JASC 5320
Service difficulty reports · 216,159
Reports filed under 5320 · Fuselage Miscellaneous Structure, 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 = '5320' 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 = '5320' 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 ASAA2024071351335Shield · corrodedAFT PIT, AFT SHIELD HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT, AFT SHIELD IAW B737-800 SRM 53-60-15-1A-1. ORIG. THICKNESS IS .050" IAW B737-800 SRM 53-60-15-01-1. REMOVED .025" REMAINING THICKNESS IS .025" AND IS FOUND TO BE OUT OF LIMITS ISDR SWAA2024072612065Channel · corrodedAFT CARGO R/H 'Z' CHANNEL FROM STA 727C TO 727D HAS 1 SPOT WITH CORROSION. (MARKED)<[01] REMOVED CORROSION; PERFORMED UT THICKNESS INSPECTION; CHECKED LIMITS OF REWORKED AREA; TREATED; PRIMED AND APPLIED TOPCOAT TO AFT CARGO R/H Z CHANNEL FROM STA 727C TO 727DSDR ASAA2024071351288Support · corrodedFWD PIT, AFT BULKHEAD LOWER SUPPORT IS CORRODED. GROUNDED - YES. REMOVED CORROSION FROM THE FWD PIT, AFT BULKHEAD LOWER SUPPORT IAW B737-800 SRM 53-30-08-1A-1.2.C AND IS FOUND TO HAVE 100% MATERIAL LOSS IAW B737-800 SRM 53-30-08-1A-1.4.(2). REMOVED AND REPLACESDR ASAA2024071351287Transition Panel · corrodedAFT PIT R/H TRANSITION PANEL STA 727 TO 727F+11 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT R/H TRANSITION PANEL AT STA 727 TO 727F+11 IAW B737-800 SRM 53-00-53-1A-2. ORIG. THICKNESS IS .040" IAW B737-800 SRM 53-60-53-01-2. REMOVED .020" REMASDR ASAA2024071351286Transition Panel · corrodedAFT PIT R/H TRANSISTION PANEL STA 727F+11 TO 767 HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM AFT PIT R/H TRANSITION PANEL AT STA 727F+11 TO 767 IAW B737-800 SRM 53-00-53-1A-2. ORIG. THICKNESS IS .040" IAW B737-800 SRM 53-60-53-01-2. REMOVED .020" REMSDR ASAA2024071351285Transition Panel · corrodedFWD PIT R/H TRANSITION PANEL STA 500C+15 TO 500I IS CORRODED. GROUNDED - YES. REMOVED THE CORROSION FROM THE FWD PIT R/H TRANSITION PANEL AT STA 500C+15 -500I IAW B737-800 SRM 53-00-53-1A-2.2.D. ORIG THICKNESS IS .040" IAW B737- 800 SRM 53-30-53-1A-2. TABLE 2.SDR DALA2024072207329Sill Drain · corroded(LOG 0452380) CORROSION ON R1 DOOR MOP SILL WL-208, STA-277 TO STA-344 RBL-54. REMOVED AND REPLACED MOP SILL ON R1 DOOR WL-208 STA 277 TO 344 PER B737-800 SRM 51-40-02-OG AND DWG 141A8310.SDR AALA202407194106Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT BS 320, LBL 45. REPLACED INTERCOSTAL PER AARD 51-00-05-01.SDR YENA2024071601023Door Sill · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / FWD FUSELAGE / FWD CARGO DOOR SILL UNDERNEATH CARGO DOOR LOWER SCUFF PLATES / CORROSION – PERMANENT REPAIR; REFERENCES: /1/ AIRBUS CANADA REO-500-53-21-879 DESCRIPTION: DURING CURRENT CHECK ON N3077J (MSN: 55124) @ YMX, AVISDR DALA2024071607179Floor Support · cracked(LOG 0446938) AFT CABIN FLOOR SUPPORT HAS CORROSION BETWEEN STA 947 AND STA 967 AT RBL 48 WL 208.SDR DALA2024071507159Cusp Web · crackedCRACK ON CUSP WEB MEMBRANE STA 674 X=-46 AT PAX CAB. SUMMARY OF NRC 00499: CUSP WEB MEMBRANE STA 674 X=-46 AT PAX CAB WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG 219. (LP #0444565)SDR AALA202409275634Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON SHEAR PLATE LOCATED AT STR 23R BETWEEN FR 