 21R TO 25R HAS HEAVY CORROSIONSDR IPXA2016071505932Skin · corrodedINSPECTION TYPE:3CAFT FUSELAGE EXTERIOR SKIN CORRODEDSTA. 2140 - 2164 L33 - 35L. REPAIRED IAW EA 011-5330-01-A6341 REV. IR AND EO MD11-5330-61287-A. MAJOR REPAIR.SDR IPXA2016071505931Skin · corrodedINSPECTION TYPE: 3C, AFT FUSELAGE EXTERIOR SKIN CORRODED BS 2120 - 2163 L33 - 35L. REPAIRED IAW EA 011-5330-01-A6341 REV. IR AND EO MD11-5330-61287-A. MAJOR REPAIR.SDR IPXA2016071505917Skin · corrodedINSPECTION TYPE: 3C, CENTER WING UPPER SKIN CORRODED ABOVE STRINGER 15 BETWEEN XCW -5 AND -20. REPAIRED IAW EA 011-5730-01-A6357 REV. IR AND EO MD11-5730-61284-A.SDR IPXA2016071505916Skin · corrodedINSPECTION TYPE: 3C, CENTER WING UPPER SKIN CORRODED ABOVE STRINGER 15 NEAR XCW102. REPAIRED NOTED CORROSION IAW EA 011-5730-01-A6357 REV. IR AND EO MD11-5730-61284-A.SDR IPXA2016071505913Skin · corrodedINSPECTION TYPE: 3C, CENTER WING UPPER SKIN PANEL CORRODED ABOVE S15 BETWEEN XCW -32 AND -45. REPAIRED IAW EA 011-5730-01-A6357 REV. IR AND EO MD11-5730-61284-A.SDR FDEA201606212080Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN AT BS 209, 10 INCHES BELOW LAP JOINT AT S20L. REPAIRED IAW SRM 53-00-01 REPAIR 2 AND EA F-5330-T0326276SDR SIMA20160621004Skin · crackedLEFT REAR FUSELAGE I SKIN CRACK AT FRAME 75, BETWEEN STR 2L AND 3L. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE I SKIN AT FRAME 75 BETWEEN STRINGERS 2L AND 3L IAW ENVOY ERS-EM-53MR-2150.SDR DALA2016062204836Doubler · corrodedCORROSION ON PREVIOUS REPAIR DOUBLER BETWEEN Y=1287 AND Y=1309 AND LONGERON 29 RT AND 30 AT C3 COMPARTMENT. DOUBLER WAS REPLACED IAW SRM 53-04-2, FIG 2.SDR KCSA201606201032Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN AT BS 443, STR 33L.SDR NACA20160620002Skin · crackedWHILE PERFORMING AD 2013-18-08, A 1" CRACK WAS FOUND AT BS 500D +18.5 BELOW S12L. THERE IS AN INTERNAL PREVENTIVE MODIFICATION AT THIS LOCATION. TEMP REPAIR INSTALLED IAW MESSAGE NAC-16-0014-10B.SDR NACA2016FA0000301Skin · crackedWHILE PERFORMING AD 2013-18-08, S, 2, A 2" CRACK WAS DISCOVERED AT BS727E S22R.SDR NACA20160619001Skin · crackedWHILE PERFORMING AD 2013-18-08, A 2" CRACK WAS DISCOVERED AT BS727E S22R. REPAIRED CRACK IAW SRM 53-00-01, REPAIR 21, DETAIL X, CAT B INSPECTIONS ADDED TO INSPECTION PROGRAM.SDR 4AER20161014002Skin · crackedLEFT FORWARD AIRSTAIR STORAGE DOORWAY CUTOUT LOWER AFT CORNER HAS A CRACKSDR SIMA20160618006Skin · dentedTRANSFERRED FROM AML PAGE 3974409 ITEM 3, REF LOG PAGE 3974408, ITEM NR 1 FOUND DENT ON THE RT SIDE FUSELAGE FRAME 21-22, STR 18R-19R APPROXIMATELY 2.5" X 2.5", DEPT=1.16. C/W REPAIR OF DENT ON RT FUSELAGE STR 21 AND STR 20 BETWEEN FRAME 24 AND FRAME 25 IAW ESDR SIMA20160618004Skin · damagedTRANSFERRED FROM AML PAGE 3974409, ITEM 2, REF LOG PAGE 3974408, ITEM NR 1 FOUND DAMAGE TO THE RT FUSELAGE AT STR 20R APPROXIMATELY 3.5" X 3" FRAME 20-21. DAMAGE IS ACTUALLY BETWEEN FRAMES 24 AND 25. REPAIRED DAMAGE TO RT FUSELAGE AT STR 20 BETWEEN FRAME 24 SDR SIMA20160618003Skin · damagedTRANSFERRED FROM AML PAGE 3974409, ITEM 1, REF LOG PAGE NR 3974408, ITEM NR1 FOUND HOLE ON RT FUSELAGE AT 17R-18R STR. APPROXIMATELY 6" X 7" FRAME 20-21. DAMAGE IS ACTUALLY BETWEEN FRAMES 24 AND 25. REPAIRED HOLE IN SKIN ON RT FUSELAGE AT STR 17R-18R AND FRSDR CALA2016062200378Skin · dentedFWD UPPER FUSELAGE HAS A DENT WITH PREVIOUS BLENDOUT IAW DAMAGE. AFTER INSPECTION C/W BLENDOUT OUT OF LIMITS, MORE THAN 10 PERCENT OF MATERIAL REMOVED. PERFORMED CATEGORY B REPAIR WITH VISUAL INSPECTION CYCLES OF 3, PERFORMED CATEGORY B REPAIR WITH INSPECTIOSDR UIEA2016062000446Skin · dentedDENT FOUND ON RT FUSELAGE SKIN AT BS 510 BETWEEN S-40R TO S-41R. REPAIR DAMAGED FUSELAGE SKIN IAW T2016A53M-1325, REV 1. