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 SWIA20240923082Skin · damagedLIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN BETWEEN FR2-3 AND STGR 12L AND 13L AS MARKED. (C-CHECK RO 9/20/2024) REMOVED LIGHTNING STRIKE BY DRILLING FASTENER HOLE (-4) AND INSTALLING BUTTON HEAD FASTENER. FWD FUSELAGE EXTERNAL SKIN BETWEEN FRAMES 2-3 AND SDR SWAA2024091128241Skin · debondedPANEL 192AL OUTER SKIN HAS AN AREA OF DISBOND NEAR FWD EDGE OF PANEL. (MARKED)<[01] 04 - REPAIRED PER [SRM 51-70-05-2R-2-B00319 (REPAIR 2 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH (12.70 MM) IN DIAMETER TO ONE SKIN AND THE HONEYCOMB CORE - AIRFRAME - PERMSDR SWIA2024090600821Skin · dentedTRANSFER FROM EAML 1414568 : DENT ON LOWER L/H SIDE OF NOSE FUSELAGE BETWEEN FS210.92 AND FS220.00 AND STGR 23L AND STGR 24L, DENT IS 0.115 INCHES DEEP BY 1.50 INCHES WIDE AND 1.75 INCHES LONG. INSPECTED DENT FOUND TO BE OUT OF LIMITS PER SRM 53-11-01 AND 53-SDR CALA2024082600490Skin · corrodedFOUND CORROSION ON SKIN AFTER REMOVAL OF LAV PAN ALONG STR. 25L,BETWEEN STA. 847 AND STA. 867.VERIFIED PART 1 STEPS 1 THRU 31 OF EC/RA 5360-01861 IS COMPLETED IN ITS ENTIRETY WITHOUT DEVIATION. CREATED LOG PAGE 9025433 TO GENERATE DIP TO ACCOMPLISH PERMANENT RSDR DALA2024082208351Skin · nicked(LOG 0513350) INITIAL INSPECTION: NICK ON SKIN (INTERNAL SIDE) ON STA 743 BTW S-27L AND S-27R AT AFT CARGO COMPARTMENT. SKIN (INTERNAL SIDE) ON STA 743 BTW S-27L AND S-27R AT AFT CARGO COMPARTMENT WAS REPAIRED PER ER/A 619929-14 REV. ORIGINAL.SDR JR2R20240821010Skin · dentedFWD FUSELAGE SKIN PANEL MULTIPLE DENTS AND HAIL DAMAGE. REPAIREDSDR DALA2024082108317Skin · gougedSHIP 3429 SMALL GOUGE FOUND FWD SKIN AFT CARGO DOOR CUTOUT. STR 41/ FRAME 59A. CORRECTIVE ACTION: BLENDED OUT DAMAGE PER SRM 53-41-11. (9995775)SDR SWIA20240820Skin · dentedDENT ON EXTERNAL SKIN FS625.3 - 640 BETWEEN STGR25L - 26L. (CIRCLED IN RED) (C-CHECK RO 11/7/2024) REPAIRED DENT ON EXTERNAL SKIN FS625.3 - 640 BETWEEN STGR25L - 26L REF REO REO 601R-53-61-8218 REV -- DATED:10/15/2024, PRESSURE LEAK CHECK WAS GOOD, COMPSDR IXXA20241003008Skin · crackedCRACK INDICATION IN THE 3RD HOLE FROM THE BOTTOM, SKIN ONLY AT THE L1 DOOR LOWER AFT CORNER. HAECO WO 320008 NON ROUTINE 40153SDR IXXA20241002004Skin · crackedCRACK FOUND IN 2ND HOLE FROM THE BOTTOM IN BOTH THE SKIN AND BEAR STRAP AT R1 DOOR LOWER AFT CORNER. HAECO WO 320008 NON ROUTINE 40152SDR HNAA2024091100760Skin · dented53-2435 DENTS ON REAR FUSE SKIN AFT OF FR65 BTW STR19-21L. REPAIRED IAW EO1-53-24-0509SDR CALA2024090402382Skin · crackedSTA 1725 STR 7R AREA SKIN FOUND CRACKED. FUSELAGE EXTERNAL SKIN STA 1725 STR 7R CHORD STRAP AND SKIN SRM 53-80-010-2R-5 REPAIR 5 FIG 201 SHEET 4 TABLE III. REPAIRED AS PER B767 SRM 53-80-01-2R-5 REPAIR 5 FIG 201 DETAIL