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 SWAA2020042730137Floor Panel · damagedPASSENGER CABIN FLOOR PANEL 242HF; UPPER FACE SHEET HAS MISSING FIBERS / REPAIRED UPPER FACE SHEET FRAYING / EXPOSED FIBER & PUNCTURE DAMAGE AT FWD EDGE IAW B 737 SRM 53-00-50-2R-4 PAR 3 (A C-K1 L1 M1 N) & SRM 53-00-50-2R-0 PAR (5) REV 70SDR SWAA2020042730130Floor Panel · damagedCABIN FLOOR BOARD PANEL 241AF UPPER SURFACE HAS FIBER DAMAGE ALONG LENGTH OF PANEL / REPLACED BY FABRICATION FLOOR PANEL 241AF. IAW B737-700 SRM 53-00-50-2R-0; DWG 144A5810SDR SWAA2020042730134Floor Panel · damagedPASSENGER CABIN FLOOR PANEL 241RF; UPPER FACE SHEET HAS MISSING FIBERS / REPLACED BY FABRICATING NEW FLOOR PANEL #241RF PER SAMPLE IAW B737-700 SRM 53-00-50-2R-0 REV 70; BOEING DWG 146A5810 - ID 0003 AND BAC 5085 REV E WN5879; A18238; A30438SDR SWAA2020041430039Insert · missingPASSENGER CABIN FLOOR PANEL;231DF MISSING MID INSERT 20' AFT OF FWD END / FABRICATED FLOOR BOARD 231DF PER SAMPLE IAW SRM 53-00-50-2R-0 PER DRW# 143A5810/513 & BAC 5085SDR SWAA2020041430041Floor Panel · peelingPASSENGER CABIN FLOOR PANEL;232FF FWD INBD CORNER COVERING PEELING / REPAIRED FWD INBD CORNER ON FLOORBOARD 232FF IAW SRM 53-00-50-2R-4; PG'S 1; 2; STEPS 3(A-N). CURED INSERTS 4 EA FOR 1 HOUR AT 150 DEGREES BY HEAT LAMP IAW SRM 53-00-50-2R-0; PG'S 11; 12; STEPSDR SWAA2020041430043Floor Panel · puncturedPASSENGER CABIN FLOOR PANEL;242AF PUNCTURE OUTBD EDGE 31' AFT OF FWD END / REPAIRED PUNCTURE IN FLOOR PANEL 242AF 31' AFT OF FWD EDGE ON OUTBD SIDE IAW SRM 53-00-50-2R-2 PARA 3SDR SWAA2020041430044Floor Panel · puncturedPASSENGER CABIN FLOOR PANEL;242LF PUNCTURE MID PANEL AND 9' AFT OF FWD END / REPAIRED PUNCTURE ON FLOOR PANEL 242LF LOCATED MID PANEL AND 9' AFT OF FWD END IAW SRM 53-00-50-2R-3 PARA 3SDR SWAA2020040930047Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL;231AF AFT LH CORNER DELAMINATED / PASSENGER CABIN FLOOR PANEL 231AF; AFT L/H CORNER DELAMINATION REPAIRED IAW SRM 53-00-50-2R-10 PARA 3 STEPS A TO GSDR SWAA2020033029472Floor Panel · damagedFLOOR PANEL 241AF UPPER SURFACE DAMAGED ALONG LENGTH OF PANEL 16-17 INCHES FROM LH EDGE(MARKED) / REPAIRED FLOOR PANEL 241AF IAW SRM 53-00-50-2R-0; SRM 53-00-50-2R-1. DAMAGE DETERMINED TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1; PARA 4B;(2). A MAXIMUMSDR SWAA2020033029476Floor Panel · delaminatedFLOOR PANEL 241DF FORWARD LEFT HAND EDGE CRUSHED/DELAMINATED (MARKED) / REPAIRED FLOOR PANEL 241DF IAW SRM 53-00-50-2R-0; SRM 53-00-50-2R-10. DAMAGE DETERMINED TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1; PARA 4B(4). A MINIMUM OF 3.0 INCHES AWAY FROM TSDR SWAA2020033029466Floor Panel · damagedFLOOR PANEL 231MF LEFT EDGE DAMAGED (MARKED) / REMOVED EDGE SPLINTERING PER ALLOWANCE IN BOEING DWG:143A5810. 