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 DALA2024012301060Skin · puncturedAIRCRAFT 1022, DURING LAYOVER IN PBI, MTC REPORTED PUNCTURE DAMAGE TO THE LH LOWER SKIN PANEL (P/N: D53474408206) LOCATED ALONG FR52 BETWEEN STRINGERS 24-25LH. THE SKIN DAMAGE IS MEASURED AS .980 X .950 AND IS LOCATED ADJACENT TO/OVERLAPPING AN EXISTING FASTSDR ASAA2024012148678Skin · dentedLESSOR ITEM 603; (74480) DENT/NICK ON FUSELAGE SKIN FR 9 AND STRG 36 LH APPROX GROUNDED - YES. STRIPPED AREA TO EVALUATE AS PER A320 SRM 51-75-11/001. DENT LOCATION IS 4.3 INCHES ABOVE STR 36 AND 3.5 INCHES FORWARD OF FRAME 8. DENT MEASURES 1.5 INCHES IN LENGTSDR VNAA202403010008Skin · damagedLIGHTNING STRIKE (1EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR15 BTW FS280 - FS264. LIGHTNING STRIKE (1EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR15 BTW FS280 - FS264 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03SDR VNAA202403010007Skin · damagedLIGHTNING STRIKE (2EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR14 BTW FS248.5 - FS233.5. LIGHTNING STRIKE (2EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR14 BTW FS248.5 - FS233.5 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03SDR VNAA202403010006Skin · damagedLIGHTNING STRIKE ( 1EA) ON FUSELAGE SKIN BTW STGR 14 RH TO STGR 15RH AND BTW FS 1051 TO FS 1069. LIGHTNING STRIKE ( 1EA) ON FUSELAGE SKIN BTW STGR 14 RH TO STGR 15RH AND BTW FS 1051 TO FS 1069. WAS BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WAS EVALSDR VNAA202403010003Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 19 RH TO STGR 20 RH AT FS 549. LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 19 RH TO STGR 20 RH AT FS 549 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03SDR VNAA202403010002Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN ON STGR 23 RH AT FS 596. LIGHTNING STRIKE ON FUSELAGE SKIN ON STGR 23 RH AT FS 596 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03SDR VNAA202402280008Skin · damagedLIGHTNING STRIKE (1EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR15 BTW FS280 - FS264. LIGHTNING STRIKE (1EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR15 BTW FS280 - FS264 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03SDR VNAA202402280007Skin · damagedLIGHTNING STRIKE (2EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR14 BTW FS248.5 - FS233.5. LIGHTNING STRIKE (2EA) ON EXTERNAL FWD FUSELAGE SKIN AREA STGR14 BTW FS248.5 - FS233.5 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03SDR VNAA202402280006Skin · damagedLIGHTNING STRIKE ( 1EA) ON FUSELAGE SKIN BTW STGR 14 RH TO STGR 15RH AND BTW FS 1051 TO FS 