JASC 5330
Service difficulty reports · 79,329
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 ASAA2024061951206Skin · puncturedL-1 DOOR DURING REMOVAL OF AFT FRAME FOUND INNER MIDDLE SKIN DAMAGED NEAR PRISM CUTOUT. GROUNDED - YES. REPAIRED INNER MIDDLE SKIN DAMAGE IAW EA CMPT-52EA-27220 REV: 00 DATED 07/10/2024.SDR CALA2024062400064Skin · canningDURING WALK AROUND FOUND DENT IN A PREVIOUS REPAIR FWD OF L2 DOOR, PERFORMED INTERIM REPAIR PER ECRA 5330-07276 PART 1 STEPS 1-4. REF EC/RA 5330-07276 PERFORMED HFEC SURFACE INSPECTION IAW NDT PART 6 51-00-19, NO CRACKS DETECTED. PERMANENT REPAIR COMPLETED SDR DALA2024062006257Skin · gouged(LOG 0402873) GOUGE ON SKIN BTW STA 360 AND STA 370. S-28R TO S-27R APPROX AT EXTERNAL FUSELAGE. SKIN BTW STA 360 AND STA 370. S-28R TO S-27R APPROX AT EXTERNAL FUSELAGE WAS REPAIRED PER ERA 618224-14.SDR SWIA20240716618Skin · dentedADM#N162SY-5352 - DENT MEASURES 2.275" LONG X 1.164" WIDE X 0.025 DEEP. NOMINAL THICKNESS IS 0.0393" AND W/D IS 46.60. LOCATED EXTERNAL LH, ZONE 100, FCBS 53-10-00-004, FORWARD FUSELAGE SKIN PANEL, FR10 TO FR11, STRG15L TO STRG17L. (C-CHECK RO 7/14/2024) SDR DALA2024061906219Skin · damagedSHIP 3422 A330-900 / FUSELAGE / AFT CARGO DOOR SURROUND SKIN / GROUND DAMAGE / PERMANENT REPAIR. CORRECTIVE ACTION: COMPLIED WITH ERA 610110-14 REV B. (0400490)SDR DALA2024061906218Skin · damagedSHIP 3422 A330-900 / FUSELAGE / AFT CARGO DOOR SURROUND SKIN / GROUND DAMAGE / PERMANENT REPAIR. CORRECTIVE ACTION: COMPLIED WITH MON INSP PER ERA 610110-14 REV B. OK TO CONTINUE. (0400472)SDR CALA2024061800024Skin · damagedFOUND SKIN DAMAGE ON FUSELAGE. R/H SIDE. BS 727F-727G S17R-19R REMOVED FASTENERS IN THE AREA, AND TRIMMED AWAY THE AREA OF DAMAGED SKIN SIZE OF CUTOUT= 24.70" LONG BY= 12.10" WIDTH, IAW SRM: 53-00-2R-1, REPAIR: 1, STEPS= 4.A.THRUGH 4.C. PERFORMED REQUIRED SKISDR SWIA20240617Skin · chafedCHAFE ON EXTERNAL SKIN INSIDE OF A PREVIOUS BLEND OR DENT. FS969.0 - FS985.00 STGR27. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)CHAFE ON EXTERNAL SKIN INSIDE OF A PREVIOUS BLEND OR DENT. FS969.0 - FS985.00 STGR27 FOUND TO BE OUT OF ALLOWABLE LIMITS DUSDR SWI2024F01004Skin · chafedCHAFE ON EXTERNAL SKIN INSIDE OF A PREVIOUS BLEND OR DENT. FS969.0 - FS985.00 STGR27. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)CHAFE ON EXTERNAL SKIN INSIDE OF A PREVIOUS BLEND OR DENT. FS969.0 - FS985.00 STGR27 FOUND TO BE OUT OF ALLOWABLE LIMITS DUSDR SWI2024F00990Skin · chafedCHAFE ON EXTERNAL SKIN INSIDE OF A PREVIOUS BLEND OR DENT. FS969.0 - FS985.00 STGR27. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)CHAFE ON EXTERNAL SKIN INSIDE OF A PREVIOUS BLEND OR DENT. FS969.0 - FS985.00 STGR27 FOUND TO BE OUT OF ALLOWABLE LIMITS DUSDR SWIA202408260017Doubler · corrodedTHE WIFI AFT ATG ANTENNA DOUBLER HAS CORROSION ON THE EXTERIOR SURFACE AND FRETTING CORROSION ON MATING SURFACE FOR ANTENNA. (MARKED) (C-CHECK RO 8/24/2024) REMOVED AND INSTALLED NEW EXTERNAL DOUBLER AT WIFI AFT ATG ANTENNA BETWEEN FS1000-FS1050 STGR 25SDR SWAA2024073102839Doubler · crackedCRACK ON EGPR LOWER SURROUND DOUBLER LOCATED BTW BS229 AND BS235.8 2024-401539<[01] TOOL USED CALIPER P/N:500-196-30; S/N:A233292368; DUE DATE:06/MAR/25;[02] TOOL USED: EDDY CURRENT EQUIPMENT P/N NORTEC 500D S/ N 500X1693P030457 DUE DATE: 15-OCT-24.;[03] ON STSDR SWIA202407290605Skin · corrodedCORROSION ON FWD SIDE OF FS 574.00 BETWEEN STGR 23R AND 24R (FILED CLOSED)PERFORMED TEMPORARY REPAIR OF CORROSION DAMAGE ON FWD SIDE OF FRAME FS 574.00 BETWEEN STR23R - 24R WITH REFERENCE TO REO 601R-53-61-8197 REV A DATED 07/11/2024. PERFORMED EDDY CURRENT ISDR SWIA202407290604Skin · corrodedCORROSION ON FWD SIDE OF FS 574.00 BETWEEN STGR 26L AND 27 (CENTER) (FILED CLOSED)PERFORMED TEMPORARY REPAIR OF FRAME FS 574.00 BETWEN STGR26L AND STGR27 WITH REFERENCE TO SRM 53-00-15 REPAIR 2, PG 204 AND REO 601R-53-61-8197 REV "A" DATED 07/10/2024. THIS DISDR SWIA20240729617Skin · corrodedCORROSION ON AFT SIDE OF FS 574.00 BETWEEN STGR 21L AND 22L (FILED CLOSED)PERFORMED TEMPORARY REPAIR OF FRAME FS 574.00 BETWEN STGR21L AND 22L WITH REFERENCE TO SRM 53-00-15 REPAIR 2, PG 204 AND REO 601R-53-61-8197 REV "A" DATED 07/11/2024. THIS DISPOSITION ISDR YENA2024061800873Skin · dentedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / PRESSURE BULKHEAD @ FR 35 & STR 30L / CRACKS AT FASTENER HOLES – TIME LIMITED REPAIR; REFERENCES: /1/ AEM EA 53-9002-24 REV 0 (COVER & PARTS 1-5) /2/ AIRBUS STAGE 1 RDAF 81405207/004/2024#A /3/ AIRBUS DOSSSDR YENA2024061800872Skin · dentedDURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / SKIN BETWEEN FR 11-12 & STGR 17L-19L / DENTS & CRACK - TEMPORARY REPAIR; /1/ STS EA 125-2024-048 REV. IR /2/ ETD2024-190-016478 REV / WITH ANAC 8165205 /3/ PREVIOUS EC E24-692-01 DURING CURRENT DROP-IN CHECK,SDR YENA2024062100890Skin · crackedDURING CURRENT DROP-IN CHECK, 2 DENTS, ONE OF WHICH HAS A CRACK DAMAGE, ON THE FWD SKIN BETWEEN FR 11-12 & STGR 17L-19L, WAS EVALUATED AFTER THE A/C WAS FERRIED WITH A TEMPORARY REPAIR. PREVIOUS EC, FOR ORIGINAL DAMAGE AND MX FERRY TEMP REPAIR ACCOMPLISHMENTSDR CALA2024061801856Skin · dentedREF AMES NON ROUTINE 171629-0100-0043. GENERATING ITEM:19-0640-1 -2100.DENT ON FUSELAGE SKIN AT STA 1400 S-25LSDR DALA2024061806170Skin · crackedCRACK ON SKIN OF CUT OUT EDGE AT AFT CARGO DOOR STA Y=992 BTW L25R. SUMMARY OF NRC 00226: CRACK ON SKIN OF CUT OUT EDGE AT AFT CARGO DOOR STA Y=992 BTW L25R WAS REPAIRED PER B717-200 SRM 53-20-15- 2R PROCEDURE 12. PERFORM AN EXTERNAL GVI EVERY 8000 CYCLES TO TSDR GTIA2024061738183Skin · corrodedCORROSION FOUND ON SKIN AREA OF SWIVEL BEARING ON NLG RAF-01 3340638-02 GENERATED-COMPLIED WITH EA 