57795U 10MAR2020 AND SRM 51-10-02-0G-0 PARA 5; D ON LEFT EDGE OF PANEL 231MFSDR SWAA2020033033861Floor Panel · dentedPASSENGER CABIN FLOORBOARD 242AF HAS DENTS. / REMOVED AND REPLACED IAW AMM 53-21-00.SDR SWAA2020033033862Floor Panel · dentedPASSENGER CABIN FLOORBOARD 242BF HAS DENTS. / REMOVED AND REPLACED IAW AMM 53-21-00.SDR SWAA2020033033860Floor Panel · dentedPASSENGER CABIN FLOORBOARD 241BF HAS DENTS. / REMOVED AND REPLACED IAW AMM 53-21-00.SDR SWAA2020032442807Panel · puncturedCABIN FLOOR BOARD PANEL 241BF LOWER SURFACE IS PUNCTURED 43" FROM FORWARD EDGE AND .75" FROM OUTBOARD EDGE REPAIRED PNL 241BF LOWERSURFACE PUNCTURE @43" FROM FWD EDGE AND .75" FROM OUTBOARD EDGE. IAW B737-700 SRM 53-00-50-2R-2 REV 70, SRM 53-00-50-2R-0SDR SWAA2020032442806Floor Panel · damagedCABIN FLOOR PANEL 242KF HAS PULLED THROUGH INSERT WITH MISSING FIBERS ON LOWER SURFACE. REPAIRED CABIN FLOORBOARD 242KF LOWER SURFACE AT INSERT LOCATION AS MARKED I/A/W SRM 53-00-50-2R-1 REV 70; SRM 53-00-50-2R-0 GENERAL REV 70.SDR SWAA2020032442805Floor Panel · damagedPASSENGER CABIN FLOOR PANEL 241VF, UPPER FACE SHEET HAS MISSING FIBERS REPAIRED PASSENGER CABIN FLOORPANEL 241VF UPPER FACE SHEET 5 MARKED IAW SRM 53-00-50-2R-1 REV 70; SRM 53-00-50-2R-0 REV 70.SDR SWAA2020032442748Floorboard · puncturedCABIN FLOOR BOARD PANEL 241BF UPPER SURFACE HAS SMALL CLUSTER OF PUNCTURES 29" FROM AFT EDGE AND 1" FROM INBOARD EDGE REPAIRED PNL 241BF UPPERSURFACE PUNCTURES 29" FROM AFT EDGE AND 1" FROM INBOARD EDGE. IAW B737-700 SRM 53-00-50-2R-2 REV 70, SRM 53-00SDR SWAA2020032442747Floorboard · puncturedCABIN FLOOR BOARD PANEL 241BF UPPER SURFACE IS PUNCTURED 29.5" FROM AFT EDGE AND 5.5" FROM INBOARD EDGE REPAIRED PNL 241BF UPPER SURFACE PUNCTURE 29.5" FROM AFT EDGE AND 5.5" FROM INBOARD EDGE. IAW B737-700 SRM 53-00-50-2R-2 REV 70, SRM 53-00-50-2R-0 RSDR SWAA2020031942609Floor Panel · damagedPASSENGER CABIN FLOOR PANEL 242NF, UPPER FACE SHEET HAS MISSING FIBERS REPAIRED PASSENGER CABIN FLOOR PANEL #242NF OF UPPER FACE MISSING FIBERS IAW B737-700 SRM 53-0-50-2R-0 REV 70 AND B737-700 SRM 53-00-50-2R-1 REV 70. A36551, A98132SDR SWAA2020031842567Floor Panel · puncturedCABIN FLOOR PANEL 241SF IS PUNCTURED THROUGH PANEL. 8" FROM FWD SIDE AND 8" FROM O/B EDGE. REPAIRED CABIN FLOOR PANEL #241SF OF PUNCTURE THROUGH PANEL 8" FROM FWD SIDE AND 8" FROM O/B EDGE ON BOTH UPPER AND LOWER SURFACE IAW B737-700 SRM 53-00-50-2R-0 SDR SWAA2020031842563Floorboard · damagedCABIN FLOOR BOARD PANEL 232JF LOWER SURFACE 35" FROM FORWARD EDGE HAS DAMAGED LAYERS AROUND 2 INSERTS ON OUTBOARD EDGE REPAIRED CABIN FLOOR BOARD PANEL 232 JF LWR SURFACE 35' FROM FWD EDGE AROUND 2 INSERTS ON O/B EDGE IAW B 737 SRM 53-00-50-2R-1 REV 70SDR SWAA2020031642464Floor Panel · delaminatedPASSENGER CABIN FLOOR BOARD 241AF IS DELAMINATED ON CORNER (MARKED) REPAIRED FLOOR BOARD 241AF IAW SRM 53-00-50-2R-0, SRM 53-00-50-2R-9. DAMAGE DETERMINED TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1; PARA 4F. DELAMINATIONS ARE NOT PERMITTED AND SDR SWAA2021081242340Floorboard · pulledPASSENGER CABIN FLOORBOARD 241BF HAS MULTIPLE FIBER STRANDS PULLED UP ON UPPER SURFACE / REMOVED AND REPLACED PASSENGER CABIN FLOORBOARD 241BF PER AMM 53-21-00.SDR SWAA2021081242339Floorboard · pulledPASSENGER CABIN FLOORBOARD 242AF DENTED AND MULTIPLE FIBER STRANDS PULLED UP ON UPPER SURFACE / REPLACED PASSENGER CABIN FLOORBOARD 242AF PER AMM 53-21-00.SDR SWAA2021080528641Floor Panel · corrodedAFT