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.

SDR SWAA2023061256856Panel · delaminatedCABIN CENTER FLOOR PANEL ROW 17 DELAMINATED<[01] R&R CABIN CENTER FLOOR PANEL ROW 17 IAW AMM 53-21-00. NO DEFECTS NOTED.Jun 7, 2023 · N8571Z · Boeing 7378H4SDR ASAA2023060644386Floorboard · delaminatedMAIN CABIN FLOOR BOARD 231FF HAS INSERT DAMAGE AT L/H. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR BOARD 231FF IAW A320 AMM 53-12-12-420-001-A.Jun 6, 2023 · N632VA · Airbus A320214SDR IPXA2023070193567Floor Panel · damagedINSPECTION TYPE:1CPANEL 232NJ DAMAGEDFABBED PNL IAW SREO A300-5320-40552-BJun 6, 2023 · N126UP · Airbus A300F4622RSDR IPXA2023070193565Floor Panel · damagedINSPECTION TYPE:1CPANEL 232XG IS DAMAGEDFABBED PNL IAW SREO A300-5320-40552-BJun 6, 2023 · N126UP · Airbus A300F4622RSDR SWAA2023062956585Floor Panel · corrodedA221-19 FWD CARGO COMPARTMENT FLOOR PNL 120DF TOP AND BOTTOM SKINS IN SEVERAL AREAS AS MARKED ARE CORRODED<[01] JOB COMPLETE; AUDIT C/WJun 6, 2023 · N8705Q · Boeing 7378SDR SWAA2023060856596Floor Panel · crackedRAMP REPORTS CRACK IN AFT CARGO COMP FLOOR<[01] MADE PERM REPAIR AFT CARGO COMP FLOOR AMM 25-52-01Jun 6, 2023 · N915WN · Boeing 7377H4SDR SWAA2023063055516Strip · corrodedFWD CARGO ALL L/H FLOOR PANEL CAP STRIPS ARE CORRODED ON LOWER SIDE. MRKD<[01] REMOVED AND REPLACED CAP STRIP P/N 453A1611-14 , 453A1611-16, 453A1611-30 PER AMM 25-52-06. [2] VERIFIED C/A #1. [3] CAP STRIP P/N 453A1611-44 REMOVED CORROSION WITH IN LIMITS PER SJun 5, 2023 · N8536Z · Boeing 7378H4SDR SWAA2023063055517Strip · corrodedFWD CARGO ALL R/H FLOOR PANEL CAP STRIPS ARE CORRODED ON LOWER SIDE. MRKD<[01] REMOVED AND REPLACED CAP STRIP PN 453A1611-17, 453A1611-31,PER AMM 25-52-06 UPON FURTHER INSPECTION AND CLEANING NO DAMAGE OR CORROSION NOTED ON CAP STRIP PN 453A1611-45 [2] CWJun 5, 2023 · N8536Z · Boeing 7378H4SDR AALA202306130309Floor Panel · damagedAIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTS FLOOR SOFT AND POPS WHEN STEPPED ON AT SEAT ROW 19. **SUPPLEMENTAL REPORT FOR AALA202306080309: REPLACED CENTER AILSE FLOOR PANEL AT SEAT ROW 19 PER AMM 53-00-00** (CLOSED)Jun 5, 2023 · N977UY · Airbus A320*SDR AALA202306080309Floor Panel · damagedAIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTS FLOOR SOFT AND POPS WHEN STEPPED ON AT SEAT ROW 19. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)Jun 5, 2023 · N977UY · Airbus A320*SDR FDEA202306050996Floorboard · damagedLWR FWD CARGO FLOORBOARD 127EF HAS HOLE DAMAGE AND EDGE DAMAGE FABRICATED FLOORBOARD 127EF REF FEDEX DWG SRZ-25-005 MAJOR REPAIRJun 5, 2023 · N597FE · Doug MD11FSDR FDEA202306050994Floorboard · damagedLWR FWD CARGO FLOORBOARD 127NF HAS PUNCTURES FABRICATED PANEL REF FEDEX DWG SRZ-25-005 MAJOR REPAIRJun 5, 2023 · N597FE · Doug MD11FSDR SWAA2023071755638Floor Panel · brokenFWD CABIN FLOOR PANEL 221BF HAS BROKEN TANG ON AFT O/B CORNER<[01] IDENTIFIED FLOOR PANEL 221BF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 2 TABLE 2. DAMAGE AT DISCREPANT LOCATION AND FOUND ADDITIONAL AREAS ON LOWER SURFACE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW Jun 4, 2023 · N963WN · Boeing 7377H4SDR SWAA2023071755628Floor Panel · pulledFWD CABIN FLOOR PANEL 221CF HAS A PULLED THROUGH INSERT ON THE LEFT SIDE<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 SHEET 1; FIGURE 2; TABLE 2; AND <BR>BOEING DWG DOC: 141A5810 ID: 0009. <BR><BR>DAMAGE ON LOWER SURFACE LEFT HAND SIDE IS OUT OF ALLOWAJun 4, 2023 · N963WN · Boeing 7377H4SDR IPXA2023060429156Unknown · unknown*MAJOR REPAIR* MAIN DECK POSITION 4 CENTER HAS A ONE INCH PUNCTURE