JASC 5321
Service difficulty reports · 49,369
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 SWAA2022011259763Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241AF HAS PULLED FACE SHEET PLIES; EVALUATED DAMAGE; UPPER FACE SHEET IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1; TAP TEST GOOD; NO DELAMINATION NOTED.<BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS A;CSDR SWAA2022011259759Floor Panel · pulledA22-05; PASSENGER CABIN FLOOR PANEL 242AF HAS PULLED FACE SHEET PLIES; MRK'D. ; / [01] EVALUATED AND FOUND MISSING FIBERS ON TOP SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1. TAP TEST GOOD.<BR><BR>CLEANED AND PREPPED SDR SWAA2022011259766Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241BF HAS PULLED FACE SHEET PLIES; EVALUATED DAMAGE; DAMAGE TO UPPER FACE SHEET IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1. TAP TEST GOOD NO DELAMINATION NOTED.<BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 53-00-50-2R-1 PAR 3 SDR SWAA2022011259762Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 231ZF HAS PULLED FACE SHEET PLIES; EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAS SRM 53-00-50-2R-1. TAP TEST GOOD. CLEANED AND PREPARED IAW SRM 53-00-50-2R-1 STEP 3SDR SWAA2022011259760Floor Panel · pulledA22-06; PASSENGER CABIN FLOOR PANEL 232RF HAS PULLED FACE SHEET PLIES; MRK'D. ; / [01] EVALUATED PANEL 232RF AND FOUND AREA OF PULLED FIBERS ON UPPER SURFACE TO ONE PLY. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A REV 75. CLEAN AND PREP AREA SDR SWAA2022011259749Floor Panel · pulledA22-04; PASSENGER CABIN FLOOR PANEL 232SF HAS PULLED FACE SHEET PLIES; MRK'D. ; / [01] EVALUATED PANEL 232SF AND FOUND AREA OF PULLED FIBER'S TO ONE PLY ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A REV75. CLEAN AND PREP AREA SDR SWIA202264690None · cracked*LEFT COCKPIT FLOOR BEAM AT BL12 IS CRACKED IN THE FLANGE ATTACH POINT WITH THE FS280.00 BULKHEAD. (C CHECK RO 02/25/2022) REPAIRED LH COCKPIT FLOOR BEAM AT LBL 12.00 FS 280.00 REF CRJ700 53-11-43-201-003-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY AND FOSDR SWIA202264689None · cracked*RIGHT COCKPIT FLOOR BEAM AT BL12 IS CRACKED IN THE FLANGE ATTACH POINT WITH THE FS280.00 BULKHEAD. (C CHECK RO 02/25/2022) REPAIRED RH COCKPIT FLORR BEAM AT RBL 12.00 FS 280.00 REF CRJ700 53-11-43-201-003-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY AND FSDR DALA2022011000184None · noneSHIP 6822 CORROSION ON STIFFENER BULKHEAD BSTA 900 AND LBBL 7.50 AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00309: STIFFENER BULKHEAD STA 900 AND LBL 7.50 AT FWD CARGO COMPARTMENT WAS REPLACED PER DWG REV. ORIGINAL AND B757-200 SRM. (2078635)SDR SWAA2022021459039Floor Panel · brokenBROKEN FLOOR PANEL 221BF AT PASSENGER CABIN ; 2021-585140 / [01] TOOL USED CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE: 29/SEP/22.; [02] TOOL USED: MICRO HOT BONDER PN:HCS8800 SN:01112550 DUE DATE:24-AUG-22.; [03] TOOL USED: SCALE PN:CL5000 SN:AE-408753 DUSDR DALA2022011000181None · noneSHIP 6822 CORROSION ON PLATE OF WASTE WATER PANEL BETWEEN S-27RH/ S-29RH AND STA 1540/ STA 1560 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00175-PLATE (INTERCOSTAL) OF