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 DALA2016090606471Skin · damagedFUSELAGE SKIN BS 207-220 18R-21R DAMAGED. INSTALLED PERMANENT SKIN REPAIR IAW ER/A 549610-14, REV 0.SDR DALA2016090606452Skin · crackedREPAIRED LT FUSELAGE EXTERIOR SKIN CRACK AT STA 1095 JUST ABOVE LONGERON 14L IAW ER/A 547512-14. FAA STAGE III APPROVAL REQUIRES INITIAL AND RECURRING GENERAL VISUAL INSPECTIONS THAT BEGIN AND ARE REPEATED EVERY 3000 CYCLES IAW ER/A 547512-14. ACCOMPLISH SECSDR DALA2016090606422Skin · cracked2" CRACK LOCATED 4 FT FWD AND 3" BELOW LOWER RT CORNER OF MID CARGO DOOR. REPAIRED ON NR 001 IAW ERA 550488-14, REV ORIGINAL.SDR SCNA20160904133Skin · crackedDURING HFEC INSPECTION, FOUND A CRACK INDICATION IN THE SKIN JUST BELOW STRINGER 22L, BS 540 BULKHEAD UPPER FRAME. REMOVED DAMAGE, HFEC CUT-OUT & HOLE, NO OTHER DEFECT NOTED, FABRICATED DOUBLER, TRIPLER, AND FILLERS. TREATED AND PRIMED ALL REPAIR. INSTALSDR WX0A2017060900240Skin · crackedDURING SCHEDULED MAINTENANCE, A CRACK WAS FOUND IN THE FUSELAGE SKIN AT BS 1309 JUST ABOVE LONGERON 7R. THE CRACK IN THE SKIN MEASURED 2.5'' LONG. THE SKIN WAS REPAIRED IAW EA 40-2016-285, REV A.SDR DALA2016090406444Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN, BS 1369 BETWEEN LONGERS 29 -30L IN AFT CARGO COMPARTMENT. REPAIRED IAW SRM 53-31-02.SDR FDEA201609033121Skin · crackedFOUND SMALL CRACK AT THE UPPER LT CORNER IN THE FUSELAGE JUST ABOVE THE NR 3 PACK BAY DOOR. INSTALLED REPAIR IN REF TO EA 8-5330-T0328078.SDR SWAA2016110209312Skin · corrodedNR 2 ADF ANTENNA FOUND FUSELAGE SKIN CORRODED BETWEEN BS 727+12 TO BS 727B, BETWEEN STR 1 TO STR 2R. REPAIRED SKIN IAW ER & EA.SDR IPXA2016092108493Skin · corrodedINSPECTION TYPE: 3C, EXTERIOR AFT SKIN PANEL LEFT SIDE AT BS 2022 TO 2055 HAS CORROSION. REPAIRED THE SKI IAW EA 011-5310-01-A6443 REV I/R AND EO MD11-5330-61884-A.SDR IPXA2016092108494Skin · corrodedINSPECTION TYPE: 3C, AFT EXTERIOR SKIN BETWEEN BS 1942-1986, LONGERON 26AL HAS AREAS OF CORROSION. REPAIRED THE SKIN IAW EA 011-5330-01-A6450 REV. I/R AND EO MD11-5330-61890-A.SDR IPXA2016091508274Skin · corrodedINSPECTION TYPE:3C, AFT LT FUSELAGE SKIN HAS CORROSION BETWEEN STA 2153-2163 AND L33L TO 35L. REPAIRED CORRODED FUSELAGE SKIN BETWEEN STA 2153-2163 AND L33L TO 35L IAW SRM 53-70-01, REPAIR 3, FIG 201, MAJOR.SDR AALA201609129007Skin · corrodedCORROSION ON THE AFT TOP SKIN PANEL OF THE CENTER WING FORWARD OF FRAME 42 AT CRUCIFORM. REPAIRED THE SKIN IAW EA 263252.SDR DALA2016090706450Skin · damagedDAMAGE FOUND ON SKIN AT BS 225 BETWEEN LONGERONS LONGERS 16 - 17L. REPAIR IAW ERA 525485-4, REV A.SDR DALA2016090206359Skin · crackedINITIAL, CRACK ON FUSELAGE SKIN ON STA Y=1380 BETWEEN LONGERONS 13R-14R. