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 DALA2025070104898Structure · corrodedCORROSION FOUND AROUND AND ON COUNTERSINK BOLT HOLES10L, 30L, AND 70L. COMPLIED WITH PRI 626953-14 REV 0, PRI 626953-14 REV 1, PRI 626953-14 REV 2 AND FINAL ER/A 626953-14 REV ORIGINAL. SECTION I , SEE LOG # 1048121. REP INSPECTIONS. COMPLIED WITH PRI 62695SDR SWIA202506300028Skin · gouged3 GOUGES TO FUSELAGE SKIN BETWEEN FS589.00 - FS605.00 AND STR 23R-24R (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSSDR UIEA2025062500807Skin · corrodedFOUND THE SKIN INSIDE CORROSION AT STA 1700 - 1720, S-42L. REMOVE EXIST SKIN REPAIR DOUBLER IAW SRM 51-10-02-0G-0 REV 62. ACCOMPLISH EI NO: T2025A53M-1083 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR UIEA2025062500808Skin · dentedFOUND FUSELAGE LOWER LOBE SKIN DENT AT STA 1925, S-31R ~ S-32R. ACCOMPLISHED EI NR: T2025A53M-996 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR UIEA2025062500809Skin · dentedDENT - FOUND FUSELAGE LOWER LOBE SKIN DENT AT STA 1935, S-31R ~ S-32R. ACCOMPLISHED EI NO: T2025A53M-996 REV 1 AND EI ATTACHED TO W/O NO: 11010065(002). JOB COMPLETED AND CONDITION CHECK NORMAL.SDR UIEA2025062500810Repair · out of dateUPGRADE THREE TEMPORARY FUSELAGE SKIN DOUBLER REPAIRS BETWEEN STA 1780 AND STA 1840, S-46L AND S-49L. REMOVED TIME LIMITED FUSELAGE SKIN REPAIR, TOTAL 3 AREA IAW SRM 51-40-02-0G-0 REV 62. ACCOMPLISHED EI NR T2025A53M-1055 REV 2. 3. JOB COMPLETED AND CONDITISDR ABXA20250628138Skin · corroded"DURING THE ACCOMPLISHMENT OF APU REPLACEMENT AT CVG/FEAM, CORROSION WAS DISCOVERED IN THE APU COMPARTMENT. ONE OF THE AFFECTED COMPONENTS IS SKIN PANEL PIN I 48T3280-2. THE CORROSION ON THIS ITEM WENT OUT OF I IM ITS. THE SKIN PANEL IS A BONDED UNIT MADE OF 2SDR CALA2025063006073Access Door · corroded(SDR) EXFOLIATION CORROSION ON PANEL 121AL (LAVATORY SERVICE) LW R NEAR LATCHES. REMOVED AND REPLACED PANEL ASSY DOOR 121AL P/N 143N3411U126 ON L AVATORY SERVICE IAW B757-200 SRM 51-40-02-06-0 AND DWG 143N3411 CLEANED AREA PAN IAW SOPM 20-30-03 AND RESTORED SDR R61A2025062800265Access Door · corrodedDURING HEAVY CHECK WASTE ACCESS DOOR FOUND CORRODED. REPLACED DOOR IAW AMM 20-10-01-910-801-ASDR SCNA20250707244Skin · corrodedR/H FUSELAGE FROM STA663 TO AFT PRESSURE BULKHEAD HAS SIGNS OF CORROSION ALONG LAP SEAM. ACCOMPLISHED EA 737-5360-72-B0528 P1, EA 737-5360-72-B0528 REV I/R AND SCA EA 53-0251. 83658 SAA001 27JUN25 CONTINUED ON SUPPLEMENT # 110668, 111233, 111241, 111242, 1112SDR CALA2025063006066Skin · corrodedAFT LAVATORY VENTILATION OUTLET INTERNAL STRUCTURE SKIN HAS CORROSION BETWEEN FR 69-70 AND STR 31 & 32 PER HAECO LCQ N/R 9290435/40435 GEN BY V937268 REMOVED AND REPLACED INTERNAL STRUCTURE SKIN (DOUBLER) AT AFT LAV VENTILATION OUTLET FR69-70, STG 31R - 32R IASDR AALA202602093161Skin · crackedCOMPONENT IN SHOP MAINTENANCE: CRACK IN SIDE SHELL AT FR 35, S30R. REPAIRED