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 SWAA2026052694954Skin · crackedFUSELAGE HAS A .72 VERTICAL CRACK AT BS 727E APPROX. 3 ABOVE STR 14R. VERIFIED WITH HFEC PER NDT PART6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRANT INSPECTION PER SOPM 20-20-02. C\W 26-153-01211.SDR SWAA2026052694660Skin · crackedSUSPECTED CRACK AT BS727A AND APPROX 3IN ABOVE S14R. REQUEST TO HAVE PAINT REMOVED TO VERIFY. REMOVED PAINT FROM BS727A APPROX 3 IN ABOVE STR14R<BR>REF AMM 51-21-11. COMPLIED WITH HFEC INSPECTION PER NDT PART 6, 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRASDR SWAA2026052694661Skin · crackedSUSPECTED CRACK AT BS727B AND APPROX 3IN ABOVE STR14R. REQUEST TO HAVE PAINT REMOVED TO VERIFY. REMOVED THE PAINT AT BS727B AND APPROX 3IN ABOVE STR14R REF AMM 51-21-11. COMPLIED WITH HFEC INSPECTION PER NDT PART 6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PESDR SWAA2026052694663Skin · crackedSUSPECTED CRACK AT BS 727D AND APPROX 3IN ABOVE S14R. REMOVED THE PAINT AT BS727D AND APPROX 3IN ABOVE STR14R REF AMM 51-21-11. COMPLIED WITH HFEC INSPECTION PER NDT PART 6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRANT INSPECTION IAW AMM 70-40-01; VERIFIESDR SWAA2026052694664Skin · crackedSUSPECTED CRACK AT BS 727E AND APPROX 3IN ABOVE S14R. REQUEST TO HAVE PAINT REMOVED TO VERIFY. REMOVED THE PAINT AT BS727E AND APPROX. 3IN ABOVE STR14R REF AMM 51-21-11. COMPLIED WITH HFEC INSPECTION PER NDT PART 6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENESDR DALA2026050202781Skin · ground damageAIRCRAFT SUSTAINED GROUND IMPACT DAMAGE DURING REPOSITIONING, RESULTING IN A DENT TO THE LH LOWER LATERAL SKIN PANEL AT FRAME 17LH S33L. TRIMMED OUT THE DENTED FUSELAGE SKIN, MANUFACTURED REPAIR PARTS ER/A 6341-14 PART 3 AND SRM 51-47-20 AND INSTALLED REPAIRSDR CALA2026082718974Skin · damagedDENT FROM BIRD STRIKE FWD OF LEFT AOA SKIN IAW SRM 53-10-01-1, 2024 T-3 .071 CHEM MILLED TO .040 IN POCKETS REF FIG 5. BLENDED DAMAGED AREA AND REMOVED PAINT REF SRM 53-00-01-1A-1 FIG103. NEEDS NDT PART 6 SRM 51-00-00 PROCEDURE 23. ACCOMPLISHED HFEC IAW 737 NDSDR AALA202605195602Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AROUND VACUUM WASTE VENT AT STA 917 AND S21L. REPAIRED SKIN PER SRM 53-70-01-2R-3.SDR DALA2026050602860Skin · crackedFOUND ONE CRACK AT NR 4 HOLE, THE CRACK AT THE SKIN OF FUSELAGE, CRACKED AT 9 O'CLOCK, AS MARKED. REPAIRED IAW PRI:633657-14AD (1572340) (AIRCRAFT GROUNDED)SDR DALA2026050602859Skin · damagedSECTION 48 LH LWR SKIN AT BS 1730, WL 200 FOUND ABRASION. REPAIRED AS PER SRM 53-80-01 (1572014) (AIRCRAFT GROUNDED)SDR DALA2026050602858Skin · damagedRIGHT FUSELAGE SKIN AT SECTION 48 BS 1725.5, WL 200 FOUND ABRASION. REPAIRED IAW SRM 53-80-01 (1572011) (AIRCRAFT GROUNDED)SDR DALA2026050602857Skin · damagedLEFT FUSELAGE SKIN AT SECTION 48 BS 1725.5, WL 200 FOUND ABRASION. REPAIRED AS PER B767-400 SRM 53-80-01 (1572006) (AIRCRAFT GROUNDED)SDR DALA2026050502816Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN BS Y= 1076 BTW LONG 13RH & 14RH. CORRECTIVE ACTION: REPAIR AND PRI 633992-14 (1571512) (AIRCRAFT GROUNDED)SDR IPXA2026050177952Skin Panel · damagedIN ORDER TO COMPLETE STEP 142 OF EA 300-5311-27-A4409, PRELIMINARY 5. ACCOMPLISHED PER STEP 142 OF EA 300-5311-27-A4409 PRELIMINARY 5. ACCOMPLISHED PER STEP 142 OF E.A.