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-04, FIG 18.SDR CALA2016090100618Skin · crackedPREVIOUS BLEND OUT FOUND ON FUSELAGE STA 1197+66 AND 1197+88 STR 35L. HFEC INSPECTION RESULTED IN A CRACK MEASUES 0.025. SKIN THICKNES S IS 0.160. REPAIRED AS PER SRM 53-00-01, REPAIR 14, FIG 201, TABLEII. PAGE 205.THIS IS A CATEGORAY B REPAIR INSPECTION REQUISDR DALA2016090106335Skin · crackedDURING WALKAROUND, A FOUND CRACK ON BELLY SKIN BY AFT EDGE OF MID CARGO DOOR. IAW ERA 550253-14 REVISION ORIGINAL.SDR DALA2016090106369Flange · crackedDURING INSPECTION FOUND EXTERNAL POWER DOOR FLANGE HAS A CRACK, SPLIT AT 9 O'CLOCK POSITION. MAINTENANCE FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-15, REPAIR 4.SDR VNAA2016083100041Skin · crackedNLG CUTOUT AT AFT RT CORNER HAS VISUAL INDICATION OF A CRACK AT FS 235.0, RBL 6.0. MAINTENANCE PREFORMED A MAJOR REPAIR TO THE EXTERNAL FUSELAGE SKIN AT THE NLG WHEEL WELL DOOR CUTOUT, RT SIDE AFT RADIUS AT FS 235.0, RBL 6.0 AND PERFORMED CHECKS IAW THE AMM.SDR DALA2016090106340Splice Plate · corrodedFUSELAGE SKIN SPLICE PLATE CORRODED BETWEEN L29L AND L30, STA 1241. ACCOMPLISHED ALL STEPS OF AND REPAIRED IAW ERA 550060-14.SDR DALA2016090106323Doubler · corrodedCORROSION ON INTERNAL DOUBLER AROUND AFT LAVATORY SERVICE PANE. CORROSION ON INTERNAL DOUBLER WAS REPAIRED IAW ER/A 549257-14, REV ORIGINAL REPETITIVE INSPECTION WILL BE PERFORMED WITH LOG 2657213, ER/A 549257-14, REV ORIGINAL, SECTION II.SDR SWAA2016100408439Skin · damagedSKIN DAMAGED BETWEEN BS 500D TO 520, BETWEEN STRINGERS 13 TO 18L. REPAIRED SKIN IAW EA.SDR SWAA2016091607861Skin · crackedAFT CARGO BAY LOWER FORWARD CORNER SKIN CUTOUT CRACKED. REPAIRED THE SKIN IAW SRM AND EA.SDR DALA2016083106337Skin · corrodedDURING INSPECTION, FOUND LOWER AFT EXTERIOR FUSELAGE SKIN HAS LIGHT SURFACE CORROSION AROUND POTABLE WATER DRAIN BS 947.5 + 6, LBL 10. MAINTENANCE REPAIRED IAW ERA 549077-14.SDR DALA2016083106311Doubler · corrodedCORROSION ON INTERNAL DOUBLER AROUND AFT LAVATORY SERVICE PANEL. FRAME CLIP STA Y=1309 & Y=1322 FROM LONGERON 18LT TO 26LT; LONGERON 20 LT & 21 LT FROM STA Y=1322 TO Y=1338; INTERCOSTALS, 2 EA, BETWEEN LONG 21 LT AND 22 LT FROM STA Y=1322 TO Y=1338; AND LONGESDR DALA2016083106310Doubler · corrodedCORROSION ON PREVIOUS REPAIR DOUBLER AND LOWER DOOR JAMB AT FWD CARGO COMPARTMENT DOOR JAMB. LOWER DOOR JAMB WAS REPAIRED IAW SRM 53-05, FIG 44A.SDR DALA2016083106300Skin · damagedINITIAL: LIGHTNING STRIKE ON LT WINDOW BELT BETWEEN STA Y:731-750, FORWARD AND AFT CORNERS. LIGHTNING STRIKE ON LT WINDOW BELT WAS REPAIRED IAW ER/A 549248-14AD REV ORIGINAL.SDR DALA2016083106294Finger Doubler · bentBENT EDGE ON FINGER DOUBLER AT FUSELAGE SKIN REPAIR BETWEEN STA Y=237 TO STA 256 AND LONGERONS 17LT TO 18LT, REF LOG NR 1542341. SECTION STRIP DOUBLER WAS REPAIRED IAW SRM 53-04-3, FIG 12.SDR DALA2016083006288Skin · bulgedBULGING FUSELAGE SKIN BS 608 - 617, LONGERONS 29 - 30R. DOUBLERS WERE REPLACED IAW SRM 51-30-2, 51-30-5, 51-30-3, 51-10-3 PARR. 14, 21, 51-20-0 AND DWG 5911412 REV. DU.SDR DALA2016083006283Skin · bulgedBULGING FUSELAGE SKIN BTW BS 636 - 655, LONGERONS 29 - 30R. DOUBLER WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.SDR DALA2016083006281Skin · buckledLOWER EMPENNAGE SKIN BUCKLED OUT WITH MISSING RIVETS AT LONGERON 27R BS 1475. REPAIRED IAW SRM 53-10-01 FIG 7.SDR DALA2016083006280Skin · buckledLOWER EMPENNAGE SKIN BUCKLED, LONGERON 26R BS 1475. REPAIRED IAW SRM 53-10-01 FIG 7 SHT. 3.SDR DALA2016082906623Skin · damagedDURING WALK AROUND FOUND DAMAGE