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 DALA2026091705190Skin · dentedNOSE FWD EXTERNAL FUSELAGE, AT FR11 BETWEEN -Z 88 AND -Z 263, L/ H SIDE, SKIN WITH DENTS. C/A: PERFORMED REPAIR AT FWD EXTERNAL FUSELAGE SKIN SECTION AT FR11 BETWEEN -Z 88 AND -Z 263 L/H SIDE AS PER DELTA ER/A NO 636719-14 REV ORIGINAL SECTION I PART A, PART BSDR DALA2026091705189Skin · scratchedNOSE FWD EXTERNAL FUSELAGE, AT FR10 -Z361 L/H SIDE, SKIN WITH SCRATCH. PERFORMED REPAIR AT FWD EXTERNAL FUSELAGE SKIN SECTION AT FR 10 -Z361 LH SIDE AS PER DELTA ER/A NO. 636719-14 REV ORIGINAL SECTION I PART A, PART B STEP 15, 19 AND 20, DATED 11-SEP-26. NOTSDR DALA2026092305314Skin · crackedFOUND CRACK AT FUSELAGE RIGHT SKIN Y=1076, BETWEEN LONGERON 13R AND 14R, COMPLIED WITH ER/A 636937-14. (1816724) (AIRCRAFT GROUNDED).SDR 9WGA2026091654684Skin · corrodedCENTER WING UPPER PANEL CORRODED AT LH AFT OF STRINGER #1 SPLICE BETWEEN LBL 84 AND LBL 98.SDR DALA2026091605173Skin · crackedCRACK INDICATIONS IN HOLES 3 AND 5 AT FRAME 37 AND AT HOLES 11, 15 AND 24 AT FRAME 37.4. REPAIRED PER ERA 588739-14 REV A. (1814571) AIRCRAFT WAS GROUNDED.SDR CALA2026091619480Skin · canningWHILE PERFORMING EA4435-04714 OP 005, RADOME AND CROWN MODIFICATION (RADOME OFF), FOUND SKIN OIL CANNING AT FR 727D TO 727E. COMPLETED ESFR FOR LOG PAGE 3333068 REF STS N0010 - REPAIR ACCOMPLISHED PER EC/RA 5360-02210 REVIEWED REPAIR DOCUMENTATION EC/RA 5360SDR JR2R20260915557Doubler · corrodedLAV WASTE SERVICE BOX AREA SKIN DOUBLER IS CORRODED. REPAIRED PER SRM.SDR 1Q2R2026091450062Skin · dentedFUSELAGE SKIN DENT FS 497 AND S17L .SDR CALA2026092819929Skin · ground damageDENT BELOW FORWARD CARGO DOOR DUE TO BELT LOADER CONTACT. DENT EVALUATED PER SRM 53-21-11-283-020. DENT MEASURES 2.5" LONG AND 1" WIDE 1" FWD OF FR 27 BTWN STRINGERS 42-43R WITH A MAX DEPTH OF 0.015". DENT IS TYPE 1 & LOCATED IN ZONE 1, FIGURE 7 & AREA 1, FSDR DALA2026091805213Skin · crackedCRACKS FOUND AFFECTING THE SKIN BETWEEN L-L2 AND L-L3 AT APPROXIMATELY STA Y=1133, COMPLIED WITH ER/A 636735-14. (1810811) (AIRCRAFT GROUNDED).SDR DALA2026091405130Skin · crackedLEFT FUSELAGE SKIN CRACKS. REPAIRED PER ERA 636735-14AD. (1810803) AIRCRAFT WAS GROUNDED.SDR DALA2026091405129Skin · crackedCRACK ON EXTERNAL SKIN STA Y=1133 BTW LONG 2LH. CORRECTIVE ACTION: REPAIRED PER ER/A 636735-14AD. (1811500) AIRCRAFT WAS GROUNDED.SDR IPXA2026102318112Skin · dentedAGING A/C INSPECTION DENT NOTED JUST AFT OF THE NOSE WHEEL IN THE VICINITY BS 324 STR ATA 51-00, PER STE-SAA EA 757-5310-01-B0844,P1 STEP 31. ACCOMPLISH THE REPAIR PER EO-98933-REQ1 AND EA 757-5310-01-B0844, REV. I/R PRIOR TO FURTHER FLIGHT.SDR IPXA2026102217366Skin · bulgedAGING A/C INSPECTION A BULGE WAS NOTED BELOW THE LH FIXED COCKPIT WINDOW OF BS 255. EVALUATED BULDGE AT LH STA 255 WL 200, FOUND TO BE DENT. MEASURED DENT, LENGTH: 3.535" WIDTH: 3.517" DEPTH: 0.045" FOUND TO BE OUT OF LIMITS DUE TO OVERLAPPING WITH FRAME IAW SDR DALA2026092105250Skin · corrodedCORROSION