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 HNAA2024052200431Skin · dented53-2020 DENT ON FUSELAGE 3" FWD OF FR23 AND 2" ABOVE STR13L. REPAIRED IAW EO1-53-24-0253SDR HNAA2024052200430Skin · gouged53-2017 MULTIPLE GOUGES FOUND ON FUSELAGE EXTERNAL SKIN AT FR7-8 STR20R-21R. REPAIRD IAW EO1-53-24-0260SDR HNAA2024052200429Skin · dented53-2014 DENT FOUND ON FUSELAGE SKIN ON FR9 AND 6" ABOVE STR20L. REPAIRED IAW EO1-53-24-0264SDR ASAA2024041049345Transition Panel · corrodedAFT CARGO RH SIDE TRANSITION PANELS HAVE VARIOUS SPOTS OF CORROSION FROM STA 727F TO 767. GROUNDED - YES. EVALUATED AFT CARGO R/H TRANSITION PANEL. REMOVED CORROSION. ORIGINAL THICKNESS .040, REMOVED .040, REMAINING .000. FOUND TO BE OUT OF LIMITS. REMOVED, FASDR ASAA2024041049132Skin · corrodedLAV DRAIN PORT HAS CORROSION LOWER SIDE OF DRAIN. GROUNDED - YES. REPAIRED DAMAGE AT LOWER LAV DRAIN PORT IAW B737-900 SRM 53-70-01-2R-3 CATEGORY B REPAIR INSPECTION REQUIREMENTS INSPECTION THRESHOLD 50,000 FLIGHT CYCLES AND REPEAT INSPECTION INTERVALS EVERY 5SDR ASAA2024041049114Skin · crackedL/H HORIZONTAL LOWER SKIN IS CRACKED AT STA 135. 33 INCHES FWD OF REAR SPAR. GROUNDED - YES. REPAIRED IAW SRM 55-10-01-2R-11 STEP 4 INSPECTION REQUIREMENTS THRESHOLD 56,000 CYCLES REPEAT INSPECTIONS IN 9,000 FLIGHT CYCLES, DVI & LFEC IAW B737-800 SRM 55-10-01-SDR 2024FA0000310Skin · puncturedSKIN PUNCTURED BEYOND LIMITS FROM FLYING DEBRIS WHILE PARKED ON RAMP.SDR SWAA2024041173254Skin · crackedFOUND 2 INCH CRACK INDICATION STARTING AT BS 559+9; ENDING AT 559+11; STR S-1. ACCOMPLISHED CRACK VERIFICATION IN REF TO NDT MANUAL PART 4 53-30-06 UTPA AND NDT MANUAL PART 6 53-30-18 CRACK INSPECTION OF OUTER SKIN AT SUBSURFACE EDGES. REPAIRED FUSELAGE CROWSDR CALA2024041801128Skin · damagedLIGHTNING STRIKE DAMAGE AT BS 500G 6.5 INCHES ABOVE STR 4R. REPAIRED.SDR AALA202404103340Skin · corrodedAIRCRAFT WAS GROUNDED: CORROSION ON FUSELAGE SKIN AROUND LAVATORY VENT AT BS 917, FROM S21L TO S22L. REPAIRED SKIN PER SRM 53-70-01-2R-3.SDR DALA2024041004271Skin · crackedCRACK INDICATION ON HOLE 21 OF THE SKIN UNDERNEATH THE HINGE FITTINGS LOCATED ON FWD CARGO DOOR. CORRECTIVE ACTION: REPAIRED PER ER/A 616466-14AD. (0285351)SDR DALA2024041004262Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN LOCATED Y=1022 BETWEEN L-9L AND L-8L. SUMMARY OF NRC 00496: CRACK ON EXTERNAL FUSELAGE SKIN LOCATED Y=1022 BETWEEN L-9L AND L-8L WAS REPAIRED PER PRI 616777-14 REV 1 AND ERA 