69 AND FR70 IN AFT GALLEY AREA. REPLACED SHEAR PLATE PER SRM 51-42-11-801.SDR AALA202409275067Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK ON AFT GALLEY SHEAR PLATE LOCATED BETWEEN FR 69 AND FR 70 AT STR 23L. REPLACED SHEAR PLATE PER SRM 51-42-11-801SDR SWIA202492000012Door Sill · corrodedGALLEY SERVICE DOOR SILL LOWER SEAL STRIKER CORRODED AT SCREW HOLES AS (MARKED) (C-CHECK RO 9/19/2024) INSTALLED NEW SERVICE DOOR SILL LOWER SEAL STRIKER P/N SH670-31412-7 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG# SH670-31950 REV-Y. ALL CHECKS GOOD. SDR VNAA202409010027Floor Support · corrodedCORROSION ON GALLEY FLOOR SUPPORTS (4EAS) LOCATED BTW FS 280.00 - FS 295.00 AND AT FUSELAGE FLOOR STRUCTURE. GALLEY FLOOR SUPPORTS (4EAS) LOCATED BTW FS 280.00 - FS 295.00 AND AT FUSELAGE FLOOR STRUCTURE WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01SDR VNAA202409010025Floor Support · corrodedCORROSION ON UPPER FACE OF FLOOR SUPORT RBL 9.00 BTW FS 1000.00 TO FS 1069.75 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE. UPPER FACE OF FLOOR SUPPORT RBL 9.00 BTW FS 1000.00 TO FS 1069.75 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPAIRED PER REO 690-53-61-1SDR AALA202408278149Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SILL AT AFT GALLEY AREA BETWEEN FR 66 AND FR 68 AT S23R. REPLACED LOWER SILL PER SRM 51-72-11.SDR SWAA2024082311854Intercostal · corrodedCORROSION ON INTERCOSTAL LOCATED BETWEEN BS 986.5 TO BS 1006 AND LBL 12 AND WL 208.1 AFT GALLEY AREA . 2024-443526<[01] REPLACED INTERCOSTAL LOCATED BETWEEN BS 986.5 TO BS 1006 AND LBL12 AND WL 208.1 AFT GALLEY AREA IAW B737-700 SRM 51-10-02 ; ITEM 9 ; SRM 51-SDR SWAA2024082311855Angle · corrodedCORROSION ON INNER CHORD LOCATED BETWEEN BS 927 TO BS 986.5 RBL 46 AND WL 208.1 AT AFT GALLEY AREA. 2024-443527<[01] TOOL USED IN STEP#4; TOOL USED: ULTRASONIC THICKNESS GAGES; P/N:45MG; S/N:130064101; CAL DUE DATE: 13-DEC-24;[02] REPLACED INNER CHORD LOCATED SDR SWAA2024082211853Strap · corrodedCORROSION ON STRAP LOCATED BETWEEN BS 1006 TO BS 1016 AND LBL 6 WL 208.1 AT AFT GALLEY AREA. 2024-443524<[01] REPLACED STRAP AND FASTENERS LOCATED BETWEEN BS 1006 TO BS 1040 LBL 6 WL 208.1 AFT GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 SDR SWAA2024082212146Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED FLOOR STRUCTURE STA 867 BTW STR 26L TO STR 27L AT AFT CARGO COMPARTMENT. REPLACED ANGLE - SUPPORT LOCATED FLOOR STRUCTURE STA 867 BTW STR 26L TO STR 27L AT AFT CARGO COMPARTMENT IAW SRM 51-10-02-0G ITEM 9; 51-40-02 & DWG 149A810SDR SWAA2024082212145Web · corrodedCORROSION BILGE AREA WEB AT S-25R AND WL 156.4 AND BETWEEN STA 767 TO STA 794 AT AFT CARGO COMPARTMENT 2024-443551<[01] REPLACED WEB AND FASTENERS LOCATED BILGE AREA AT STRINGER 25R AND WL 156.4 AND BETWEEN STA 767 TO STA 794 AT AFT CARGO COMPARTMENT IAW BOEINSDR SWAA2024082212148Angle · crackedCRACK ANGLE FWD POSITION LOCATED BTW STA 907 TO STA 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT 2024-443556<[01] REPLACED ANGLE FWD POSITION LOCATED BTW STA 907 TO STA 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-0SDR SWAA2024082212149Angle · crackedCRACK ANGLE AFT POSITION LOCATED BTW STA 907 TO STA 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT 2024-443558<[01] REPLACED ANGLE AFT POSITION LOCATED BTW STA 907 TO STA 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-0SDR SWAA2024082212147Scuff Plate · crackedCRACK SCUFF PLATE SERVICE DOOR AT FWD GALLEY AREA 2024-443559<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N:B23272676; DUE DATE: 17-MAR-25.;[02] STEP 4 RADIOMETER TOOL USED PN: XRP -3000; SN: 1753759. DUE DATE: 07-DEC-24;[03] REPAIRED CENTER SCUFF PLATE SDR SWAA2024081511961Support Angle · crackedMAIN EBAY OXYGEN BOTTLE SUPPORT ANGLE CRACKED BS362 RBL10 WL158. MARKED<[01] REMOVED AND REPLACED NEW OXYGEN CYLINDER SUPPORT RING ON BS362 RBL10 WL158 IAW SRM 51-40-02;[02] VERIFIED CORRECTIVE ACTIONSDR SWAA2024081411842Intercostal · crackedINTERCOSTAL CRACKED AT STR15L STA.294.5<[01] JOB WAS ACCOMPLISHED ON EA 24-153-02000 FAULT # TTG8Q00USB2D;[02] VERIFIED STEP 1SDR SWAA2024080912038Intercostal · crackedPASSENGER CABIN; L-1 DOOR; FWD SIDE; STRUCTURAL INTERCOSTAL HAS CRACK BTW STA 294.5 & 303.9; STR 16L. MARKED.<[01] INSTALLED NEW INTERCOSTAL AT L1 DOOR FWD SIDE BS 294.5 TO 309.9; STR 16L PER SRM 51-40-02-0G-0 AND DWG 141A8180;[02] REMOVED REVEAL PANEL TO BE ISDR SWAA2024080811648Channel · corroded**CORROSION** AFT CARGO L/H SIDE 'Z' CHANNEL FASTENER HOLE AT STA 774.5 HAS CORROSION **CORROSION** AFT CARGO R/H SIDE 'Z' CHANNEL FASTENER HOLE AT STA 774.5 HAS CORROSION<[01] REFERED TO TASK CARD TTG8Q00UJU5V.;[02] VERIFIED STEP 1. TTG8Q00UJU5VSDR SWAA2024080811649Channel · corroded**CORROSION** AFT CARGO R/H SIDE 'Z' CHANNEL FASTENER HOLE AT STA 727A+2 HAS CORROSION<[01] REFERED TO TASK CARD TTG8Q00UJU5V.;[02] VERIFIED STEP 1. TTG8Q00UJU5VSDR SWAA2024080811652Channel · corroded**CORROSION** AFT CARGO R/H SIDE 'Z' CHANNEL FASTENER HOLE AT STA 727A+6 HAS CORROSION<[01] REMOVED AND REPLACED Z CHANNEL AT AFT CARGO COMPT R/H SIDE FROM STA 727 TO STA 767 PER REF SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 53-00-53-2R-5 AND DWG#146A7502.;[02SDR SWAA2024080811653Channel · corroded**CORROSION** AFT CARGO R/H SIDE 'Z' CHANNEL FASTENER HOLE AT STA 727C HAS CORROSION<[01] REFERED TO TASK CARD TTG8Q00UJU5V.;[02] VERIFIED STEP 1. TTG8Q00UJU5VSDR SWAA2024080811654Channel · corroded**CORROSION** AFT CARGO R/H SIDE 'Z' CHANNEL FASTENER HOLE AT STA 749 HAS CORROSION<[01] REFERED TO TASK CARD TTG8Q00UJU5V.;[02] VERIFIED STEP 1. TTG8Q00UJU5VSDR SWAA2024080811655Channel · corroded**CORROSION** AFT CARGO R/H SIDE 'Z' CHANNEL FASTENER HOLE AT STA 757 HAS CORROSION<[01] REFERED TO TASK CARD TTG8Q00UJU5V.;[02] VERIFIED STEP 1. TTG8Q00UJU5VSDR SWAA2024080811656Channel · corroded**CORROSION** AFT CARGO R/H SIDE 'Z' CHANNEL FASTENER HOLES AT STA 727E+2; 727E+6; 727E+10 HAS CORROSION<[01] REFERED TO TASK CARD TTG8Q00UJU5V.;[02] VERIFIED STEP 1. TTG8Q00UJU5VSDR SWAA2024080811657Channel · corroded**CORROSION** AFT CARGO R/H SIDE 'Z' CHANNEL FASTENER HOLES (2EA) AT STA 727E+14; AND 727E+18 HAVE CORROSION<[01] REFERED TO TASK CARD TTG8Q00UJU5V.;[02] VERIFIED STEP 1. TTG8Q00UJU5VSDR SWAA2024080811658Channel · corroded**CORROSION** AFT CARGO R/H SIDE 'Z' CHANNEL FASTENER HOLES (2EA) AT STA 727D+15; AND 727D+19 HAVE CORROSION<[01] REFERED TO TASK CARD TTG8Q00UJU5V.;[02] VERIFIED STEP 1. TTG8Q00UJU5VSDR SWAA2024080811662Channel · corroded**CORROSION** AFT CARGO