JASC 5330
Service difficulty reports · 79,281
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 SWIA2026042477437Skin · dentedPROTRUDING DENT FOUND ON FUSELAGE SKIN BETWEEN FS 333 AND FS 349, AND BETWEEN STR23L AND STR24L. PERFORMED CUTOUT OF DENT AND APPLIED DOUBLER AT FUSELAGE SKIN BETWEEN FS333 - FS349, STGR 23L - 24L REF REO 670-53-21-2876 REV --.SDR R61A2026051800137Skin · dentedDURING HEAVY CHECK FOUND DENT ON THE RIGHT SIDE OF THE NOSE UNDER THE RIGHT DV WINDOW AFT. REPAIRED DENT IAW EMB ETD 2026-170-007353SDR EE4Y2026042424376Skin · damagedDURING THE STRUCTURAL INSPECTION, EXISTING SKIN BLEND-OUTS AND LIGHTNING STRIKES DAMAGE WERE FOUND BETWEEN FR23-24, NEAR STRINGER 27R. THE BLEND-OUTS WERE REWORKED IN ACCORDANCE WITH SRM PART II 51-10-03 REQUIREMENTS. ADDITIONALLY, LIGHTNING STRIKES DAMAGE WERSDR EE4Y2026042424374Skin · canningDURING A STRUCTURAL INSPECT, AN EXISTING REPAIR DOUBLER BETWEEN FR08 AND FR09, AND BETWEEN STRINGER 20L AND 21L WAS IDENTIFIED. ACCORDING TO PREVIOUS OPERATOR RECORDS, THIS REPAIR WAS INSTALLED IN ACCORDANCE WITH ETD2017-190-105910 GUIDELINES. THE RECORDS DID SDR EE4Y2026042424373Skin · not reportedDURING THE REMOVAL OF THE LIVE TV KA BAND CONNECTIVITY SYSTEMS STRUCTURAL PROVISIONS IN ACCORDANCE WITH SB 190-53-0125 (UNDER ETD2026-190-001029 EFFECTIVITY), THE FOLLOWING DISCREPANCIES WERE IDENTIFIED. THE SB 190-53-0125 DOES NOT INCLUDE INSTRUCTIONS TO INSTSDR 1Q2R2026090250020Skin · damagedDURING INSPECTIO, FOUND 3 SPOTS OF LIGHTNING DAMAGE ON SKIN @ STR26R BTWN FS31-FS333SDR SWAA2026052792188Access Panel · delaminatedDELAMINATED ACCESS PANEL 193AR LOWER FUSELAGE. REPAIRED ACCESS PANEL 193AR LOWER FUSELAGE IAW B737-800 SRM 51-70-05-2R-10 REPAIR 10.SDR DALA2026042802658Skin · wornFOUND FUSELAGE LOWER SKIN WORN AT BS 1730, S21R AND S20R. DAMAGED AREA REPAIRED PER SRM53-80-01 (1558233) (AIRCRAFT GROUNDED)SDR DALA2026042802657Skin · wornFOUND LT FUSELAGE LOWER SKIN WORN AT BETWEEN BS 1730 , S21L & S20L. DAMAGED AREA REPAIRED IAW SRM 53-80-01-2R (1558230) (AIRCRAFT GROUNDED)SDR U2RA2026042800008Skin · puncturedPUNCTURED FUSELAGE SKIN BETWEEN BS 2742.64 AND BS 2753.10 AND BETWEEN BL0 AND RBL15.0 - ACCOMPLISHED MAJOR REPAIR.SDR U2RA2026042800009Skin · puncturedPUNCTURED FUSELAGE SKIN BETWEEN BS 2742.64 AND BS 2753.10 AND BETWEEN LBL 1.57 AND LBL 10.0. ACCOMPLISHED MAJOR REPAIR.SDR DALA2026042402617Skin · corrodedRH UPPER SKINS BS 960 - 1000 / CORROSION / TIME LIMITED REPAIR. CORRECTIVE ACTION: REF ERA 617062-14. (1558934) AIRCRAFT WAS GROUNDEDSDR CALA2026042415680Skin Panel · crackedWHILE PERFORMING EXTERNAL CROWN INSPECTIONS FOUND NUMEROUS DISCREPANCIES IN THE EXTERNAL FUSELAGE SKIN AREA BETWEEN STA.727C & STA727F BETWEEN STR4L & STR4R. REPAIRED DISCREPANCIES IN THE EXTERNAL FUSELAGE CROWN SKIN AREA BETWEEN STA.727C & STA727F BETWEEN