616777-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR.SDR DALA2024040904246Skin · damagedAIRCRAFT 3007, LIGHTING STRIKE AT STA 4546/ FR 5 AND APPROXIMATELY STRINGER 33 ON RIGHT SIDE OF AIRCRAFT. CORRECTIVE ACTION: BLENDED PAINT. FOUND STRIKE TO BE OUTSIDE OF ALLOWABLE LIMITS. REMOVED EXISTING FASTENERS IN REPAIR AREA. CUT OUT DAMAGED SKIN PER A321SDR IPXA2025021290881Skin · dented*** MAJOR REPAIR *** FOUND TWO DENTS ON FUSELAGE AT STA 1480+60 AND STA 1520 AND STRINGER S-44 - S45R REVIEW COMPLETEDSDR SWAA2024041872226Doubler · crackedLOWER ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER HAS A CRACK.<[01] ACCOMPLISHED REPAIR PARTS IAW SRM 53-10-15-2R-4 REPAIR 4;[02] VERIFIED TASK COMPLETESDR QXEA2024041500099Finger Doubler · corrodedCORROSION AFT CARGO DOOR CUTOUT FWD FINGER PLATE. REMOVED AND REPLACED AFT CARGO DOOR CUTOUT FWD FINGER PLATE REF SRM 51-40-08.SDR AALA202404102305Doubler · crackedAIRCRAFT WAS GROUNDED: EXTERNAL POWER DOOR CUTOUT LOWER FLANGE AND BACKING DOUBLER CRACKED AT BS 230, S23R. REPAIRED PER SRM 53-10-15-1A PROCEDURE 4 AND SRM 53-10-15-2R-4.SDR VNAA202404160014Skin · gougedNUMEROUS NICKS, GOUGES AND DENTS ON FUSELAGE SKIN BETWEEN FS1031.00 - FS1051.30 AND STR22R - STR25R. DAMAGE CAUSED BY LP PNEUMATIC DUCT PLUG TETHERED BY LANYARD COMING LOOSE IN FLIGHT AND IMPACTING AGAINST THE FUSELAGE REPEATEDLY. CLASSIFIED AND REPAIRED IAW SDR VNAA202404160008Skin Panel · burnedLIGHTNING STRIKE DAMAGE (SMALL HOLE IN SKIN PANEL) AT APPROXIMATELY FS 440.0 AND STGR 3R, CLASSIFIED IN MHIRJ REO 690-53-21-1744SDR VNAA202404160007Skin · scratchedSCRATCH IN FUSELAGE SKIN AT APPROXIMATELY FS 310.0 AND STGR 25L. DAMAGE WITHIN SRM ALLOWABLE LIMITS PER 53-21-01-101-002-A04SDR SWIA20240502405Skin · dentedBIRD STRIKE ON NOSE JUST IN FRONT OF THE LOWER LEFT PITOT TUBE WITH DENT IN THE YELLOW BOXED PORTION. FURTHER REMAINS NOTED ON THE LEFT WING LEADING EDGE AND LEFT ENGINE. (FILED CLOSED)COMPLIED WITH BIRD STRIKE INSPECTION PER AMM 05-50-02-200-801-A. DENT FOUNSDR ASAA2024040548985Skin · dentedFOUND DENT ON R/H SIDE OF FUS. AT STA 905 +9" 3" BELOW STR 17R GOUGE IN CENTER OF DENT. GROUNDED - YES. (RESOLVED ON W/O: 1996489 TASKCARD: N/R-00001 ) DENT ON R/H SIDE OF FUSELAGE AT STA 905+9" 3" BELOW STR 17R REPAIRED IAW EA 800-53EA-26862. THIS IS A CATEGOSDR GTIA2024040938051Skin · damagedJETBRIDGE OPERATOR DRAGGED JETBRIDGE ALONG SIDE OF AIRPLANE RESULTING IN SEVERAL AREAS OF DAMAGE.