DAMAGE WAS FOUND AROUND THE LAVATORY VENT LOCATED BETWEEN FR 69 AND FR 70, AT STRG 31RH AND STRG 32RH. REWORKED BY BLENDING THE CORRODED AREA AROUND THE LAV VENT AREA PER A320 SRM 53-41-11-101, SUBSECTION 53-41-11-283-065 FOR FR64- FR70. THE REMOVEDSDR SIMA20260912001Skin · dentedDURING RE-CONTOURING OF 2 DENTS FOR TDMI786T5322 (NON-ROUTINE #F144316) DAMAGE OCCURRED TO FUSELAGE SKIN BETWEEN FR5-6, STRG'S 10R & 12R (PROTRUSION SKIN DENT). (MAJOR REPAIR) NOT AN SSI ITEM. REPAIRED IAW ERS-EJ-53MR-5532.SDR DALA2026091305112Skin · corrodedLEVEL 2 CORROSION, LOWER FUSELAGE AFT CARGO COMPARTMENT FROM FR56 TO FR 57 BETWEEN STRG-42L AND STRG-43L AFT ATG4 ANTENNA INTERNAL DOUBLER WITH CORROSION. PERFORMED REPAIR AT LOWER FUSELAGE AFT CARGO COMPARTMENT SKIN PANEL SECTION FROM FR 56 TO FR 57, BETWEENSDR SWAA2026102197527Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 193AR AT LOWER FUSELAGE. THE REPAIR REFERENCE OF PRE PREG SEND TO THE WET LAY UP REPAIR FOR THAT REASON WAS DOCUMENTED BOTH ON STEPS 3 AND 4. REPAIRED ACCESS PANEL 193AR AT LOWER FUSELAGE IAW SRM 51-70-05-2R-9 REPAIR 9.SDR CALA2026092819861Skin · corrodedWASTE PAN SHOWS SIGNS OF POSSIBLE CORROSION. SKIN BULGING AROUND FASTENERS AND MISSING AREAS OF FILLET SEALANT. PERFORM THE REPAIR TO THE AREA OF SKIN IAW ECRA 5360-02202.SDR DALA2026091705193Skin · damagedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR FUSELAGE SKIN R EPAIR AT FR11LH, -Z88 & -Z263 PER ER/A 636719-14. C/A: SECTION I IS LIMITED TO SOONER OF 60000FC OR 120000FH. ER/A TO B E REVISED PRIOR TO THIS DATE ELSE REMOVE A/C FROM SERVICE. . (LP: 1807237,SDR DALA2026091505149Skin · corrodedWHILE PERFORMING REP INSPECTION PER ER/A 612524-14 REV C. FOUND CORROSION ON SKIN FWD OF WASTE PNL. BLENDED SKIN MINIMUM AMOUNT TO REMOVE CORROSION IAW ASRP 51 -21. .25" X 2.5" GRIDED OUT OF BLENDED AREA (127702). REQUESTING UT OF BLENDED AREA (127702). ACCOMPSDR CALA2026091419406Skin · dentedFUSELAGE SKIN AT LOWER PORTION OF EXTERNAL POWER DOOR CUTOUT IS DAMAGED. REPAIRED FUSELAGE SKIN AT LOWER PORTION OF EXTERNAL POWER DOOR CUTOUT ALL WORK DONE IAW SRM 53-10-15-2R-4 THIS REPAIR IS CATEGORY A REPAIR NO FOLLOW ACTION REQUIRE. REPAIRED FUSELAGESDR VNAA2026091129Doubler · corrodedFWD CARGO DOOR LOWER SILL -H- DOUBLER IS CORRODED AT FS 533. REMOVED AND REPLACED THE DOUBLER IAW SRMS 51-42-21-001-001-A01, 51-42-27-001-001-A01, AND 51-40-11-001-001-A01.SDR SWAA2026100702039Skin · corrodedCORROSION ON EXTERNAL SKIN AROUND DRAIN, BS 967 4 INCHES ON LOWER FUSELAGE. EVALUATED CORRODED AREA AND FOUND WITHIN LIMITS IAW SRM 53-00-01-1A-1, ALLOWABLE DAMAGE 1, PARAGRAPH 4.B(2)(D), FIGURE 103 SHEET 1, DETAIL C.SDR SWIA2026091077384Skin · mechanic errorMIS-DRILL CONDITION HAS OCCURRED DURING STARLINK WIFI ANTENNA TRAY FWD DOUBLER INSTALLATION AT UPPER FUSELAGE SKIN FS 437 BETWEEN STR 2R AND STR 2L DAMAGE DETERMINED TO BE A MAJOR REPAIR. INSTALLED PERMANENT REPAIR DOUBLER INSTALLATION AT UPPER FUSELAGE SKIN SDR