1069. LIGHTNING STRIKE ( 1EA) ON FUSELAGE SKIN BTW STGR 14 RH TO STGR 15RH AND BTW FS 1051 TO FS 1069. WAS BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WAS EVALUSDR VNAA202402280003Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 19 RH TO STGR 20 RH AT FS 549. LIGHTNING STRIKE ON FUSELAGE SKIN BTW STGR 19 RH TO STGR 20 RH AT FS 549 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03SDR VNAA202402280002Skin · damagedLIGHTNING STRIKE ON FUSELAGE SKIN ON STGR 23 RH AT FS 596. LIGHTNING STRIKE ON FUSELAGE SKIN ON STGR 23 RH AT FS 596 WAS REPAIRED PER PER CRJ-900 SRM 53-00-00-201-003-A03SDR SWAA2024012243272Doubler · cracked23-153-03732-TLD (N8523W - SWA - REPAIR - EXTERNAL GROUND POWER RECEPTACLE DOOR SURROUND DOUBLER BENT AND CRACKED AT LOWER TAB - PERMANENT)<[01] REMOVED DAMAGE PER SRM 52-10-15-2R-4;[02] ACCOMPLISHED HFEC INSPECTION OF CUTOUT PER 737 NDT MANUAL PART 6 51-00-00SDR IPXA2024030757600Skin · corrodedSTR - MAIN CABIN CTR WING BOX R/H SURFACE HAS CORROSION AT STRINGER 15 AND 96 INCH FROM CL (114-23) ACCOMPLISHED REPAIR PER EO-89363-REQ1. REVIEWEDSDR ASAA2024011948088Skin · damagedLESSOR ITEM: DB#39, EVIDENCE OF LIGHTNING STRIKE FWD FUSE .6" AFT OFFR5, 13.5" ABOVE LWR SKIN SPLICE, PLEASE PROVIDE NOMINAL SKIN THICKNESS OFDAMAGE, PROVIDE CUTOUT MEASURES, P/N OF RIVETS USED IN DOUBLER,PROVIDE SRM DFPS,REPAIR LOCATION&MEASURES+SKETCH OR PSDR SWAA2024022242881Support Angle · crackedFWD CARGO COMPARTMENT BILGE SUPPORT CLIP CRACKED AT S-26L STA 500H BELOW Z CHANNEL MKD DOT<[01] REMOVED AND REPLACED FWD CARGO COMPARTMENT BILGE SUPPORT CLIP CRACKED AT S-26L STA 500H BELOW Z CHANNEL PER REF SRM 51-40-02-0G-0 AND DWG#143A7505.;[02] CORRECTION SDR JJBA20240207010Skin · crackedCRACKS SUSPECTED (17X) ON RH SKIN AROUND FASTENERS BTW FR77-80 BTW STR 3R-9R. AFTER NDT INSPECTION, 13X CRACK CONFIRMED. ALL 13X CRACKS REPAIREDSDR JJBA20240130056Doubler · corrodedTRACE OF CORROSION FOUND ON INNER DOUBLER AT ELT ANTENNA LOCATION. INNER DOUBLER REMOVED AND REFABRICATED AND INSTALLEDSDR DALA2024012501125Skin · gouged(LOG 0160441) DURING ROUTINE INSPECTIONS, GOUGE DAMAGE WAS DISCOVERED ON THE FUSELAGE SKIN (PN 148A3595-21) AT APPROX. BS 1145, ABOVE STR 5AR. DAMAGE REPAIRED PER ERA 615068-14.SDR SWAA2024012243009Skin · crackedEXTERNAL POWER PANEL OPENING HAS CRACK ON LOWER EDGE OF CUTOUT. MEASURES 1.5' LONG THRU 1 RIVET; PARALLEL AND 0.25' FROM TOP EDGE. LOCATION IS STA 231 AT STRINGER 23R. TSR 202400406 WAS OPENED FOR ENGINEERING HELP.