SSDR 2026F00083Deflector · corrodedFOUND 7 AREAS OF CORROSION ON DEFLECTORS ON PANEL 323AC. MECHANICALLY REMOVED 7 AREAS OF CORROSION ON DEFLECTORS ON PANEL 323AC IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNA SRM 51-70-02 EXCEEDING .002" OF MATERIAL REMOVEDSDR JR2R20260423645Doubler · corrodedLAV WASTE DOOR CUTOUT INTERNAL DOUBLER FWD I/B SIDE CORRODED. REPAIREDSDR SWAA2026052791990Access Panel · damagedELONGATED HOLE ACCESS PANEL 193D AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 193D AT LOWER FUSELAGE IAW SRM 51-70-05-2R-10 REPAIR 10.SDR SWIA2026042276025Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 1000.00 - FS 1015.00 AND STRG 25R - STRG 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FSDR SWIA2026042276024Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394.00 - FS 409.00 AND STRG 13L - STRG 14L DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR). PERFORMED PERMANENT DOUBLER REPAIR INSTALLASDR SWIA2026042276023Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 581.00 - FS 597.00 AND STRG 24R - STRG 25R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR). PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO SDR SWIA2026042276022Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RT FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394.00 - FS 409.00 AND STRG 13R - STRG 14R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE SKIN LOCATEDSDR IPXA2026050122864Skin · dentedDENTED SKIN , L/H FWD UPPER FUSELAGE EXTERNAL SKIN , AT STA 212.5. (EVALUATE) 1. ACCOMPLISHED REPAIR I.A.W EO-97318-REQ1 REV. 2.<BR>2. JOB COMPLETED.<BR>3. ATTACHMENTS ARE UPLOADED.SDR DALA2026042802656Skin · dentedSKIN DAMAGED ON LOWER CORNER, AFT OF CARGO DOOR CUTOUT. DAMAGE FOUND TO BE DENTED, DIMENSIONS 4" X 6" AND .100 DEEP. DAMAGE IS AT BS 1351. C/W ERA 634010-14. (1557762) (AIRCRAFT GROUNDED)SDR SIMA20260422002Doubler · corrodedWASTEWATER BOX DOUBLER SKIN HAS MINOR CORROSION. (MAJOR REPAIR) (LEVEL 2 CORROSION) REPAIRED WASTEWATER BOX DOUBLER IAW ERS EJ-53MR-5397. REPAIRED WASTE WATER BOX DOUBLER IAW ERS EJ-53MR-5397.SDR DALA2026042302602Skin · damagedDAMAGE ON FWD CARGO COMPARTMENT OPENING SKIN APPROX 12 INCHES ABOVE FWD LWR CORNER. REPAIRED PER A330 SRM 53-21-11-283-017. (8717524) AIRCRAFT WAS GROUNDED.SDR CALA2026042315650Skin · crackedRIGHT FR 35 STR 30 HOLE 2 HAS CRACK INDICATION IN FWD SKIN LAYER, 70% S.H. AT 8 O CLOCK POSITION. UPDATED PERFORMED INTERIM REPAIR ON RH FR 35 STR 30 HOLE 2 IAW ECRA 5331-03188 PART 1 INTERIM REPAIR.SDR ENYR20260422002Doubler · corrodedWASTEWATER BOX DOUBLER SKIN HAS MINOR CORROSION. (MAJOR REPAIR) (LEVEL 2 CORROSION) REPAIRED WASTE WATER BOX DOUBLER IAW ERS EJ-53MR-5397.SDR 2A6R2026042175306Skin · corrodedMULTIPLE AREAS OF CORROSION DAMAGE OF VARYING DIMENSIONS AND DEPTHS WAS DISCOVERED ON THE AFT