WASTE WATER PANEL BETWEEN S-27RH/ S-29RH AND STA 1540/ STA 1560 IN AFT CARGSDR AALA202201076845Floor Panel · delaminatedAIRCRAFT WAS GROUNDED: AFT CARGO COMPARTMENT PANEL 151LF DELAMINATED/SPONGY. REPLACED AFT CARGO COMPARTMENT FLOOR SECTION 151LF AS PER AMM 53-42-14.SDR DALA2022010700126None · noneSHIP 3267 CORROSION FLOOR BEAM +Y512 LOCATED BETWEEN FR67 TO FR70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11, AND 51-72-11. (2077330)SDR AALA202201066745Floor Panel · delaminatedAIRCRAFT WAS GROUNDED: FORWARD CARGO COMPARTMENT PANEL 131EF DELAMINATED / SPONGY. REPLACED FORWARD CARGO COMPARTMENT FLOOR SECTION 131EF AS PER AMM 53-22-12.SDR SWAA2022013158749Floor Panel · crackedSUPPLEMENTAL INFORMATION: CRACK ON PASSENGER CABIN FLOOR PANEL SUPPORT AT BS 540 LBL 1-22. ; / [01] NO LIMITS FOUND FOR CRACK ON SRM FOR PANEL BREAK SUPPORT PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C; [02] REMOVED PANEL BREAK SUPPORT BS540SDR SWAA2022013158746Support · crackedSUPPLEMENTAL INFORMATION: CRACK ON PASSENGER CABIN FLOOR PANEL SUPPORT AT BS 540 RBL 1-22. ; / [01] REMOVED FLOOR PANEL 231UF FOR ACCESS I.A.W AMM 53-21-00-000-801; [02] NO LIMITS FOUND FOR CRACK ON SRM FOR PANEL BREAK SUPPORT PART TO BE REMOVED AND REPLACED ISDR SWIA202264524None · crackedCENTER COCKPIT FLOOR BEAM AT RBL12 FS274 CRACK (C CHECK RO 2/17/2022) CUT OUT DAMAGED COCKPIT FLOOR BEAM SECTION AT RBL 12, FS274.00. FABRICATED AND INSTALLED NEW FLOOR BEAM SECTION. REF. CRJ700 SRM 53-11-43-201-003-A01 REPAIR TYPE 4, FIG. 53-11-43-995-819SDR SWIA202264523None · crackedCENTER COCKPIT FLOOR BEAM AT LBL12 FS274 CRACK (C CHECK RO 2/17/2022) INSTALLED ALL REPAIR PARTS LH COCKPIT FLOOR BEAM SECTOR, 2EA ANGLE AND 2EA SPLICES AT LBL12 FS274 REF. CRJ700 SRM 53-11-43-201-003-A01 TYPE 4. ALSO COMPLIED WITH 51-900-1002-SKY. SEE CONSDR SWAA2022020858732Floor Panel · delaminatedFORWARD CABIN FLOOR PANEL 222AF HAS A DELAMINATION ON THE UPPER SKIN AT AFT O/B CORNER ; / DAMAGE WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4F.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1.; REMOVED ALL DAMAGED SKIN AND LOOSE PIECESDR SWAA2022013158696Floor Panel · pulledA-061 DOT 016. CABIN FLOORBOARD 221BF UPPER SURFACE FIBERS PEELING ; / [01] EVALUATED AND FOUND DAMAGED FIBERS ON UPPER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED AREA FOR REPAIR IAW SRM 53-00-50-2RSDR SWAA2022013158698Floor Panel · damagedA-061 DOT 017. CABIN FLOORBOARD 221AF R/H OUTBD EDGE DAMAGED ; / [01] EVALUATED AND FOUND EDGE DAMAGE WITH DAMAGED FIBERS TO UPPER FACE SHEET AND REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53SDR SWAA2022013158694Floor Panel · crackedA-061 DOT 018. CABIN FLOOR BOARD 222CF FACE SHEET CRACKED UPPER SURFACE ; / [01] EVALUATED AND FOUND MULTIPLE AREAS OF DAMAGED FIBERS TO UPPER FACE SHEET AND REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACSDR SWAA2022013158938Floor Panel · pulledCABIN FLOOR PANEL 231CF; UPPER SURFACE HAS PULLED FACE SHEET PLIES. ; / [01] EVALUATED AND FOUND DAMAGED FIBERS ON UPPER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1 <BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2RSDR SWAA2022011058546Floor Panel · crackedAFT CARGO FLOOR PANEL 