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 SWAA2025012377907Web · crackedCRACK ON WEB LOCATED BTW BS 328 TO BS 344 LBL 47.5 WL 208.1 AT FWD GALLEY AREA 2024-766856<[01] REPLACED WEB LOCATED BTW BS 328 TO BS 344 LBL 47.5 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 DWG 141A5400 SHEET 44 REV-.SEE INDIVIDUAL SIGN OFF BELOW.;[SDR SWAA2025012378182Stiffener · corrodedCORROSION STIFFENER LOCATED BTW BS947.5 TO BS967 RBL 50 WL 208.1 AT AFT GALLEY AREA 2024-764549<[01] TOOL USED P/N: 45MG; S/N: 130066401; CAL DUE: 21-OCT-25.;[02] REPLACED STIFFENER AND FASTENERS LOCATED BTW BS947.5 TO BS967 RBL 50 WL 208.1 AT AFT GALLEY AREA SDR SWAA2025012378184Stiffener · corrodedCORROSION STIFFENER LOCATED BTW BS967 TO BS986.5 LBL 17 WL 208.1 AT AFT GALLEY AREA 2024-764554<[01] REPLACED STIFFENER AND FASTENERS LOCATED BTW BS967 TO BS986.5 LBL 17 WL 208.1 AT AFT GALLEY AREA IAW B737-800 SRM-51-40-02; SRM-51-10-02 ITEM 9 AND DWG:140A987SDR SWAA2025012378183Angle · corrodedCORROSION ANGLE LOCATED BTW BS927 TO BS947.5 LBL 23 WL 208.1 AT AFT GALLEY AREA 2024-764553<[01] REPLACED ANGLE LOCATED BTW BS927 TO BS947.5 LBL 23 WL 208.1 AT AFT GALLEY AREA I.A.W B373-800 SRM 51-40-02; SRM 51-10-02 ITEM 9. AND DWG 147A5400 SHEET: 21; REV: -SDR SWAA2025012378185Stiffener · corrodedCORROSION STIFFENER LOCATED BTW BS967 TO BS986.5 RBL 17 WL 208.1 AT AFT GALLEY AREA 2024-764557<[01] REPLACED STIFFENER AND FASTENER LOCATED BTW BS967 TO BS986.5 RBL 17 WL 208.1 AT AFT GALLEY AREA IAW B737-800 SRM-51-40-02; SRM-51-10-02 ITEM 9 AND DWG:140A9870SDR SWAA2025012378025Tie Clip · crackedCRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2024-766864<[01] REPLACED TIE CLIP LOCATED 277 AND S-10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A1110 SHEET 17 REV - DWG 141A8380 SHEET 1 REV D SEE INDIVIDUAL SIGN OFF BELOW.SDR SWAA2025012278210Intercostal · corrodedDOT#44 A-043 AFT CARGO COMPARTMENT RH INTERCOSTAL UNDER 'Z' ANGLE CORRODED AROUND NUTPLATE HOLES STA 747 TO 767 LBL 24 WL 156<[01] REMOVED CORROSION AND EVALUATED DAMGE ORIG 'T'.032 REMAINING .025 LOSS .007 FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-1 REMOVED ANDSDR SWAA2025012277912Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 294.5 TO BS 303.9 RBL 53 WL 208.1 AT FWD GALLEY AREA 2024-766859<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 294.5 TO BS 303.9 RBL 53 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A8310 SHEET 25.<BR>SDR SWAA2025012277911Web · crackedCRACK ON WEB LOCATED BTW BS 312 TO BS 328 LBL 47.5 WL 208.1 AT FWD GALLEY AREA 2024-766855<[01] REPLACED WEB LOCATED BTW BS 312 TO BS 328 LBL 47.5 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV -.SEE INDIVIDUAL SIGN OFF BELSDR SWAA2025012278219Angle · corrodedDOT#54 A-043 AFT CARGO COMPARTMENT AFT BKHD LOWER STAINTION ANGLE CORRODED STA 947 RBL 20 WL 156<[01] 04 - REPAIRED PER [EA EA-GENERAL (EA ATTACHED TO AN AIRCRAFT FAULT)];[02] COMPLETE<BR>AUDIT C/WSDR SWAA2025012288480Angle · crackedCRACK ON INNER CHORD LOCATE BS 303.9 LBL 53 WL 208.1 AT FWD GALLEY AREA 2024-766860<[01] REPLACED INNER CHORD AND INSULATION ANGLES (4 E/A) LOCATED BS 303.9 LBL 53 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0 AND DWG 142A0050 SHEET 15 REV-.;[02] SDR SWAA2025012277909Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1 AT FWD