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 AALA202607289726Skin · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT SIDE OF FUSELAGE SKIN IS CRACKED AT EXTERNAL POWER SERVICE PANEL LOWER CUTOUT. MAINTENANCE REPAIR RH FUSELAGE SKIN AT EXTERNAL POWER IAW SRM 53-10-15-2R-4, REPAIR 4.SDR HNAA2026082400777Doubler · misinstalledUN RECORDED DOUBLER FOUND BTW FR 67-68 AND STR 4-5R. R & R DOUBLER IAW SRM 51-40-02 AND EO1-53-26-0361.SDR HNAA2026081900739Skin · corrodedREAR FUSE I FR61 STR19L CORRODED. REPAIRED IAW SRM 53-00-03SDR SCNA20260811345Skin · damagedFUSELAGE SKIN, BS 351 TO 380, S23R TO S25R, CORROSION AND SCRIBE LINE. PERFORMED ENGINEERING TASK CARD NUMBER ENG-53SCA-11906 N5479A FUSELAGE SKIN STA 351 TO 380 - S23R TO S25R CORROSION SCRIBE LINE REPAIR.SDR SWIA2026072076663Skin · 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 (MAJOR REPAIR).SDR SWIA2026072076662Skin · demodificationPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGE SKIN LOCATED BETWEEN BS 394 - 409, STR 13L - 14L DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (MAJOR REPAIR).SDR SWIA2026072076661Skin · demodificationPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE SKIN LOCATED BETWEEN BS 394 - 409, STR 13R - 14R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM ( MAJOR REPAIR).SDR SWIA2026072076660Skin · demodificationPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN BS 830.40 - 847, STRG 1L - 0 DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (MAJOR REPAIR).SDR R61A202607200194Skin · dentedMAJOR REPAIR, DENT ON PREVIOUS ANTENNA DOUBLER AREA CF111 FUSE LT BTWN FR 89-90 AND STGR 10L-11L. MX, DENT WAS REPAIRED IAR EMB ETD2026-170-011924 REV B. SEE AAR NRC 4502648-7000-0017.SDR IPXA2026080944430Skin · damagedPOSSIBLE LIGHTING STRIKE, TOP OF CROWN AT RT BS 1478 STR 4. INSTALLED FASTENER OF REPAIR IAW SRM 53-00-01-2R-6 AND SRM 51-40-02-0G-0.SDR KCSA2026071942Skin · damagedTAIL STRIKE ON GO AROUND. ACCOMPLISHED CONDITION INSPECTION IAW B777-300 AMM 05-51-32. REF E-50 19433 FOR CORRECTIVE ACTION & OPERATIONAL LIMITS. THIS AC HAS BEEN INSPECTED & FOUND TO BE SAFE FOR OPERATION & INTEND FERRY FLIGHT CKS-9778.SDR DALA2026072104278Doubler · damagedDAMAGE TO AFT CARGO DOOR JAMB DOUBLER. REPAIRED PER B717 SRM 53-20-15-2R. (1707868) AIRCRAFT GROUNDED.SDR DALA2026072104277Skin · damagedDAMAGE TO FUSELAGE SKIN. REPAIRED PER B717 SRM 53-20-15-2R. (1708438) AIRCRAFT GROUNDED.SDR DALA2026072004250Skin · damagedLEFT FUSELAGE APPROX FR34 - FR38 AND STR 34L - STR 33L HAS IMPACT DAMAGE.PERFORMED REPAIR TO SKIN AT FRAME 34 THROUGH FRAME 38 BETWEEN STRINGER 33 LEFT AND 34 LEFT IAW ER/A 635574-14, REV O. REPAIR IS LIFE LIMITED FOR 200 FLIGHT CYCLES AT THIS TIME. A/C OK FORSDR AALA202607204490Skin · bulgedAIRCRAFT WAS GROUNDED: SKIN BULGE ;OCATED AFT OF STA 360 BUTT JOINT ALONG STRINGER 23L THE BULGE MEASURES APPROXIMATELY 1.2" BY 1.1" WITH 0.05" PROTUSION. SKIN AND STRINGER REPAIRED (DOUBLER) PER EA 376958 AND SRM 53-30-01-1A-1, 53-30-01-0L-1.SDR CNMA2026080005Skin · dentedDENT BY L1 DOOR REQUIRES PERMANENT REPAIR AT NEXT C CHECK PER STS EA 124-2025-122 REV A, AND ECRA 26-0001.SDR DALA2026072404319Skin · scratchedSCRATCH FOUND OH RH FUSELAGE ON STA 325, BETWEEN STR30RH AND STR31RH. C/W WITH ER/A 635853-14 REV A (8762589)(AIRCRAFT GROUNDED)SDR DALA2026072004259Skin · crackedCRACKED FUSELAGE SKIN. REPAIRED PER ER/A 605226-14. (1705409) AIRCRAFT GROUNDED.SDR FDEA202607170944Skin · damagedFUSELAGE SKIN EXTERNAL SURFACE FOUND 1EA LIGHTNING STRIKE AT STA1109 - STA1131 STR10L - STR11L. REPAIRED THE DAMAGED FUSELAGE SKIN AT STA1109-STA1131 STGR10L-STGR11L PER B767 SRM53-00-01-2R REPAIR 1. MAJOR REPAIR IAW FEDEX GMM6-2-100.SDR DALA2026071804233Skin · dentedSKIN DENTED 20" AFT OF AFT CARGO DOOR OPENING 30" UP FROM CARGO DOOR OPENING. CAUSED BY CARGO LOADER. TRIMMED OUT DAMAGED AREA, FABRICATED DOUBLER AND TRIPLER, AND REPAIRED PER ER/A 635730-14. (LP 8814845, 1705270 - AIRCRAFT WAS GROUNDED)SDR SWIA2026071677778Skin · chafedRIGHT APRON SKIN CHAFED FROM UPPER WING SKIN AND STUB FAIRING CONTACT. REPAIRED RT APRON SKIN IAW SRM 51-42-06, REV 39, AND REO 601R-53-41-115, REV A.SDR DALA2026082504825Skin · corrodedERA 627451-14 REV B: MID FUSELAGE SKIN - FRAME 34-35, S36L-S36R - CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH SECTION II WITHIN 52,500 FLIGHT HOURS OR 30,000 FLIGHT CYCLES FROM TIME OF SECT. I REPAIR AT 15,269 FH AND 6,972 FC (WITHIN AIRCRASDR HNAA2026082400756Skin · crackedFUSELAGE EXTERNAL SKIN HAS A POSSIBLE CRACK AT AFT SIDE OF OXYGEN SERVICING DOOR, IN THE RH RVSM AREA. REMOVED CRACKED AREA OF FUSELAGE SKIN AT AFT EDGE OF OXYGEN SERVICING DOOR CUTOUT IAW ETD2026-145-012451 REV: A. FABRICATED, INSTALLED REPAIR DOUBLER AND FISDR SCNA20260814362Skin · damagedINITIAL INSPECTION: ELONGATED FASTENER HOLE ON EXTERNAL FUSELAGE SKIN BTW STA 500G/500H AND STGR S-25L/ S-24L - - ELONGATED FASTENER HOLE ON EXTERNAL FUSELAGE SKIN BTW STA 500G/-500H AND STGR S-25L/ S-24L WAS REPAIRED PER ETI-737-26-071 REV. 2, MM4-SCA-26-0024SDR CALA2026072017884Skin · ground damageWHILE SERVICING OXYGEN, LIFT TRUCK RAILING CAME INTO CONTACT WITH THE RT SIDE OF THE FUSELAGE AFT OF THE FWD CARGO DOOR. FOUND THE DENT BETWEEN STR 22 AND 23 RT, BS 657, DEPTH IS .105 INCHES; LENGTH IS 4 INCHES; WIDTH IS 3-28/32 INS IAW SRM 53-00-00 DENT ISDR CALA2026072017856Skin · dentedREF LOG PAGE #9623921 NEED TO COMPLY WITH AVO 17872. STEPS 1-6 WERE ACCOMPLISHED BY DAYSHIFT SHEETMETAL SEE PARENT LOG PAGE FOR SIGNOFF. STEP 7 THRU 10 