#: 300-5311-27-A4409 PRELIMINARY 5 AS A REQUIREMENT OF THE T3F18E008CUAT REPAIR.SDR DALA2026050402806Skin · damagedAD RELATED IN REF TO AMDS 5331-01293-02B-01 STEP 2C: EXISTING REPAIR WAS FOUND IN THE INSPECTION AREA (REAR LOWER CORNER OF THE AFT CARGO DOOR CUT OUT). REAR LOWER CORNER STA 1440, BETWEEN S-25R AND S-28R OF THE AFT CARGO DOOR CUT OUT WAS REPAIRED PER ERA 6SDR UIEA2026043000275Skin · damagedLEFT LOWER FUSELAGE SKIN JUST AFT OF RADOME HAS LIGHTNING STRIKE. REMOVED PAINT AT LIGHTNING STRIKE DAMAGED AREA IAW B747-400 AMM TASK 51-21-01-150-814. MECHANICALLY MEASURED LIGHTNING STRIKE AT LT FUSELAGE SKIN STA 176.5 1 INCH ABOVE STR 41L, ORIGINAL SKIN TSDR SWIA2026043076374Repair · corrodedEXTERNAL FUSELAGE STATION 985 STG27, REPAIR PATCH HAS CORROSION IN VARIOUS AREAS, BLENDED AND TREATED CORROSION ON REPAIR PATCH ON EXTERNAL SKIN AT FS985.00 AND STGR27 PER MHIRJ REO 670-53-51-395 REV-- DATED 2026-05-06, REO 670-53-00-290 REV. -F DATED 2019-0SDR SWAA2026052894463Skin · corrodedCORROSION ON FWD EXTERNAL SKIN AT BS1016, STR 25R. REMOVED CORROSION AND EVALUATED REWORK AREA IAW SRM 53-00-01-1A-1, ALLOWABLE DAMAGE 1.SDR SWAA2026052894465Skin · corrodedCORROSION ON AFT EXTERNAL SKIN AT BS1016 AT LEVEL STR 27L LOWER FUSELAGE. REMOVED CORROSION LOC. ON EXTERNAL SKIN AT BS1016 AT STR 27L LOWER FUSELAGE IAW SRM 51-10-02 AND EVALUATED REWORKS AREAS LOC. ON FWD AND AFT EXTERNAL SKIN AT BS1016 AT STR 27L LOWER FUSSDR SWAA2026052894464Skin · corrodedCORROSION ON FWD EXTERNAL SKIN AT BS 1016 AT STR 27R LOWER FUSELAGE. REMOVED CORROSION LOC. ON EXTERNAL SKIN AT BS 1016 AT STR 27R LOWER FUSELAGE IAW SRM 51-10-02 AND EVALUATED REWORKS AREA LOC. ON FWD AND AFT EXTERNAL SKIN AT BS 1016 AT LEVEL STR 27R LOWER SDR DALA2026050502817Skin · ground damageBELT LOADER DMG TO AFT CARGO DOOR JAMB, AFT EDGE. CORRECTIVE ACTION: REPAIRED PER PRI 634141-14. (1571522) (AIRCRAFT GROUNDED)SDR GTIA2026043039362Skin Panel · damagedTAIL STRIKE FINAL REPAIR.-RETURN TO SERVICE IN ACCORDANCE WITH FAR 49.9. AS AUTHORIZED BY THIS REPAIR STATION MANUAL, THE FOLLOWING PERSON CERTIFIES THAT THE WORK SPECIFIED BY THE CUSTOMER/OPERATOR WAS CARRIED OUT IN ACCORDANCE WITH FAA AIRWORTHINESS REGULATIOSDR CALA2026050115918Skin · damagedFUESLAGE SKIN DAMAGE AT BS 500B - 500C, S24L INTERIM REPAIR TO ACCOMPLISH INTIAL SUPPLEMENT INSPECTION PER PART 2 OF ECRA 5330-07744 (LATEST REVISION) NO LATER THAN APRIL 29APR 2028. PER ECRA5330-07744 A/C 0811 SECT 43 FUESLAGE SKIN DAMAGE AT STA 500B-500C ANDSDR DALA2026043002740Skin · crackedFOUND 01 EA CRACK AT STA 1654.50 - STA 1678, STR 13AL, BELOW THE SIXTH STRINGER-ATTACH RIVET COUNT FROM STA 1654.50, REPAIRED AS PER B767-400 SRM 53-80-01 (1570152) (AIRCRAFT GROUNDED)SDR UIEA2026042700251Skin · dentedDENT ON RH