JASC 5321
Service difficulty reports · 49,402
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 IPXA11164572Floorboard · delaminatedINSPECTION TYPE:10YR, FLOORBOARD 241JN DELAMINATED. REPAIRED FLOORBOARD 241JN IAWEO A300-5320-38221-B, PARA 6 A (1).SDR IPXA11164539Floorboard · brokenINSPECTION TYPE:10YR, FLOORBOARD 241RN HAS BROKEN CORNER. FABRICATED FLOORBOARD 241RN IAW EO A300-5320-16407-E, APPENDIX A/B.SDR IPXA1564489Floor Panel · delaminatedINSPECTION TYPE:C4, MAIN CARGO BAY FLOOR PANEL BS 900-1020, LBL 45-65 WL 208 IS DELAMINATED. REMOVED AND FABRICATED IAW EO #B757-5320-9692-G.SDR IPXA1564488Floor Panel · puncturedINSPECTION TYPE:C4, MAIN CARGO BAY FLOOR PANEL BS 1060-1100, LBL 25-45, WL 208 IS PUNCTURED. REMOVED AND FABRICATED FLOOR PANEL IAW B757-5320-9692-G.SDR ASOA201100163Floor Panel · corrodedLT SIDE PRESSURE FLOOR CORRODED AT SEVERAL LOCATIONS BETWEEN FS 409 AND FS 559. REPAIRED IAW REO 601R-53-41-666.SDR ASOA201100162Floor Panel · corrodedRT SIDE PRESSURE FLOOR CORRODED AT SEVERAL LOCATIONS BETWEEN FS 409 TO 559. BLENDED CORROSION IAW REO 601R-53-41-666.SDR IPXA11564433Floor Panel · delaminatedINSPECTION TYPE:C4, MAIN CARGO BAY FLOOR PANEL BS 1020-1060, LBL 45-60, WL 208, FWD INBD CORNER IS DELAMINATED (DAMAGE BEYOND SRM LIMITS). FABRICATED REPLACEMENT PANEL IAW EO B757-5320-9692-G.SDR DALA1105789864Floor Panel · chafedMAIN CABIN FLOOR PNL 62 FASTENER HOLES ELONGATED, CHAFED AND BROKE OUT. ORIG MATERIAL THICKNESS .025 IAW SRM 53-23-0. MATERIAL LOSS MAXIMUM .009 MATERIAL REMAINING .016 IAW SRM 53-01, FIG 1. RECEIVED MATERIAL FOR WEB AND HAT CHANNEL IAW DWG 9957919. DRILLESDR DALA1105769857Floor Panel · corrodedMAIN CABIN METAL SKIN FLOOR PANEL NR21 HAS CORROSION ON SKIN AND ON COVER PLATE. FLOOR PANEL EXFOILIATED LOSS OUT OF LIMITS IAW SRM 53-01, FIG 1. RECEIVED NEW PANEL AND DRILLUP IAW SRM 51-10-4 AND 51-10-2.SDR USAA2011012090301Floor Panel · delaminatedCLT - DROP-IN - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 221PF BETWEEN FR12 TO FR24. REPLACED FLOOR PANEL 221PF BETWEEN FR12 TO FR24 IAW JOB CARD 26C22053014.SDR IPXA11164571Floorboard · crackedINSPECTION TYPE:10YR, FLOORBOARD 252MG CRACKED. REPAIRED FLOORBOARD 252MG IAW EO A300-5320-38221-B, PARA 6 A (1).SDR IPXA11164540Floorboard · crackedINSPECTION TYPE:10YR, FLOORBOARD 252NM IS CRACKED. FABRICATED FLOORBOARD 252NM IAW EO A300-5320-16407-E, APPENDIX A/B.SDR IPXA1164514Floor Panel · delaminatedINSPECTION TYPE:10YR, FLOOR PANEL 251BN DELAMINATED. REPAIRED FLOOR PANEL 251BN IAW EO A300-5320-38221-B, PARA 6A.SDR IPXA1164513Floor Panel · crackedINSP TYPE:10YR, FLOOR PANEL 252LG CRACKED. REPAIRED FLOOR PANEL 252LG IAW EO A300-5320-38221-B, PARA 6A.SDR IPXA1164511Floor Panel · delaminatedINSPECTION TYPE:10YR, FLOOR PANEL 251EN DELAMINATED. REPAIRED FLOOR PANEL 251EN IAW EO A300-5320-38221-B, PARA 6A.SDR IPXA1164510Floor Panel · crackedINSPECTION TYPE:10YR, FLOOR PANEL 252KM CRACKED. REPAIRED FLOOR PANEL 252KM IAW EO A300-5320-38221-B, PARA 6A.SDR IPXA1164509Floor Panel · delaminatedINSPECTION TYPE:10YR, FLOOR PANEL 251DF DELAMINATED. REPAIRED FLOOR PANEL 251DF IAW EO A300-5320-38221-B, PARA 6A.SDR IPXA1164508Floor Panel · delaminatedINSPECTION TYPE:10YR, FLOOR PANEL 261KF DELAMINATED. REPAIRED FLOOR PANEL 261KF IAW EO A300-5320-38221-B, PARA 6A.SDR IPXA1164512Floor Panel · crackedINSPECTION TYPE:10YR, FWD CARGO FLOOR PANEL 132MG CRACKED. REPAIRED FLOOR PANEL 132MG IAW EO A300-5320-38221-B, PARA 6A.SDR IPXA1164507Floor Panel · puncturedINSPECTION TYPE:10YR, FLOOR PANEL 252JF PUNCTURED. REPAIRED FLOOR PANEL 252JF IAW EO A300-5320-38221-B, PARA 6A.SDR DALA1104903242Floor Panel · damagedAFT CARGO COMPARTMENT FLOOR PANEL 151EF HAS DAMAGE ON UPPER SURFACE. REMOVED, FABRICATED & INSTALLED NEW PANEL IAW AMM 53-42-14-400-001 AND AMM 53-42-14-420-050-A.SDR DALA1104553706Floor Panel · corrodedFWD CARGO COMPARTMENT PANEL 120DF CORRODED. REPLACED FLOOR PANEL.SDR DALA1105299864Floor Panel · crackedCABIN FLOOR PANEL NR 75 CRACKED AND PUNCTURED AT AFT INBD SIDE. CUT OUT DAMAGE 2EA PLACES 1" X 2". NO DEFECTS IAW NDT SPM 06-10-01. FABRICATED AND REINSTALLED 2EA FILLERS AND 1EA DOUBLER FROM .025, 7075-T6 PO 1120034 IAW SRM 53-01, FIG 4, SHEET 4.SDR DALA1105219857Floor Panel · corrodedMAIN CABIN METAL SKIN FLOOR PANEL NR31 HAS CORROSION AROUND FASTENER HOLES. REMOVED CORROSION FROM MAIN CABIN FLOOR PANEL NR31 ORIGINAL THICKNESS .020, REMOVED .007 WITH .013. REMAINING FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. RECEIVED CUST FURNISHED SDR DALA1105209857Floor Panel · corrodedMAIN CABIN METAL SKIN FLOOR PANEL NR20 HAS CORROSION. REMOVED CORRSION FROM MAIN CABIN METAL SKIN FLOOR PANEL NR20 IAW SRM 51-10-3. ORIGINAL MATERIAL THICKNESS .025 MATERIAL LOSS.013, REMAINING MAT .012 FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1, SHEET 3SDR DALA1105189857Floor Panel · corrodedMAIN CABIN METAL SKIN FLOOR PANEL NR45 HAS CORROSION AROUND EDGES. CORRECTED, RECIEVED NEW FLOOR PANEL FROM SUPPLY PN 09-5300-3-1731, PO 1011W022.SDR USAA2011012090300Floor Panel · delaminatedCLT - DROP-IN - MAJOR REPAIR - DELAMINATION ON FORWARD LAV SHROUD FLOOR PANEL BETWEEN FR12 TO FR24. REPLACED FORWARD LAV SHROUD FLOOR PANEL BETWEEN FR12 TO FR24 IAW JOB CARD 26C22053014.SDR USAA2011012090299Floor Panel · delaminatedCLT- DROP-IN - MAJOR REPAIR - DELAMINATION ON FORWARD LAV SHROUD FLOOR PANEL BETWEEN FR12 TO FR24. REPLACED FORWARD LAV SHROUD FLOOR PANEL BETWEEN FR12 TO FR24 IAW