L/H SIDE 'Z' CHANNEL FASTENER HOLE AT STA 761 HAS CORROSION<[01] REFERED TO TASK CARD #TTG8Q00UJUB5;[02] VERIFIED--TTG8Q00UJUB5SDR SWAA2024080811659Channel · corroded**CORROSION** AFT CARGO L/H SIDE 'Z' CHANNEL FASTENER HOLE AT STA 757 HAS CORROSION<[01] REMOVED AND REPLACED L/H Z CHANNEL AT AFT CARGO COMPT FROM STA 727 TO STA 847 PER REF SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 53-00-53-2R-5 AND DWG#146A7502.;[02] VERIFISDR SWAA2024080811660Channel · corroded**CORROSION** AFT CARGO L/H SIDE 'Z' CHANNEL FASTENER HOLE AT STA 753 HAS CORROSION<[01] REFERED TO TASK CARD #TTG8Q00UJUB5;[02] SEE CUSTOMER BARCODE TTG8Q00UJUB5 FOR CORRECTIVE ACTION.SDR SWAA2024080811661Channel · corroded**CORROSION** AFT CARGO L/H SIDE 'Z' CHANNEL FASTENER HOLES (2EA) AT STA 727D+9; AND 727D+10 HAS CORROSION<[01] REFERED TO TASK CARD #TTG8Q00UJUB5.;[02] SEE CUSTOMER BARCODE TTG8Q00UJUB5 FOR CORRECTIVE ACTION.SDR AALA202408046428Floor Support · brokenAIRCRAFT IN BASE MAINTENANCE: PASSENGER CABIN INTERCOSTAL FROM STA 328 TO STA 344, LBL 45, BROKEN. REPLACED INTERCOSTAL PER AARD 51-00-05 01.SDR AALA202408044860Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON R2 DOOR SILL INNER CHORD (CREASE ANGLE) FROM STA 967 TO STA 986.5, RBL 54. REPLACED CHORD PER AARD 51-00-05 .SDR R61A2024072900341Shear Angle · corrodedDUE TO AFT LAV SPILL,CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 76 BETWEEN STRINGERS 28R-29R CORRODED. REMOVED AND REPLACED CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 76 BETWEEN STRINGERS 28R-29R REFER SRM 51-40-08SDR R61A2024072900340Shear Angle · corrodedDUE TO AFT LAV SPILL,CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 76 BETWEEN CENTER LINE AND STRINGER 29L CORRODED. REMOVED AND REPLACED CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 76 BETWEEN CENTER LINE AND STRINGER 29 REFER SRM 51-40-08 .SDR R61A2024072900339Shear Angle · corrodedDUE TO AFT LAV SPILL,CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 75 BETWEEN STRINGERS 28R-29R CORRODED. REMOVED AND REPLACED CENTER FUSELAGE III AFT CARGO, SHEAR CLIP AT FRAME 75 BETWEEN STRINGERS 28R-29R. REF EMB SRM 51-40-08SDR R61A2024072900338Shear Angle · corrodedDUE TO AFT LAV SPILL,CENTER FUSELAGE III AFT CARGO, SHEAR CLIP ON FRAME 74 BETWEEN CENTER LINE AND STRINGER 29L CORRODED. REMOVED AND REPLACED CENTER FUSELAGE III AFT CARGO, SHEAR CLIP AT FRAME 74 BETWEEN CENTER LINE AND STRINGER 29L. REF EMB SRM 51-40-- 08.SDR IPXA2024072076571Bracket · crackedCRACKED BRACKET MEC INTERIOR COMPARTMENT LH FWD UPPER FLIGHT DECK COCKPIT FLOOR BEAM SUPPORT AT STA 246 LBL 50. (REPLACE) 1.FABRICATE P/N(141T5146-16) PER BOEING DWG NO.141T5146 SH 15 REV."B";PL REV."F";PSDL REV."-"AND ORIGINAL PART AS A SAMPLE I.A.W. GMM-MTX SDR DALA2024072207339Channel · corroded(LOG 0452658) CORROSION ON L/H AFT CARGO ZEE CHANNEL STA 727B-827 LBL 21 WL 156. REMOVED & REPAIRED L/H ZEE CHANNEL IN AFT CARGO FROM STA 727-STA 847 W/REPAIR SPLICES @ STA 767+8" & 727G+11" IAW B737 SRM 53-00-53-2R-5 & BOEING DWG# 146A7500 REV: C.SDR DALA2024072207335Channel · corroded(LOG 0452529) CORROSION ON REPAIR REINFORCEMENT CHANEL AT STA 727I+5", RBL3 AND WL155. REMOVED AND REPLACED REPAIR REINFORCEMENT CHANNEL PER B737-800 SRM 53-00-53-2R-2.
Back to JASC 5320