GALLEY AREA 2024-766858<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 143A5400 SHEET 38 REVSDR SWAA2025012277908Web · crackedCRACK ON INTERCOSTAL WEB LOCATED BTW BS 344 TO BS 360 RBL 33 WL 208.1 AT FWD GALLEY AREA 2024-766857<[01] REPLACED INTERCOSTAL WEB LOCATED BTW BS 344 TO BS 360 RBL 33 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 33 REV- SSDR AALA202501224374Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN CRASE ANGLE AT STA 994, RBL 45. REPAIRED ANGLE PER EA 360706.SDR AALA202501228190Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT STA 959 AT RBL 50. REPLACED INTERCOSTAL PER AARD 51-00-05-1.SDR SWAA2025012178198Web · corrodedDOT#23 A-043 FWD CARGO COMPARTMENT SILL WEB CORRODED STA 440 TO 480+10' RBL 26 WL 156<[01] LIMITS VERIFIED; ORIGINAL THICKNESS .045'; REMAINING THICKNESS .030'; MATERIAL LOSS OF .015'; LOSS OF UP TO .004' ALLOWED-OUT OF LIMITS IAW SRM 53-30-15-1A-1LOCATED & DRSDR SWAA2025012178200Angle · corrodedDOT#26 A-043 FWD CARGO COMPARTMENT LH 'Z' ANGLE CORRODED STA 500 TO 500I LBL 24 WL 156<[01] REMOVED CORROSION IAW SRM 51-10-02-0G-0; AND VERIFIED WITH 10X MAGNIFIER ALL REMOVED VERIFIED LIMITS; ORIGINAL THICKNESS .040'; REMAINING THICKNESS .033'; MATERIAL LOSSSDR SWAA2025012178202Web · corrodedDOT#34 A-043 AFT CARGO COMPARTMENT SILL WEB CORRODED AT STA 787+7' TO 847 RBL 24 WL 156<[01] REMOVED SILL WEB IAW SRM 51-40-02 VERIFIED NEW PART WITH PN 146A8123U25ATSMRO A TAG WN49364 IAW DRAWING 146A8340; REV: A STARTED DRILLING HOLES IAW SRM 51-40-05 FINISHSDR SWAA2025012178214Strap · corrodedDOT#46 A-043 AFT CARGO COMPARTMENT THRESHOLD STRAP BOTTOM SIDE NUTPLATE STRAP CORRODED AT STA 787+3' RBL 20 WL 156<[01] REMOVED AND REPLACED PER BOEING DWG: 146A8128 REV: B.;[02] COMPLETE<BR>AUDIT C/WSDR SWAA2025012178215Strap · corrodedDOT#47 A-043 AFT CARGO COMPARTMENT THRESHOLD STRAP BOTTOM SIDE NUTPLATE STRAP CORRODED AT STA 794.3' RBL 20 WL 156<[01] REMOVED AND REPLACED PER BOEING DWG: 146A8128 REV: -;[02] REFER TO FAULT TTG8Q00XNBFR WHERE E.A. 25-153-0082 WAS ADDED AS A SUBTASK;[03] COMSDR SWAA2025012177952Web · crackedCRACK WEB LOCATED BTW BS 270 TO BS 294 AT LEVEL BL0 AT FWD GALLEY AREA 2024-764534<[01] REPLACED WEB AND FASTENERS LOC. BTW BS 270 TO BS 294 AT LEVEL BL0 AT FWD GALLEY AREA IAW B737-800 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 141A5400; SHEET: SDR SWAA2025012177950Web · crackedCRACK WEB LOCATED BTW BS 340 TO 360 AT LBL 12 AT FWD GALLEY AREA 2024-764536<[01] REPLACED WEB AND FASTENERS LOCATED BTW BS 340 TO 360 AT LBL 12 AT FWD GALLEY AREA IAW B737-800 SRM-51-40-02; SRM-51-10-02 ITEM 9 AND DWG:141A5400 SHEET:46 REV:A. SEE INDIVIDUAL SSDR SWAA2025012177951Web · crackedCRACK WEB LOCATED BTW BS 340 TO BS 360 AT RBL 13 AT FWD GALLEY AREA 2024-764535 CRACK WEB LOCATED BTW BS 344 TO BS 360 AT RBL 13 AT FWD GALLEY AREA<[01] TOOL USED: ET EQUIPMENT; P N: NORTEC600D; SN: 60007161486; CAL DUE DATE: 06-SEP-25.;[02] PERFORMED PERMANENSDR SWAA2025012178199Shield · corrodedDOT#23 A-043 FWD CARGO COMPARTMENT AFT SHEILD CORRODED STA 500+6' TO 500+18' RBL 24 WL 156 CORRECTION: DOT 24<[01] REMOVED CORROSION IAW SRM 51-10-02-0G-0 AND VERIFIED WITH 10X MAGNIFIER GLASS; <BR>LIMITS VERIFIED; ORIGINAL THICKNESS .032'. REMAINING THICKNESSSDR SWAA2025012178205Angle · corrodedDOT#25 A-043 FWD CARGO COMPARTMENT RH 'Z' ANGLE