CARGO COMPARTMENT FLOOR PANEL 140AF IS CORRODED ALONG EDGES / REMOVED DAMAGES ON AFT CARGO PIT FLOOR PNL 140AF IAW SRM 51-10-02; EVALUATED MAT LOSS FOUND TO BE OUT OF LIMITS LENGTH IS GREATER THAN 20' IAW SRM 53-00-53-1A-1 FIG 102; VERIFIED AND FABRICATED SDR SWAA2021080528640Floor Panel · corrodedAFT CARGO COMPARTMENT FLOOR PANEL 140BF IS CORRODED ALONG EDGES / REMOVED CORROSION FROM FLOOR PANEL 140BF & EVALUATED MATERIAL LOSS IAW SRM 53-00-53-51-1A-1; FIG 102 FOUND TO BE OUT OF LIMITS; LEN GTH B7 DAMAGED AREA IS GREATER THAN 20' FABRICATED NEW FLOOR PSDR SWAA2021080528638Floor Panel · corrodedAFT CARGO COMPARTMENT FLOOR PANEL 140DF IS CORRODED ALONG EDGES / REMOVED DAMAGE & EVALUATED MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-053-1A-1; FIG 102. LENGTH IS GREATER THAN 20' FABRICATED NEW FLOOR PANEL 140DF IAW AMM BOEING DWG #453A2610 TY: PSDR SWAA2021080528623Floor Panel · corrodedFWD CARGO COMPARTMENT FLOOR PANEL #120AF UPPER SURFACE CORRODED. / FABRICATED FWD CARGO COMPARTMENT FLOOR PANEL #120AF I/A/W 737 AMM 25-52-01-201-801; 737 AMM 51-21-41-370-802; AND 737 AMM 51-21-72-370-804 CORROSION WAS MORE THAN 20' IN LENGTH OUT OF LIMITS PESDR SWAA2021080528622Floor Panel · corrodedFWD CARGO COMPARTMENT FLOOR PANEL #120CF UPPER SURFACE CORRODED ADRUND EDGES. / FWD CARGO CPT FLOOR PANEL #120CF UPPER SURFACE CORRODED AROUND EDGES. REMOVED DAMAGE FROM PANEL IAW SRM 51-10-02-0G. EVALUATED MATERIAL LOSS; FOUND TO BE OUT OF LIMITS IAW SRM 53-0SDR SWAA2021080528621Floor Panel · corrodedFWD CARGO COMPARTMENT FLOOR PANEL #120EF UPPER SURFACE CORRODED L/H AND R/H PANEL EDGES. / FWD CARGO FLOOR PNL 120EF UPPER SURFACE CORRODED BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 FABRICATED NEW PNL 120EF IAW SRM 51-40-05-0G-0 ANDSDR SWAA2021080508958Floor Panel · damagedAFT CABIN FLOOR PANEL 241XF HAS DAMAGED UPPER SURFACE SKIN / AFT CABIN FLOOR PANEL 241XF WITH DAMAGED UPPER SURFACE SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9.A.(1).SDR SWAA2021080508962Floor Panel · damagedAFT CABIN FLOOR PANEL 242UF HAS DAMAGED UPPER SURFACE SKIN / AFT CABIN FLOOR PANEL 242UF WITH DAMAGED UPPER SURFACE SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0; PARA 9.A.(1).SDR SWAA2021080508963Floor Panel · damagedAFT CABIN FLOOR PANEL 242WF HAS DAMAGED UPPER SURFACE SKIN / AFT CABIN FLOOR PANEL 242WF WITH DAMAGED UPPER SURFACE SKIN WAS REPLACED WITH A SERVICABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0 PARA 9.A.(1)SDR SWAA2021080508959Floor Panel · damagedAFT CABIN FLOOR PANEL 241AAF HAS DAMAGED UPPER SURFACE SKIN / AFT CABIN FLOOR PANEL 241AAF WITH DAMAGED UPPER SURFACE SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0 PARA 9.A.