FOUR FEET FORWARD OF L2 DOOR LOWER AND CORNER . DAMAGE REMOVED IAW SRM 53-00-01.SDR IPXA2016091008084Skin · corrodedINSPECTION TYPE: 1C, SKIN FRAMES 47 - 48 CORRODED AT BASE OF VHF ANTENNA. REPAIREDN IAW EO A300-5310-61808-ASDR SIMA20160828007Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN BETWEEN FRAMES 13 AND 14 STR 21L AND 20L. REPAIRED INTERNAL FUSELAGE SKIN BETWEEN FRAMES 13 AND 14, STR 21L AND 20L BY INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-75-01,53-21-01, CPM 51-21-05,51-21-06 AND ETN-GN-51-011, SDR SWAA2016090755554Bear Strap · crackedL1 DOOR LOWER AFT CORNER BEARSTRAP CRACKED AT BS 345, WL 210. REPAIRED THE BEAR STRAP IAW SRM.SDR VNAA2016082800035Doubler · chafedFS 987.0, STR 27 HAS CHAFTED REPAIR DOUBLER. MAINTENANCE PERFORMED A MAJOR REPAIR TO THE CHAFED REPAIR DOUBLER AT FS 987.0, STR 27 AND PERFORMED CHECKS IAW REO 670-53-00-466, REV DATED 8-19-16 AND REO 670-53-00-290, REV D DATED 9-10-15. THE AIRCRAFT WAS RELESDR DALA2016082906254Skin · not reportedPERFORM PERMANENT REPAIR ON FUSELAGE SKIN BS 229 - 260 BETWEEN LONGERONS 16 - 18L SRM 53-04 FIG 12C.SDR C77A20160829001Skin · gougedDENT AND GOUGE DAMAGE IN THE CENTER FUSELAGE SKIN FRAMES 84 - 85 BETWEEN STRINGERS 26 - 27R.SDR SWAA2016091607860Skin · crackedR1 DOOR AFT LOWER CORNER CUTOUT CRACKED BETWEEN BS 312 TO 344, BETWEEN STRINGERS 15 - 18R. REPAIRED THE SKIN IAW EA.SDR SWAA2016090955628Skin · crackedL1 DOOR AFT LOWER REVEAL CUTOUT CRACKED. R & R CUTOUT IAW SRM AND DWG.SDR AALA201609059006Skin · corrodedACFT IN BASE MAINTENANCE: CORROSION ON SKIN BETWEEN FRAME 73 AND FRAME 74 AT STR 29 LT. REPAIRED SKIN IAW EA 262904.SDR DALA2016082706270Skin · crackedFOUND FASTENER HOLE CRACKED AFTER HFES INSPECTION AT RADOME ADAPTER RING PERIMETER BS 1360 BETWEEN L2L AND L3L. ACCOMPLISHED REPAIR AT ON THE LT TEAR STRAP IAW ERA 548927-14AD REV O.SDR DALA2016082706249Skin · crackedCRACK WAS FOUND ON FUSELAGE SKIN AT BS 1418 AND BETWEEN LONGERON 2 AND 3R.SDR DALA2016082706244Skin · damagedLIGHTNING STRIKE ON LEFT WINDOW BELT BETWEEN BS 693 - 712. THE WINDOW BELT WAS REPAIRED IAW ER/A 549290-14 REV. ORIGINAL SECTION I.SDR DALA2016082706243Skin · damagedLIGHTNING STRIKE ON LT WINDOW BELT BETWEEN BS 636 - 655. THE WINDOW BELT WAS REPAIRED IAW ER/A 549289-14 REV. ORIGINAL SECTION I.SDR DALA2016082706242Skin · damagedLIGHTNING STRIKE ON LEFT WINDOW BELT BETWEEN BS 617 - 636. THE WINDOW BELT WAS REPAIRED IAW ER/A 549288-14 REV. ORIGINAL SECTION I.SDR SWAA2016110409386Skin · crackedSKIN CRACKED AT BS 540, STR 22L. REPAIRED SKIN PER ER & EA.SDR AALA20160825002Skin · gougedGOUGED, WITH DENT, IN FUSELAGE SKIN BS 354, ABOVE STRINGER 19R. CUT OUT DAMAGE AND REPAIRED IAW SRM 53-00-01-2R-20 AND EA 263086.SDR DALA2016100306998Skin · damagedPREVIOUS BLEND OUT ON EXTERNAL FUSELAGE SKIN BTW STA 351-370 AND LONG 9R-10R. REPAIRED PER SRM 53-04-2 FIG 2 SHEET 5.SDR Q2SA20160824260Skin · dentedSKIN DENTED AT TWO PLACES, BS 950 & 970, STRINGER 5R. ONE DENT FWD OF BS 947.5 AND ONE DENT AFT OF STA 967. AIRCRAFT GROUNDED. REPAIRED THE SKIN IAW SRM 53-00-01 REPAIR 31.
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