INSPECTION THRESHOLD 6000 FLIGHT CYCLES SDR NXTA202408260204Skin Panel · damagedAFT BELLY SKIN, FORWARD OF AFT CROSS TUBE WAS DAMAGE, WHEN THE PILOT ATTEMPTED TO LIFT HELICOPTER WITH HELI-PORTER. LEFT SIDE WAS PUNCTURED IN TWO PLACE, AND THE RIGHT WAS DENTED RESULTING IN TWO AREAS OF DE-LAMINATION.SDR WRXR202408200001Skin · dentedPERM REPAIR - SKIN, FUSELAGE - BETWEEN FS1031.00 AND FS 1051.30 AND STR 22R AND STR 25R. PERFORMED PERM REPAIR - SKIN, FUSELAGE - BETWEEN FS1031.00 AND FS 1051.30 AND STR 22R AND STR 25R IAW REO-670-53-61-2326 REV--.SDR JR2R20240820026Skin · gougedFORWARD CARGO CUTOUT, GOUGE IN FUSLAGE SKIN AT AFT LOWER CORNER FR27, O/B OF STR25RSDR HNAA2024100100885Skin · crackedE050563 LH SIDE FUSELAGE UPPER SKIN HAS POSSIBLE CRACK AROUND (2) FASTENERS AT FRAME 78. REPAIRED IAW EO1-53-24-0570SDR DALA2024091008902Skin · corroded(LOG 0510803) FUSELAGE / SKIN, SKIN DOUBLER AND BULKHEAD CHORD STA 500H TO 540 & S-26L TO S-26R / CORROSION, CRACK. REPAIRED PER ERA 619586-14.SDR IXXA2024091002Bear Strap · crackedFWD FUSELAGE SKIN AND BEAR STRAP R1 DOOR CUTOUT HAS CRACK INDICATION LOWER FASTENER HOLE STA 335 JUST ABOVE STRINGER 20R. CRACKED LENGTH .5.SDR DALA2024082208346Skin · corroded(LOG 0510791) FUSELAGE / SKIN, SKIN DOUBLER AND BULKHEAD CHORD STA 500H TO 540 & S-26L TO S-26R / CORROSION, CRACK. REPAIRED PER ERA 619586-14.SDR HNAA2024092300852Shear Tie · crackedE050029 CRACKED SHEAR CLIP AT FR80, BETWEEN STRG 07L-05L. RAR SHEAR CLIP AT FR80, BETWEEN STRG 07L-05L IAW EMB 145 SRM 51-40-02.SDR HNAA2024092300843Skin · corrodedE050234 CORROSION IN CARGO ON LOWER SKIN PLATE BETWEEN FRAMES 61-62 STRINGERS 19L-20L. RAR THE CARGO UNDERFLOOR LOWER SKIN PLATE BETWEEN FRAMES 61-62 STRINGERS 19L-20L IAW EMB 145 SRM 51-40-02.SDR FDEA202408181146Skin · dentedLWR FUSELAGE - EXTERNAL SKIN FR1-FR2 8-9 O'CLOCK FOUND A DENT REPAIRED THE LWR FUSELAGE EXTERNAL SKIN FR1-FR2 8-9 O'CLOCK DENT AREA PER A300-600 SRM 53-11-12-201 FIG 201. THIS IS CAT B REPAIR. THE FIRST INSPECTION WAS 51000FC / 89000FH WHICHEVER OCCURS FISDR HNAA2024092300851Shear Tie · crackedE050028 CRACKED SHEAR CLIP AT FR80, BETWEEN STRG 09R-07R. : RAR SHEAR CLIP AT FR80, BETWEEN STRG 09R-07R IAW EMB 145 SRM 51-40-02.SDR SWIA20250106816Skin · dentedADM# N374CA-7225 - LH FUSELAGE SKIN AT FS 220.00, BETWEEN STR20L AND STR21L. ONE DENT MEASURING 3.25" DIAMETER X .025" MAX DEPTH. AFTER DRESSBACK, NEW DENT DIMENSIONS ARE 2.3"L BY 1.7"W BY .010" DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITSDR SWIA202412240816Skin · dentedLH FUSELAGE SKIN AT FS 220.00, BETWEEN STR20L AND STR21L. ONE DENT MEASURING 3.25" DIAMETER X .025" MAX DEPTH. AFTER DRESSBACK, NEW DENT DIMENSIONS ARE 2.3"L BY 1.7"W BY .010" DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMSDR HNAA2024092300850Skin · scratchedE049491 SCRATCH ON REAR FUSELAGE SKIN BETWEEN FR79-FR80 AND STRG 03L-04L. RFORMED CUTOUT, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER AND APPLIED EDGE SEALANT FOR REPAIR OF DAMAGED SKIN BTW FR79-80, STGR 3L-4L IAW EMB 145 SRM 53-32-01 ITEM 2 FIGURE 2SDR SWIA202409200009Skin · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA92805-ETD2024-170-021422 MXCODEID76852-PR - AT 2500 FT BIRD STRIKE, NOSE RADOME AND WINDSHIELD FIRST OFFICER WAS IMPACTED. PERFORMED BIRD STRIKE INSPECTION PER AMM05-50-02-200-801-A. DAMAGE FOUND ON SKIN AT FRAME 4 STRSDR SWIA202408270016Skin · damagedCOMPLY WITH PERMANENT REPAIR FOR TEMPORARY REO 690-53-00-454 TEMPORARY REPAIR FOR LIGHTNING STRIKE DAMAGE ON LH FUSELAGE SKIN BETWEEN FS 280 - FS 847+32 AND STR 9 - STR 15. ITEMS # 16, 17, 18, AND 19. (C-CHECK RO 8/27/2024) COMPLIED WITH PERMANENT REPASDR AALA202408235663Doubler · gougedAIRCRAFT IN BASE MAINTENANCE: SKIN GOUGE LOCATED AT BS 228 AND RBL12 FORWARD OF NLG CUT-OUT. INSTALLED DOUBLER REPAIR PER EA 356544A.SDR LR7A2024081603474Skin · damagedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH CENTER FUSELAGE SKIN WITH DAMAGED FASTENER HOLES AT FS245.5, WL267-276, RBL29-54. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001173642.SDR LR7A2024081603472Skin · damagedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE RING SEGMENT WITH DAMAGED FASTENER HOLES AT FS324, WL146-156, LBL173. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-21. NR# 1001172156.SDR LR7A2024081603471Skin · damagedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH FUSELAGE SKIN DAMAGED AT FS284-289, RBL80, WL165.5. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001171602.SDR LR7A2024081603468Skin · damagedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE SKIN WITH DAMAGED FASTENER HOLES AT FS305-310, LBL61, WL144. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-10. NR# 1001168527.SDR LR7A2024081603466Skin · crackedDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH CENTER FUSELAGE SKIN CRACKED AT FS341, LBL61, WL144. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-10. NR# 1001165811.SDR LR7A2024081603433Skin · dentedDURING SCHEDULED C-15 CHECK UNDER JOB CARD HC5321, FOUND RH FUSELAGE SKIN DENTED AT FS267, RBL70, WL154. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001133058.SDR IXXA2024081607Skin · dentedAFT FUSELAGE, LOWER SKIN IS DENTED AT APPROX STA1790 BETWEEN STRINGERS 38R & 39RSDR ASAA2024081553102Lap Joint · corrodedFUSELAGE SKIN AT LOWER LAP SEAM BETWEEN STA 927-951 STGR 23R HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR TO AFT EXTERNAL FUSELAGE SKIN PANELS 147A3110-4 AND 147A3400-4 AT LAP SEAM BETWEEN STA 927-967 STGR 23R IAW EA 800-53EASDR IPXA2024090674434Skin · dentedSKIN DENTED, RT