-REF CAERTIFIED AVIATION SERVICES W/O 603-305469. RETRUNED TO SERVICE IN ACCORDANCE WITH FAR 43.9. AS AUTHORIZED BY THIS REPAIR STATION MANUAL, THE FOLLOWING PERSOSDR DALA2024040904251Skin · corrodedSHIP 5803 SECONDARY NRC IN REF NRC #00137: CORROSION ON INTERNAL SKIN BTW STA 1787.45 AND 1864 AND STGRS 25L TO 27L AT AFT ACCESORY COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00193: CORROSION INTERNAL SKIN BTW STA 1787.45- 1825 AND STA. 1850-1864 AND STGRSSDR SWI2024F00425Skin · gougedAIRCRAFT LOWER EXTERNAL FUSELAGE IN BETWEEN FS 913 JUST FWD OF FS 927 THERE IS A DEEP SCREW GOUGE ON FUSELAGE SKIN.(MARKED) AT STR27 MX# 28040473 (C-CHECK RO 5/28/2024) REPAIRED AIRCRAFT LOWER EXTERNAL FUSELAGE SKIN BETWEEN FS 913 JUST FWD OF FS 927 REF RESDR SWI2024F00423Skin · corrodedCORROSION BETWEEN FS295.0 AND FS310.0 AT STGR27 AS MARKED (C-CHECK RO 5/25/2024) INSTALLED NEW DOUBLER AT STGR27 BETWEEN FS295.00 AND FS310.00 CRJ700 SRM 51-42-06-001-001-A01 REV. 38 JUL/2020 AND BOMBARDIER DWG SH670-30023 REV. G. COMPLIED WITH ALL STEPS OSDR SWIA202404250004Skin · dentedMULTIPLE FUSELAGE SKIN DENTS BETWEEN FS605.00 - FS589.00 AND STRINGERS 23R - 26R. (C-CHECK RO 4/24/2024) PERFORMED TEMPORARY REPAIR OF 3 FUSELAGE SKIN DENTS BETWEEN FS605.00 - FS589.00 AND STRINGERS 24R - 26R IN REF TO REO 601R-53-61-8184, REV--, DATED 202SDR MASA20240409008Skin · handler errorPILOT REPORT- LH SIDE FUSELAGE LARGE DENT ( HIT BY JET BRIDGE ) AFTER FLIGHT 6030 ATL - IAH. CORRECTIVE ACTION: PERMANENT REPAIR HAS BEEN COMPLIED WITH REF MESA RO# E175-53-4612 R1 (MRO38602) 04/08/2024.SDR DALA2024040504135Skin · dentedDENT ON EXTERNAL FUSELAGE SKIN STA Y=588 AND LONG 30 ABOVE BUTT SPLICE. SUMMARY OF NRC 00338: DENT ON EXTERNAL FUSELAGE SKIN STA Y=588 AND LONG 30 ABOVE BUTT SPLICE WAS REPAIRED PER PRI 616805-14 REV 1 AND ER/A 616805-14 REV ORIG. SECTION I. ACCOMPLISH SECTIONSDR ASAA2024040350523Skin · gougedAFT LOWER EXTERNAL FUSELAGE, FRAME 58 TO 59 AT ANTENNA MOUNT, SKIN IS GOUGED GROUNDED - YES. REMOVED ANTENNA IAW AMM A320 34-42-11-000-001A REV 10. ORIGINAL MAT .118" IAW A320 SRM 53-41-11-42B REV 148. BLENDED DAMAGE, REMAINING MAT .115, LENGT 1.2", WIDTH .800SDR ASAA2024040350522Skin · gougedAFT LOWER EXTERNAL FUSELAGE, BELOW AFT CARGO DOOR, FRAME 55 TO 56 AT ANTENNA MOUNT, SKIN IS GOUGED GROUNDED - YES. REMOVED ANTENNA IAW A320 AMM 34-42-11-000-001-A REV 10. ORIGINAL MAT .118 IAW A320 SRM 53-41-11-42B REV 148. BLENDED DAMAGE, REMAINING MAT .110, SDR SWI2024F00421Skin · crackedPOSSIBLE