JASC 5321
Service difficulty reports · 49,350
Reports filed under 5321 · Fuselage Floor Panel, 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 = '5321' 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 = '5321' 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 SWAA2025030693047Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] COMPLETE;[02] AREAS OF PULLED STRANDS ON UPPER SURFACE OF AFT FLOOR PANEL 242VF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[03] VERIFIED CORRECTIVE ACTION ITEM 1 AND 2.SDR SWAA2025030693051Floor Panel · pulledFWD FLOOR PANEL 221EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221EF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.SDR SWAA2025030693058Floor Panel · pulledFWD FLOOR PANEL 222A UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222A UPPER SKIN STRAND DAMAGE WAS REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2025030693039Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241AAF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.SDR SWAA2025030693048Floor Panel · crackedAFT FLOOR PANEL 242XF IS CRACKED ACROSS CENTER OF PANEL.<[01] AFT FLOOR PANEL 242XF WITH CRACK ACROSS CENTER OF PANEL WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF DAMAGE.SDR SWAA2025030693056Floor Panel · pulledFWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.SDR SWAA2025030693053Floor Panel · pulledFWD FLOOR PANEL 221GF FWD O/B TANG IS CRACKED.<[01] FWD FLOOR PANEL 221GF O/B TANG REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2025030693055Floor Panel · pulledFWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222CF UPPER SKIN AREAS OF PULLED STRANDS WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2025022793536Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231AF IS DELAMINATED AT AFT L/H CORNER (MARKED) <[01]. REMOVED PASSENGER CABIN FLOOR PANEL 231AF PER AMM 53-21-00-000-801; [02] REMOVED & REPLACED; & INSTALLED FLOOR PANEL 231AF PER MM 53-21-00-000-801; SRM 51-10-02-0G-0 PARA 9 & ISDR AALA202502173288Floor Panel · puncturedAIRCRAFT IN BASE MAINTENANCE: CENTER TANK IN MID CABIN, LOCATED AT BS 540 AND RBL 25 THROUGH 41 PUNCTURE ON THE FLOOR PANEL. REMOVED AND REPLACED NEW PANEL CENTER TANK IN MID CABIN. PER B737-NG SRM 51-40-05-NG & SRM 51-40-02-0G.SDR FDEA202502050179Floor Panel · damagedVERIFY AFT R/H FLOOR PNL 252MWF HAS THE WRONG INSERTS INSTALLED AND HAS MISSING INSERTS AND HAS COMPOSITE DAMAGE THE ENTIRE LENGTH FABRICATED FLOOR PANEL 252MWF ON VTMAE TRAVELER #T25/1798171 IAW VTMAE DWG #11864182-49, MAJOR REPAIRSDR ASAA2025020456545Floor Panel · damagedFLOOR PANEL PN 146A5810-466 REQUIRES 2 INSERTS,. GROUNDED - YES. REPAIRED FLOOR PANEL 146A5810-466 OF 2 INSERTS IAW B737-800 SRM 53-00-50-2R-0.SDR SWAA2025030692615Floor Panel · pulledFLOOR PANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231YF; WITH UPPER SKIN AREAS OF PULLED STRANDS; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.SDR SWAA2025030692621Floor Panel · pulledFLOOR PANEL 241CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241CF UPPER SKIN HAS PULLED STRANDS REPAIRED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]SDR SWAA2025030692616Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241DF UPPER SKIN HAS PULLED STRAINDS REPAIRED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]SDR SWAA2025030692623Floor Panel · pulledFLOOR PANEL 241FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241FF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025030692619Floor Panel · pulledFLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 231ZF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025030692620Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025030692622Floor Panel · pulledFLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241EF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025030692624Floor