<[01] PERFORMED LIMITED TIME REPAIR AS REQ PERSDR DALA2024012200989Skin · damagedSHIP 696 SCRATCH AND DENT AFT OF DOOR 4L. APPEARS TO BE FROM CATERING: DENTS (2 EAS) OUT OF LIMITS. CORRECTIVE ACTION: SUMMARY OF NRC 00134: SCRATCH AND DENT AFT OF DOOR 4L WAS REPAIRED PER B757-200 SRM 53-00-01-2R REPAIR 29. (0160570)SDR DALA2024012200933Skin · gouged(LOG 0160521) GOUGE IN FUSELAGE SKIN ABOVE R/H HORIZONTAL STAB BELOW STRINGER 4R BETWEEN STA 1121 & 1138. C/W ER/A 615068-14 REV ORIGINAL.SDR SWIA20240418117Skin · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA81321-690-53-61-1160 PER REO 690-53-61-1160, TEMPORARY DISPOSITION FOR BLENDED DAMAGE TO FUSELAGE SKIN BETWEEN FS1108.00 - FS1126.00 & STR15L - STR16L IS STRUCTURALLY ACCEPTABLE FOR 1850 FLIGHT HOURS FROM TIME OF INCOSDR WX0A2024032231993Skin · dented(MAJOR REPAIR- DISCREPANCY NOTED DURING HEAVY MX VISIT) EXTERNAL FUSELAGE SKIN, DENT FOUND BTW FR 9-11 AND BTW 2-508 AND 2-650. / EXTERNAL FUSELAGE SKIN, DENT BTW FR 9-11 AND BTW Z-508 AND Z-650 PERMANENTLY REPAIRED PER AIRBUS DOSSIER# 80116220 AND ALLEGIANT ASDR SWIA20240320117Skin · dentedUPPER AFT FUSELAGE FS672.00 TO F.S. 682.20 AT STR 3 HAS DENT (C-CHECK RO 3/19/2024) PERFORMED PERMANENT REPAIR ON UPPER AFT FUSELAGE F.S 672.00 TO F.S 682.00 STGR 3 LH IAW MHIRJ REO 601R-53-61-8148 REV -- DATED 2024-01-25 NDT PERFORMED BY BARRON NDT FAA CSDR ASAA2024011748002Skin · dentedLESSOR ITEM: DB#44, FWD FUSELAGE L/H DENTED BELOW L-2 COCKPIT WINDOW, WO-375836 NR-G176016. OIL #19. RE-EVALUATE REPAIR. REQUIRED ACTION1. PLEASE PROVIDE SRM DFP'S REF USED FOR EVAL. 2. PLEASE PROVIDE EXACT DAMAGE LOCATION.3. PLEASE PROVIDE PHOTO OR SKETCH SDR JJBA20240207017Skin · crackedCRACKS SUSPECTED (13X) ON LH SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3L-9L. AFTER NDT INSPECTION, 11X CRACKS ONLY CONFIRMED. ALL 11X CRACKS REPAIRED.SDR ASAA2024011747565Cargo Track · corrodedAFT CARGO FLOOR RAIL SPLICE STA 727I, RBL 8.1 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION ON FLOOR RAIL SPLICE STA. 727I RBL 8.1,ORIGINAL MAT.080,MAT REMOVED .016,MAT REMOVED .064,FOUND OUT OF LIMITS,REMOVED CARGO SLOOR RAIL SPLICE, LOCATED AND DRILLED NESDR YENA2024012400087Skin · dentedDURING HEAVY MAINTENANCE: DENTS ON EXTRENAL SKIN LOCATED EXISTING REPAIR BTE 23 - FR24 & R40R - STR 43R AT LOWER FUSLELAGE / (RESOLVED ON W/O: 1243677 TASKCARD: NR-00043) REF AEROMAN WO 2023- 464/1 NR 2023-731807 PERFORMED PERMANENT REPAIR LOCATED ON EXTERNAL SDR FDEA202401170083Skin · dentedUPPER FUSELAGE SKIN CROW AREA BETWEEN STA 1480/1510.5 AND STG 3 / 4 LH WITH DENT. UPPER FUSELAGE SKIN CROW AREA BETWEEN STA 1461/1480 AND STGR 3/4 LH WAS REPAIRED I.A.W. SRM 53-00-01-212 REPAIR 14 FIG. 201 AND INSPECTION REQUIREMENTS SEE TABLE V ZONE A - SDR FDEA202401170082Skin · dentedUPPER FUSELAGE SKIN CROW AREA BETWEEN STA 