L/H FUSELAGE SKIN PANELS AROUND THE GROUND PORT, LOWER MAINTENANCE STEP, UPPER AND LOWER CLAMSHELL DOOR HINGE LOCATIONS AND SURROUNDING THE FUEL DOOR, AS WELL AS ON TSDR SWIA2026042077007Skin · corrodedEXTERNAL SKIN AT FS 559+90 STGR 23 HAS EVIDENCE OF CORROSION. MARKED WITH TAPE. (C-CHECK RO 08/28/2026)BLENDED, LPI, PAINTED, AND CIC CORRODED AREA OF EXTERNAL SKIN AT FS559+00 STGR 23 IAW MHIRJ REO 601R-53-51-742, REV--, DATED 2026-05-15. PERFORMED LEAK TESTSDR SWIA2026042076417Skin · crackedLEFT TRU BAY DOOR CUT-OUT, AFT LOWER CORNER POSSIBLE FUSELAGE SKIN CRACKED AT THE RADIUS. REPLACED LT HYDRAULIC BAY SKIN PANEL, JUST BELOW TRU BAY DOOR CUT OUT, REF SRM 51-42-06-001-001-A01 & SRM 51-42-13-001-001-A01 & DWG CC670-33040 REV G AND DWG CC670-320SDR SWIA2026042076377Skin · crackedRH TRU BAY DOOR CUT-OUT, AFT LOWER CORNER POSSIBLE FUSELAGE SKIN CRACKED AT THE RADIUS. REPLACED ADG SKIN WITH SERVICEABLE SKIN PANEL REF. DWG CC670-33040 REV-G, DWG CC670-32010 REV-F, SRM 51-42-06-001-001-A01 REV. 38, SRM 51-42-21-001-001-A01 REV. 38, SRM 5SDR SWIA2026042076115Skin · corrodedCORROSION FOUND AROUND FASTENERS ON SKIN BETWEEN STR 23R AND 24R @ FRAME 559+96. PERFORMED BLEND REPAIR AROUND FASTENERS ON SKIN BETWEEN STR 23R AND 24R @ FRAME 559+96 IAW REO 601R-53-51-740 REV--SDR SWIA2026042076113Skin · corrodedEXTERIOR SKIN CORRODED BETWEEN FS 559+80 AND FS559+96 AT STRINGERS 21R AND 23R. COMPLIED WITH BLEND REPAIR TO EXTERIOR SKIN BETWEEN FS559+80 - FS559+96 AT STGR 21R AND 23R IAW REO 601R-53-51-740 REV--. COMPLETE TASK CARD 51-900-1003-SKY.SDR AALA202605218276Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TO FUSELAGE SKIN AT STA 892 AND S27R. ACCOMPLISHED DOUBLER REPAIR PER SRM 51-40-02.SDR AALA202605217573Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER FUSELAGE SKIN AROUND DRAIN HOLE AT BS 727E AND BL 0. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-60-01-2R-4.SDR QXEA2026051100112Doubler · corrodedDOUBLER AT FRAME 16 LBL 11 IS CORRODED. REMOVED DAMAGED AREAS AND FOUND TO BE OUT OF LIMITS. REPAIRED PER ETD 2026-170-006563.SDR IPXA2026050282674Skin Panel · corrodedMAJOR REPAIR, CORROSION-FUSELAGE SKIN IMMEDIATELY SURROUNDING THE DRAIN VALVE AT STA 1410 BETWEEN S-38R AND S-39R. (REPAIR) INSTALLED BULK CARGO FLOOR PANEL IAW AMM 53-01-05-404-004 REV.1472. CONDITION CHECK NORMAL.SDR IXXA20260420002Skin · crackedCRACK FOUND AT FORWARD ENTRY DOOR CUT OUT AFT LOWER CORNER BETWEEN STA 340- STA 332 - 1" ABOVE S-20LSDR HNAA2026050500369Skin · corrodedCORROSION FOUND ON FUSELAGE SKIN UNDER TCAS ANTENNA AFTER ANTENNA REMOVAL. PERFORMED DOUBLER REPAIR ON FUSELAGE SKIN UNDER LOWER TCAS ANTENNA IAW EMB 145 SRM 53-00-23.SDR ASAA2026041965746Skin · damagedTRANSFERRED FROM MIG-2C #40-0085469, ITEM 4. POSSIBLE LIGHTINING STRIKE ON R/H UPPER FUSELAGE AT APPROXIMATELY STA 