(1) 59812U 03/10/2020SDR SWAA2021080508960Floor Panel · damagedAFT CABIN FLOOR PANEL 241ABF HAS DAMAGED UPPER SURFACE SKIN / DAMAGED FLOOR PANEL 241ABF WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-22-0G-0 PAR. 9SDR SWAA2021071528639Floor Panel · corrodedAFT CARGO FLOOR PANEL 140CF IS CORRODED ALONG EDGES AND HEAVILY DINGED AND GOUGED / AFT CARGO FLOOR PANEL 140CF IS CORRODED ALONG EDGES AND HEAVILY DINGED AND GOUGED. REMOVED DAMAGE FROM PANEL IAW SRM 51-10-02-0G. EVALUATED MATERIAL LOSS; DETERMINED TO BE OUT SDR SWAA2020042040936Floor Panel · dentedFLIGHT DECK FLOOR PANEL IS DENTED AT B.S. 259 - 270; R.B.L. 10 - L.B.L. 10; W.L. 207.54. / FABRICATED NEW FLOOR PANEL FROM 2024-T3 0.040' C LOT # 1422864-1 LOCATED DRILLED APPLIED CHEMICAL CONVERSION COAT AND PRIMED ALL I.A.W BOEING DWG 141A5133 AND SRM 51-40-SDR SWAA2020042034988Floor Panel · dentedFLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. / ACCOMPLISHED FLIGHT DECK FLOOR REPAIR AT B.S 255; WL 207 IAW EA 1-A53-33179 REV IRSDR SWAA2020041420397Floor Panel · damagedAFT CABIN FLOOR PANEL 242UF HAS DAMAGED AND MISSING INSERTS / AFT CABIN FLOOR PANEL 242UF WITH DAMAGED AND MISSING INSERTS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9.A.(1)SDR SWAA2020041420396Floor Panel · brokenAFT CABIN FLOOR PANEL 242XF IS BROKEN / BROKEN FLOOR PANEL 242XF WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-02-0G-0 PAR. 9SDR SWAA2020041420399Floor Panel · brokenFWD CABIN FLOOR PANEL 221GF TANG ON FWD O/B CORNER IS BROKEN / BROKEN PANEL 221GF WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-02-0G-0 PAR. 9SDR SWAA2020041420394Floor Panel · damagedAFT CABIN FLOOR PANEL 241AAF HAS DAMAGED INSERTS / DAMAGED AFT CABIN FLOOR PANEL 241AAF WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-02-0G-0 PARA 9. 59401U 13MAR20SDR SWAA2020041420395Floor Panel · damagedAFT CABIN FLOOR PANEL 241ACF HAS DAMAGED INSERTS / DAMAGED AFT CABIN FLOOR PANEL 241ACF WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-02-0G-0 PARA 9. 59401U 13MAR20SDR SWAA2020041420401Floor Panel · damagedFWD CABIN FLOOR PANEL 222AF HAS DAMAGED UPPER SURFACE SKIN / DAMAGED PANEL 222AF WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-02-0G-0 PAR. 9.SDR SWAA2020041420398Floor Panel · damagedFWD CABIN FLOOR PANEL 221DF HAS DAMAGED UPPER SURFACE SKIN / FWD CABIN FLOOR PANEL 221DF WITH DAMAGED UPPER SURFACE SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9.A.(1).SDR SWAA2020041420400Floor Panel · damagedFWD CABIN FLOOR PANEL 222BF HAS DAMAGED UPPER SURFACE SKIN / FWD CABIN FLOOR PANEL 222BF WITH DAMAGED UPPER SURFACE SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9.A.(1).SDR SWAA2020040720390Splice Plate · corroded***CORROSION*** FLOOR PANEL SPLICE PLATE AT B.S. 773; W.L. 155; L.B.L. 20 - R.B.L. 20. / REMOVED AND REPLACED ON ACB NEW FLOOR PANEL SPLICE PLATE AT BS773 LBL20 - RBL20 IAW DWG 146A7500 AND SRM 53-60-53-01-2.SDR SWAA2020032729661Floorboard · damagedPASSENGER CABIN FLOOR BOARD 231WF UPPER SURFACE HAS FIBER DAMAGE ALONG LENGTH OF PANEL / REPAIRED PNL 231WF UPPER SURFACE FIBER DAMAGE LENGTH OF PANEL. IAW B737-800 SRM 53-00-50-2R-1 REV 69; SRM 53-00-50-2R-0 REV 69 A98132; A36551SDR SWAA2020032729662Floorboard · damagedPASSENGER CABIN FLOOR BOARD 231MF UPPER SURFACE HAS FIBER DAMAGE ALONG LENGTH OF PANEL / REPAIRED PASSENGER CABIN FLOOR BOARD #231MF OF UPPER SURFACE FIBER DAMAGE ALONG LENGTH OF PANEL (AS MARKED) WITH NO DAMAGE TO COMPOSITE SUBSTRAITE IAW B737-800 SRM 53-00-5
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