SIDE SHELL PER EA 366098.SDR CNMA2025090002Skin · dentedDENT NR 12 LT FUSELAGE STATION 368 +8 INCHES, STRINGER 17L +4 INCHES. DURING SCHEDULED MAINTENANCE, TWO DENT DAMAGES WERE FOUND COMMON TO THE LOWER FUSELAGE SKIN BETWEEN STA 368 - STA 390 AND STGR 17L - STGR 19L..SDR SIMA20250626021Skin · corrodedINTERNAL FUSELAGE SKIN DOUBLER IS CORRODED AT INBD SIDE OF WASTE SERVICE BUCKET. REMOVED AND REPLACED INTERNAL FUSELAGE SKIN DOUBLER AT WASTE SERVICE BUCKET IAW SRM 51-40-08.SDR DALA2025063004863Skin · corrodedSHIP 6807 DURING LCK, CORROSION WAS NOTED ON THE WING CENTER SECTION UPPER SKIN, STA 1000-1040. ER/A 626574-14AD SECT. I REPAIR WAS ACCOMPLISHED. CORRECTIVE ACTION: REF ERA 626574-14. (1048406)SDR AALA202506303573Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION EXTERNAL SKIN LOC. BTW FR65/FR66 AND BTW STR31R/STR32R LOWER FUSELAGE. MAINTENANCE PERFORMED TIME LIMITED REPAIR LOC.BTW FR65 TO FR66 AND BTW STR31R TO STR32R. IAW EA 364966.SDR DALA2025062704815Skin · dentedSHIP 3135 FOUND 2 DENTS LOCATED BELOW F/O SLIDING WINDOW- DENT ARE CREASED AGAINST THE INTERIOR FRAME STRUCTURE. CORRECTIVE ACTION: COMPLIED WITH ER/A 626900-14. (1048079).SDR SWAA2025072985125Panel · debondedPANEL 193AR OUTER SKIN IS DISBONDED. REPAIRED IAW SRM 51-70-05-2R-4.SDR IPXA2025070315311Skin · gougedGOUGE FWD OF LOWER FWD CARGO DOOR EO-94202-REQ1 C/W.REMOVED GOUGE COMMON TO LWR FWD CARGO DOOR BY BLENDING IAW SRM 51-10-02.CUT OUT DAMAGE TO FUSELAGE SKIN AT STR 25R BETWEEN FS473 AND FS465.LOCATED DRILL AND FABRICATED -1 REPAIR DOUBLER USING 2024T3 .160" PO SDR SWIA20250625Skin · damagedFWD FUSELAGE FR 10 HAS ELECTRICAL ARCING DAMAGE BETWEEN STGR 12L -13L. REPAIRED FR 10 BETWEEN STGR 12L-13L. REF ETD 2025-170-923684 REV. A.SDR CALA2025062706000Skin · damagedREMOVE DAMAGED DOUBLER, MAP OUT DAMAGE OF SKIN PANEL. REMOVED DAMAGED DOUBLER IAW SRM 51-42-11/001 FABRICATED NEW REPAIR DOUBLER AS DIRECTED BY RFTS 60004 PG2 A319 SRM 53-21-11- 300-093. INSTALLED REPAIR DOUBLER IAW A319 SRM 51-42-11/001.SDR DALA2025062604797Skin · chafedSHIP 3135 CHAFING MARK ON EXTERNAL FUSELAGE SKIN AT FRAME 34 BETWEEN STRINGER 43 LH AND RH. CORRECTIVE ACTION: COMPLIED WITH ER/A 575113-14AD. (1045547).SDR DALA2025062604795Skin · crackedSHIP 9574 FUSELAGE SKIN. VISUAL INDICATION OF CRACK. LOCATED ABOVE #1 PYLON AT STA 1022. CORRECTIVE ACTION: REPAIRED PER E/RA 624873-14 REV. ORIG. (1045993)SDR R61A2025062600264Skin · damagedFOUND PRE-EXISTING LIGHTING STRIKE DAMAGE IN FUSELAGE SKIN AFT OF L1 DOOR AFTER PAINT REMOVAL , FR23-24 STR 14L-15L, CORRECTED IAW SRM 53-21-01 REPAIR 10SDR AALA202506263083Skin · bulgedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE LOWER SKIN ADJACENT TO AFT LAVATORY SERVICE PANEL FROM BS 847 TO BS 867, FROM S23L TO S25L. REPARED SKIN PER EA 365547.SDR DALA2025062504741Skin · damagedSIX INCHES AFT OF FRAME 61 BETWEEN STRINGER 2R AND 3R SUPPORT HAS TOOLING MARKS. CORRECTIVE ACTION: REPAIRED PER ERA 626805-14 REV. B. SECTION III.SDR KCSA202506251097Bear Strap · crackedFOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT STA 2231 STR 25R LWR FWD HOLESDR SWIA202511030624Skin · dentedADM# N803SK-9303 LH FUSEWLAGE ABOVE FWD CARGO DOOR. BLENDED AREA IS BETWEEN STGR 18L AND 19L AND FS 549.00 AND 565.00 WITH MAX DEPTH OF .0030. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTISDR SCNA20250725273Skin · damagedWO 95798, NR ENG53SCA-11680: N835SY: FUSELAGE SKIN, STA 420 TO 460 BETWEEN S-21R AND S-26R - REPAIR - RESOLUTION: C/W BY FAS 4686SDR SCNA20250725274Skin · damagedWO 95798, NR 00001: REF EA 53-0249 ACCOMPLISH A PERMANENT REPAIR OF THE FUSELAGE SKIN BETWEEN STRA 370 – 380 AT S-24R PER SRM 53-00-01-2R-3 WITHIN 5 FLIGHT HOURS OR 2 FLIGHT CYCLES, WHICHEVER OCCURS FIRST ( REINSPECT - TEMP REPAIR, SPEED TAPE, FASTENERS OR TEMSDR AALA202507146680Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK EXTERNAL SKIN BTW FR69-FR70 STR23R, L=0.362 INCHES.SDR SCNA20250722270Skin · damagedFUSELAGE SKIN, STA 420 TO 480 BETWEEN S-26R AND S-27L - REPAIR - C/W BY FAS 4686SDR SCNA20250722269Skin · damagedWO95798, ENG-53SCA-11679, N835SY: FUSELAGE SKIN, STA 370 TO 385 BETWEEN S-22R AND S-25R - REPAIR - RESOLUTION: C/W BY FAS 4686SDR SWIA202507150622Skin · chafedCHAFING FOUND ON LOWER FUSELAGE SKIN BETWEEN FS977.00 AND FS985.00 STGR 27 DUE TO CONTACT ON AFT FAIRING PANEL C-CHANNEL. REMOVED CHAFING FOUND ON LOWER FUSELAGE SKIN BETWEEN FS977.00 AND FS985.00 STGR 27 REF CRJ700 SRM 51-12-00-001-001-A01. FOUND AREA TO BESDR CALA2025062605919Skin · damagedPER SRM 53-00-01-2R-12 SEC. 5(B), AFTER 50,000 TOTAL AIRPLANE CYCLES, PERFORM EXTERNAL DETAILED VISUAL (DET) IN SPECTIONS AT 4,000 FLIGHT CYCLE INTERVALS OF THE REPAIR AREA FOR SKIN CRACKS AT THE OUTER PERIMETER ROW OF FASTENERS COMMON TO T HE REPAIR DOUBLER ASDR JR2R20250622903Skin · dentedFUSELAGE SKIN JUST AFT OF FRAME 96 ABOVE STRINGER 26AR IS DENTED AND GOUGED. REPAIREDSDR IPXA2025081650158Skin · dentedMAJOR REPAIR, DENT WITH GAUGE FWD OF TAIL STAND ON RIGHT HAND SIDE. ACCOMPLISHED REPAIR DAMAGE IAW SRM 53-10-12-201, PARAGRAPH 11 AND FIGURE 208 (SHEET 1).SDR SWAA2025063084175Skin · corrodedCORROSION ON SKIN UNDER WASTE PAN STA 847 TO STA 867 BETWEEN STR23L TO STR 25L<[01] REPAIRED PER EA 25-153-01658 WITH AN INSPECTION THRESHOLD DEFINED IN 25-153-01658-DT;[02] VERIFIED <BR>REPAIRED PER EA 25-153-01658 WITH AN INSPECTION THRESHOLD DEFINED IN 25-1SDR CALA2025062605917Skin · dentedDENT IN FUSELAGE SKIN FS500B PLUS 12" STRINGER 27RC/W REPAIR PER SRM 53-00-01-2R-3. REF NR 2723023 FOR WORK ACCOMPLISHED. ESFR INFORMATION ENTERED. REFERENCE NON-ROUTINE 002723023 FOR WORK DETAILS ACCOMPLISHED. DIP INITIATED TO ACCOMPLISH INSPECTIONS PER SRM 5SDR AALA202506235494Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AROUND AFT LAVATORY VENT BETWEEN BS 907 AND