JASC 5330
Service difficulty reports · 79,329
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 SWAA2022031017892Scuff Plate · crackedFWD CARGO BAY FWD CORNER SCUFF PLATE CRACKED / ACCOMPLISHED REPAIR PER EA NO 1-A53-2076 REV. 11. 92892U 15JUN19.SDR CA190617007Landing · corroded(CAN) DURING CHECK, OPERATOR FOUND CORROSION ON THE AFT TOILET SERVICE ACCESS DOOR LANDING. THERE IS NO CORROSION FOUND ON THE OUTSIDE, ONLY ON THE INSIDE AS VISIBLE ON THE PICTURE ATTACHED. (TC# 20190617007)SDR IPXA201906143250Skin · corrodedINSPECTION TYPE:12YRBULK PIT DOOR CUTOUT IS CORRODED AT AFT LOWER CORNER.REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW A300 SRM 51-74-10. RESTORED SURFACE IAW A300-600 SRM 51-21-10 AND 51-75-10.SDR CALA2019061400939Skin · crackedRT SIDE FUSELAGE. AT STA 1664, STRINGER 13RT,JUST ABOUT STAB L/E, FOUND A CRACK 4 INCH LONG. COMPLIED WITH EWIS W/REF TO AMM 20-60-07-912-011 AND GMM 05-35-51. 53-80-01, REPAIR 7, PARAGRAPH 4.B. REMOVED 11 FASTENERS IN STR. 13R COMMON TO CRACKED AREA PER SRM SDR SWAA2022031028455Skin · corrodedFORWARD CARGO DOOR CUTOUT EXTERNAL FUSELAGE SKIN AT SCUFF PLATE FOOTPRINT HAS CORROSION AROUND FASTENER HOLES STA 440-492 BETWEEN STR 25R-26R / FWD CARGO DOOR CUTOUT EXTERNAL SKIN AT SWFF PLATE FOOT PRINT AROUND FASTENER HOLES BS 440 - 497 STR 25R - 26R; BLENDSDR SWIA2019080546122Skin · corrodedFRETTING CORROSION ON AIRCRAFT SKIN AROUND FASTENERS LH FS 409.00+80 TO 409.00+112 STR 20L (C-CHECK) RO: 08/01/2019 REMOVED DAMAGE, ON AIRCRAFT SKIN AROUND FASTENERS LH FS 409.00+80 TO 409.00+112 STR 20L IAW REO.SDR SWIA2019080546121Skin · corrodedFRETTING CORROSION ON AIRCRAFT SKIN AROUND FASTENERS RH FS 409.00 TO 409.00+96 STR 20R. REMOVED DAMAGE IAW REO.SDR REXA2019061101009Doubler · corrodedLWR SURFACE OF DOUBLER FOR REAR SERVICING POINT BETWEEN FS559.0+112 TO FS559.0+80 AND STRR21 AND STR 24 HAS CORROSION. REPAIRED LWD SURFACE OF DOUBLER FOR REAR SERVICING POINT BETWEEN FS559.0+112 TO FS559.0+80 AND STR 21 TO STR 24 IAW EA CRJ 253-09151.SDR IPXA2019062843853Skin · corrodedUPPER AFT SKIN BETWEEN X=104 AND X=-104 HAS AREAS OF CORROSION AT STRINGER 15. REPAIRED THE SKINS BETWEEN STRINGER 14 AND 16 IAW 011-5730-01-A7814 IR AND EO MD11-5730-72997-A.SDR V0XR20190624002Skin · corrodedMULTIPLE FASTENERS ON EXTERNAL SKIN AT F.S. 939 TO F.S. 953 STGR 20R-25R AND AT STGR 27 HAVE SIGNS OF CORROSION. CLEANED, EVALUATED, AND REPAIRED AREAS WITH CORROSION AND REPLACED FASTENERS IAW BOMBARDIER REO 670-53-51-146 DATED 2019-06-15.SDR V0XR20190624001Tripler · gougedTRIPLER REPAIR AT F.S. 977.00 STGR 27 IS GOUGED. REMOVED EXISTING REPAIR AND FABRICATED NEW REPAIR PARTS AND INSTALLED THEM IAW REO 670-53-00-290 REV-F, AND DWG PL BA670-39313 