FUSELAGE TAIL SECTION BS 1915.1 - 1923.5. MEASURED THE DENT DIMENSION LENGTH= 1" WIDTH(A)= 0.4" DEPTH(Y)=0.006" AND A/Y = 66 FOUND TO BE IN LIMIT PER SRM 53-00-01-1A-1 FIGURE 101 DETAIL III REV.126SDR IPXA2024090674300Skin · dentedDENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1746-1767 S-36R (EVALUATE) MEASURED THE DENT DIMENSION LENGTH= 1" WIDTH(A)= 0.6" DEPTH(Y)=0.007" AND A/Y = 85 FOUND TO BE IN LIMIT PER SRM 53-00-01-1A-1 FIGURE 101 DETAIL III REV.126SDR ASAA2024081552156Skin · crackedEXTERNAL POWER RECEPTICAL CUTOUT, FORWARD DOUBLER IS CRACKED MARKED WITH DOT. GROUNDED - YES. REPAIRED EXTERNAL RECEPTICAL CUT OUT IAW B737-70 SRM 53-10-15-2R-5.SDR CALA2024081602229Skin · corrodedGENERATING ITEM: 19-5310-1-2576 APU DOOR EXTERNAL SURROUND STRUCTURE LIFTED AFT LWR.SDR IPXA2024081574422Skin · dentedDENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1788 S-38R~S-39R (EVALUATE) OK TO WORKSDR IPXA2024081574300Skin · dentedDENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1746-1767 S-38R ~ S39R (EVALUATE) OK TO WORKSDR IPXA2024081574434Skin · dentedDENT - SKIN, R/H FUSELAGE TAIL SECTION STA 1915.1 - 1923.5 (EVALUATE) OK TO WORKSDR SWAA2024092326060Skin · corrodedCORROSION INTERNAL SKIN LOCATED BTW BS727 TO BS727A AND BTW STR27R TO STR27L WL148.5 AT AFT CARGO COMPARTMENT 2024-504273<[01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45 MG; S/N: 221859911; DUE DATE: 17-NOV-24.;[02] REWORKED AND EVALUATED INTERNAL SKIN LOCASDR SWAA2024091826006Doubler · crackedEGPR DOOR CUT OUT LOWER INTERNAL DOUBLER CRACKED<[01] REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER IAW B737-800 SRM 53-10-15-2R-4 REPAIR 4;[02] REMOVED DAMAGE AND INSTALLED FILLER AND DOUBLER IAW B737-800 SRM 53-10-15-2R-4 REPAIR 4;[03] VERIFIED REMOVED DAMSDR IXXA2024091101Skin · crackedRI LOWERR AFT DOOR CORNER CUTOUT CRACKEDSDR CALA2024081600439Skin · crackedCROWN SKIN EXTERNAL EDDY CURRENT INSP STA 297-439, ALONG S-4L & S-4R (ZONE 1) - FUSELAGE CROWN SKIN AT STA 345, STR4R CHEM-MILL POCKET HAS CRACK CONFIRMED PER NDTM 53-30-14 PT6. CONFIRMED CRACK FINDING DISPOSITION (APPLICABLE AT ALL LOCATIONS):A) CONTACT USDR DALA2024081508165Skin · crackedCORROSION ON UPPER SKIN OF CENTRAL FUEL TANK STA Y=748, X=55 APPROX AND Z=-10 IN THE FRONT WALL ON LH MLG WHEEL WELL. SUMMARY OF NRC 00384: CORROSION LEVEL 2. CORROSION ON UPPER SKIN OF CENTRAL FUEL TANK STA Y=748, X=55 APPROX AND Z=-10 IN THE FRONT WALL ON LHSDR DALA2024081508164Skin · crackedCORROSION ON UPPER SKIN OF CENTRAL FUEL TANK STA Y=748, X=55 APPROX AND Z=-10 IN THE FRONT WALL ON LH MLG WHEEL WELL. SUMMARY OF NRC 00384: CORROSION LEVEL 2. CORROSION ON UPPER SKIN OF CENTRAL FUEL TANK STA Y=748, X=55 APPROX AND Z=-10 IN THE FRONT WALL ON LH
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