IN FLOOR***SM12/LMX2*** INSTALLED NEW PANEL AND REINSTALLED LOCKS AND ROLLERS IAW AMM 53-01-01.Jun 4, 2023 · N472UP · Boeing 75724APFSDR DALA2023060804663Unknown · unknownCRACK ON FLOOR PANEL OF FWD CARGO COMPARTMENT. SUMMARY OF NRC 00499: FLOOR PANEL OF FWD CARGO COMPARTMENT WAS MANUFACTURED PER ER/A 591778-14TR REV ORIGINAL SECTION I PERMANENT REPAIR. PANEL INSTALLED PER AMDS 2040-0006. ASSOCIATED ER/A 14-591778 ADDED FOR AC Jun 4, 2023 · N924AT · Boeing 717200SDR SWAA2023070554705Floor Panel · pulledAFT FLOOR PANEL 242RF UPPER SKIN HAS PULLED STRANDS.<[01] AFT FLOOR PANEL 242RF UPPER SKIN WITH 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.;[02] VERIFIED CORRECTIVE ACTION #1Jun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070554709Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS PULLED STRANDS.<[01] DUE TO AMOUNT OF DAMAGE FLOOR PANEL 241AAF WILL BE REPLACED WITH NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 PARA 1A NOTE. <BR><BR>FABRICATED PANEL USING BMS 4-17 TY6 LOT#1526676-1; APPLIED ALL Jun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070554719Floor Panel · pulledFWD FLOOR PANEL 221BF UPPER SKIN HAS PULLED STRANDS.<[01] FWD FLOOR PANEL 221BF UPPER SKIN WITH 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.;[02] VERIFIED CORRECTIVE ACTION #1Jun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070554721Floor Panel · pulledFWD FLOOR PANEL 221FF UPPER SKIN HAS PULLED STRANDS.<[01] FWD FLOOR PANEL 221FF UPPER SKIN WITH 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.;[02] VERIFIED CORRECTIVE ACTION #1Jun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070554722Floor Panel · brokenFWD FLOOR PANEL 221GF FWD O/B TANG IS BROKEN.<[01] FWD FLOOR PANEL 221GF WITH BROKEN FWD O/B TANG WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1Jun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070565053Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED 241XF PANEL IAW SRM 53-00-50-0I-1 PARA FIGURE 6; TABLE 6.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>WILL PERFORM WORK IAW SRM 53-00-50-2R-1<BR>REMOVED 2Jun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070554702Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS PULLED STRANDS.<[01] VERIFIED COMPLETION OF PANEL FABRICATION IAW EA 23-153-01769;[02] VERIFIED CORRECTIVE ACTION 1Jun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070554703Floor Panel · pulledAFT FLOOR PANEL 241ADF UPPER SKIN HAS PULLED STRANDS.<[01] VERIFIED COMPLETION OF PANEL FABRICATION IAW EA 23-153-01770;[02] VERIFIED CORRECTIVE ACTION 1Jun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070554704Floor Panel · pulledAFT FLOOR PANEL 241AEF UPPER SKIN HAS PULLED STRANDS.<[01] VERIFIED COMPLETION OF PANEL FABRICATION IAW EA 23-153-01781;[02] VERIFIED CORRECTIVE ACTION 1Jun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070554713Floor Panel · pulledAFT FLOOR PANEL 242TF UPPER SKIN HAS PULLED STRANDS.<[01] VERIFIED COMPLETION OF PANEL FABRICATION IAW EA 23-153-01777;[02] VERIFIED CORRECTIVE ACTION 1Jun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070565056Floor Panel · crackedAFT FLOOR PANEL 241ABF LOWER SKIN IS CRACKED AT THE FWD O/B CORNER.<[01] IDENTIFIED PANEL 241ABF IAW SRM 53-00-50-0I-1 FIGURE 6; TABLE 6.<BR><BR>DAMAGE ON PANEL IS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4 F.<BR><BR>DAMAGE TO BE REPAIRED PER SRM 53-Jun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070565057Floor Panel · pulledAFT FLOOR PANEL 242SF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED 242SF PANEL IAW SRM 53-00-50-0I-1 PARA FIGURE 6; TABLE 6.