FUSELAGE SKIN BS 154, STRINGER 24R. DENT ON RH FUSELAGE SKIN STA 154 STRINGER 24R COMPLIED WITH FINAL EN #3246 REV 0. NO FURTHER DEFECTS NOTED.SDR LR7A2026042903820Window Frame · crackedDURING SCHEDULED A-1 CHECK UNDER JOB CARD HA1201, FOUND LH WINDOW FRAME CRACKED AT FS140, LBL42, WL251. REPAIRED IAW LAC MEA 382-53-26-062.SDR DALA2026043002752Skin · damagedREPAIR TO FUSELAGE SKIN BETWEEN BS 1405-1450 AND STRINGERS 24R- 28R. REF ERA 633423-14AD. AIRCRAFT WAS GROUNDEDSDR YENA2026042900444Skin · crackedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR35 & STR 30R SIDESHELL AREA / HOLE #2 / CRACK DAMAGE - PERMANENT REPAIR; REFERENCES: /1/ AAR-LCQ FINAL REO-L25784 REV. IR /2/ AIRBUS DOSSIER 81748154 /3/ AIRBUS RDAF 81748154/003/2026#B /4/ AIRBUS SB A32SDR YENA2026042900442Skin · crackedDURING HEAVY MAINTENANCE: FUSELAGE / SB 53-1372 / LH CENTER FUSELAGE / FR35 STGR30 / MULTIPLE HOLES -CRACK & ELONGATION - TEMPORARY REPAIR; REFERENCES: /1/ AAR-LCQ FINAL REO-L25785 REV. IR /2/ AIRBUS DOSSIER 81750093 /3/ AIRBUS RDAF 81750093/003/2026 ISSUE B /SDR ABXR2026042900006Skin · crackedFOUND CRACK ON UPPER FUSELAGE CROWN SKIN AT STA. 654+22, SR-1 SR-2SDR CALA2026050415954Skin · damagedCATERING REPORTS DAMAGE UNDER DOOR 2LHOLE PUNCTURED IN AFT LEFT HAND FUSELAGE AROUND STATION 951, PICTURES ARE ATTACHED HOLE IN AIRCRAFT IS LOCATED BETWEEN STRINGERS 20L AND 21L AT STA 954 TO STA 963. THE TOP OF THE SCRATCH STARTS ON S20L AND MAY HAVE AFFECTEDSDR AALA202605017715Skin Panel · crackedAIRCRAFT IN BASE MAINTENANCE: 3 CRACKS IN LEFT FORWARD FUSELAGE SKIN PANEL AT FR 14 AND S11L. REPAIRED SKIN PANEL PER EA 374636.SDR AALA202604309456Skin Panel · crackedAIRCRAFT IN BASE MAINTENANCE: 2 CRACKS RADIATING FROM FATENER HOLE AT FR13-FR14, Z780-Z950 RH. MAINTENANCE CUT OUT DAMAGE AND FABRICATED A FILLER AND DOUBLER IAW EA 374637.SDR KCSA202604281033Skin · damagedEVIDENCE OF LIGHTNING STRIKE DAMAGE ON L/H UPPER FUSELAGE APPROX STA 1965 S-10L - 11L.SDR 2026F00090Skin · corrodedFOUND MULTIPLE AREAS OF CORROSION UNDER AFT CHIN FAIRING. MECHANICALLY REMOVED AREAS OF CORROSION LOCATED UNDER AFT CHIN FAIRING ON FUSELAGE OUTER SKIN IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNA 680 SRM 51-70-02 EXCEEDINSDR AALA202605212302Splice Strap · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN BUTT SPLICE STRAP INTERNAL SURFACE AT STA 887 AND S27R. REPAIRED STRAP PER EA 374829 AND SRM 51-40-02.SDR DALA2026042802694Skin · not reportedER/A 093358-14AD REV. E, FUSELAGE SKIN, L-1 DOOR CUTOUT LOWER, FWD CORNER. REF ERA 093358-14AD (1564736) AIRCRAFT WAS GROUNDED.SDR SWAA2026051192887Skin · corrodedCORROSION ON LH EXTERNAL SKIN SECTION 47 STA935 8' BELOW FROM WASTE EXHAUST HOLE. REPAIRED PER EA 26-153-01138 WITH AN INSPECTION THRESHOLD DEFINED IN 26-153-01138-DTI..SDR SWIA2026042875914Skin · scratchedFOUND SCRATCH ON RH FUSELAGE STARTING AT FS1039.5 TO FS1029.62 LOCATED ON STGR19R MEASURING 11-3/8" LONG; MAX DEPTH: .0022". INSPECTED RH FUSLAGE SKIN AT FS1029.62 - FS1039.5 ON STGR 19R WITH NO DAMAGE FOUND; LOCATED