5311-2459.SDR SWAA2024071802270Angle · crackedAFT OF FWD CARGO COMPARTMENT DRAG ANGLE AFT END CRACKED @ S-25R BETWEEN STA 500D AND STA 520 MKD DOT<[01] REMOVED; FABRICATED AND INSTALLED DRAG ANGLE FROM AFT OF FWD CARGO COMPARTMENT AT S-25R BETWEEN STA 500D AND STA 520 IN REF SRM 51-40-05-0G-0; SRM 51-40-0SDR IPXA2024070284184Skin · dentedDENT ON AFT UPPER FUSELAGE VERIFIED ALL REPAIR STEPS COMPLETED REF EO-90533-REQ3 [T3F18E004RSS0].SDR IPXA2024061684184Skin · dentedDENT ON AFT UPPER FUSELAGE.SDR CALA2024062601902Skin · crackedDURING INSPECTION WAS FOUND INDICATION CRACK AT FWD PASSENGER DOOR (LH SIDE) ON THE AFT. LOWER CORNER BTW STA.325/347 AND STGR 18/21L. THE LATEST REVISION OF ECRA# 5330-07278 ON OR BEFORE THE AC REACHES 37,500 TOTAL FC. ACCOMPLISH REPEAT INSPECTION AT INTERVALSDR CALA2024062601901Bear Strap · crackedDURING INSPECTION WAS FOUND INDICATION CRACK AT FWD SERVICE DOOR (LH SIDE) ON THE AFT. LOWER CORNER BTW STA.325/347 AND STGR 18/21L. THE CORRECT LOCATION OF THE CRACK IS AT FWD SERVICE DOOR (RH SIDE) ON THE AFT. LOWER CORNER BTW STA.325/347 AND STGR 18/21R. ISSDR DALA2024061806195Skin · damaged(LOG 6205842) LIGHTNING STRIKE JUST AFT OF NOSE OF AIRCRAFT @ 7,000 ON APPROACH TO SEA. ADRESSED LIGHTNING ENTRY DMG AT NBR2 PYLON PER SRM 54-50-70-1A.C.(1).(C). BLENDED WINGLET SKIN DAMAGE TO VERIFY DEPTH AND SIZE AND BLENDED EDGE DAMAGE PER ER/A 618849-14.SDR CALA2024061701833Skin · dentedLOWER AFT FUSELAGE APPROX FR71-72 AROUND SAFETY STAY AREA HAS MU LTIPLE DENTS AND CREASES (4EA). REPAIRED FUSELAGE SKIN LOWER PANEL IAW A319 SRM 53-51-29-300-002 .SDR CALA2024061801851Skin · damagedECRA 5331-03043 REV A PART 3 STEP 1 INSTRUCTS TO CONTACT ENGINEE RING BEFORE A/C REACHES 36,859 TFC FOR PERMANENT REPAIR INSTRUCT IONS. CURRENT CYCLES 35441. REQUIRES RFTS.SDR HNAA2024071900568None · none53-2091 REAR FUSE I, UNRECORDED PATCH AT FR67 STR17-18R. RAR PATCH IAW EO1-53-24-0370SDR SWAA2024071801520Bear Strap · crackedCRACK INDICATION ON FRAME ON BS 294.5 BEAR STRAP AROUND FASTENER HOLE BETWEEN S-8R AND S-9R AT FWD GALLEY AREA. PERFORMED PERMANENT REPAIR ON FRAME ON BS 294.5 BEAR STRAP BETWEEN S-6R AND S-11R AT FWD GALLEY AREA IAW B737-700 SRM 53-10-01-2R-6 REPAIR 6 AND ESDR SWIA20240614Skin · gougedGOUGE IN FUSELAGE SKIN BELOW PASSENGER DOOR, BETWEEN FS333.00 AND FS349.00, STRGR 19LH AND STRGR 20LH.PERFORMED TEMPERARY REPAIR FUSELAGE SKIN BELOW PASSENGER DOOR, BETWEEN FS333.00 AND FS349.00, STRGR 19LH AND STRGR 20LH IAW REO 670-53-21-2419 REV-- DATED 20SDR CALA2024061701826Bear Strap · crackedL-1 DOOR CUTOUT AFT LOWER CORNER HAS A CRACK INDICATION IN BEARS TRAP ONLY AT THE LOWEST HOLE OUT OF FIVE LOCATIONS. REPAIRED CRACK IN L1 DOOR BEARSTRAP AT THE LOWEST HOLE OUT OF FIVE LOCATIONS IAW B767-300 SRM 53-10-01-2R-1 REPAIR 1.SDR JR2R20240614126Skin · crackedFWD FUSELAGE UPPER SKIN DENT AT