JASC 5330
Service difficulty reports · 79,312
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 SWIA2025110700005Skin · damagedLIGHTNING STRIKE DAMAGE TO LOCK FASTENER LOCATED AT STRG 25 AND FR 11 FOUND LOCK FASTENER WITH INTERFACE DAMAGE AT STRG 25 AND FR 11. COMPLIED WITH FREEZE PLUG INSTALLATION IAW SRM 51-10-07 AND ETD2025-170-930286 REV.SDR DALA2025102007645Skin · corrodedSHIP 1812 AFT CARGO COMPARTMENT FOUND DRAIN HOLE AREA CORROSION AT BS 1087 BETWEEN S39R AND 39L. THE PRI629503-14 REV.0 COMPARED AND COMPLIED WITH (1253239)SDR FDEA202510152010Skin · crackedDURING PERFORMANCE OF WORK CARD: E G-5710-E0376285E, P12, STEP 3.B.(1), STEP 5.A.(2), & FOUND TWO CRACKS AT HOLE NR 5 OF RT UPPER WING SKIN COMMON TO FASTENERS 0-5. RT WING UPPER WING SKIN REPAIRED IAW SRM 51-40-05-0G, SRM 51-40-02-0G, SRM 51-40-04-0G, REV 51,SDR FDEA202510152009Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285E P11 STEP 3.B.(1)&STEP 5.A.(2) AND FOUND TWO CRACKS AT HOLE #5 OF LH UPPER WING SKIN COMMON TO FASTENERS 0-5. LH WING UPPER SKIN TRAILING EDGE #5 HOLE CRACK REPAIRED AS PER B777 SRM 51-50-02-0G, SRM 51-40-02-0G, SRSDR HNAA2025112000771Skin · crackedPOSSIBLE SKIN CRACK AT RIVET ON LH REAR FUSELAGE 2 AT FR 79, STGR 3L-4L. ACCOMPLISHED SKIN BUSHING REPAIR AT RIVET ON LH REAR FUSELAGE 2 AT FR 79 BETWEEN STGR 3L-4L IAW EMB145 SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-25-0396.SDR JR2R20251014077Skin · dentedPROTRUDING DENT ON FUSELAGE AFT OF FR85 AND IN BETWEEN STR25R AND STR26R. REPAIRSDR VNAA20251014019Skin · corrodedFUSELAGE EXTERNAL SKIN IS CORRODED BETWEEN F.S. 501 TO F.S. 503 STGR 26R TO STGR 26L. REPAIRED CORRODED AREA OF FUSELAGE EXTERNAL BELLY SKIN IAW MHIRJ REO 670-53-31-993 REV..SDR DALA2025101407502Skin · gougedSHIP 3314 FUSELAGE SKIN FOUND GOUGE ON FR 35A STGR 23 RH TO STGR 24 RH. CORRECTIVE ACTION: REPAIRED PER A330 SRM 53-21-11-283-005. OK FOR SERVICE. (1251305)SDR SWIA2025101375776Skin · corrodedCORROSION FOUND ON SKIN @ R1 DOOR SKIN CUTOUT 2 INCHES BELOW LWR EDGE (C-CHECK RO 04/17/2026)BLENDED OUT CORROSION IN DICREPANT AREA. AREA WAS BLESSED WITHIN LIMITS AS PER MHIRJ REO 690-53-21-2046 REV. -- DATED: 2025-11-04. COMPLIED WITH ALL STEPS OF REO. SEESDR AALA202510236114Skin · wornAIRCRAFT IN BASE MAINTENANCE: WEAR TO UPPER FUSELAGE CROWN SKIN AT BS 847, S1. ACCOMPLISHED REPAIR PER SRM 53-00-01-2R-35 AND EA 368897.SDR DALA2025101507523Skin · dentedLOWER FUSELAGE SKIN DENTED BETEWEEN FRAME 35.3 AND FRAME 35.4 STGR 44 AND 43L. EVALUATED AND REPAIRED FUSELAGE SKIN DENTED AREA LOCATED BETWEEN FR35.3 AND 35.4 STGR 44 AND 43L IAW A321-200 SRM 