CORRODED STA 500A TO 500I RBL 24 WL 156<[01] REMOVED CORROSION IAW SRM 51-10-02-0G-0; AND VERIFIED WITH 10X MAGNIFIER ALL REMOVED VERIFIED LIMITS; ORIGINAL THICKNESS .040'; REMAING THICKNESS .028'; MATERIAL LOSS SDR SWAA2025012178208Angle · corrodedDOT#40 A-043 AFT CARGO COMPARTMENT LH 'Z' ANGLE CORRODED STA 727D+10 TO 827 LBL 24 WL 156<[01] 01 - REMOVED AND REPLACED PER [SRM 53-00-53-2R-5-B00308 (REPAIR 5 - CARGO COMPARTMENT SIDEPLATE REPAIR BETWEEN FLOOR PANEL SPLICES - PERMANENT)];[02] C/W<BR>AUDIT C/SDR SWAA2025012178212Shield · corrodedDOT#43 A-043 AFT CARGO COMPARTMENT FWD SHIELD CORRODED AROUND NUTPLATE HOLES TOP AND BOTTOM STA 767 TO 787 RBL 24 WL 156<[01] REMOVED CORROSION AND EVALUATED DAMAGE IAW SRM .050 ORIG 'T' .035 REMAINING .015 LOSS FOUND OUT OF LIMITS IAW SRM 53-60-15-1A-1 REMOVESDR SWAA2025012178213Strap · corrodedDOT#45 A-043 AFT CARGO COMPARTMENT TOP STRAP AT THRESHOLD CORRODED AT NUTPLATE HOLE STA 787+8' RBL 20 WL 156<[01] REMOVED AND REPLACED PER BOEING DWG: 146A8120 REV: -;[02] C/W<BR>AUDIT C/WSDR SWAA2025012077814Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED BS867 BTW STR2R AND STR3R AT PASSENGER CABIN. REPLACED SUPPORT BRACKET AND FASTENERS LOCATED BS867 BTW STR2R AND STR3R AT PASSENGER CABIN IAW B737-800 SRM 51-40-02 AND DWG 146A7901 REV:A SHEET 66.SDR SWAA2025012078302Bracket · crackedCRACK BRACKET BS 947.5 AND STRINGER 26L AFT CARGO COMPARTMENT. REPLACED BRACKET BS 947.5 AND STRINGER 26L AFT CARGO COMPARTMENT I.A.W. SRM 51-40-02 AND DWG 149A8103 SHEET 8 REV. -SDR SWAA2025011678297Web · corrodedCORROSION SHIELD WEB BETWEEN BS 492 TO BS 500A AND RBL 21 WL 156 AT FWD CARGO COMPARTMENT 2024-763309<[01] REPLACED SHIELD WEB BETWEEN BS 492 TO BS 500A AND RBL 21 WL 156 AT FWD CARGO COMPARTMENT AND FASTENERS I.A.W B737-800 SRM 51-40-02; SRM 51-10-02 ITEM 9 ASDR SWAA2025011678300Web · corrodedCORROSION FLOOR STRUCTURE SHIELD WEB BETWEEN BS 767 TO BS 794 AND RBL 21 WL 156 AFT CARGO COMPARTMENT 2024-763317<[01] REPLACED SHIELD WEB BETWEEN BS 767 TO BS 794 AND RBL 21 WL 156 AFT CARGO COMPARTMENT IAW B737-800 SRM 51-40-02; DWG 146A0081; SHEET 46 AND RESDR SWAA2025011678303Intercostal · crackedCRACK WEB - INTERCOSTAL BETWEEN BS 927 TO BS 947.5 AND STRINGER 25R AFT CARGO COMPARTMENT 2024-763320<[01] REPLACED WEB-INTERCOSTAL BETWEEN BS 927 TO BS 947.5 AND STRINGER 25R AFT CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM AND 9; SRM 51-40-02 AND DWG: 14SDR DALA2025011600362Threshold · corrodedCORROSION ON FWD CARGO DOOR TRESHOLD LOCATED AT BETWEEN STA 440 TO STA 492, RBL 24 AND WL 156. REMOVED AND INSTALLED FWD CARGO DOOR THRESHOLD WEB FROM STA 440- STA 492.4 RBL 24 WL 156 IAW B737 SRM 51-40-02-0G AND BOEING DRAWING #143A8330, REV: A.SDR SWAA2025011577946Support Bracket · crackedCRACK SUPPORT BRACKET BODY STATION 540 AND RBL6 KEEL BEAM 2024-759614<[01] REPLACED SUPPORT BRACKET BODY STATION 540 AND RBL6 KEEL BEAM IAW B737-700 SRM51-10-02 ITEM 9;B737-700 SRM 51-40-02 AND DRAWING 212A1101 REV.;[02] CORRECTED STEP 1:<BR>REPLACED SUPPORT BSDR SWAA2025011577947Support Bracket · crackedCRACK SUPPORT BRACKET BODY STATION 540 AND LBL6 KEEL BEAM. REPLACED SUPPORT BRACKET BODY STATION 540 AND LBL6 KEEL BEAM IAW B737-700 SRM 51-10-02 ITEM 9 ;B737-700 SRM51-40-02 AND DRAWING 212A1101 REV.