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>WILL PERFORM WORK IAW SRM 53-00-50-2R-1<BR>REMOVED 1Jun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070565058Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 242UF IAW SRM 53-00-50-0I-1 FIG 6 TABLE 6 AND BOEING DWG 147A5810-95.<BR><BR>FOUND DAMAGE TO UPPER SURFACE SKIN PLIES TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAJun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070554706Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS PULLED STRANDS.<[01] VERIFIED COMPLETION OF PANEL FABRICATION IAW EA 23-153-01779;[02] VERIFIED CORRECTIVE ACTION 1Jun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070565052Floor Panel · pulledAFT FLOOR PANEL 242WF UPPER AND LOWER SKINS HAVE PULLED STRANDS.<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 SHEET 1; FIGURE 6; <BR>TABLE 6; AND BOEING DWG DOC: 147A5810 ID: 0010.<BR><BR>PANEL DAMAGE TO UPPER SKIN PLIES IS OUT OF ALLOWABLE DAMAGE LIMIJun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070565062Floor Panel · pulledFWD FLOOR PANEL 221AF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 SHEET 1; FIGURE 2; TABLE 2; <BR>AND BOEING DWG DOC: 141A5810 ID: 0728.<BR><BR>PANEL DAMAGE TO UPPER SKIN PLIES IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM <Jun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070565059Floor Panel · pulledFWD FLOOR PANEL 221DF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED PANEL 221DF MATERIAL IAW SRM 53-00-50-0I-1 FIG 2; TABLE 2.<BR><BR>CLEANED PANEL REPAIR AREA IAW SRM 53-00-50-2R-0 PARA 5. A. (1).<BR><BR>FOUND DAMAGE TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-Jun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070565060Floor Panel · pulledFWD FLOOR PANEL 222AF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED PANEL 222AF IAW SRM 53-00-50-0I-1.<BR>FOUND DAMAGE ON UPPER SURFACE TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1.PARA 4.F.<BR>DAMAGE SHOULD BE REPAIRED PER SRM 53-00-50-2R-1.<BR><BR>REJun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070565061Floor Panel · pulledFWD FLOOR PANEL 222BF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 222BF IAW SRM 53-00-50-0I-1 FIGURE 2 TABLE 2 <BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR.4 B<BR><BR>DAMAGE TO BE REPAIRED IAW SRM 53-00-50-2R-1 <BR><BJun 1, 2023 · N962WN · Boeing 7377H4SDR SWAA2023062955205Floor Panel · pulledAFT CABIN FLOOR PANEL 241VF HAS A PULLED THROUGH INSERT HOLE<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW FLOOR PANEL USING BMS4-23 TYPE II LOT 1525675-1 AND BMS5-107 LOT AK2KP8383K-1 RESIN; CURED RESIN WITH A HEAT LAMP USING THERMOMJun 1, 2023 · N295WN · Boeing 7377H4SDR SWAA2023062955231Floor Panel · brokenFWD CABIN FLOOR PANEL 221BF AFT O/B CORNER IS BROKEN (TANG)<[01] IDENTIFIED PANEL 221BF IAW SRM 53-00-50-0I-1 FIGURE 2. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.E.(2).(B) AND WILL BE REPAIRED IAW SRM 53-00-50-2R-6. REMOVED NUMEROUS IJun 1, 2023 · N295WN · Boeing 7377H4SDR SWAA2023062955233Floor Panel · brokenFWD CABIN FLOOR PANEL 221GF FWD O/B CORNER IS BROKEN (TANG)<[01] IDENTIFIED FLOOR PANEL 221GF IAW SRM 53-00-50-0I-1 FIGURE 2 TABLE 2 <BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR.4 B<BR><BR>DAMAGE TO BE REPAIRED IAW SRM 53-00-50-2R-1Jun 1, 2023 · N295WN · Boeing 7377H4SDR SWAA2023062955204Floor Panel · pulledAFT CABIN FLOOR PANEL 241VF HAS A PULLED THROUGH INSERT HOLE<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW FLOOR PANEL USING BMS4-23 