53-21-11-283-022 AND 53-21-11-300-036, REPAIR CAT B. (LP 1250149)SDR SWIA2025101275775Skin · crackedRIGHT FUSELAGE ADG SKIN HAS POSSIBLE CRACK AT AFT LOWER CORNER OF TRU BAY DOOR OPENING (C-CHECK RO 04/17/2026)REMOVED AND REPLACED ADG SKIN AT RH FUSELAGE IN REF. TO CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6.B, 51-42-13-001-001-A01 PAR. 6.B AND REO #690-53-11-SDR R61A2025111500503Skin · dentedJET BRIDGE DAMAGE CAUSED DENT TO LOWER LH FUSELAGE. AIRCRAFT WAS FERRIED TO EAMS BNA. REMOVED AND REPLACED LH FUSELAGE SKIN FR9-12. STGR 8L-19L PER SRM 51-40-08.SDR CALA2025110410884Skin · corrodedCORROSION AND SMALL HOLE AT LOWER FUSELAGE SKIN AROUND BS 965 B. ACCOMPLISHED REPAIR OF LOWER FUSELAGE SKIN BETWEEN STA 947.5 AND 967 AT STR 27L-27R AS PER SRM 53-00-01-2R-3 AND ECRA 5370-01202,SDR R61A2025101300432Skin · dentedDENT ON LH SIDE OF FUSELAGE AT FRA 80 BETWEEN STR 22L AND 23L. REPAIRED USING FILLER,DOUBLER AND TRIPLER IAW EMB ETD2025-170-927669 REV A. ALSO REF VP-043665-2025 N/R #1 FOR WORK ACCOMPLISHED.SDR KCSA202510111184Skin · damagedPOSSIBLE LIGHTNING STRIKE STA 550 L/H SIDE BETWEEN S-7L AND S-6LSDR SWIA20251110001Skin · chafedAFTER REMOVAL OF L/H WING AUX SPAR FOUND FUSELAGE APRON SKIN CHAFED. REPAIRED THE LH APRON SKIN PANEL ASSY PER REO 601R-53-41-115 REV A.SDR SWAA2025110327427Skin · puncturedHOLE IN FUSELAGE SKIN, BS 188 STR 23-24R. FWD EDGE OF THE PART [4] STRUCTURAL FILLER IS 2.5 INCHES FROM NEAREST ROW OF STA 178 BUTT SPLICE. MINIMUM 3.00 INCHES REQUIRED IAW SRM 53-10-01-2R-8 FIGURE 202, FLAGNOTE 8. SEE STEP 15. OUTER RIVET ROWS HAVE BBAD RIVSDR DALA2025101507545Skin · crackedOPEN HOLE HFEC INSPECTION PERFORMED ON THE ALL FASTENNER HOLE(5 EA) AT THE FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER, FOUND CRACK ON THE NO.4 HOLE,THE CRACK AT 12:00 O'CLOCK DIRECTION. REPAIRED IAW B767-400 SRM53-10-01 (1244345)SDR DALA2025101307467Skin · damagedLIGHTNING STRIKE STA 500L BETWEEN STR 2R AND 3R. C/W ER/A 629736-14 REV ORIG.SDR DALA2025101307466Skin · damagedLIGHTNING STRIKE BETWEEN STA 500C AND STA 500D JUST ABOVE STR 3R. C/W ER/A 629735-14 REV ORIG.SDR DALA2025101307465Skin · damagedLIGHTNING STRIKE BETWEEN STA 360 AND STA 380 JUST BELOW STR 3R. C/W ER/A 629728-14 REV ORIG.SDR KCSA202510101183Skin · damagedFASTENER DAMAGED ON TOP OF UPPER FUSELAGE EXTERIOR AT S-2 L, APPROX STA 697SDR KCSA202510101181Skin · damagedLIGHTNING STRIKE DAMAGE ON THE FUSELAGE SKIN LAP SEAM EXTERNAL SURFACE AT STATION 2072 AT STRINGER 5LSDR KCSA202510101179Skin · damagedLIGHTNING STRIKE DAMAGE FOUND ON TOP OF UPPER FUSELAGE AT S-1L APPROX STA 772.SDR KCSA202510101178Skin · damagedR/H LOWER FUSELAGE APPROX STA 1951 APPROX STRINGER 42 EXTERNAL SKIN HAS EVIDENCE OF LIGHTNING STRIKESDR JR2R20251010082Skin · dentedDENT ON FUSELAGE FWD OF FR83 AND BETWEEN STRINGERS 29L AND 20L. REPAIREDSDR DALA2026100805571Skin · dentedWHILE ACOMPLISHING A ZONAL INSPECTION, FUSELAGE CROWN SKIN DENTS AT BS 727E TO 727G AND S3L TO S3R. REF ERA 629296-14. (1243111) AIRCRAFT WAS GROUNDED.SDR U2RA2025110300024Skin · damagedAIRCRAFT SUSTAINED GROUND DAMAGE TO THE LOWER FUSELAGE SKIN, FORWARD OF THE FORWARD LOWER CARGO DOOR, STA 539.125, BETWEEN STRINGERS S-33R AND S-34R, MEASURING 3.875" LONG AND STA 574.750 BETWEEN STRINGERS S-33R AND S-34R MEASURING 4.875" LONG - ACCOMPLISHED CSDR SIMA20251009003Skin · corrodedAFT CARGO COMPARTMENT SKIN PANEL HAS CORROSION AT FRAME 80-81 STR27R. (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED CORROSION ON CENTER FUSELAGE III SKIN LOCATED BETWEEN FR80 AND FR81, STR25R AND STR26R REF EMBRAER 175 SRM 51-10-03. BLENDED AREA MEASURES L= 1.25"SDR DALA2025101007402Skin · damagedWHILE IN ATL, MTC IS ADDRESSING LIGHTNING STRIKE DAMAGES TO THE CROWN SKIN FUSELAGE OF THE AIRCRAFT. THERE ARE A TOTAL OF FIVE (5) LIGHTING STRIKE LOCATIONS FOUND BETWEEN STR 2R 3R AND STA 380-787. MAINTENANCE REPAIRED DAMAGE PER ERA 629735-14, 629736-14 ANDSDR DALA2025101007400Skin · corrodedCORROSION ON INB SKIN FUSELAGE AND DOUBLER SUPPORT(NATS AIRPHONE ANTENNA) STA 747,STA 757 AND STA 797 BTWN S27L TO 27R (BILGIE AREA) CARGO COMPARMENT C2.SDR DALA2025101007399Skin · dentedTHREE DENTS BETWEEN STA 727F+7 TO 727E AND S2R - S3R, ALSO 8 DENTS BTW STA 727E +15 TO 727G STGR 2L/3L AT EXTERNAL FUSELAGE SKIN. FUSELAGE SKIN (VIASAT) BTW STA 727E TO 727G STGR 3L/3R WAS REPAIRED PER PRI 629345-14 REV 0 TO 4 AND ERA 629345-14AD REV. ORIGINALSDR DALA2025101007398Skin · dentedTHREE DENTS BETWEEN STA 727F+7 TO 727E AND S2R - S3R. FUSELAGE SKIN BTW STA 727E TO 727G STGR 3L /3R WAS REPAIRED PER PRI 629296-14 REV 0 TO 3 AND ERA 629296-14AD REV. A.SDR CALA2025101009904Skin · nickedRT FUSELAGE AT FWD FIRST OFFICER STATIC PORT HAS SURFACE SC RATCHES. WORKED PER UAL ECRA 5330-07628, REWORKED R/FUS FWD FIRST OFFICER STATIC PORT, NO DEVIATIONS'SDR IXXA20251009003Skin · corrodedAFT CARGO COMPARTMENT AFT OF BULHEAD STA 1087-1109 STRINGER SKIN FOUND CORROSIONSDR SWAA2025102822826Tail Cone · delaminatedDELAMINATED TAIL CONE RIGHT SIDE ON EXTERNAL SKIN. REPAIRED TAIL CONE RIGHT SIDE ON EXTERNAL SKIN IAW SRM 51-70-04-2R-1, REPAIR 1.SDR CALA2025101309988Skin · dentedRAMP CREW NOTIFIED MX TECH ON DEPARTURE UPON REMOVING JETWAY DISCOVERED DENT AFT OF L1 DOOR. DENT