1480/1510.5 AND STG 3 / 4 LH WITH DENT. UPPER FUSELAGE SKIN CROW AREA BETWEEN STA 1461/1480 AND STGR 3/4 LH WAS REPAIRED I.A.W. SRM 53-00-01-212 REPAIR 14 FIG. 201 AND INSPECTION REQUIREMENTS SEE TABLE V ZONE A - SDR ASAA2024011647654Transition Panel · corrodedAFT PIT RIGHT SIDE TRANSITION PANEL HAS UPPER AND LOWER SURFACE HAS CORROSION NUMEROUS PLACE BETWEEN BS767 AND BS727I+10 STR26R AS MARK. GROUNDED - YES. REMOVED CORROSION, ORIGINAL THICKNESS .040, REMOVED .005, REMAINING .035 FOUND TO BE OUT OF LIMITS. IAW B73SDR ASAA2024011647461Baffle · corrodedAFT PIT RIGHT SIDE STIFFENER HAS CORROSION ATTACH WITH TRANSITION PANEL AT BS747 AND BS767 STR25R AND STR26R AS MARK STREAMER ATTACH. GROUNDED - YES. REMOVED CORROSION AT STA BS747 AND STA BS767 STR 25R AND STR 26R, ORIGINAL MAT .032, MAT REMOVED .007, REMAINISDR ASAA2024012417460Intercostal · corrodedAFT PIT RIGHT SIDE TRANSITION PANEL HAS UPPER AND LOWER SURFACE HAS CORROSION NUMEROUS PLACE BETWEEN BS727I+10 AND BD727 STR26R AS MARK GROUNDED - YES. REMOVED CORROSION ORIGINAL THICKNESS .040, REMOVED .006, REMAINING THICKNESS .034 FOUND TO BE OUT OF LIMITS SDR CALA2024012200166Skin · crackedDURING NDT PROCEDURE, IT WAS FOUND 02 HOLES WITH CRACKS INDICATION AT FORWARD DOOR CUTOUT AFT CORNER ON LH SIDE AT STA 340. PERFORM INSPECTION AS REQUIRED ON TABLE 202 FROM SRM AIRPLANE DELIVERY OR 6,000 MAXIMUM FLIGHT CYCLES FROM THE REPAIR INSPECTION INTERVASDR DALA2024011700712Skin · damagedSHIP 697 PLUG WAS FOUND ON SKIN FRAME AROUND THE FASTENER STA: 560 STRINGER - 01 AT CABIN PAX. CORRECTIVE ACTION: SUMMARY OF NRC 00085. FRAME STA 560 BTW STR 3LH TO 4 RH WAS REPAIRED PER B757-200 SRM 53-00-07-2R REPAIR 1 AND ER/A 614618- 14 REV ORIGINAL SECTIOSDR AALA202401178256Doubler · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK LOCATED ON EXTERNAL SKIN AT BS 2195.75 TO BS 2221.65 AT STR 35L LOWER FUSELAGE. PERFORMED PERMANENT REPAIR AT BS 2195.75 TO STA 2221.65 AND STR 41L TO STR 43L ON LOWER FUSELAGE. PER B777-200 SRM 53-00-01-2R REPAIR 7.SDR DALA2025011600376Skin · damagedERA 610713-14 REV C PERMANENT REPAIR HAS DTE DAMAGE TOLERANCE LI MIT. ERA 610713-14 REV C REQUIRES ENGINEERING REVISION TO OPERATE BEYOND 12 MONTHS FROM SECTION III REPAIR INSTALL. ASSOCIATED ER/A 00-610713 ADDED FOR AC 8120. PER ER/A 610713-14AD REV D, DTE STSDR SWIA20240320115Skin · damagedADM# N939SW-8619 BETWEEN STGR 15L/16L F.S. 404.00. 