JOB CARD 26C22053014.SDR USAA2011020890627Floor Panel · delaminatedCWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 271HF BETWEEN FR73 TO FR75 & BETWEEN Y953 TO Y1456. REPAIRED FLOOR PANEL 271HF BETWEEN FR73 TO FR75 & BETWEEN Y953 TO Y1456 IAW A330 SRM 53-02-00.SDR USAA2011020890626Floor Panel · delaminatedCWF - S2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 251NF BETWEEN FR39 TO FR40.1 & BETWEEN Y953 TO Y1456. REPAIRED FLOOR PANEL 251NF BETWEEN FR39 TO FR40.1 & BETWEEN Y953 TO Y1456 IAW A330 SRM 53-02-00.SDR IPXA11164541Floorboard · damagedINSPECTION TYPE:10YR, AFT CARGO FLOORBOARD 161GF WARPED AND DENTED. FABRICATED FLOORBOARD 161GF IAW EO A300-5320-16407-E, APPENDIX A/C.SDR DALA1104423242Floor Panel · damagedFWD CARGO COMPARTMENT, FLOOR PANEL 131AF HAS DAMAGE. REMOVED FWD CARGO COMPARTMENT FLOOR PANEL 131AF IAW AMM 53-22-14 PB401. REPLACED PANEL IAW AMM 53-22-14 PB401. FABRICATED PANEL ON STAM TRAVELER IAW DWG 3D25-37705. RETAIN FOR RECORDS.SDR ASOA201100169Floor Panel · corrodedRT PRESSURE FLOOR CORRODED AT SEVERAL LOCATION BETWEEN FS 409 TO 559. REPAIRED IAW REO 601R-53-41-666.SDR ASOA201100168Floor Panel · corrodedRT PRESSURE FLOOR CORRODED AT SEVERAL LOCATION BETWEEN FS 409 AND 559. PERFORMED UT THICKNESS INSPECTION OF BLEND AREAS IAW MAC NDT INSPECTION PROCEDURE UT-3. BLENDS AREAS ARE WITHIN ALLOWABLE LIMITS OF REO 601R-53-41-666 TABLE 2.SDR ASOA201100134Doubler · corrodedLT PRESSURE FLOOR SKIN DOUBLER OTBD OF LBL 36 JUST FWD OF FS 544 IS CORRODED. REMOVED CORROSION ON LT PRESSURE FLOOR SKIN DOUBLER IAW REO 601R-53-41-666. REF MATERIAL LOSS FOR PREVIOUS BLENDOUT WAS .010. REMOVED .003 MORE MATERIAL MAKING .013 TOTAL MATERIAL SDR ASOA201100133Doubler · corrodedRT PRESSURE FLOOR SKIN DOUBLER OTBD OF RBL 36 AT FS 529 IS CORRODED. REMOVED CORROSION ON RT PRESSURE FLOOR SKIN ASSY IAW REO 601R-53-41-666. REF MATERIAL LOSS FOR PRESSURE FLOOR SILL ASSY ANGLE WAS .010 FROM PREVIOUS BLENDOUT. REMOVED .004 MORE MATERIAL MASDR ASOA201100132Floor Skin · corrodedLT PRESSURE FLOOR SKIN OTBD OF LBL 36 IS CORRODED AT FS 461. REMOVED CORROSION ON RT PRESSURE FLOOR SKIN ASSY IAW REO 601R-53-41-666. REF MATERIAL LOSS FOR PRESSURE FLOOR SILL ASSY ANGLE WAS .010 FROM PREVIOUS BLENDOUT. REMOVED .002 MORE MATERIAL MAKING .012SDR ASOA201100131Doubler · corrodedLT PRESSURE FLOOR SKIN DOUBLER AT FS 461 OTBD OF LBL 36 IS CORRODED. REMOVED CORROSION ON LT PRESSURE FLOOR DOUBLER IAW REO 601R-53-41-666. REF MATERIAL LOSS FOR PRESSURE FLOOR SILL ASSY ANGLE WAS .010 FROM PREVIOUS BLENDOUT DATED 1/21/09. REMOVED .002 MORE MSDR ASOA201100130Doubler · corrodedLT PRESSURE FLOOR SKIN DOUBLER OTBD OF LBL 36 AT FS 424 IS CORRODED. REMOVED CORROSION ON LT PRESSURE FLOOR SILL ASSY (SKIN DOUBLER) IAW REO 601R-53-41-666. MATERIAL LOSS IS .003, REMAINING MATERIAL IS .077. MINIMUM ALLOWABLE MATERIAL THICKNESS IS .055. ARESDR ASOA201100129Doubler · corrodedLT PRESSURE FLOOR SKIN DOUBLER OTBD OF LBL 36 AT FS 449+85 IS CORRODED. REMOVED CORROSION ON LT PRESSURE FLOOR SILL ASSY (SKIN DOUBLER) IAW REO 601R-53-41-666. REF MATERIAL LOSS FOR PRESSURE FLOOR SILL ASSY ANGLE WAS .010 FROM PREVIOUS BLENDOUT DATED 1/21/09.SDR ASOA201100128Doubler · corrodedLT PRESSURE FLOOR SKIN DOUBLER OTBD OF LBL 36 AT FS 544 IS CORRODED. REMOVED CORROSION ON LT PRESSURE FLOOR SILL ASSY (SKIN DOUBLER) IAW REO 601R-53-41-666. REF MATERIAL LOSS FOR PRESSURE FLOOR SILL ASSY ANGLE WAS .010 FROM PREVIOUS BLENDOUT. REMOVED .002 MOSDR DALA1103999864Floor Panel · crackedFLOOR PANEL NR 68, 1 EA CRACK ON FASTENER HOLE. REMOVED CRACK IAW SRM 53-01, FIGURE 2. FABRICATED DOUBLER AND FILLER IAW SRM 53-01, FIG 2. INSTALLED DOUBLER AND FILLER IAW SRM 51-30-2. REQUIRED INSP COMPLETED.SDR IPXA11664542Floor Panel · puncturedINSPECTION TYPE:C, FLOOR PANEL FOUND 7EA PUNCTURES TOGETHER WITH DENT RUNNING THROUGH AT STA 930 TO STA 975, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.SDR IPXA1664516Floor Panel · puncturedINSPECTION TYPE:C, FLOOR PANEL FOUND 7EA PUNCTURES AND 3EA DENT MARKS AT STA 1540 TO STA 1598, LBL 55 TO LBL 88. FLOOR PANEL FABRICATE IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.SDR IPXA1664515Floor Panel · puncturedINSPECTION TYPE:C, FLOOR PANEL FOUND 7EA PUNCTURES TOGETHER WITH DENT RUNNING THROUGH AT STA 1351 TO STA 1480, LBL 11 TO RBL 11. FLOOR PANEL FABRICATE IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.SDR IPXA11664453Floor Panel · puncturedINSPECTION TYPE:C, FLOOR PANEL FOUND 11EA PUNCTURES TOGETHER WITH DENT RUNNING THROUGH AT STA 985 TO STA 1090, LB 77 TO LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.SDR IPXA11664452Floor Panel · puncturedINSPECTION TYPE:C, FLOOR PANEL FOUND 8EA PUNCTURES TOGETHER WITH DENT RUNNING THROUGH AT STA 873 TO STA 933 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.SDR IPXA11664451Floor Panel · crackedINSPECTION TYPE:C, FLOOR PANEL FOUND 5EA PUNCTURES AND CRACK AT MIDDLE TOGETHER WITH DENT RUNNING THROUGH AT STA 933 TO STA 985, LBL 77 TO LBL 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.SDR IPXA11664450Floor Panel · brokenINSPECTION TYPE:C, FLOOR PANEL FOUND BROKEN AT STA1041 TO STA1114, LBL33 TO LBL55. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.SDR IPXA11664449Floor Panel · puncturedMCD FLOOR PANEL FOUND 9EA PUNCTURES TOGETHER WITH DENT RUNNING THROUGH AT STA 975 TO STA 1114, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-01.
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