Panel · pulledFLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 242AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025030592618Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF; WITH UPPER SKIN AREAS OF PULLED STRANDS; WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.SDR DALA2025020500880Spar Cap · crackedA CRACK COMMON TO THE RH WING LOWER REAR SPAR CAP. AS A PRECAUTION AN ER/A HAS BEEN ISSUED REQUIRING MAINTENANCE TO ACCOMPLISH INSPECTIONS OF THE LH WING LOWER REAR SPAR CAP TO ENSURE NO CRACKS ARE FOUND. SUMMARY SEE NRC 003-0001:0514-2001/042 00042: NR TRANSFSDR SWAA2025031492827Floor Panel · crackedCRACK FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT 2025-112623 <[01]. FABRICATED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT I.A.W B737-700 AMM 25-52-01-201-801 AND DWG 453A1610 SHEET: 7 REV: C. MATERIAL USED: ALUMINUM SHEET P/N: 2024T3-071 P/O: 2025 103758.; [0SDR FDEA202502030169Floor Panel · damagedMAIN DECK FLOOR PANEL 323MXF IN ZONE 230 DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 232MXF ON VT MAE TRAVELER # T25/1795188 IAW DWG 11862182 REV H. MAJOR REPAIR.SDR SWAA2025031092350Floor Panel · crackedCRACK FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT 2025-110408 <[01]. REPLACED FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801; B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 453A2610 SHEET 20 REV E. SEE INDIVIDUAL SIGN OFF BELOW.;SDR SWAA2025031091880Floor Panel · crackedCRACK FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT 2025-110336 <[01]. REPLACED FLOOR PANEL 140CF LOCATED AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DRAWING # 453A2610 SHEET 11 REV C. SEE INDIVIDUAL SIGN-OFF BELOW.; [02] CORRECTESDR IPXA2025020608620Floor Panel · corrodedDURING RCB WALL PREP FOR INSTALLATION, FOUND COURIER SIDE LWR SECTION CORRODED AT MULTIPLE AREAS, 25-59. REMOVE AND REPLACE RIGID CARGO BARRIER ASSEMBLY P/N WSP0798-505 PER MD11 AMM 25-59-13, DAC DWG SP11250229, AND PER MD11 SRM CHAPTER 51 GUIDELINES.SDR DALA2025042103113Floor Panel · puncturedON SVC CHECK FOUND PUNCTURE IN AFT CARGO FLOOR PANEL IN 36L LOCATION 3RD PANEL OUTBOARD FWD OF CARGO DOOR OPENING PANEL, REMOVED FOR REPAIRS. PERFORMED DAMAGE EVALUATION PER A350 ASR - A-51-77-10-00ZZZ- 660Z-A, DAMAGE FOUND OUT OF LIMITS, FABRICATED DOUBLER UPSDR SWAA2025030591460Floor Panel · crackedCRACK INNER CHORD LOCATED BS303.9 LBL55 AT FWD GALLEY AREA 2025-94180<[01] REPLACED INNER CHORD LOCATED AT BS 277 TO BS360 LBL55 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG:141A8110 SHEET: 9 REV:A. SEE INDIVIDUAL SIGN OFF BELOW;[0SDR ASAA2025013056109Floor Panel · delaminatedFLOOR PANEL PN 147A5810-23, HAS A DELAMINATION. GROUNDED - YES. PERFORMED PERMANENT REPAIRS ON FLOOR PANEL PN: 147A5810-23 IAW ASA B737-800 SRM 53-00-50-2R-0, ASA B737-800 SRM 53-00-50-2R-1, ASA B737-800 SRM 53-00-50-2R-7 & ASA B737-800 SRM 53-00-50-1A-1. NO FSDR FDEA202501300157Floorboard · dentedMAIN CARGO COMP. AT APROX. STA 360 & RBL54.75 TO RBL77.5 11 PANEL 222CFF ABOVE FLOOR SKIN HAS INDENTATION (MARKED) REPAIRED MAIN CARGO COMPT. (MARKED) DENTED AREAS AT STA.360 LBL 54.75 TO RBL 77.5 PNL# 222CFF MPN: 141T5856-116 TOP SKIN OF FLOORBOARD. IN SDR FDEA202501300156Floor Panel · dentedMAIN CARGO COMP. AT APROX. STA. 360 & RBL33 TO RBL11 PANEL 222AFF ABOVE FLOOR SKIN HAS INDENTATION (MARKED) REPAIRED MAIN CARGO COMPT. (MARKED) DENTED AREAS AT STA.360 RBL 33 TO RBL 11 PNL# 222AFF MPN: 141T5856-107 TOP SKIN OF FLOORBOARD. IN REF. TO 767 SRSDR FDEA202501300155Floor Panel · dentedMAIN CARGO COMP. AT APROX. STA 360 & LBL11 TO LBL33 PANEL 221DFF ABOVE FLOOR SKIN HAS INDENTATION (MARKED). REPAIRED MAIN CARGO COMPT. (MARKED) DENTED AREAS AT STA.360 LBL 11 TO LBL 33 PNL# 221DFF MPN: 141T5856-117 