2ND PANEL FROM FRONT CRACKED APPROX 20 INCHES / [01] INSTALLED NEW PANEL REF AMM 25-52-10; [02] C/WSDR DALA2022011000171None · noneSHIP 6822 DENT ON FRAME AT STA 1540 AND S-26L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00316-DENT ON FRAME AT STA 1540 AND S-26L IN AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM. (2075513)SDR FDEA202201050009Floor Panel · damagedMAIN CABIN, APPROX. STA. 745 LBL 8, FLOOR IS DAMAGED. FABRICATED NEW FLOOR PANEL PER FEDEX INTERNAL DRAWING SRZ-25-005SDR SWIA202264636None · crackedCOCKPIT CENTER FLOOR BOARD RH SUPPORT ANGLE P/N CC670-33199-4 IS CRACKED. (C CHECK RO 02/22/2022) REMOVED AND REPLACED COCKPIT CENTER FLOOR BOARD RH SUPPORT ANGLE P/N CC670-33199-4. REF. CRJ700 SRM 51-42-06-001-001-A01 AND DWG# CC670-33052 REV. -F / COMPLSDR SWAA2022020757925Floor Panel · delaminatedMAIN CABIN FLOOR PANEL #222DF HAS A HOLE ELONGATED AND DELAMINATION. ; / [01] CLEANED AND PREPARED FOR REPAIR AT MAIN CABIN FLOOR PANEL #222DF AS PER B737-700 SRM 53-00-50-2R-9; [02] VERIFIED STEP 1. OK TO INSTALL REPAIR.; [03] INSTALLED REPAIRED AT MAIN CABINSDR SWAA2022013158472Floor Panel · pulledA22-012; CABIN FLOOR PANEL 241UF; UPPER SURFACE HAS PULLED FACE SHEET PLIES; MRK'D ; / [01] EVALUATED PANEL 241UF AND FOUND AREA'S OF PULLED FIBER'S ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B 737-800 SRM 53-00-50 2R -1 PAR 1A REV74. CLEAN AND PREP FOR REPSDR SWAA2022013158471Floor Panel · pulledA22-010; CABIN FLOOR PANEL 231DF; UPPER SURFACE HAS PULLED FACE SHEET PLIES; MRK'D ; / [01] EVALUATED DAMAGE; UPPER FACE SHEET IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1. TAP TEST GOOD; NO DELAMINATION NOTED.<BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 5SDR SWAA2022013158469Floor Panel · pulledA22-008; CABIN FLOOR PANEL 231FF; UPPER SURFACE HAS PULLED FACE SHEET PLIES; MRK'D ; / [01] EVALUATED AND FOUND DAMAGED FIBERS ON UPPER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SSDR SWAA2022013158465Floor Panel · pulledA22-011; CABIN FLOOR PANEL 232CF; UPPER SURFACE HAS PULLED FACE SHEET PLIES; MRK'D ; / [01] EVALUATED AND FOUND DAMAGED FIBERS ON UPPER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SSDR SWAA2022013158124Floor Panel · corrodedA125-20 - AFT CARGO BAY - FLOOR PANEL - 140BF - PERIMETER CORRODED ; / [01] MEASURED TOTAL ACCUMULATED LENGTH OF CORROSION DAMAGE TO BE = 27 ' LIMIT = 20'. PANEL 140BF IS OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 102; [02] VERIFIED MATERIAL FOR NEW FLOOR PANEL TSDR SWAA2022013158125Floor Panel · corrodedA125-21 - AFT CARGO BAY - FLOOR PANEL - 140CF - PERIMETER CORRODED ; / [01] VERIFIED LIMITS; FOUND OUT OF LIMITS ( MORE THAN 20' LENGTH ) IAW 25-52-01-201-801.; [02] IDENTIFIED MATERIAL FOR PNL # 140CF AS: 2024 - T3-071 A TAG # A84104. IAW AMM 25-52-01-201-801SDR DALA2022010700136None · noneSHIP 6822 CORROSION ON SHEAR CLIP STA 860 AND STGR 28L/STGR 27L AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00609 SHEAR CLIP STA 860 AND STGR 28L/STGR 27L AT FWD CARGO COMPARTMENT WAS REPLACED PER DRAWING NUMBER:140N2002 REV.