REV-A.SDR A6WA2019061246659Skin · crackedNOSE GEAR SPADE DOOR CUTOUT AFT R/H CORNER IS CRACKED. REPAIRED CUTOUT SKIN IAW REO 601R-53-11-048 REV-D.SDR REXA2019062000935Landing · crackedAFT SIDE OF GROUND AIR DOOR LANDING CRACKED. REMOVED AND REPLACED LANDING.SDR REXA2019062000932Repair · gougedREPAIR DOUBLER AFT OF LOW PRESS. GROUND AIR DOOR GOUGED. REPAIRED DAMAGE PER REO 601R-53-61-7014.SDR IPXA201906143249Skin · crackedINSPECTION TYPE:12YRFWD LOWER CARGO DOOR SURROUNDING HAS GOUGE ON EDGE OF FUSELAGE SKIN FR20 APPROX. STGR 40RH.BLENDED DAMAGE, FOUND TO BE WITHIN LIMITS AND RESTORE SURFACE IAW A300-600 SRM 53-13-12.SDR RU3A201906130022Skin · crackedFRAME CRACK AND MULTIPLE SKIN CRACKS IN THE LOWER FUSELAGE SKIN AT THE COMMUNICATION ANTENNA WERE DETECTED WHILE IN CHECK. EXTERNAL DOUBLER PART NUMBER 53-0048-401 HAS BEEN INSTALLED PER MAJOR REPAIR ENGINEERING ORDER 19-28-31 "REPAIR OF CRACKS AT FS180 LOWER SDR DALA2019061103495Skin · dentedDENTS ON FUSELAGE SKIN AT STA 427 BETWEEN LONGERON 27L AND 29L. ACCOMPLISHED PERMANENT REPAIR REF PRI #578768-14, REV. 1 AND ER/A #578768 -14 REV. ORIGINAL. REQUIRED INSPECTION COMPLETE QC1981. (LP #1116346)SDR IXXA2019062029012Skin · corrodedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE C-17. IN COMPLIANCE OF GENERAL VISUAL INSPECTION-CORROSION PREVENTION TASK CARD 53-800-10-01, THE FOLLOWING FINDINGS WERE NOTED: BULGED SKIN AT STA 1400 BETWEEN STRINGER 26L AND 27L. WORK IN PROGRESS. REPAIRED BULGED SKISDR DALA201906113489Skin · dentedDENT ON FUSELAGE SKIN AT STA 524 TO 527 1" BELOW LONG 26L LAP SEAM. PER B717 SRM 53-01-01-1A-3 CONDITION 5 DENT IS OUT OF LIMITS. REMOVED DAMAGE 1" X 3" PER B717 SRM 53-03-01-2R-1 FIG. 110 SHEET 3. FUSELAGE SKIN MISDRILLED AT STA 520 ON LONG 26L, REMOVED DAMAGSDR CALA2019061000919Skin · corrodedLAV EXHAUST VENT AFT FASTENER HOLE AT FUSELAGE EXTERIOR SKIN EXI STING DOUBLER HAS CORROSION FR 69 EA5100-02750 002 PER HAECO LCQ NON ROUTINE 9292341 GENERATED BY V061623 REMOVED AND REPLACED LAV EXHAUST VENT DOUBLER IAW A320 SRM53-41- 11-300-004 PERFORMED BY SDR ASOA2019061094027Skin · dentedFLIGHT 4126 A SMALL DENT WAS DISCOVERED IN THE LEFT HAND AFT FUSELAGE APPROXIMATELY 8" BELOW THE LAST PAX WINDOW. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A TYPE A1 REPAIR IAW EMB-145 SRM 53-24-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR DALA2023031702018Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 465 AND LONGERON 20. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANESDR DALA2023031702014Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 503 AND LONGERON 19. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANESDR DALA2023031702013Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 465 AND LONGERON 21. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANESDR DALA2023031702012Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 446 AND LONGERON 20. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANESDR DALA2023031702011Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 332 AND LONGERON 20. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANESDR DALA2023031702010Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 313 AND LONGERON 21. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANESDR DALA2023031702009Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 256 AND LONGERON 21. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANESDR CA190611004Skin · corroded(CAN) SKIN + SKIN DBLR BLENDED BELOW LAV SERVICE 6EA PLACES. SKIN P/N: 601R38328-47 LAVATORY SERVICE DOOR DOUBLER P/N: 601R38363-2 (TC# 20190611004)SDR SWIA2019080546117Skin · corrodedCORROSION ON THE EXTERNAL SKIN AT FS755.0, AT APPROXIMATELY STRINGER 18R. BLENDED OUT CORROSION ON EXTERNAL SKIN AT F/S 775.0 AT STR. 18R.IAW SRM. C/W REO ALL STEPS COMPLETED OF PERMANENT REPAIR.SDR YENA2019061270319Skin · dentedDURING OOS VISIT, 2 DENTS WERE FOUND ON THE EXTERNAL SKIN PN 170-03344-005 & 170-03705-007 BTWN FR11-13 & STGR 4L-5L AT THE FWD FUSELAGE. SEE ATTACHED REF /1/ EA FOR MORE DETAILS. THE DENTS WERE FOUND TO BE OUTSIDE OF SRM ALLOWABLE LIMITS AND THERE’S NO PERMANSDR GTIA2019061073410Skin · puncturedPUNCTURE FOUND ON FUSELAGE SKIN PANEL BTW FR.82-83 AND STR.1L-2L REF LTPR NRI 5000889965-0010. RAF-01 GENERATED-REF LTPR NR#5000889965-0010 REPAIR WAS PERFORMED AT FUSELAGE SKIN BTW FR 82-83 STRG 1-2 LH SIDE AS PER SRM TASK 53-11-11-300-041 REV.128SDR GTIA2019061073408Skin · dentedREF MWI 235363102 DENT BETWEEN FR9/FR10 STGR 22 WITH DEPTH: 1.016 MM LENGHT: 25.4 MM AND WIDTH 4.76 MM-RAF-01 239561801 CREATED FOR TECHNICAL SUPPORT DEPARTMENT REVIEW. THIS CLEARS MWI# 235363102 MOC NOTIFIEDSDR CALA2019060700909Skin · puncturedPUNCTURE IN SKIN IN LINE WITH AFT EDGE OF PANEL 197GB ON GOLD ST RIPE, APPROX 4" X 3". THIS IS LEFT SIDE OF FUSELAGE APPROX STA 2 2428/FR56 AT FLOOR LINE. REPAIR ACCOMPLISHED ON LOG PAGE 3415550SDR UIEA2019060704417Skin · corrodedCORROSION - SKIN AFT CGO FUSELAGE SKIN INNER SURFACE STA 1720-1740. S-48R ~ S-49R.(<P>ACCOMPLISHED EI NO. T2019A53M-2774 REV. 2. JOB COMPLETED AND CONDITION CHECK NORMAL. </P>)SDR UIEA2019060704418Skin · corrodedCORROSION - SKIN, AFT CGO FUSELAGE SKIN INNER SURFACE STA 1660 S-50R ~ S-51R.(<P>ACCOMPLISHED EI NO. T2019A53M-2774 REV. 2. JOB COMPLETED AND CONDITION CHECK NORMAL. ORIGINAL EI ATTACHED WITH WO 3487178.