7/8" LONG BY 3/8 WIDE WITH A DEPTH OF .0040" DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED. ELIMINATE EVIDENCE OF DAMAGE USING STANDARD ACFT PRACTICES. (C-CHECK RO 3/19/2024SDR A6WA202401158715Skin · dentedDENT ON LEFT AFT FUSELAGE SKIN AT FS755.00 TO 67.5% SPAR DATUM S24L. AIRCRAFT REMOVED FROM SERVICE EVALUATED DENT ON AFT FUSELAGE SKIN AT FS755.00 Ï¿½ 67.5% SPAR DATUM AND S21L TO S23L. ACCOMPLISHED DOUBLER REPAIR IAW EA AWAC-CRJ253-02025 REV IR DATED 01/SDR YENA2024011700067Skin · damagedDURING HEAVY MAINTENANCE: DAMAGE ALL OVER A/C EXTERIOR OF AIRCRAFT- RADOME- ENG NARCELLS -WING LEADING EDGE; CHAPTER 05-50-28-210-801A INSPC/W TOMX WO 2296, NR 00068, CH 05-50-60 HAIL STRIKE INSP C/W TOMX WO 2296 NR 00010 RADOME REPL NR00042, ENGINLET REPLACEMSDR YENA2024011600045Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FWD LOWER SKIN BETWEEN FR1-7 & STGR 24R-25R AND 24L-25L / HAIL DAMAGE - TEMPORARY REPAIR (CONSIDERED A MAJOR REPAIR)SDR DALA2024011600587Unknown · unknownELONGATED HOLES AT EXTERNAL FUSELAGE SKIN SCUFF PLATE AREA BTWN STA 954/STA 986 OF AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00064: EXTERNAL FUSELAGE SKIN SCUFF PLATE AREA BTWN STA 954/STA 986 OF AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 614841-14 REV SDR VNAA20240214011Skin · damagedFUSE SKIN LIGHTING STRIKE DAMAGE REPAIR. FUSE SKIN LIGHTING STRIKE DAMAGED WERE REPAIRED PER CRJ-900 SRM 53-00-00-201-003-A03 AND REO 690-53-11-1676 REV. --SDR DALA2024011600592Skin · damagedFUSELAGE / SKIN / AFT CARGO DOOR CUTOUT, STA Y=954, L-26R TO L-28R / ELONGATED HOLES & CORROSION TIME LIMITED. REPAIRED FUSELAGE / SKIN / AFT CARGO DOOR CUTOUT, STA Y=954, L- 26R TO L-28R / ELONGATED HOLES & CORROSION PER ERA 614841-14 REV ORIGINAL SECTIONI TISDR HNAA2024012500035Skin Panel · corrodedSKIN PANEL 145-35010-003 HAS CORROSION. R&R'D IAW EO1-53-24-0043SDR IPXA2024011726100Skin Panel · damagedFWD CARGO COMPT. FR 20 R/H SIDE HAS UPPER SKIN DAMAGE CEILING PANEL 132 NC. INSTALLED SKIN PANEL IAW SREO A300-2550-21666 JL 07586.SDR DALA2024011600601Skin · gouged(LOG 4412634) GOUGE ON SKIN AT APPROX 2" AFT OF STA 727F BETWEEN STRINGER 21L AND 22L. DOUBLERS DRILLED UP AND FABRICATED PER SRM 53-00-01-2R-36. TREATED AND PRIMED PARTS. INSTALLED DOUBLER AND TRIPLER PER SRM 53-00-01-2R-36.SDR DALA2024011400565Unknown · unknownSHIP 3251 DISC: PERFORM PERMANENT REPAIR ON FR29 TO FR 30 AT LEVEL STRG 1L TO STRG 1R / TIMING ANTENNA COVER PLATE. C/A: COMPLIED WITH ER/A 604897-14 REV. B MATCHES WITH ALL STEPS ON PRI 604897-14 REV.B PRI REV.0, PRI 604897-14 REV.B PRI REV.1, PRI604897-14 RESDR COEA2024022101819Skin · crackedWO 251965 NR 200050 HEAVY CHECK COE/MAJOR REPAIR: UPPER FUSELAGE SKIN IS CRACKED FWD OF FRAME 24 BETWEEN STRINGERS 1L AND 1R AT THE END OF THE M7 HARDPOINT. CORRECTIVE ACTION: REPAIRED PER M7 REPAIR DRAWING 72R1101-03.
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