CRACK ON THE LH SIDE OF THE FUSELAGE SKIN AT TRU PANEL 211AL LOWER AFT CORNER AREA (MARKED) . (C-CHECK RO 5/25/2024) REMOVED AND REPLACED LH SIDE OF THE FUSELAGE SKIN AT TRU PANEL 211AL (P/N CC670-33106-5S ). IAW CRJ 700 SRM 51-42-06-001-001-A01 SDR SWIA2024052900403Skin · gougedGOUGING MARKS ON EXTERNAL SKIN OF DOUBLER, FWD ATG ANTENNA MATING SURFACE BETWEEN FS 501.00 - 517.00, STGR 25R - 26R. (C-CHECK RO 5/25/2024) INSTALLED NEW FWD ATG ANTENNA DOUBLER REF, CRJ700 SRM 51-42-20-001-001- A01 REV 38 JUL 25/2020 AND AIRCELL DRW. D1SDR DALA2024040804143Skin · damagedSHIP 3248 DISC: BURN MARK JUST FWD OF FR 6 LH FUSELAGE C/A: 473292 W REPAIRED BURN MARK JUST FWD OF FR 6 LH FUSELAGE WITH TEMPORARY BLIND FASTENER REPAIR REF A320 SRM 53-11-11-300-033. PERMANENT REPAIR REQUIRED IN 5000 FC/10000FH WHICHEVER COMES FIRST. CATEGORSDR DALA2024040804142Skin · damagedSHIP 3248 DISC: BURN MARK JUST AFT OF FR 5 LH FUSELAGE. C/A: REMOVED FASTENER REF A320 SRM 51-42-11(43292). C/A: REMOVED FASTENER REF A320 SRM 51-42-11(473292). PERFORMED BHEC ON REMOVED FASTENER HOLE. NO DEFECTS NOTED. REF A320 NTM 51-10- 01.(QC5350). INSTALLSDR DALA2024040804141Skin · damagedSHIP 3248 DISC: BURN MARK JUST FWD OF FR 5 LH FUSELAGE. C/A: REPAIRED BURN MARK JUST FWD OF FR 5 LH FUSELAGE WITH TEMPORARY BLIND FASTENER REPAIR REF A320 SRM 53-11-11-300-033. PERMANENT REPAIR REQUIRED IN 5000 FC/10000FH WHICH EVER COMES FIRST. CATAGORY C REPSDR DALA2024040804140Skin · damagedSHIP 3248 DISC: BURN MARK AT FR 3 LH FUSELAGE. C/A: REMOVED FASTENER REF A320 SRM 51-42-11(473292). PERFORMED BHEC ON REMOVED FASTENER HOLE. NO DEFECTS NOTED. REF A320 NTM 51-10- 01.(QC5350). INSTALLED PERMANENT REPAIR REF A320 SRM 53-11-11. (LP: 0276181)SDR DALA2024040404085Skin · damagedSHIP 3248 DISC: BURN MARK JUST AFT OF FR 6 LH FUSELAGE. C/A: REPAIRED BURN MARK JUST AFT OF FR 6 LH FUSELAGE WITH TEMPORARY BLIND FASTENER REPAIR REF A320 SRM 53-11-11-300-033. PERMANENT REPAIR REQUIRED IN 5000 FC/10000FH WHICHEVER COMES FIRST. CATEGORY C REPASDR JR2R20240403861Doubler · corrodedDOUBLER AT FR90 RBL12 CORRODED. REMOVED AND REPLACEDSDR JR2R20240403860Doubler · corrodedTEXAS DOUBLER AT FR90 RBL24 CORRODED. REMOVED AND REPLACEDSDR 21GA20240403004Skin · damagedFUSELAGE SECT 43 AT FUSLEAGE SKIN BETWEEN F.S. 632-654 AT STR 25 LH ELONGATED HOLE.SDR ASAA2024040250001Skin Panel · corrodedFWD LOWER EXTERNAL FUSELAGE SKIN BETWEEN FRAME 33 AND 34 HAS CORROSION AT DRAIN/VENT PORT GROUNDED - YES. REMOVED FASTENERS TO FOM CORROSION REMOVAL IAW A320 SRM 51-42-11/001, PARA ZE, REV148. REMOVED CORROSION IAW A-320 SRM 51-74-00/001, PARA 5-A3, REV148 ANDSDR SWIA2024053000402Doubler · gougedGOUGING MARKS ON EXTERNAL SKIN OF DOUBLER, FWD ATG ANTENNA MATING SURFACE BETWEEN FS 501.00 - 517.00, STGR 25R - 26R. MARKED. (C-CHECK RO 5/28/2024) REMOVED AND INSTALLED NEW FWD ATG ANTENNA DOUBLER BETWEEN FS501.00 - FS517.00 REF CRJ900 SRM 51-42-20-001SDR ASAA2024040249499Skin · corrodedAFT FUSELAGE ACCESS DOOR 311BL AFT LWR CUTOUT HAS SURFACE CORROSION ON SKIN SURFACE GROUNDED - YES. REMOVED CORROSION AFT FUSELAGE DOOR 311BL IAW B737-800 SRM 53-00-01-1A-1. ORIG THICKNESS .080" PER B737-800 53-80-01 (LOCATION ONE STA 1064) REMOVED .005", SDR ASAA2024040249498Skin · corrodedAFT FUSELAGE SKIN JUST BELOW ACCESS DOOR 311BL AT INTERPHONE JACK HAS SURFACE CORROSION GROUNDED - YES. REMOVED CORROSION ON FUSELAGE SKIN, ORIG THICKNESS .080", REMOVED .004", REMAINING .076". FOUND TO BE WITHIN LIMITS IAW B737-800 SRM 53-00-01-1A 1. RESTOSDR SWAA2024050969571Skin · debondedPANEL 192JR OUTER SKIN IS DISBONDED NEAR CENTER OF PANEL. (MARKED)<[01] PANEL 192JR OUTER SKIN WAS DISBONDED NEAR CENTER OF PANEL AND REPAIRED IAW SRM 51-70-05-2R-2;[02] JOB COMPLETE.SDR FDEA202404020431Skin · damagedTO REPAIR SKIN & STRINGERS AT LH F.STA 508-STA529, BETWEEN S-39L AND S-41L. SKIN & STRINGERS AT LH F.STA508-STA529, BETWEEN S-39L AND S-41L REPAIRED AS PER B777 SRM 51-40-02-0G, SRM 51-10-02-0G, SRM 53-10-03-2R REPAIR 1, SRM 51-40-05-0G, SRM 51-20-01-0G, SSDR CALA2024040300969Repair · inadequateCONVERT TEMPORARY REPAIR TO PERMANENT REPAIR AT RH SIDE SKIN PAN EL BETWEEN FR2-3 FWD OF RH REF LOG PAGE 7270995 AND ECRA 5330-07 208 PER HAECO LCQ NR 9298002/22002. CONVERSION FROM TEMPORARY TO PERMANENT SKIN REPAIR NOT POSSIBLE D53118296 RH LATERAL SKIN PNL SDR CALA2024040300963Repair · inadequateCONVERT TEMPORARY REPAIR TO PERMANENT REPAIR AT RH SIDE SKIN PAN EL BETWEEN FR2-3 FWD OF RH CONVERSION FROM TEMPORARY TO PERMANENT SKIN REPAIR NOT POSSIBLE D53118296 RH LATERAL SKIN PNL FROM FR 1 - FR 12 PN D531100752010 3 STEP 6 OF ECRA INSTRUCTS TO CLOSE DIPSDR MASA20240705017Skin · gougedBIRD STRIKE: MAJOR REPAIR: GOUGE TO ELECTRICAL BAY FLOOR WEB BETWEEN FS177.00-FS185.00 & OUTBOARD OF RBL22.00 BLENDED GOUGE TO ELECTRICAL BAY FLOOR WEB.BETWEEN FS177.00-FS185.00 & OUTBOARD OF RBL22-.00 PER RO# CRJ9-53-5310
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