440. GROUNDED - YES. (RESOLVED ON W/O: 2099657 TASKCARD: N/R-00002 ) ACCOMPLISHED DOUBLER REPAIR PER B737-900ER SRM 53-00-01-2R-35. CATEGORY B RESDR VNAA202606060001Skin · damagedLIGHTNING STRIKE DAMAGE TO FUSELAGE SKINS BETWEEN FS234.00 - FS364.00 AND BETWEEN STR 20L - STR24L. REPAIRED PER REO 690-53-00-656 REV -A AND REO 690-53-21-2139 REV -.SDR IPXA2026042265192Skin · dentedDURING WALK AROUND INSPECTION FOUND DENT /HOLE IN FUSELAGE LEFT SIDE BELOW MAIN CARGO DOOR LEFT AND DOWN OF THE FORWARD STATIC PORT ABOUT STATION 478. CATEGORY B PERM SKIN REPAIR PERFORMED PER EO-97184-REQ1.SDR IPXA2026041865192Skin · dentedMAJOR REPAIR. DURING WALK AROUND INSPECTION FOUND DENT /HOLE IN FUSELAGE LEFT SIDE BELOW MAIN CARGO DOOR LEFT AND DOWN OF THE FORWARD STATIC PORT ABOUT STATION 478 FASTENERS REMOVED IN AREA OF REPAIR DOUBLER AND DAMAGED STRINGER REF SRM 51-40-02. DAMAGED SECSDR DALA2026042002463Repair · not reportedREMOVE EXISTING EXTERNAL REPAIR LOCATED BTWN FR1 AND FR3 STRG 34R AND RT LOWER STRG AND PERFORM VISUAL INSPECTION OF THE UNDERLYING STRUCTURE. REPAIRED R/H NOSE FWD FUSELAGE SKIN BETWEEN FRI-FR3 BETWEEN STRG -34R-36R I/A/W DELTA ER/A 633282-14AD REV: ORIGINAL SDR VNAA20260418022Skin · dentedTOOL MARKS AND DENTS ON SETTLEMENT AREA OF VENTRAL FIN FAIRINGS BTW FS 997 TO FS1162, STGRS 21LH-22LH AND BTW STRGS 21RH-22RH. REPAIRED PER PER REO 690-53-61-1762 REV. - - AND REO 690-53-61-1761 REV - -SDR VNAA20260418021Skin · dentedTOOL MARKS AND DENTS ON SETTLEMENT AREA OF VENTRAL FIN FAIRINGS BTW FS 1162 TO REAR SPAR DATUM 67.50%, STGRS 21LH-22LH AND BTW STRGS 21RH-22RH. TOOL MARKS AND DENTS ON SETTLEMENT AREA OF VENTRAL FIN FAIRINGS BTW FS 1162 TO REAR SPAR DATUM 67.50%, STGRS 21LH-SDR HNAA2026052000416Doubler · not reportedFUSELAGE EXTERNAL SKIN REPAIR DOUBLER BETWEEN FR 35/36 AT STR 1L HAS NO REPAIR INFORMATION. RE-ACCOMPLISHED DOUBLER REPAIR ON FUSELAGE EXTERNAL SKIN BETWEEN FR 35/36 AT STR 1L IAW ETD2026-145-007253-A AND EO1-53-26-0222.SDR IPXA2026050856714Skin · ground damageK-LOADER HAND RAIL STRUCK AIRCRAFT FWD OF CARGO DOOR 1. I.A.W AMM 25-53-03-404-030 REV.148 INSTALLED FORWARD CARGO BALL PANEL NEAR STA 511 RBL 33.SDR AALA202605053536Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AROUND LAVATORY VENT OPENING AT BS 917. REPAIRED SKIN. PER SRM 51-10-02-0G.SDR AALA202605057990Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AROUND DRAIN AT STATION AT BS 727A BETWEEN STR 26R AND 27R. REPAIRED SKIN. PER SRM 51-10-02-0G.SDR CALA2026050115920Skin · damagedRAMP REPORTS LD CONTAINER EMBEDDED INTO AIRCRAFTDAMAGE TO LEFT SIDE OF FUSELAGE BS 500 D-E, S18 -20R, IAW SRM 53-00-01-1A-5 FIGURE 101 . REMOVED FWD CARGO SIDEWALL LINER IAW AMM 25-52-06-000-801 PER AVO17236 ITEM 1 THRU 7 PERFORMED HFEC PER 737 NDT MANUAL PART
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