REQUIRE HFEC INSPECTION. REF. AVO 17872, STEP 7 HFEC ONLY ACP. REF. 757 NDT PT6, 51-00-19. NO DEFECTS NOTEDSDR DALA2026071704221Skin · crackedFOUND STR 11 LT CRACKED APPROX BS 160 AND 3 SKIN CRACKS , 2 AT HOLE S4 AND 1 EMANATING FROM HOLE S3, COMPLIED WITH ER/A 633840-14. (1702209) (AIRCRAFT GROUNDED).SDR DALA2026071704215Skin · corrodedCORROSION ON WING BOX UPPER SKIN AREA BTW STA 716 TO 737 X=-44.5 TO X=-56.0, COMLIED WITH ER/A 634543-14AD. (1702309) (AIRCRAFT GROUNDED).SDR DALA2026071704214Doubler · corrodedCORROSION ON DOUBLER STA Y=1053 BTW LONG'S 29RH TO 29LH APROX LWR AREA AT AFT CARGO COMPARTMENT, REPLACED DOUBLER IAW SRM 51-41-05-0G AND SRM 51-41-02-0G. (1702152) (AIRCRAFT GROUNDED).SDR SIMA20260716001Skin · gougedDURING REMOVAL OF TCAS ANTENNA DOUBLER, FUSELAGE SKIN WAS GOUGED UNDER DOUBLER BETWEEN FR18 AND FR19. (MAJOR REPAIR). REPAIRED IAW ERS-EJ-53MR-5470.SDR JR2R20260716725Skin · not reportedFUSELAGE SKIN BEWTEEN FR11 - FR12 AND STR13L - STR15L. REPAIRSDR IPXA2026090880597Skin · dentedMAJOR REPAIR, UPPER FUSELAGE EXTERNAL SKIN EXISTING REPAIR TRIPLER HAS 4 EA DENTED, APPROX BTW BS 377 AND BS 395, STR 2L THRU STR 3L, INSTALLED NEW REPAIR DOUBLER, TRIPLER AND 3 EACH ORIGINAL FILLERS, AT UPPER FUSELAGE EXTERNAL SKIN APPROX BTW BS 377 & BS 39SDR HNAA2026081700729Doubler · damagedFRAMES 14 - 15, BTW STR 4 - 5L, LWR INNER DOUBLER HAD ELONGATED HOLE. REPAIRED IAW SRM 53-21-02.SDR VNAA202608010016Skin · dentedINITIAL INSPECTION: SEVERAL DENTS BELOW VENTRAL FIN FARING RH, LH AREA BTW FS 1069.75 - FS 1162.00 AND STGR 21 - 22 RH, LH AT REAR FUSELAGE. SEVERAL DENTS BELOW VENTRAL FIN FARING RH, LH AREA BTW FS 1069.75 - FS 1162.00 AND STGR 21 - 22 RH, LH AT REAR FUSELAGSDR CALA2026071617809Skin · damagedLIGHTNING STRIKE ON FASTNER AT STA 4546. 18.25 INCHES ABOVE STRINGER. PERFORMED MATERIAL LOSS MEASUREMENT INSP PER NTM TASK 51-10-04-270-802-A WITH REMAINING MATERIAL AT THINNEST IN BLENDED AREA AT 0.081 AND THICKNESS BARE METAL AREA AT 0.093. REMOVED LIGHTNSDR DALA2026081004594Skin · corrodedFWD LAV TANK EXHAUST PORT HAS CORROSION. REPAIRED FWD LAV EXHAUST PORT IAW SRM 53-60-01-2R-3 (8393110) (AIRCRAFT GROUNDED)SDR CALA2026080318232Skin · nickedNICK WAS FOUND OUT OF LIMITS ON FUSELAGE SKIN BETWEEN BS 500AD - 500E, STR 27R - 26R. PERFORMED REPAIR AT EXTERNAL FUSELAGE SKIN BETWEEN STA 500D 500E AND STR 27R / STR26R - ALL WORKS WERE ACCOMPLISHED IAW SRM 53-00-01-2R-1, SRM-51-20-01-0G-0,AMM 20-60-07-913SDR K11A2026071400382Skin · no discrepancyBIRD STRIKE UNDER R2 WINDOW. PERFORMED BIRD STRIKE CONDITIONAL INSPECTION IAW AMM 5-51-18. NO DEFECTS NOTED AT THIS TIME.SDR CALA2026083119104Skin · chafedEXTERNAL SKIN AT FR34, STR 43L AND STR 43R HAD CHAFE DAMAGE 14CM LONG X 2CM WIDE TO INCLUDE SIX DAMAGED