SCRATCH ON RH FUSELAGE FS1029.62 TO FS1039SDR 1Q2R2026070600001Skin · crackedTEMPORARY TO PERMANENT REPAIR REQUIRED TO FUSELAGE SKIN BETWEEN FS280 AND FS310, AND STGR 12R TO 15R. PERMANENT REPAIR PERFORMED THROUGH SKIN REPLACEMENT. REPLACEMENT PERFORMED BY MHI RJ MRT (MIS-6317).SDR SCNA20260601232Skin · dentedDENT WAS FOUND ON FUSELAGE SKIN CROWN AREA AT STA 380 + 6'' AND 0.25'' ABOVE STR4R. DENT WAS EVALUATED IAW A WORK INSTRUCTION BOEING MESSAGE #XTV-SCA-26-0015-03C AND XTREME RES #014944-12-1SDR SCNA20260601231Skin · dentedDENT WAS FOUND ON FUSELAGE SKIN CROWN AREA AT STA 380 + 14'' AND 0.25'' ABOVE STR 4R. DENT WAS EVALUATED IAW A WORK INSTRUCTION, MESSAGE # XTV-SCA-26-0015-03C AND XTREME RES # 014944-12-1SDR SCNA20260529227Skin · dentedFUSELAGE SKIN RT SIDE BS 500G + 8.5'' BETWEEN S7R GALLEY R2 DOOR DENT WAS FOUND. XTREME W.O 014944 - NRC053: FUSELAGE SKIN R/H SIDE STA 500G + 8.5'' BETWEEN STRG 7R DENT WAS FOUND .SDR SCNA20260529226Skin · dentedFUSELAGE SKIN DENT WAS FOUND AT STA 440 + 8'' AND 2.50'' BELLOW STR 3L. ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AND STRUCTURAL FILLER AT FUSELAGE SKIN STA 440 + 8" AND 2.50" BELLOW STR 3L PER BOEING MESSAGE: XTV-SCA-26-0018-03B. XTREME RESSDR SCNA20260529224Skin · dentedFUSELAGE SKIN R/H SIDE STA 380 + 2'' BETWEEN STRG 6R GALLEY DOOR DENT WAS FOUND. ACCOMPLISHED PERMANET REINFORCING REPAIR DOUBLER ALUMINUM 2024TS 0.040" IN, TRIPLER REPAIR 0.063"IN, STRUCTURAL FILLER 0.080" IN, TEAR STRAP 0.050"IN AND TAPER FILLER 0.050"IN ALSDR SCNA20260529223Skin · dentedFUSELAGE SKIN, DENT WAS FOUND AT STA 500 + 0.50'' AND 0.25'' BELLOW STR 2R. ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER ALUMINUM 2024-T3 0.040" TRIPLER REPAIR 0.063", STRUCTURAL FILLER 0.080" TEAR STRAP 0.050" AND TAPER FILLER 0.050" AND 0.250"SDR SWIA2026042575973Skin · dentedINSPECTED DENT REPORTED BY RAMP. MEASURED TO BE APPROXIMATELY 0.085" DEEP, 12" LONG AND 3.5" WIDE AND SLIGHTLY CREASED OVER FR 11 BETWEEN STGR 18L AND 19L. OUT OF LIMITS PER SRM 53-10-01. (FLIGHT 3896) COMPLIED WITH PERMANENT REPAIR ON LT FWD FUSELAGE SKIN ASDR DALA2026042602633Skin · dentedAIRCRAFT ARRIVED INTO SEA, THE A/C EXPERIENCED HEAT DAMAGE DUE TO ELECTRICAL ARCING NEAR THE POWER RECEPTABLE DOOR. FRAME 7 HAS SEVERAL DENTS ON FLANGE THAT MATES WITH SKIN BETWEEN STR 42L AND STR 42R. CORRECTIVE ACTION: FR7 REPAIR SPLICE WAS REMOVED, FABRICATSDR DALA2026042602632Skin · mechanic errorWHILE DRILLING NEW SKIN ASSY, FOUND NEW STR41 LH AND STR41 RH DO NOT ALIGN WITH EXISTING END FITTINGS AT FR 24. PERFORM CUTOUT OF S-41RH (P/N D53137178200) FWD OF FR24 AS DEFINED IN FIGURE 29, SHEET 2 PER SRM 51-27-00. PLUG THE TEN MISDRILLED HOLES IN THE LOSDR DALA2026042602630Skin · damagedAIRCRAFT ARRIVED INTO SEA, THE A/C EXPERIENCED HEAT DAMAGE DUE TO ELECTRICAL ARCING NEAR THE POWER RECEPTABLE DOOR. FR 6-12 MULTIPLE HOLES FOUND IN OUT OF ROUND CONDITION. PERFORMED TRIMOUT OF FUSELAGE SKIN, FABRICATED REPAIR PARTS AND INSTALLED PER ER/A 617
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