TYPE II LOT 1525675-1 AND BMS5-107 LOT AK2KP8383K-1 RESIN; CURED RESIN WITH A HEAT LAMP USING THERMOMJun 1, 2023 · N295WN · Boeing 7377H4SDR SWAA2023062954606Floor Panel · pulledFLOOR PANEL 232RF UPPER SKIN HAS PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 232RF USING BMS 4-23TY2 LOT#1525675-1. INSTALLED INSERTS USING BMS 5-107 LOT#AK2KP8383K-1; CURED WITH THERMOMETER ID:ATS2208 CAL DUE 10/2023; APPLIED Jun 1, 2023 · N960WN · Boeing 7377H4SDR DALA2023060204425Unknown · unknownDELAMINATION AND BROKEN COMPOSITE MATERIAL AND SHEET ON FWD CARGO FLOOR PANEL 121CF AND 121NF (C1). SUMMARY OF NRC 00376: FWD CARGO FLOOR PANEL 121CF AND 121NF WERE MANUFACTURED PER ERA 544901-14 REV A PAR 6. AND FIGURE 5 AND ERA 591778-14TR REV ORIGINAL SECTIJun 1, 2023 · N899AT · Boeing 717200SDR SWAA2023070554175Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS PULLED STRANDS. THIS FAULT SHOULD BE FOR FLOOR PANEL 231DF NOT 241DF. THIS FAULT WAS GENERATED FROM A 231DF OPEN TASK AND UPPER SKIN PULLED STRANDS HAVE BEEN VERIFIED AS A VALID DISCREPANCY ON 231DF.<[01] IDENTIFIED FLOOR PANELMay 31, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070554179Floor Panel · pulledFLOOR PANEL 241VF UPPER SKIN HAS PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW BOARD USING BMS4-17 TYPE VI LOT 1526676-1 AND BMS5-107 CLASS 1 RESIN LOT AK2KP8383K-1; CURED RESIN UNDER A HEAT LAMP USING THERMOMETER ID: May 31, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070565023Floor Panel · pulledFWD FLOOR PANEL 222CF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 222CF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6.<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. <BR><BR>DAMAGE IS REPAIRABLE IAW SRM 53-0May 31, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070565025Floor Panel · pulledFLOOR PANEL 231GF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED 231GF PANEL IAW SRM 53-00-50-0I-1 PARA FIGURE 3; TABLE 3.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F. DUE TO THE EXTENT OF DAMAGE A NEW BOARD WILL BE FABRICATED.May 31, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070565021Floor Panel · pulledFLOOR PANEL 231KF UPPER SKIN HAS PULLED STRANDS.<[01] DUE TO AMOUNT OF DAMAGE; FLOOR PANEL 231KF WILL BE REPLACED WITH NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.PARA 1.A.NOTE.<BR><BR>STARTED FABRICATING FLOOR PANEL FROM BMS 4-23 TY 2 LOT#1525675-1; LOMay 31, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070554177Floor Panel · pulledFLOOR PANEL 241RF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 241RF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 5 TABLE 5.<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. <BR><BR>DAMAGE TO FLOOR PANEL IS BEYOND ECONOMay 31, 2023 · N962WN · Boeing 7377H4SDR SWAA2023070554178Floor Panel · pulledFLOOR PANEL 241UF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 241UF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 5 TABLE 5.<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. <BR><BR>DAMAGE TO FLOOR PANEL IS BEYOND ECONOMay 31, 2023 · N962WN · Boeing 7377H4SDR ASAA2023053043600Floor Panel · delaminatedFLOOR PANEL 147A5810-439 INSERTS CORRODED. GROUNDED - YES. REPAIRED FLOOR PANEL 147A5810-439 IAW V737-900ER SRM 53-00-50-2R-0.May 30, 2023 · N281AK · Boeing 737900ERSDR ASAA2023053043599Floor Panel · delaminatedFLOOR PANEL 147A5810-477 INSERTS CORRODED. GROUNDED - YES. REPAIRED FLOOR PANEL 147A5810-477 IAW B737-900ER SRM 53-00-50-2R-0.May 30, 2023 · N281AK · Boeing 737900ER
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