</P>)SDR SWAA2022031076865Doubler · crackedEXTERNAL FUSELAGE; EXTERNAL POWER RECEPTACLE DOOR CUTOUT; AFT LOWER CORNER; FLANGE DOUBLER IS CRACKED / TRIMMED OUT DAMAGED AREA OF FLANGE DOUBLER AT EXTERNAL POWER RECEPTACLE CUTOUT FWD LWR CORNER PERFORMED HFEC INSPECTION WITH NO DEFECTS NOTED; AND RESTORED SDR CA190621002Doubler · corroded(CAN) DURING CHECK, OPERATOR FOUND CORROSION ON THE AFT WASTE SERVICE PORT DOUBLER (DOOR LANDING AREA). DAMAGE REWORKED (CORROSION BLENDED) PER REO-500-53-61-043 ISSUE COVERED UNDER PROJECT CAW-BD5-53-0153 (TC# 20190621002)SDR CA190610010Buttstrap · corroded(CAN) FS280 BUTT STRAP BLENDED TO REMOVE LIGHT SURFACE CORROSION BETWEEN STRINGER 26R AND STRINGER 27 (TC# 20190610010)SDR SWAA2019072235163Skin · wornSKIN WORN BETWEEN BS. 845 TO BS. 870, BETWEEN STR. 1R TO STR. 2R. REPAIRED SKIN PER SRM AND EA.SDR SWAA2019062434051Skin · dentedFUSELAGE SKIN DENTED AT BS. 360+8, BELOW STR. 5L. REPAIRED SKIN PER EA.SDR SWAA2019062434050Skin · dentedFUSELAGE SKIN DENTED AT BS. 360+8.5, BELOW STR. 5L. / REPAIRED SKIN PER EA.SDR SWAA2019062434049Skin · dentedFUSELAGE SKIN DENTED AT BS. 360+5, BELOW STR. 5L. REPAIRED SKIN PER EA.SDR SWAA2019062434048Skin · dentedEXTERNAL SKIN DENTED AT BS. 350+5, BELOW STR. 5L. REPAIRED SKIN PER EA.SDR ABXA2019061706116Bear Strap · corrodedCORROSION ON THE LOWER (INTERNAL SURFACE) BEAR STRAP, RIGHT OVERWING EMERGENCY EXIT, STA 859.5 – 871.5, STR 16AR – 18R. THE BEAR STRAP WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR REXA2019061360829Doubler · crackedAC GROUND POWER DOOR 122BR LANDING, FWD EDGE IS MISSING. REPAIRED AC GROUND POWER DOOR 122BR LANDING, FWD EDGE I.A.W. BOMBARDIER REO 601R53-11-569SDR YENA2019061060318Skin · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON THE FUSELAGE RH CENTER WING BOX PRESSURE PANEL ATTACHMENT HOLE B BETWEEN FR 35& FR 36. NOTE: NO INDICATIONS WERE FOUND ON THE L/H SIDE OF THE PRESSURE PANEL. THE SUBJECT HOLE WAS REAMED TO REMOVE THE DAMAGE SDR SWAA2022031029021Scuff Plate · crackedAFT CARGO AFT CORNER SCUFF PLATE BROKEN. 8-22 (OFF AIRCRAFT) / AFT CARGO AFT CORNER SCUFF PLATE WELD REPAIRED ACCOMPLISHED ON EA NO: 1-A53-2076 REV 11 REF W/O 2015067 ; 1000 ; 0048SDR FDEA201906051219Skin · cracked#3 PACK BAY CUT-OUT APPEARS TO HAVE A CRACK AT THE UPPER AFT CORNER. COUNTER SUNK HOLES AS REQUIRED IN DOUBLER AND TRIPLER. ALODINED AND PRIMED, IAW MD-11 SRM 53-20-15-2R. AND OK TO INSTALL EXTERNAL ALUMINUM REPAIR DOUBLER AND TRIPLER. SHGN 06JUN19 20:39 SDR 39LA2019061105182Skin · puncturedDURING SCHEDULED INSPECTIONS, A PUNCTURE WAS FOUND IN THE FUSELAGE SKIN JUST FORWARD OF THE TAIL STAND MOUNT. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY IN WORK. ONCE THE REPAIR IS COMPLETED, OPEN
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