MEASURES 4.0" WIDTH X .150" DEPTH. OUT OF SRM LIMITS. LOCATION BS 380 AND STRINGER 13L. ACCOMPLISHED INTERIM REPAIR TO FUSELAGE WINDOW BELT SKIN BS 360 -400, SSDR YENA2025100901016Skin · damagedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / RHS SKIN PANEL AT FR63 - FR64 AND STGR40R STGR42R / DENTS AND GOUGES - TIME-LIMITED REPAIR; REFERENCES: /1/ DAMAGE REPORT, MAPPING, AND REQUEST /2/ SRM TASK 53-41-11-283-024 - ADL /3/ AIRBUS DOSSIER 81653487SDR DALA2025100907368Skin · ground damageFOUND GROUND DAMAGE AT FR13 AND APPROXIMATELY 12 INCHES ABOVE LAP JOINT. COMPLIED WITH ER/A 628891-14. (1241211).SDR DALA2025100907362Skin · puncturedFOUND PUNCTURE AT FR13 AND APPROXIMATELY 12 INCHES ABOVE LAP JOINT. COMPLIED WITH ER/A 628891-14. (1241292).SDR CALA2025100909854Skin · nickedRIGHT FUSELAGE AT FWD ALTERNATE STATIC PORT HAS SEVERAL SMALL NICKS. REWORKED RT FUSELAGE FWD AITERNATE STATIC PORT.SDR N6WA2025100901Skin · gougedGOUGES ON LOWER SKIN AT FS977.00 STGR27. PERFORMED SKIN REPAIR AND DOUBLER ON LOWER SKIN AT FS 969.99 - 985 IAW EO-C550-53MR-091.SDR WX0A2025101332598Skin · dented(AIRCRAFT NOT GROUNDED) MAJOR REPAIR REF.NR-00009, FOR DENT ON UPPER AFT FUSELAGE, LOG PAGE 2050750, MDDR 215213, DENT ON UPPER AFT FUSELAGE SKLN BTW FR8 L-82 AND BTW STGR 1 AND 2L PERMANENTLY REPAIRED AS PER SRM 53-51-11-300-002 REV. I 54. REPAIR CATEGORY A,SDR N6WA2025100801Skin · corrodedCORROSION ON SKIN BETWEEN STGR25L-26L. COMPLETED SKIN REPAIR BETWEEN STGR25L-26L IAW EO-C550-53MR-094SDR CALA2025100809797Skin · nickedFUSELAGE ALTERNATE LEFT STATIC PORT HAS EVIDENCE OF CORROSION . WORKED PER ECRA 5330-07627.SDR DALA2025100707279Skin · ground damageFOUND GROUND DAMAGE AT FR13 AND APPROXIMATELY 12 INCHES ABOVE LAP JOINT. COMPLIED WITH ER/A 628891-14. (1238415).SDR DALA2025100707297Skin · corroded(LOG 1237864) CORROSION ON CUT OUT OF FUSELAGE SKIN UNDER PAN (VACCUM WASTE TANK) BTW STA 847 TO 867 AND STGR 23LH-25LH AT AFT CARGO COMPARTMENT.SDR EE4Y2025100623291Skin · damagedAZORRA REPORTS THAT DURING THE STRUCTURE INSPECTION, WE FOUND THE CENTER FUSELAGE I – AT FR31+380MM, S-26R+30MM EXTERNAL SKIN WITH LIGHTNING STRIKE. THE DAMAGE WAS REMOVED BY DRILLING A HOLE (Ø4.0MM). THIS CONDITION WAS REPORTED AND REPAIRED IAW ETD2025-190-92SDR EE4Y2025100623290Skin · damagedAZORRA REPORTS THAT DURING THE STRUCTURE INSPECTION, WAS FOUND THE CENTER FUSELAGE I – AT FR27+370MM, S-26R+60MM EXTERNAL SKIN WITH LIGHTNING STRIKE. THE DAMAGE WAS REMOVED BY DRILLING A HOLE (Ø4.0MM). DURING THE DOCUMENT CLOSING PROCESS, THE DAMAGE WAS LOCATE
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