BS 927, BETWEEN S21L AND S22L. ACCOMPLISHED DOUBLER REPAIR PER EA 365723.SDR DALA2025062204661Skin · ground damageAIRCRAFT 3092, WHILE ON THE LINE IN DCA, MAINTENANCE REPORTS A/C 3230 WING TIP FENCE MADE CONTACT WITH A/C 3092 ON THE NOSE RADOME (P/N: D53132210000) AND RH NOSE FWD FUSELAGE, SKIN PANELS (P/N: D5311007520100 & D5313320020000). THE RH FUSELAGE SKIN PANELS HAVSDR ASAA2025062059615Doubler · corrodedFWD CARGO ANTENNA DOUBLER STA 500 TO 500A BETWEEN STR 28L AND 28R HAS CORROSION. GROUNDED - YES. FWD CARGO ANTENNA DOUBLER STA 500-500A FOUND TO BE OUT OF LIMITS WITH 100% MATERIAL LOSS REMOVED AND REPLACED ANTENNA DOUBLER IAW B737-700 SRM 51-40-02-0G-0. W=3"SDR R61A2025071000302Doubler · corrodedUPON REMVOAL OF WASTE PAN NOTED CORROSON ON FWD LOWER CORNER. REMOVED AND REPLACED CFIII WASTE BOX DOUBLER. REF: EMB SRM 51-40-08SDR SWAA2025063083536Service Panel · corrodedPOSSIBLE CORROSION AT STA 850 AT THE WASTE TANK SERVICE PANEL ALONG STRINGER 25L.<[01] REMOVED AND REPLACED WASTE TANK SERVICE PAN ASSY IAW B737 SRM 51-40-02 AND BOEING DWG#DWG 146A7400-16#B ID:22;[02] 02 - INSPECTED PER B737 SRM 51-40-02 AND BOEING DWG# 146A7SDR DALA2025062404699Skin · damaged(LOG 1036381) DURING INSPECTION, DENT DAMAGE WAS DISCOVERED TO THE FUSELAGE SKIN AT STA 363 BETWEEN S-17L AND S-18L. DAMAGE REPAIRED PER ERA 626317-14.SDR DALA2025062004658Skin · corrodedAIRCRAFT 9509, CORROSION AT LOWER SKIN DOOR JAMB ON MIDDLE DOORSTOP (AFT CARGO COMPARTMENT). CORRECTIVE ACTION: (CORROSION LEVEL 2) DOOR JAMB ON MIDDLE DOOR TOP (AFT CARGO COMPARTMENT) WAS REPLACED PER B717-200 SRM 51-41-02-0G, B717-200 SRM 51-41-05-0G AND B71SDR DALA2025100207161Skin · corrodedFUSELAGE SKIN HAS CORROSION IN TWO AREAS ADJACENT TO THE FORWARD CARGO COMPARTMENT LOWER SCUFF PLATE ATTACH FASTENER HOLE 12OL. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 049-0001:5331-01297- 01C/003 00130 REPAIRED PER ER/A PRI 626491-14 REV. 0, REV. 1, REV. 2,SDR SWAA2025072983670Skin · corrodedCORROSION ON EXTERNAL SKIN VACUUM WASTE VENT CUTOUT LOCATED BTW BS 907 TO BS 927 AND BTW STR 21L TO STR 22L. PERFORMED PERMANENT REPAIR CATEGORY B LOC BTW BS 907 TO BS 927 AND BTW STR 20L TO STR 23L IAW B737-700 SRM 53-70-01-2R-3 AND EA#25-153-01844-WIP1 AND SDR ASAA2025061959414Doubler · corrodedBELLY DRAIN DOUBLER BS.737.37 BL.0 SHOWS SIGNS OF CORROSION. GROUNDED - YES. REMOVED CORROSION ON BELLY DRAIN DOUBLER AT STA.737.37 BL.0 ORIGINAL MAT .063" IAW BAC DWG #146A3239 REV:C, LOST .008", REMAINING .055" OF MATERIAL FOUND BEYOND LIMITS IAW B737-800 SRSDR GTIA2025062338964Skin Panel · corrodedCORROSION ON INTERNAL STRUCTURE BTW FR.16 AND FR.17 AT LEVEL OF LH LO WER STRINGER IN LATERAL AVIONIC COM LH (CPCP RELATED REFER TO THE MPD TASK: 531164-01) PERFORMED PERMANENT REPAIR OF THE LH NOSE FWD FUSELAGE NLG REINFORCEMENT DOUBLER AT STR 40L BTW FR 16-
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