DALA2026091605179Skin · corrodedER/A 612524-14 SECTION VII TIME LIMITED REPAIR VI WAS ISSUED FOR CORROSION FOUND ON THE FUSELAGE EXTERIOR SURFACE ADJACENT TO THE WASTE SERVICE CUTOUT, DURING SECTION V REPEAT INSPECTIONS PER LOG PAGE 0678171. CURRENT REV IS 'D'. ACCOMPLISH SECTION VIII REPEATSDR DALA2026091305105Skin · damagedER/A 636728-14 IS ISSUED FOR FUSELAGE SKIN REPAIR INSTALLED AT F R56/57, S42/43LH WHICH WAS INSTALLED PER SRM 53-00-11-300-013. F OLLOW ON ACTION IS REQUIRED. SECTION II, AS REQUIRED IAW SRI 53-00-11-205-035, REQUIRED PRIOR TO SOONER OF 33600FC OR 67200FH & ESDR SWIA2026091077126Skin · demodificationPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RT FWD FUSLEAGE SKIN LOCATED BETWEEN BS 394 - 409, STR 13R - 14R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO RT FWD FUSLESDR SWIA2026091077125Skin · demodificationPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LT FWD FUSLEAGE SKIN LOCATED BETWEEN BS 394 - 409, STR 13L - 14L DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO LT FWD FUSSDR SWIA2026091077124Skin · demodificationPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN BS 1000 - 1015, STR 25R - 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOSDR SWIA2026091077123Skin · demodificationPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN BS 581 - 597, STR 24R - 25R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCASDR DALA2026091105094Skin · damagedLIGHTNING STRIKE EXTERNAL FUSELAGE SKIN APPROX ST 350LT WL 208.1. COMPLIED WITH PERMEANT REPAIR ON THE LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN STA 35 L/H WL 208.1 & APPLIED DENT DOT IAW ERA 636856.14 REV. (1805779) AIRCRAFT WAS GROUNDEDSDR VNAA202610230056Skin Panel · burnedFUSELAGE LIGHTNING STRIKE DAMAGE, FS169.00 TO FS1162.00 REPAIRS PERMANENT REPAIR (APPLICABLE TO RIVETS DIAMETER 4 AND 5 ONLY). THIS TEMPORARY REPAIR IS VALID FOR 8000 FLIGHT HOURS OR UNTIL THE NEXT SCHEDULED HEAVY MAINTENANCE CHECK (WHICHEVER COMES FIRST). LSDR SWAA2026100509361Skin · crackedPOSSIBLE CRACK AT BS 780, STR 1. C\W 26-153-02475. REPAIRED THE FUSELAGE SKIN, BTW BS 767 & 787, BELOW S-1.SDR SWIA2026090977116Skin · demodificationPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN BS 830.40 - 847 AND STR 1L - 0 DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLSDR SWIA2026090977115Skin · demodificationPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RT FWD FUSLEAGE SKIN LOCATED BETWEEN BS 394 - 409 AND STR 13R - 14R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSDR SWIA2026090977114Skin · demodificationPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LT FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394 - 409 AND STR 13L - 14L DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO LT FWD FUSSDR SWIA2026090977113Skin · demodificationPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN BS 1000 - 1015 AND STG 25R - 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN ISDR SWIA2026090977112Skin · demodificationPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN BS 581- 597 AND STG 24R - 25R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM, DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN IAWSDR DALA2026091005067Skin · damagedUPPER FUSELAGE FROM FR 29 TO FR 30 BETWEEN STRG 1L TO STGR 1R PCS/TIMING ANTENNA AREA BELOW COVER PLATE WITH SCRATCHES. PERFORMED PERMANENT MAJOR REPAIR AT FWD UPPER FUSELAGE SKIN SECTION AROUND PCS/TIMING ANTENNA BETWEEN FR 29 AND FR 30 AT STGR 1L - 1R I.A.WSDR 2026FA0000687Skin · damagedAT ITS ARRIVAL IN GUATEMALA, DAMAGE ON THE FUSELAGE WAS DETECTED UN WALK AROUND CHECK. SKIN SEEMED TO BE SEVERLY DAMAGE. AFTER INSPECTION FOUND SEVERAL FRAMES AND STRINGERS DAMAGED, BENT OR BROKEN. ALSO THE SKINS HAS SEVERAL CRACKS. STATION 350 TO 360 STRINGERSDR KCSA202609091206Skin · damagedFOUND LIGHTNING STRIKE DAMAGES ON THE UPPER FUSELAGE AREA BS 600 S-0 TO S-1L ( 2 SPOTS).SDR KCSA202609091205Skin · damagedFOUND A LIGHTNING STRIKE DAMAGE ON THE UPPER FUSELAGE AREA. STA 680 TO 700, S-0 TO S-1RSDR SWAA2026091494051Skin · crackedEXTERNAL FUSELAGE CHEM-MILL SKIN INSPECTION A CRACK INDICATION WAS OBSERVED AT BS 780 AT STR 1. AT OVER 65% FULL SCREEN HEIGHT (FSH). WITH PAINT REMOVED THE INDICATION WAS CONSISTENT AND REPEATABLE AT OVER 70% FSH AND THEREFORE REJECTABLE PER NDT MANUAL PART SDR CALA2026091019365Skin · dentedUPON WALK AROUND FOUND SMALL DENT ON RT LOWER HALF FUSELAGE BETWEEN BS 500E & 500F. FOUND DENT TO BE .8 INCH BY .7 INCH WIDE AND .063 INCH DEEP, W/Y 11.11 UNDER THE REQUIRED 30 OR OVER, PER SRM 53-00-01-1A-1. ON BS 500E TO 500D,STRINGER S-21R , S-22R. FOUND DSDR DALA2026091005065Skin · damagedER/A 636530-14 ISSUED FOR SKIN REPAIR INSTALLED BETWEEN FR29 & F R30, S1 LH & RH. PERFORM SECTION II THE SOONER OF 30600FC/61200FH AFTER SECTION I AND EVERY SOONER OF 1200FC/2400FH THEREAFTER. ASSOCIATED ER/A 00-636530 ADDED FOR AC 3253. (LP: 1801765, AIRCRAFSDR LR7A2026090603901Skin · damagedDURING SCHEDULED FLIGHT AND SUBSEQUENT INSPECTION, FOUND DAMAGED SKIN AND MISSING RIVER HEADS JUST FORWARD OF THE BELLY BUMPER ASSEMBLY DUE TO TAIL STRIKE / REPAIR IN WORK.SDR YENA2026091000746Skin · not reportedDURING HEAVY MAINTENANCE, WEIGHT VARIANT UPGRADE - SRM REPAIR SURVEY, DEFECTS 153 6503, 7265500087; (RESOLVED ON W/O: 1474396 TASKCARD: NR-00037 ) PERFORMED PERMANENT REPAIR LOCATED ON LOWER FUSELAGE AT FR68 PLUS 14 INCH AND BTW STR42L TO STR43L, THIS REPAIRSDR YENA2026091000743Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION TRAILING EDGE AREA LOCATED OVERHANG BTW RIB 8 TO RIB 9 ON LT WING; (RESOLVED ON W/O: 1474396 TASKCARD: NR-00048 ) REF AEROMAN 2026-252/1, NR 354594, ACCOMPLISH REPAIR OF CORROSION DAMAGES AFFECTING THE LT WING TOP SKIN PANESDR YENA2026091000741Skin · corrodedDURING HEAVY MAINTENANCE, AFT FUSELAGE, FR56-61 & STGR 37L-38L CORRODED. PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR A26-610-01)
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