FASTENERS. PERFORMED REWORK ON EXTERNAL SKIN AT FR34 BTWN STR 43L & STR 43R IAW EA 5300-02120, SRM 53-21-11-283-018. AS PER SRM 53-21-11-283-018, DAMAGE ISDR IPXA2026082645373Skin · damagedRIGHT FR 58, FWD FASTENER ROW, 6TH HOLE OTBD FROM STRINGER 4R HAD DAMAGE INDICATION OVER 100% FSH. ACCOMPLISH THE REPAIR IAW EO-98380-REQ1 AND EA 300-5316-27-A4573, REV-.SDR HNAA2026082400749Skin · crackedPOSSIBLE CRACK AROUND RIVET, AT FR 77 STGR 6L-7L. REPAIRED CRACKED SKIN AROUND RIVET AT FR 77 STGR 6L-7L IAW SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-26-0394.SDR HNAA2026082400748Skin · crackedPOSSIBLE CRACK AROUND RIVET, AT FR 77, STR 5L-6L. REPAIRED THE CRACKED SKIN AROUND RIVET AT FR 77, STR 5L-6L IAW SRM 53-32-01RE, ITEM 9, FIG 213, AND EO1-53-26-0394.SDR MASA20260807206Doubler · corrodedDURING HEAVY CHECK INSPECTIONS ON CFIII NTERNAL FUSELAGE, AFT WASTE SERVICE BOX INTERNAL DOUBLER HAS BEEN REPLACED IAW SRM 51-41-02 AND SRM 51-43-04. AAR YQG NRG 4502680-8000-0006.SDR SWAA2026071750882Skin · damagedFUSELAGE SKIN IS CREASED AND HAS SEVERAL SCRATCHES IN SKIN AT STA 927+9, 0.50" ABOVE STR 22L REPAIRED PER EA 26-153-01877 ON NRC TTG8Q01D63L2. REPAIRED PER EA 26-153-01877 ON NRC TTG8Q01D63L2SDR FDEA202607130923Skin · misrepairedEXISTING REPAIR ON FUSELAGE SKIN BETWEEN FR54.2-FR54.3,STGR46L-STGR49L REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE SKIN BETWEEN FR54.2-FR54.3,STGR46L-STGR49L. NO RECORD FOUND. REMOVED THE EXISTING REPAIR AND PERFORMED THE NEW REPAIR SDR JR2R20250713589Skin · dentedTHERE IS A DENT AROUND THE CUTOUT FROM AN UNUSED ANTENNA RISER DOUBLER BETWEEN FRAMES 82-83 AND STRINGERS 27L-28L. REPAIREDSDR SWIA2026071277739Skin · damagedDURING FRAME SECTOR REPLACEMENT ON BS 349 BETWEEN STR 23L AND 24L, FOUND MULTIPLE ELONGATED HOLES WITH SURROUNDING DENTS AND EVIDENCE ON PREVIOUS BLEND. PERFORMED CUT AWAY OF DAMAGE FROM FUSELAGE SKIN AT BS 349 BETWEEN S23L & S24L INSTALLED REPAIR DOUBLER ANDSDR REXA2026082401629Skin · corrodedCORROSION AND SCRATCHES AROUND OF SETTLEMENT AREA WERE FOUND. CORROSION AND SCRATCHES AROUND OF SETTLEMENT AREA WERE REPAIRED PER EA NO. CRJ953-22761 REV. IRSDR SWIA2026071177228Skin · repair malfunctnDURING ELECTROMAGNETIC DENT REMOVAL OF PRE-EXISTING HAIL DAMAGE, THE VENDOR EXPERIENCED EQUIPMENT MALFUNCTION RESULTING IN INDUCED DAMAGE TO THE FUSELAGE SKIN, A LARGE DENT WAS CREATED APPROX AFT OF BS 559.112 ABOVE STRINGER 10R DAMAGE WAS CAUSED DURING THE ASDR CALA2026072617992Skin · scratchedSCRATCHES ON RH ALTERNATE STATIC PORT (A-73). BLENDED AND EVALUATED SCRATCHES (2EA) ON RT ALTERNATE STATIC PORT. : BLEND NR 1. LOCATED BTW BS 433 AND 3.5" ABOVE S23R, ORIGINAL THICKNESS: 0.090" MATERIAL LOSS: 0.003" MATERIAL REMAINING: 0.087", BLEND NR 2 LOC
Back to JASC 5330