- AND B757-200 SRM.SDR AALA202201050044Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: MAIN CABIN AFT DRY AREA FLOOR PANEL #251 YF DELAMINATED. REPAIRED FLOOR PANEL PER SRM 53-02-00-300-013.SDR SWAA2022013157613Floor Panel · corrodedA-125-06 - FORWARD CARGO BAY - FLOOR PANEL - 120DF - PERIMITER CORRODE ; / [01] EVALUATED DAMAGE FOUND DAMAGE TO BE LONGER THEN 20' FOUND FLOOR PANEL TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1; [02] VERIFIED NEW FLOOR PANEL MATERIALS AS P/N <BR>2024-T3-071 ATAGSDR SWAA2022013157614Floor Panel · corrodedA-125-08 - FORWARD CARGO BAY - FLOOR PANEL - 120CF - PERIMETER CORRODED ; / [01] EVALUATED DAMAGE : CORROSION IS MORE 20 INCH FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-1; [02] VERIFIED MATERIAL ID : IS 2024 T3 .071 TAG #A105083 IAW AMM 25-52-01-201-801; [03] VERSDR SWAA2022013157615Floor Panel · corrodedA-125-09 - FORWARD CARGO BAY - FLOOR PANEL - 120AF - PERIMETER CORRODED ; / [01] VERIFIED LIMITS ON FWD PIT FLOOR PANEL 120AF. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. FIG 102.; [02] VERIFIED MATERIAL FOR REPLACEMENT PANEL AS .071; 2024-T3; IAW AMM 25-SDR DALA2022010600091None · noneAFT CARGO. FLOOR BOARD SUPPORT/FORMER CORRODED AT STA 973 STRINGERS 29 AND 30 ATTACH POINTS, 6 INCHES FWD OF ANTENNA DOUBLER. (M) FLOOR BOARD SUPPORT/FORMER AT STA 973 STRINGERS 29 AND 30 ATTACH POINTS, 6 INCHES FWD OF ANTENNA DOUBLER FOUND CRACK, FOUND TO BE SDR DALA2022010500089None · noneSHIP 3248 CORROSION STRINGER 38R BTW FR 32 AND FR 33 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: FOUND AREA WITHIN LIMITS. CONTINUE ON MON. (2073933)SDR DALA2022010400066None · noneSHIP 3248 CRACK PROFILE LOCATED BTW FR 50 TO FR 54 LEVEL STR 35L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ER/A #559065-14MA REV. ORIGINAL (2073939)SDR DALA2022010400065None · noneSHIP 3248 CORROSION STRINGER SPLICE LOCATED STR26R AT LEVEL FR67 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER SPLICE PER A320 SRM 51-72-11. (2074229)SDR DALA2022010400062None · noneSHIP 3248 CORROSION INTERNAL STRUCTURE STRAP LOCATED AT FR 67 BTW STR 27L TO STR 28L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ERA 596106-14AD REV ORIGINAL. (2074183)SDR DALA2022010400061None · noneSHIP 3248 CORROSION FRAME 67 SUPPORT ANGLE LOCATED BTW STR42R TO STR42L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SUPPORT ANGLE PER A320 SRM 51-72-11. (2074120)SDR DALA2022010400060None · noneSHIP 3248 CORROSION STRINGER 43L BTW FR32 AND FR 34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ERA 596001-14 REV ORIGINAL. (2073932)SDR DALA2022010400059None · noneSHIP 3248 CORROSION STRINGER 43R LOC. BTW FR 31 AND FR 33 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER ERA 596001-14 REV ORIGINAL. (2073931)SDR SWAA2022010457662Floor Panel · crackedCRACK IN FLOOR OF FORWARD CARGO BIN ; / [01] OK TO CONTINUE PER MEL 25-16-01 SP1B AUTH #41605; [02] R & R PANEL PER AMM 25-52-10 REF LOG PAGE 1784237SDR DALA2022010400050None · noneFLOOR BEAM CRACKED AT STATION Y=737 RH OVERWING FRAME ATTACH POINT. REPLACED FLOOR BEAM PER B717 SRM 51-40-02. (LP #2072760)SDR DALA2022010400049None · noneFLOOR BEAM CRACKED AT STATION Y=737 LH OVERWING FRAME ATTACH POINT. MAINTENANCE REPLACED FLOOR BEAM PER B717 SRM 51-40-02. (LP #2072758)
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