-;[02] REPLACED SUPPORT BRACKET BODY STATION 540 AND LBL6 KSDR SWAA2025010877963Intercostal · corrodedINTERCOSTAL LOCATED BETWEEN STAS 947-967; LBL 50 CORRODED ON UPPER SURFACE.<[01] EVALUATED CORROSION DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] COMPLIED WITH INSP.<BR>1. EVALUATED CORROSION DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM 53SDR SWAA2025010877964Intercostal · corrodedINTERCOSTAL LOCATED BETWEEN STAS 947-967; RBL 50 HAS CORROSION ON UPPER SURFACE.<[01] EVALUATED CORROSION DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] COMPLIED WITH INSP.<BR>1. EVALUATED CORROSION DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRSDR SWAA2025010877965Intercostal · corrodedINTERCOSTAL LOCATED BETWEEN STAS 947-967; RBL 25 HAS CORROSION ON UPPER SURFACE.<[01] EVALUATED CORROSION DAMAGE AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] COMPLIED WITH INSP.<BR>1. DAVID BELL (TECHNICIAN); 16-DEC-2024 18:06 UTC<BR>EVALUATED CORSDR AALA202501073251Fitting · wornAIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL FITTING WORN BETWEEN FR 23 AND FR 24 AT S32L. REPLACED LEFT HAND LATERAL FITTING PER EA 360120.SDR DALA2025010300038Floor Support · damaged(LOG 0741435) AFT WET AREA FLOOR SUPPORT STA 947-967 RBL 51 DAMAGED. REMOVED AND REPLACED FLOOR SUPPORT AT STA 947 TO 967 RBL 51 PER B737 - 800 SRM 51-40-02-0G AND DWG 147A5650 REV. A.SDR SWAA2024123077904Scuff Plate · crackedAFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] REPAIRED AFT CARGO BAY FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITHS STEPSSDR AALA202412247148Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT INTERCOSTAL LOCATED FROM STA 380 TO STA 400 AT LBL 12. REPLACED INTERCOSTAL PER AARD 51-00-05-1.SDR AALA202412249042Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL L BRACKET LOCATED FROM STA 380 TO STA 400 AT BL0 REPLACED L BRACKET PER SRM 53-00-02 AND AARD 51-00-05-1.SDR DALA2024121911848Channel · corrodedL4 DOOR THRESHOLD CENTER CHANNEL HAS CORROSION CENTER SCUFF PLATE. CORRECTIVE ACTION: ACCOMPLISHED L4 DOOR THRESHOLD CENTER CHANNEL PER ER/A 622637-14 REV ORIGINAL (0713232)SDR JJBA20241219046Floor Support · corrodedCF4, CENTER OMEGA BEAM FOUND CORRODED BTW FR 60-61. REPAIR DOUBLER ON CENTER FUSE IV CENTER OMEGA BEAM ON UPPER SURFACE BTW FR 60-61SDR JJBA20241219041Floor Support · corrodedCF3, LH OMEGA BEAM OUTBD STUB ANGLE BTW FR 46-50 FOUND CORRODED. LH OMEGA BEAM OUTBD STUB ANGLE BTW FR46-50 BLENDED OUT OF LIMITS. LH OMEGA BEAM OUTBD STUB ANGLE REMOVED FOR REPLACEMENT. NEW OMEGA BEAM OUTBD STUB ANGLES INSTALLED AND REPLACEDSDR BAGA2024121700319Pan · corrodedWASTEWATER PAN INTERNAL DOUBLER FOUND WITH CORROSION. PERFORMED REPAIR IN ACCORDANCE WITH EA.SDR DALA2024121711774Support · corrodedSHIP 3145 CORROSION INTERNAL STRUCTURE SUPORT BTW FR12 TO FR13 IN LATERAL AVIONIC COMP LH. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE SUPORT(WEB) LOCATED BTW FR12 TO FR13 IN LATERAL AVIONIC COMPART LH AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0713877)SDR DALA2024121711767Cusp Web · corrodedCORROSION ON LH CUSP WEB BTW STA Y=908 TO STA Y=927. SUMMARY OF NRC 00725: CORROSION LEVEL 2. CORROSION ON LH CUSP WEB BTW STA Y=908 TO STA Y=927 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4, PAR 6 FIG 208. (LP #0713769)
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