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR DALA2016061904766Doubler · corrodedCORROSION ON PREVIOUS REPAIR UNDER AFT LAVATORY SERVICE PANEL ACCESS AT FUSELAGE SKIN. AREA WAS REPAIRED IAW ER/A 547808-14, REV ORIGINAL.SDR SWAA2016071853926Skin · crackedSKIN CRACKED BETWEEN BS 500D TO BS 540, BETWEEN STR 20L TO STR 23L. REPAIRED SKIN IAW EA.SDR SWAA2016071853925Skin · crackedSKIN CRACKED AT BS 540, STR 22R. REPAIRED SKIN IAW EA.SDR DALA2016061804852Skin · dentedDENT LOCATED AT EXTERNAL FUSELAGE 750, BETWEEN L26R & L27R. FOUND DENT TO BE OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED REPAIR AND INSTALLED REF ERA 546689-14, REV O.SDR AALA20160617001Skin · crackedAIRCRAFT WAS IN BASE MAINTENANCE. WHILE PERFORMING J1724AB A CRACK INDICATION WAS OBSERVED IN THE FUSELAGE EXTERNAL SKIN AT STA 540 AND S22R. REPAIRED SKIN IAW SB 737-53-1294 AND EA 260495.SDR DALA2016061804755Skin · damagedOUT OF LIMITS FOR THICKNESS REMAIN ON PREVIOUS BLEND OUT, STA Y= 355 BETWEEN LONGERON 18 LT TO 19 LT AT OUTER FUSELAGE SKIN. AREA OUT OF LIMITS WAS REPAIRED. PERFORMED GENERAL VISUAL INSPECTION, INITIAL 8000 CYCLES REPETITIVE EVERY 8000 CYCLES IAW SRM 53-04-SDR UHLA201606160340Skin · dentedAFT FUSELAGE, JUST FWD OF FRAME 99, JUST ABOVE STRINGER 25AR, THERE IS A SHARP OUTWARD DENT. REPAIRED DAMAGED AREA IAW SRM 53-30-01. MAJOR REPAIR.SDR IPXA2016063005237Skin · dentedINSPECTION TYPE: C13, LOWER SKIN EXTERNAL FUSLAGE BS 610 S25L DENTED. REPAIRED IAW SRM 53-00-01 REPAIR 3.SDR QXEA2016062800411Doubler · corrodedLOWER TCAS ANTENNA EXTERIOR DOUBLER IS CORRODED. REMOVED LOWER TCAS ANTENNA EXTERIOR DOUBLER, PN 85314193-103, REF SRM 51-42-05-02-01. INSTALLED NEW LOWER TCAS ANTENNA EXTERIOR DOUBLER, PN QX85314193-103, REF SRM 51-42-05-02-01 AND DWG:85310015, REV I. NO PISDR QMLA2016061616066Skin · corrodedCORROSION ON SKIN OF ACFT, CORROSION ON THE RT SIDE PENETRATED IN TO THE OUTER FRAME OF THE RT ENGINE DECK ASSY. DISCOVERED DURING SCHEDULED MAINTENANCE EVENT.SDR HEER20160616726Skin · corrodedFORWARD LOWER SHELL OUTER SKIN WAS FOUND CORRODED, RIGHT SIDE, UNDER/NEAR SIDE BODY FAIRING. THE REPAIR DOCUMENTATION WILL BE SUBMITTED TO A STRUCTURAL FAA-DER FOR APPROVAL. THE FORWARD LOWER SHELL WILL THEN BE REPAIRED IAW THE FAA-APPROVED REPAIR DATA.SDR FDEA201606162022Skin · crackedFOUND FUSELAGE SKIN BULGED AT INBD AFT CORNER OF LAV SERVICE DOOR FRAME WITH SKIN CRACKS. COMPLIED WITH EA F-5330-TO326081, PARTS 1 AND 2 THIS A MAJOR REPAIR.SDR SWAA2016071954025Skin · crackedSKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED THE SKIN IAW ER AND EA.SDR SWAA2016071954024Skin · crackedSKIN CRACKED AT BS 540, STRINGER 22L. REPAIRED THE SKIN PER ER AND EA.SDR DALA2016062104886Skin · crackedSKIN CRACK CANTED FRAME STA 1531, RT SIDE UP FROM AIR STAIRS CUTOUT.SDR DALA2016061604700Doubler · dentedDENT