TOP SKIN OF FLOORBOARD. IN REF. TO 767 SSDR FDEA202501300150Floor Panel · damagedMAIN CARGO COMP. AT APROX. STA 360 & LBL11 TO RBL 11 PANEL 221CFF ABOVE FLOOR SKIN HAS INDENTATION (MARKED). REPAIRED MAIN CARGO DECK FLOORBOARD AT STA. 360 LBL 11 TO RBL 11 (MPN: 141T5856-105 / PNL# 221CFF) IN REF. B767 SRM 53-00-50-2R REPAIR 1 FIG.201 SSDR 2A6R2025013072201Floor Panel · chafedCHAFE DAMAGE WAS DISCOVERED ON THE COCKPIT FLOOR (PN: B531M8002101) WHERE THE SLANT CONSOLE MEETS THE COCKPIT FLOOR. AN APPROVED REPAIR PROCEDURE WAS COMPLIED WITH PER AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-BK117-53-2024-3227, ISSUE A DATED 17 OCT 2024, WHISDR SWAA2025022590999Floor Panel · pulledDOT#28 A-043 AFT CABIN FLOOR PANEL 241WF HAS PULLED FIBERS <[01]. REPAIRED IAW EA 25-153-00249 AND SRM 53-00-50-2R-1.;[ 02] C/W. AUDIT COMPLETE.SDR SWAA2025022590993Floor Panel · pulledDOT#36 A-043 AFT CABIN FLOOR PANEL 241ZF HAS PULLED FIBERS <[01]. 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.';[02] C/W;[03] C/W. AUDIT COMPLETE.SDR SWAA2025022590997Floor Panel · pulledDOT#41 A-043 AFT CABIN FLOOR PANEL 241ABF HAS PULLED FIBERS <[01]. 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.';[02] C/W;[03] C/W. AUDIT COMPLETE.SDR SWAA2025022591005Floor Panel · pulledDOT#42 A-043 AFT CABIN FLOOR PANEL 241AAF HAS PULLED FIBERS <[01]. 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.';[02] C/W;[03] C/W. AUDIT COMPLETE.SDR SWAA2025022591096Floor Panel · corrodedDOT L7-005: AFT CARGO FLOOR PANEL 140BF HAS CORROSION AT FASTENER HOLES<[01] EVALUATED CORROSION ON FLOOR PANEL 140BF WITH THE TOTAL ACCUMULATED DAMAGE LENGTH IS 32' WERE IS A MAXIMUM OF 20' ON ALLOWABLE DAMAGE; THEREFORE IS OUT OF LIMITS; MECHANICALLY MEASURESDR SWAA2025022591098Floor Panel · pulledDOT L7-006: AFT CARGO FLOOR PANEL 140EF HAS CORROSION AT FASTENER HOLES<[01] FABRICATED NEW FLOOR PNL. 140EF IAW AMM 25-52-10-400-801;[02] VERIFIED STEP 1.<BR>AUDIT C/WSDR SWAA2025022190990Floor Panel · pulledDOT#29 A-043 AFT CABIN FLOOR PANEL 241UF HAS PULLED FIBERS <[01]. 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.'; [02] C/W AUDIT COMPLETE.; [03] C/W AUDIT COMPLETE.SDR SWAA2025022191002Floor Panel · pulledDOT#33 A-043 AFT CABIN FLOOR PANEL 242UF HAS PULLED FIBERS <[01]. 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.';[02] C/W;[03] C/W AUDIT COMPLETE.SDR SWAA2025022191003Floor Panel · pulledDOT#34 A-043 AFT CABIN FLOOR PANEL 242D HAS PULLED FIBERS <[01]. 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.';[02] C/W;[03] C/W AUDIT COMPLETE.SDR SWAA2025022190992Floor Panel · pulledDOT#35 A-043 AFT CABIN FLOOR PANEL 241XF HAS PULLED FIBERS <[01]. 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.';[02] C/W;[03] C/W AUDIT COMPLETE.SDR SWAA2025022190994Floor Panel · pulledDOT#37 A-043 AFT CABIN FLOOR PANEL 241D HAS PULLED FIBERS <[01]. 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.';[02] C/W;[03] C/W. AUDIT COMPLETE.SDR SWAA2025022190998Floor Panel · pulledDOT#43 A-043 AFT CABIN FLOOR PANEL 242F HAS PULLED FIBERS <[01]. 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.'; [02] C/W; [03] C/W. AUDIT COMPLETE.SDR SWAA2025022191006Floor Panel · pulledDOT#44 A-043 AFT CABIN FLOOR PANEL 241F HAS PULLED FIBERS<[01] 'REFER TO FAULT TTG8Q00YEEQ1 WHERE EA 25-153-00249 WAS ADDED AS A SUBTASK.';[02] C/W;[03] C/W. AUDIT COMPLETE.SDR SWAA2025021991051Floor Panel · pulledFLOOR PANEL 231XF HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 231XF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2025021991052Floor Panel · pulledFLOOR PANEL 241DF HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 241DF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED PER [SRM 53-00-50-2R-0-A00938 (REPAIR GENERAL - COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.
Back to JASC 5321