FR01-FR02. REPAIREDSDR KCSA202406141076Skin · damagedEVIDENCE OF LIGHTNING STRIKE ON FUSELAGE SKIN @ STA 464 APPROX LS-1SDR KCSA202406141075Skin · damagedEVIDENCE OF LIGHTNING STRIKE ON FUSELAGE SKIN @ STA 435 APPROX LS-1SDR KCSA202406141074Skin · damagedEVIDENCE OF LIGHTNING STRIKE ON FUSELAGE SKIN @ STA 591 ABOVE LS-19SDR KCSA202406141073Skin · damagedLOWER HALF OF FUSELAGE EXTERNAL SKIN HAS EVIDENCE OF LIGHTNING STRIKE LEFT SIDE APPROX STA 160 AND S-41SDR KCSA202406141072Skin · damagedLOWER HALF OF FUSELAGE EXTERNAL SKIN HAS EVIDENCE OF LIGHTNING STRIKE RIGHT SIDE APPROX STA 208 AND S-42ASDR ASAA2024061350702Doubler · corrodedFUSEKAGE STA 1064 TAIL BUMP HOUSING DOUBLER LH SIDE CORRODED. GROUNDED - YES. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-01-1A-1. APPROVED TO BE ACCEPTABLE AS IS IAW ASA EA. 800-53EA-27163W=1 O=.080 R=.065 L=4 D=.015.SDR AALA202407018421Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON CENTER WING BOX LEFT SIDE SKIN. REPAIRED SKIN PER EA 355468.SDR SWIA202406240013Skin · damagedC=SEE CP28379507 DAMAGE BELOW RH SERVICE DOOR. BETWEEN FR-14 TO: FR-16 AND STGR-21R TO: STGR-22R. CLASSIFIED AS MAJOR REPAIR. INITIATED FORM 337 (FILED CLOSED) REFERENCE CP28407575 FOR DETAILED DAMAGE EVALUATION AND CP28379507 FOR DETERMINATION OF MAJOR SDR DALA2024061706148Skin · damagedTOOL MARKINGS AND ELONGATES HOLES ON OUTER SKIN BETWEEN BS 565 - 620 AT THRESHOLD AREA OF FWD CARGO COMPARTMENT. OUTER SKIN BETWEEN BS 565 - 620 AT THRESHOLD AREA OF FWD CARGO COMPARTMENT WAS REPAIRED PER ER/A 618195-14AD REV. ORIGINAL SECTION I.SDR DALA2024061406100Skin · damagedFUSELAGE / EXTERNAL SKIN / FWD CARGO DOOR CUTOUT/ BTW BS 560 & 620 AT S-26R, ELONGATED HOLES. REF ERA 618195-14.SDR KCSA202406131071Skin · damagedLOWER HALF OF FUSELAGE EXTERNAL SKIN HAS EVIDENCE OF LIGHTNING STRIKE RIGHT SIDE APPROX STA 200 AND S-42ASDR HNAA2024072600612Skin · not reported53-2324 RF1 RH EXTERNAL SKIN HAS UNRECORDED DOUBLER AT FR75 BTW STR1-3R. RAR DOUBLER IAW EO1-53-24-0413SDR HNAA2024072600611Skin · not reported53-2321 FF2 LH EXTERNAL SKIN HAS UNRECORDED DOUBLER BTWFR11-12 STR15-17L. RAR DOUBLER IAW EO 1-53-24-0380.SDR HNAA2024072600610Skin · not reported53-2320 CF2 EXTERNAL SKIN HAS UNRECORDED DOUBLER AT FR28-29 STR 16R. R & R DOUBLER IAW EO1-53-24-0409. REPAIRED UNDERLYING SURFACE IAW SRM53-22-01 AND 51-40-02SDR HNAA2024072600609Skin · none53-2319 CF1 EXTERNAL SKIN HAS UNRECORDED DOUBLER AT FR21 BELOW STR18R. RAR DOUBLER IAW EO1-23-24-0379SDR SWAA2024071800871Doubler · unknownREJECT - IMPROPERLY GROUND SERVICE DOOR 114AR FABRICATED REPAIR DOUBLER AT LOWER FUSELAGE (REPAIR DOBLER MADE THICK 0.040 INCHES INSTEAD 0.050 INCHES) 2024-376672<[01] MADE AND DRILLED REPAIR PARTS [2] DOUBLER WITH MATERIAL USED ALUMINUM SHEET P/N: 2024T3 0.05
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