ON FUSELAGE SKIN PREVIOUS DOUBLER REPAIR STA Y=256 BETWEEN AND LONGERON 19LT. REPAIR DOUBLER AND FILLER WERE REPLACED IAW ER/A 332142-14, REV A.SDR JR2R20160615416Doubler · gougedAFT CARGO DOOR CUTOUT DOUBLER UNDER BEAM GOUGED IN SEVERAL PLACES FROM FS 1160 TO FS 1193. REPAIRED AFT CARGO DOOR CUTOUT INTERNAL DOUBLER IAW EA 40-2016-177.SDR COEA2016061404901Skin · corrodedEXTERNAL LEFT LOWER FUSELAGE SKIN HAS CORROSION AT STRINGER 17L LAP JOINT, BETWEEN FRAMES 22A-23A. REPAIRED IAW ES-2757/16.SDR IPXA2016070205317Skin · corrodedINSPECTION TYPE:1C, FUSELAGE EXTERIOR SKIN CORRODED STA 2138-2163, L33R - L35R, CORROSION REPAIRED IAW EA 011-5330-01-A6323, REV IR AND UPS EO MD11-5330-61142-A.SDR IPXA2016062805166Skin · damagedINSPECTION TYPE:SV, FUSELAGE SKIN DENTED AND GOUGED STA 1921, L48L-L48R. REPAIRED NOTED SKIN DAMAGED BETWEEN STA 1921-1941, L48L-L48R IAW EA 011-5330-01-A6316, REV IR AND EO MD11-5330-61108-A.SDR LR7A2016061400798Skin · damagedDURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5321, FOUND THE RT LOWER MAIN WHEEL WELL SKIN WITH MULTIPLE WARP, REPAIR PATCHES AND LOOSE RIVETS, FS491-FS617; AND CRACKED AT FS 537 WL135, RBL42-RBL45. REPAIRED IAW MEA 382-53-06-097, R4.SDR LR7A2016061400797Skin · damagedDURING SCHEDULED C-12 CHECK UNDER JOB CARD HC5321, FOUND THE LT LOWER MAIN WHEEL WELL SKIN WITH MULTIPLE WARP, REPAIR PATCHES AND LOOSE RIVETS, FS 491-FS 617; AND CRACKED AT FS 537 WL135, LBL42-LBL45. REPAIRED IAW MEA 382-53-06-097, R4.SDR DALA2016061504664Doubler · wornWEAR ON DOUBLER PRODUCTION AT INNER RT PAN A SIDE LOWER HINGE AFT EMERGENCY EXIT. DOUBLER PRODUCTION WAS REPAIRED IAW SRM 52-10-02, FIG 201, REP 16. MEASURE: OT IS 0.050" AND REMAINING THICKNESS IS 0.028". THEREFORE OUT LIMITS. EQ: DIGITAL ULTRASONIC THICKSDR DALA2016061504663Doubler · crackedCRACK ON PRODUCTION DOUBLER BS 1178 CANT BETWEEN LONGERON NR 1 AND NR 2 LT AT AFT ACCESSORY COMPARTMENT, SM. PRODUCTION DOUBLER WAS REPAIRED IAW ER/A 546495-14, REV ORIGINAL, PERFORM REPETITIVE INSPECTIONS AT EVERY, C-CHECK OR 3000 CYCLES WHICHEVER COME FIRSTSDR DALA2016061504662Skin · crackedCRACKED FUSELAGE SKIN ON CUTOUT OF RT/LT NLG AFT DOOR AFT HINGE. SKIN WAS REPLACED IAW SRM 53-10-01, 51-41-02, 51-41-05, 51-10-3 P. 21, 15.SDR DALA2020011500311Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON EXTERNAL SKIN LOC BTW FR72 TO FR73 AND BTW STR 31R TO STR 32R AT LOWER FUSELAGE, PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED BTW FR 72 TO FR 73 AND BTW STR 31R TO STR 32R AT LOWER FUSELAGE AS PER SRM 53-SDR REXA2016061301172Skin Panel · corrodedEXTERIOR SKIN PANEL BETWEEN FS 559.0 TO FS 559.0+112 AND STR L25 AND STR R25 HAS MULTIPLE AREAS OF CORROSION ON LOWER SURFACE. REPAIRED SKIN BETWEEN FS 559 TO FS 559+112 AND STR 25R AND STR 25L IAW EA 253-04446.SDR DALA2016061504674Skin · damagedDURING INSPECTION, FOUND LIGHTNING STRIKE DAMAGE TO A FASTENER LOCATION AT FS 500G AND NEAR STR S-27R. THE FASTENER IS COMMON TO A SHEAR TIE. MAINTENANCE REPAIRED IAW ERA 547964-14.SDR AALA20160613009Skin · crackedDURING ACCOMPLISHMENT OF ECO J1724AB ON THE RT SIDE, THE AFT FASTENER HOLE IN THE THIRD ROW DOWN PRODUCED A CRACK INDICATION IN THE FUSELAGE SKIN. REPAIRED SKIN IAW EA 260616.
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